Top Banner
CTR No #00072628 This document (and the information shown thereon) is PROPRIETARY to Cummins Inc. and shall not be disclosed to others in hard copy or electronic form, reproduced by any means, or used for any purpose without consent of Cummins, Inc. (0702-FIN-11-00-01) SUMMARY Purpose – This report documents the work done under EWR#19888 – To perform DVA for understanding assembly tolerances from Flywheel housing to engine mounts, fan support & Charge Air Pipe on Keb Engine, ISB6.7L Config no. D313017BX03 for OEM Scania Background – Scania team requested to perform DVAs between flywheel housing datum A, B & C and Fan support, Charge air pipe & left and right engine mounts in all 3 directions for understanding assembly tolerances for engine positioning in Vehicle. Conclusion – Detailed analysis results are shared with Scania team and received their confirmation. From Flywheel housing datums to Datum A – Z-dir Datum B X-dir Datum B Y-dir Datum C X-dir Datum C Y-Dir Nominal Tol± Nominal Tol ± Nominal Tol± Nominal Tol± Nominal Tol± Engine Mount RH 846.736 0.471 302.15 0.739 28.3 0.718 370.765 0.699 284.376 0.853 Engine Mount LH 846.636 0.471 373.85 0.807 28.3 0.718 233.534 0.753 284.376 0.853 Fan Support 1065.59 0.78 24 1.004 226 0.979 92.615 1.025 30.076 1.017 Charge Air pipe 727.5 1.678 342.369 0.877 116.13 0.924 273.75 0.833 139.943 0.833 Action Items – None
51

EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

Jul 16, 2020

Download

Documents

dariahiddleston
Welcome message from author
This document is posted to help you gain knowledge. Please leave a comment to let me know what you think about it! Share it to your friends and learn new things together.
Transcript
Page 1: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

CTR No #00072628

This document (and the information shown thereon) is PROPRIETARY to Cummins Inc. and shall not be disclosed to others in hard copy

or electronic form, reproduced by any means, or used for any purpose without consent of Cummins, Inc. (0702-FIN-11-00-01)

SUMMARY

Purpose –

This report documents the work done under EWR#19888 – To perform DVA for understanding

assembly tolerances from Flywheel housing to engine mounts, fan support & Charge Air Pipe on Keb

Engine, ISB6.7L Config no. D313017BX03 for OEM Scania

Background –

Scania team requested to perform DVAs between flywheel housing datum A, B & C and Fan support,

Charge air pipe & left and right engine mounts in all 3 directions for understanding assembly tolerances

for engine positioning in Vehicle.

Conclusion –

Detailed analysis results are shared with Scania team and received their confirmation.

From Flywheel

housing datums

to

Datum A – Z-dir Datum B X-dir Datum B Y-dir Datum C X-dir Datum C Y-Dir

Nominal Tol± Nominal Tol ± Nominal Tol± Nominal Tol± Nominal Tol±

Engine Mount RH 846.736 0.471 302.15 0.739 28.3 0.718 370.765 0.699 284.376 0.853

Engine Mount LH 846.636 0.471 373.85 0.807 28.3 0.718 233.534 0.753 284.376 0.853

Fan Support 1065.59 0.78 24 1.004 226 0.979 92.615 1.025 30.076 1.017

Charge Air pipe 727.5 1.678 342.369 0.877 116.13 0.924 273.75 0.833 139.943 0.833

Action Items – None

Page 2: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential3

DVA Details

Flywheel housing to Engine mounts:

1. DVA is performed from Datum A of Flywheel housing to engine mount isolator mounting hole in Z-direction for both right and left engine mounts.

2. DVA is performed from Datum B of Flywheel housing to engine mount isolator mounting hole center in both X&Y-directions for both left and right engine mounts

3. DVA is performed from Datum C of Flywheel housing to engine mount isolator mounting hole center in both X&Y-directions for both left and right engine mounts

Flywheel housing

datum details

Engine mount

end point details

Page 3: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential4

Flywheel housing to Charge Air Pipe:

1. DVA is performed from Datum A of Flywheel housing to Charge Air Pipe end face in Z-direction

2. DVA is performed from Datum B of Flywheel housing to Charge Air pipe outlet center in both X&Y-directions

3. DVA is performed from Datum C of Flywheel housing to Charge Air pipe outlet center in both X&Y-directions

DVA Details

Flywheel housing

datum details

Charge air pipe

end point details

Page 4: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential5

Flywheel housing to Fan Support:

1. DVA is performed from Datum A of Flywheel housing to Fan Support end face in Z-direction

2. DVA is performed from Datum B of Flywheel housing to Fan Support center in both X&Y-directions

3. DVA is performed from Datum C of Flywheel housing to Fan Support center in both X&Y-directions

DVA Details

Fan support end

point detailsFlywheel housing

datum details

Page 5: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential6

DVA Loop details

Flywheel housing to Engine mounts:

1. DVA is performed from Datum A of Flywheel housing to engine mount isolator mounting hole in Z-direction right engine mount.

1. Width of Flywheel housing2. Width of rear gear housing3. Rear face cylinder Block to thrust face

datum D of Block4. Thrust face datum D to front face of

Block5. Datum B of engine mount to datum E6. Datum E of engine mount to isolator

mount hole center point B

Page 6: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

Dimensional Variation Analysis Interface / Worksheet

DVA Objective: Assumptions: GUI Info DATE: Note: Do Not Modify or Type In Any Colored Cells.

Author : Output Units : OUTPUT SPEC. (If Known) Parameter Classification

CTR # : Default Input PPK: 1 USL:

Engine Model : MC Mean Shift = Cc: 0.25 LSL:(Enter a space if no SL) Selection

# Part Name - Feature Description + or -Drawing Nominal (Used in Formula)

Drawing Tol (Used in Formula)

Input Ppk ST Formula Nominal± Formula

ToleranceTolerance

Squared100.00% Rank % Cont Item/Part Number Rev No. Assumptions/Comments/Issues

1 Flywheel Datum A to gear housing face + 128.6 0.1 128.6 0.1 0.01 5.71% 4 5402303_Page3_H7 0

2Gear housing width from flywheel mounting face

to Block mounting face+ 47 0.2 47 0.2 0.04 22.83% 2 5311333_Sheet2_B2 4

3

4 Rear face Datum G to Datum D + 150.115 0.1 150.115 0.1 0.01 5.71% 4 5253196_page5_H7 13

5

6 Datum D to front face datum E of Block + 597.885 0.1 597.885 0.1 0.01 5.71% 4 5253196_page5_H3 13

7

8 Datum B of engine mount to Datum E - 106.6 106.6 0.00% 8 5396552_page1_H7 0

9 Position tol 0.2 0.1 0.01 5.71% 4 5396552_page1_E4 0

10

11 Datum E to isolator mounting hole + 29.73641174 29.73641174 0.00% 8 5396552 0

12 position tol 0.4 0.2 0.04 22.83% 2 5396552_Page1_H3 0

13 Datum Shift

14 hole dia, tol' 12.135 0.135

15 position tol 0.2

16 LMC 12.27

17 MMC 12

18 VC 11.8

19 Shift 0.235 0.235 0.055225 31.52% 1

20

21

22

51

Output Distribution Results: Std. Dev. Nominal Total ± Min Max Output Distribution Using MRSS

Worst Case N/A 846.7364 1.0350 845.7014 847.7714 None None

RSS (± 3 Std. Dev.) 0.1395 846.7364 0.4186 846.3178 847.1550 LSL Lower Upper USL

X MRSS (± 3 Std. Dev.) 0.1570 846.7364 0.4709 846.2655 847.2073 Design PPK = =Design PPK

Monte-Carlo (± 3 Std. Dev.) Or Desired PPK=

N=1: Linear Stack-Up (Worst Case)

Place an "X" Next To Method N=2: .92 x Worst Case (Gilson) 99.7300%

N=3: .80 x Worst Case (Gilson)Y or Blank (Gaussian) (per QSP 3-15-01) N=4: .72 x Worst Case (Gilson) 0.13499% 0.13499%

5 N=5 or greater: 1.5 x RSS (Bender)

N (Uniform) Std. Dev. % in 1 Side out 1 Side out PPK MC Output 846.2655 846.7364 847.2073

± 3 99.7300% 0.135% 1350 PPM 1 Decimal Places 3 MIN @ 3 Std. Dev. 3 3 MAX @ 3 Std. Dev.

WC (Discrete Uniform) ± 4 99.9937% 0.00317% 32 PPM 1.33 Std. Dev. = 0.1570

CC (Discrete Uniform; only 1 Feature @ a Time) ± 4.5 99.9997% 0.00034% 3.4PPM 1.5 Σ WC = 0 Output = 846.736 ± 0.47

Distance from flywheel housing

datum A to right engine mount

Sravanthi K

ISB6.7L engine -Keb

ST Statistical Tolerance Column

PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT PRIOR APPROVAL IN ACCORDANCE WITH TFE-CTC-0271

9/9/2016 Page 1 dva_flywheel&engine mount.xlsm

Page 7: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential7

DVA Loop - Results

Flywheel housing to Engine mounts:

1. DVA is performed from Datum A of Flywheel housing to engine mount isolator mounting hole in Z-direction right engine mounts.

� Total distance from datum A of Flywheel housing to isolator mounting hole is 846.7mm

in Z-direction.

� Total assembly variation observed is 0.47mm fro MRSS in Z-direction

Page 8: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

Dimensional Variation Analysis Interface / Worksheet

DVA Objective: Assumptions: GUI Info DATE: Note: Do Not Modify or Type In Any Colored Cells.

Author : Output Units : OUTPUT SPEC. (If Known) Parameter Classification

CTR # : Default Input PPK: 1 USL:

Engine Model : MC Mean Shift = Cc: 0.25 LSL:(Enter a space if no SL) Selection

# Part Name - Feature Description + or -Drawing Nominal (Used in Formula)

Drawing Tol (Used in Formula)

Input Ppk ST Formula Nominal± Formula

ToleranceTolerance

Squared100.00% Rank % Cont Item/Part Number Rev No. Assumptions/Comments/Issues

1 Axis of datum B(Scania) to center of Flywheel 0 0

2 Position tol 0.08 0.04 0.0016 0.50% 8

3

4

5 Flywheel B to dwg datum B + 147 0 147 0 0.00% 9 5402303_page2_H4 0

6 Position tol 0.08 0 0.04 0.0016 0.50% 8 5402303_page2_C2 0

7 Datum Shift of B datum, hole dia, tol 13.125 0.125 5402303_page2_C2 0

8 position tol 0.08 5402303_page2_C2 0

9 LMC 13.25

10 MMC 13

11 VC 12.92

12 Shift 0.165 0.165 0.027225 8.45% 4

13 Bonus 0.25 0.125 0.015625 4.85% 5

14

15 Float is neglected as dowels are interference fit

16

17 Block mounting hole to Datum A of Block + 16 16 0.00% 9 4990454_Page2_C6 11

18 Position tol 0.8 0.4 0.16 49.68% 1 4990454 11

19 Datum shift of Datum A 15.09 0.14 4990454 11

20 Hole dia, tol 0.2

21 LMC 15.23

22 MMC 14.95

23 VC 14.75

24 Shift 0.24 0.24 0.0576 17.89% 2

25

28

29 Datum A of Block to Datum A of mount + 12 12 0.00% 9 4990454_Page2_C3 11

30

31 Datum A to mount hole + 108.1 108.1 0.00% 9 5396552_Page1_G4 0

32 Position tol 0.2 0.1 0.01 3.11% 6 0

33

34 mount hole to datum E + 38.1 38.1 0.00% 9 5396552_Page1_F4 0

35 Position tol 0.2 0.1 0.01 3.11% 6 5396552_Page1_E4 0

36

37 datum E to isolator mounting hole - 19.05 19.05 0.00% 9 5396552_Page1_F4 0

38 0.4 0.2 0.04 12.42% 3 5396552_Page1_G3 0

39

60

Output Distribution Results: Std. Dev. Nominal Total ± Min Max Output Distribution Using MRSS

Worst Case N/A 302.1500 1.3700 300.7800 303.5200 None None

RSS (± 3 Std. Dev.) 0.1892 302.1500 0.5675 301.5825 302.7175 LSL Lower Upper USL

X MRSS (± 3 Std. Dev.) 0.2466 302.1500 0.7398 301.4102 302.8898 Design PPK = =Design PPK

Monte-Carlo (± 3 Std. Dev.) Or Desired PPK=

N=1: Linear Stack-Up (Worst Case)

Place an "X" Next To Method N=2: .92 x Worst Case (Gilson) 99.7300%

N=3: .80 x Worst Case (Gilson)Y or Blank (Gaussian) (per QSP 3-15-01) 4 N=4: .72 x Worst Case (Gilson) 0.13499% 0.13499%

N=5 or greater: 1.5 x RSS (Bender)N (Uniform) Std. Dev. % in 1 Side out 1 Side out PPK MC Output 301.4102 302.1500 302.8898

± 3 99.7300% 0.135% 1350 PPM 1 Decimal Places 3 MIN @ 3 Std. Dev. 3 3 MAX @ 3 Std. Dev.

WC (Discrete Uniform) ± 4 99.9937% 0.00317% 32 PPM 1.33 Std. Dev. = 0.2466

CC (Discrete Uniform; only 1 Feature @ a Time) ± 4.5 99.9997% 0.00034% 3.4PPM 1.5 Σ WC = 0 Output = 302.15 ± 0.739

Distance from flywheel housing

datum B - Xdir to right engine

mount

Sravanthi K

ISB6.7L - Keb Program

ST Statistical Tolerance Column

PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT PRIOR APPROVAL IN ACCORDANCE WITH TFE-CTC-0271

9/9/2016 Page 2 dva_flywheel&engine mount.xlsm

Page 9: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential8

DVA Loop - Details

Flywheel housing to Engine mounts:

2. DVA is performed from Datum B of Flywheel housing to engine mount isolator mounting hole center in both X&Y-directions right engine mount

1. Flywheel housing center (Scania dtm B) to datum B (on drwg)2. Flywheel house mounting hole on Block to Datum A on Block3. Datum A on Block to Datum A on engine mount4. Datum A on engine mount to mounting hole on isolator pad5. Mounting hole on isolator pad to datum E of engine mount6. Datum E on engine mount to isolator mounting hole

Page 10: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential9

DVA Results

Flywheel housing to Engine mounts:

2. DVA is performed from Datum B of Flywheel housing to engine mount isolator mounting hole center in both X&Y-directions right engine mount

� Total distance from datum B of Flywheel housing to isolator mounting hole is 302.15mm

in X-direction for datum B

� Total assembly variation observed is ~0.74mm fro MRSS in X-direction

Page 11: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential10

DVA Loop - Results

Flywheel housing to Engine mounts:

2. DVA is performed from Datum B of Flywheel housing to engine mount isolator mounting hole center in both X&Y-directions right engine mount

1. Flywheel housing center (Scania dtm B) to datum B (on drwg)2. Flywheel house mounting hole on Block to Datum C on Block3. Datum C on Block to Datum C on engine mount4. Datum C on engine mount to isolator mounting pad surface (datum E hole center)5. Datum E hole center to isolator mounting hole center surface

Page 12: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

Dimensional Variation Analysis Interface / Worksheet

DVA Objective: Assumptions: GUI Info DATE: Note: Do Not Modify or Type In Any Colored Cells.

Author : Output Units : OUTPUT SPEC. (If Known) Parameter Classification

CTR # : Default Input PPK: 1 USL:

Engine Model : MC Mean Shift = Cc: 0.25 LSL:(Enter a space if no SL) Selection

# Part Name - Feature Description + or -Drawing Nominal (Used in Formula)

Drawing Tol (Used in Formula)

Input Ppk ST Formula Nominal± Formula

ToleranceTolerance

Squared100.00% Rank % Cont Item/Part Number Rev No. Assumptions/Comments/Issues

13

14 Axis of Datum B(Scania) to Flywheel center 0

15 Position tol 0.08 0.04 0.0016 0.46% 7

16 Bonus 0.25 0.125 0.015625 4.54% 5

17

18

19 flywheel center to datum B of flywheel drwg + 75 75 0.00% 8 5402303_Page2-D2 0

20 Position tol 0.08 0.04 0.0016 0.46% 7 5402303_Page2-C2 0

21 datum shift of Flywheel datum B

22 Hole dai, tol 13.125 0.125

23 position tol 0.08

24 LMC 13.25

25 MMC 13

26 VC 12.92

27 Shift 0.165 0.165 0.027225 7.90% 4

28

29 Datum B(flywheel drwg), block mounting hole to

datum C of Block+ 15 15 0.00% 8 4990454_Page3_C6 11

30 position tol of hole 0.8 0.4 0.16 46.45% 1 4990454_Page3_B8 11

31

32 Datum C of Block to Datum C of mount - 33.5 33.5 0.00% 8 4990454_Page2_C3 11

33

34 Datum C to Datum E - 30.8 30.8 0.00% 8 5396552_page1_G8 0

35 positiol tol 0.2 0.1 0.01 2.90% 6

36 datum shift of datum C

37 Hole dai, tol 13 0.2

38 position tol 0.2

39 LMC 13.2

40 MMC 12.8

41 VC 12.6

42 Shift 0.3 0.3 0.09 26.13% 2

43

44 Datum E to isolator mounting hole + 2.6 2.6 0.00% 8 5396552 0 Creo measured value

45 position tol 0.4 0.2 0.04 11.61% 3

46

66

Output Distribution Results: Std. Dev. Nominal Total ± Min Max Output Distribution Using MRSS

Worst Case N/A 28.3000 1.3300 26.9700 29.6300 None None

RSS (± 3 Std. Dev.) 0.1956 28.3000 0.5869 27.7131 28.8869 LSL Lower Upper USL

X MRSS (± 3 Std. Dev.) 0.2394 28.3000 0.7182 27.5818 29.0182 Design PPK = =Design PPK

Monte-Carlo (± 3 Std. Dev.) Or Desired PPK=

N=1: Linear Stack-Up (Worst Case)

Place an "X" Next To Method N=2: .92 x Worst Case (Gilson) 99.7300%

N=3: .80 x Worst Case (Gilson)Y or Blank (Gaussian) (per QSP 3-15-01) 4 N=4: .72 x Worst Case (Gilson) 0.13499% 0.13499%

N=5 or greater: 1.5 x RSS (Bender)N (Uniform) Std. Dev. % in 1 Side out 1 Side out PPK MC Output 27.5818 28.3000 29.0182

± 3 99.7300% 0.135% 1350 PPM 1 Decimal Places 3 MIN @ 3 Std. Dev. 3 3 MAX @ 3 Std. Dev.

WC (Discrete Uniform) ± 4 99.9937% 0.00317% 32 PPM 1.33 Std. Dev. = 0.2394

CC (Discrete Uniform; only 1 Feature @ a Time) ± 4.5 99.9997% 0.00034% 3.4PPM 1.5 Σ WC = 0 Output = 28.3 ± 0.718

Distance from flywheel housing

datum B Ydirection to right

engine mount

Sravanthi K

ISB6.7L - Keb program

ST Statistical Tolerance Column

PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT PRIOR APPROVAL IN ACCORDANCE WITH TFE-CTC-0271

9/9/2016 Page 3 dva_flywheel&engine mount.xlsm

Page 13: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential11

DVA Loop - Results

Flywheel housing to Engine mounts:

2. DVA is performed from Datum B of Flywheel housing to engine mount isolator mounting hole center in both X&Y-directions right engine mount

� Total distance from datum B of Flywheel housing to isolator mounting hole is 28.3mm in

Y-direction for datum B

� Total assembly variation observed is ~0.72mm for MRSS in Y-direction

Page 14: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential12

DVA Loop - Results

Flywheel housing to Engine mounts:

3. DVA is performed from Datum C of Flywheel housing to engine mount isolator mounting hole center in both X&Y-directions for right engine mount

1. Datum C of flywheel housing (Scania dtm) to center of housing2. Flywheel housing center to datum B of housing (on drwg)3. Flywheel house mounting hole on Block to Datum A on Block4. Datum A on Block to Datum A on engine mount5. Datum A on engine mount to mounting hole on isolator pad6. Mounting hole on isolator pad to datum E of engine mount7. Datum E on engine mount to isolator mounting hole

Page 15: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

Dimensional Variation Analysis Interface / Worksheet

DVA Objective: Assumptions: GUI Info DATE: Note: Do Not Modify or Type In Any Colored Cells.

Author : Output Units : OUTPUT SPEC. (If Known) Parameter Classification

CTR # : Default Input PPK: 1 USL:

Engine Model : MC Mean Shift = Cc: 0.25 LSL:(Enter a space if no SL) Selection

# Part Name - Feature Description + or -Drawing Nominal (Used in Formula)

Drawing Tol (Used in Formula)

Input Ppk ST Formula Nominal± Formula

ToleranceTolerance

Squared100.00% Rank % Cont Item/Part Number Rev No. Assumptions/Comments/Issues

1

2

3 Datum C(scania) to flywheel center [arc length] + 68.61551705 68.61551705 0.00% 11

4 position tol 0.5 0.25 0.0625 16.19% 2

5

6 Axis of Datum B(Scania) to Flywheel center 0 0

7 Position tol 0.08 0.04 0.0016 0.41% 9

8 Bonus 0.25 0.125 0.015625 4.05% 6

9

21

22 Flywheel B to dwg datum B + 147 0 147 0 0.00% 11 5402303_page2_H4 0

23 Position tol 0.08 0 0.04 0.0016 0.41% 9 5402303_page2_C2 0

24 Datum Shift of B datum, hole dia, tol 13.125 0.125 5402303_page2_C2 0

25 position tol 0.08 5402303_page2_C2 0

26 LMC 13.25

27 MMC 13

28 VC 12.92

29 Shift 0.165 0.165 0.027225 7.05% 5

30

31 Float neglected - dowel interference fit 0

32 0

33

34 Block mounting hole to Datum A of Block + 16 16 0.00% 11 4990454_Page2_C6 11

35 Position tol 0.8 0.4 0.16 41.43% 1 4990454 11

36 Datum shift of Datum A 15.09 0.14 4990454 11

37 Hole dia, tol 0.2

38 LMC 15.23

39 MMC 14.95

40 VC 14.75

41 Shift 0.24 0.24 0.0576 14.92% 3

42

45

46 Datum A of Block to Datum A of mount + 12 12 0.00% 11 4990454_Page2_C3 11

47

48 Datum A to mount hole + 108.1 108.1 0.00% 11 5396552_Page1_G4 0

49 Position tol 0.2 0.1 0.01 2.59% 7 0

50

51 mount hole to datum E + 38.1 38.1 0.00% 11 5396552_Page1_F4 0

52 Position tol 0.2 0.1 0.01 2.59% 7 5396552_Page1_E4 0

53

54 datum E to isolator mounting hole - 19.05 19.05 0.00% 11 5396552_Page1_F4 0

55 0.4 0.2 0.04 10.36% 4 5396552_Page1_G3 0

56

Output Distribution Results: Std. Dev. Nominal Total ± Min Max Output Distribution Using MRSS

Worst Case N/A 370.7655 1.6600 369.1055 372.4255 None None

RSS (± 3 Std. Dev.) 0.2071 370.7655 0.6214 370.1441 371.3869 LSL Lower Upper USL

X MRSS (± 3 Std. Dev.) 0.2330 370.7655 0.6991 370.0664 371.4646 Design PPK = =Design PPK

Monte-Carlo (± 3 Std. Dev.) Or Desired PPK=

N=1: Linear Stack-Up (Worst Case)

Place an "X" Next To Method N=2: .92 x Worst Case (Gilson) 99.7300%

N=3: .80 x Worst Case (Gilson)Y or Blank (Gaussian) (per QSP 3-15-01) N=4: .72 x Worst Case (Gilson) 0.13499% 0.13499%

5 N=5 or greater: 1.5 x RSS (Bender)

N (Uniform) Std. Dev. % in 1 Side out 1 Side out PPK MC Output 370.0664 370.7655 371.4646

± 3 99.7300% 0.135% 1350 PPM 1 Decimal Places 3 MIN @ 3 Std. Dev. 3 3 MAX @ 3 Std. Dev.

WC (Discrete Uniform) ± 4 99.9937% 0.00317% 32 PPM 1.33 Std. Dev. = 0.2330

CC (Discrete Uniform; only 1 Feature @ a Time) ± 4.5 99.9997% 0.00034% 3.4PPM 1.5 Σ WC = 0 Output = 370.765 ± 0.699

Distance from flywheel housing

datum C - Xdirection to right

engine mount

Sravanthi K

ISB6.7L - Keb Program

ST Statistical Tolerance Column

PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT PRIOR APPROVAL IN ACCORDANCE WITH TFE-CTC-0271

9/9/2016 Page 4 dva_flywheel&engine mount.xlsm

Page 16: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential13

DVA Loop - Results

Flywheel housing to Engine mounts:

3. DVA is performed from Datum C of Flywheel housing to engine mount isolator mounting hole center in both X&Y-directions for right engine mount

� Total distance from datum C of Flywheel housing to isolator mounting hole is 370.76mm

in X-direction for datum C

� Total assembly variation observed is ~0.69mm for MRSS in X-direction

Page 17: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential14

DVA Loop - Results

Flywheel housing to Engine mounts:

3. DVA is performed from Datum C of Flywheel housing to engine mount isolator mounting hole center in both X&Y-directions for right engine mount

1. Datum C of flywheel housing (Scania dtm) to center of housing2. Flywheel housing center to datum B of housing (on drwg)3. Flywheel house mounting hole on Block to Datum A on Block4. Datum A on Block to Datum A on engine mount5. Datum A on engine mount to mounting hole on isolator pad6. Mounting hole on isolator pad to datum E of engine mount7. Datum E on engine mount to isolator mounting hole

Page 18: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

Dimensional Variation Analysis Interface / Worksheet

DVA Objective: Assumptions: GUI Info DATE: Note: Do Not Modify or Type In Any Colored Cells.

Author : Output Units : OUTPUT SPEC. (If Known) Parameter Classification

CTR # : Default Input PPK: 1 USL:

Engine Model : MC Mean Shift = Cc: 0.25 LSL:(Enter a space if no SL) Selection

# Part Name - Feature Description + or -Drawing Nominal (Used in Formula)

Drawing Tol (Used in Formula)

Input Ppk ST Formula Nominal± Formula

ToleranceTolerance

Squared100.00% Rank % Cont Item/Part Number Rev No. Assumptions/Comments/Issues

1 Datum C(scania) to flywheel center [arc length] + 256.0765958 256.0765958 0 0.00% 9

2 position tol 0.5 0.25 0.0625 15.36% 3

3

6 0

7 Bonus 0.25 0.125 0.015625 3.84% 6

8 flywheel center to datum B of flywheel drwg + 75 75 0.00% 9 5402303_Page2-D2 0

9 Position tol 0.08 0.04 0.0016 0.39% 8 5402303_Page2-C2 0

10 datum shift of Flywheel datum B

11 Hole dai, tol 13.125 0.125

12 position tol 0.08

13 LMC 13.25

14 MMC 13

15 VC 12.92

16 Shift 0.165 0.165 0.027225 6.69% 5

17

18 Datum B(flywheel drwg), block mounting hole to

datum C of Block+ 15 15 0.00% 9 4990454_Page3_C6 11

19 position tol of hole 0.8 0.4 0.16 39.32% 1 4990454_Page3_B8 11

20

21 Datum C of Block to Datum C of mount - 33.5 33.5 0.00% 9 4990454_Page2_C3 11

22

23 Datum C to Datum E - 30.8 30.8 0.00% 9 5396552_page1_G8 0

24 positiol tol 0.2 0.1 0.01 2.46% 7

25 datum shift of datum C

26 Hole dai, tol 13 0.2

27 position tol 0.2

28 LMC 13.2

29 MMC 12.8

30 VC 12.6

31 Shift 0.3 0.3 0.09 22.12% 2

32

33 Datum E to isolator mounting hole + 2.6 2.6 0.00% 9 5396552 0 Creo measured value

34 position tol 0.4 0.2 0.04 9.83% 4

35

55

Output Distribution Results: Std. Dev. Nominal Total ± Min Max Output Distribution Using MRSS

Worst Case N/A 284.3766 1.5800 282.7966 285.9566 None None

RSS (± 3 Std. Dev.) 0.2126 284.3766 0.6379 283.7387 285.0145 LSL Lower Upper USL

X MRSS (± 3 Std. Dev.) 0.2844 284.3766 0.8532 283.5234 285.2298 Design PPK = =Design PPK

Monte-Carlo (± 3 Std. Dev.) Or Desired PPK=

N=1: Linear Stack-Up (Worst Case)

Place an "X" Next To Method N=2: .92 x Worst Case (Gilson) 99.7300%

N=3: .80 x Worst Case (Gilson)Y or Blank (Gaussian) (per QSP 3-15-01) 4 N=4: .72 x Worst Case (Gilson) 0.13499% 0.13499%

N=5 or greater: 1.5 x RSS (Bender)

N (Uniform) Std. Dev. % in 1 Side out 1 Side out PPK MC Output 283.5234 284.3766 285.2298

± 3 99.7300% 0.135% 1350 PPM 1 Decimal Places 3 MIN @ 3 Std. Dev. 3 3 MAX @ 3 Std. Dev.

WC (Discrete Uniform) ± 4 99.9937% 0.00317% 32 PPM 1.33 Std. Dev. = 0.2844

CC (Discrete Uniform; only 1 Feature @ a Time) ± 4.5 99.9997% 0.00034% 3.4PPM 1.5 Σ WC = 0 Output = 284.376 ± 0.853

Distance from flywheel housing

datum C Y-driection to right

engine mount

Sravanthi K

ISB6.7L - Keb Program

ST Statistical Tolerance Column

PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT PRIOR APPROVAL IN ACCORDANCE WITH TFE-CTC-0271

9/9/2016 Page 5 dva_flywheel&engine mount.xlsm

Page 19: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential15

DVA Loop - Results

Flywheel housing to Engine mounts:

3. DVA is performed from Datum C of Flywheel housing to engine mount isolator mounting hole center in both X&Y-directions for right engine mount

� Total distance from datum C of Flywheel housing to isolator mounting hole is 284.37mm

in Y-direction from datum C

� Total assembly variation observed is ~0.85mm for MRSS in Y-direction

Page 20: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential16

DVA Loop - Results

Flywheel housing to Charge Air Pipe:

1. DVA is performed from Datum A of Flywheel housing to Charge Air Pipe end face in Z-direction

1. Width of Flywheel housing

2. Width of rear gear housing

3. Rear face cylinder Block to head deck dowel

hole center on Block

4. Datum B on Head to datum A on head

5. Datum A on head to exhaust Manifold mounting

hole center (datum B)

6. Datum B on Manifold to datum ZE center point

7. Datum ZE to datum F (turbo mounting hole

center)

8. Turbo mounting hole center to turbo air outlet

center

9. Turbo air outlet center to charge air pipe outlet

center

Page 21: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

Dimensional Variation Analysis Interface / Worksheet

DVA Objective: Assumptions: GUI Info DATE: Note: Do Not Modify or Type In Any Colored Cells.

Author : Output Units : OUTPUT SPEC. (If Known) Parameter Classification

CTR # : Default Input PPK: 1 USL:

Engine Model : MC Mean Shift = Cc: 0.25 LSL:(Enter a space if no SL) Selection

# Part Name - Feature Description + or -Drawing Nominal (Used in Formula)

Drawing Tol (Used in Formula)

Input Ppk ST Formula Nominal± Formula

ToleranceTolerance

Squared100.00% Rank % Cont Item/Part Number Rev No. Assumptions/Comments/Issues

1 Flywheel Datum A to gear housing face + 128.6 0.1 128.6 0.1 0.01 0.45% 10 5402303_page3_H7 0

2Gear housing width from flywheel mounting

face to Block mounting face+ 47 0.2 47 0.2 0.04 1.80% 8 5311333_page2_B2 4

3

4 Rear face Datum G to Datum D + 150.115 0.1 150.115 0.1 0.01 0.45% 10 5253196_page5_H7 13

5

6Datum D to Head deck dowel Datum B of

cylinder head- 16.115 0.075 1.33 16.115 0.075 0.00317994 0.14% 12 5253196_page6_C6 13

7

8 Float neglected as for dowel it is interference fit

9

10 Datum B to Datum A of cylinder head + 600 600 0.00% 14 5309649_page3_A6 8

11 Position tol 0.14 1.33 0.07 0.00277008 0.12% 13

12

13 Datum B to Manifold mounting hole datum B - 460.5 460.5 0.00% 14 5309649_page2_E7 8

14 Position tol 0.7 0.35 0.1225 5.51% 6

15

16 float between manifold and Head 0.723320023 0.361660012 0.13079796 5.88% 5

17 Float tol 0.640428509 0.320214254 0.10253717 4.61% 7

18

19 Manifold Datum B to Datum ZE + 57.7 57.9 0.00% 14 5396617_page3_F6 0

20

21 Datum ZE to Datum F + 43 40.1 0.00% 14 5396617_page2_C6 0

22 position tol 0.8 0.4 0.16 7.19% 4

23

24 float between manifold and turbo 0.974660461 0.48733023 0.23749075 10.68% 3

25 Float tol 0.238759884 0.119379942 0.01425157 0.64% 9

26

27 Turbo mounting hole air outlet center + 78.2 0.625 73.9 0.625 0.390625 17.56% 2 5352931

28

29 Airoutlet center to charge air pipe outer surface + 106.5 106.5 0.00% 14 5366563_page1_C6 0

30 position tol 2 1 1 44.96% 1

31

54

Output Distribution Results: Std. Dev. Nominal Total ± Min Max Output Distribution Using MRSS

Worst Case N/A 727.5000 4.2086 723.2914 731.7086 None None

RSS (± 3 Std. Dev.) 0.4971 727.5000 1.4914 726.0086 728.9914 LSL Lower Upper USL

X MRSS (± 3 Std. Dev.) 0.5593 727.5000 1.6778 725.8222 729.1778 Design PPK = =Design PPK

Monte-Carlo (± 3 Std. Dev.) Or Desired PPK=

N=1: Linear Stack-Up (Worst Case)

Place an "X" Next To Method N=2: .92 x Worst Case (Gilson) 99.7300%

N=3: .80 x Worst Case (Gilson)Y or Blank (Gaussian) (per QSP 3-15-01) N=4: .72 x Worst Case (Gilson) 0.13499% 0.13499%

5 N=5 or greater: 1.5 x RSS (Bender)N (Uniform) Std. Dev. % in 1 Side out 1 Side out PPK MC Output 725.8222 727.5000 729.1778

± 3 99.7300% 0.135% 1350 PPM 1 Decimal Places 3 MIN @ 3 Std. Dev. 3 3 MAX @ 3 Std. Dev.

WC (Discrete Uniform) ± 4 99.9937% 0.00317% 32 PPM 1.33 Std. Dev. = 0.5593

CC (Discrete Uniform; only 1 Feature @ a Time) ± 4.5 99.9997% 0.00034% 3.4PPM 1.5 Σ WC = 0 Output = 727.5 ± 1.677

ST Statistical Tolerance Column

Distance from flywheel housing

datum A to Charge Air pipe in

Z-direction

Sravanthi K

ISB6.7L - Keb Program

PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT PRIOR APPROVAL IN ACCORDANCE WITH TFE-CTC-0271

9/9/2016 Page 1 dva_flywheel&chargeairpipe_rev1.xlsm

Page 22: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential17

DVA Loop - Results

Flywheel housing to Charge Air Pipe:

1. DVA is performed from Datum A of Flywheel housing to Charge Air Pipe end face in Z-direction

� Total distance from datum A of Flywheel housing to Charge Air pipe outlet surface in Z-

direction is 727.5mm

� Total assembly variation observed is ~1.68mm for MRSS in Z-direction

Page 23: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential18

DVA Loop - Results

Flywheel housing to Charge Air Pipe:

2. DVA is performed from Datum B of Flywheel housing to Charge Air pipe outlet center in both X&Y-directions

1. Flywheel housing center (Scania dtm B) to

datum B (on drwg)

2. Flywheel house mounting hole on Block to

Datum A on Block

3. Datum A on Block to head deck dowel hole

center (Datum B/Datum A)

4. Datum A on Cylinder head to exhaust Manifold

mounting surface

5. Thickness of gasket

6. Manifold mounting face to intersect point of ZE

& ZD

7. Datum point of turbo mounting face to turbo

exhaust outlet center

8. Turbo exhaust outlet center to air outlet center

9. Air outlet center to charge air pipe outlet

center

Page 24: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

Dimensional Variation Analysis Interface / Worksheet

DVA Objective: Assumptions: GUI Info DATE: Note: Do Not Modify or Type In Any Colored Cells.

Author : Output Units : OUTPUT SPEC. (If Known) Parameter Classification

CTR # : Default Input PPK: 1 USL:

Engine Model : MC Mean Shift = Cc: 0.25 LSL:(Enter a space if no SL) Selection

# Part Name - Feature Description + or -Drawing Nominal (Used in Formula)

Drawing Tol (Used in Formula)

Input Ppk STFormula

Nominal

± Formula

ToleranceTolerance

Squared100.00% Rank % Cont Item/Part Number Rev No. Assumptions/Comments/Issues

1 Axis of datum B(Scania) to center of Flywheel 0 0 5402303

2 Position tol 0.08 0.04 0.0016 0.26% 12

3 Bonus

4

5

6 Flywheel B to dwg datum B - 147 0 147 0 0.00% 13 5402303_page2_G4 0

7 Position tol 0.08 0 0.04 0.0016 0.26% 12

8 Datum Shift of ZB datum, hole dia, tol 13.125 0.125

9 position tol 0.08 5402303_page2_C2 0

10 LMC 13.25 5402303_page2_C2 0

11 MMC 13 5402303_page2_C2 0

12 VC 12.92

13 Shift 0.165 0.165 0.027225 4.37% 7

14

15 Float neglected for interfernce fit 0

16 Float tol 0

17

18 Block mounting hole to Datum A of Block - 16 16 0.00% 13 4990454_page3_C6 11

19 Position tol 0.8 0.4 0.16 25.66% 2

20 Datum shift of Datum A 15.09 0.14

21 Hole dia, tol 0.2 4990454_page5_B8 11

22 LMC 15.23 4990454_page5_B8 11

23 MMC 14.95 4990454_page5_B8 11

24 VC 14.75

25 Shift 0.24 0.24 0.0576 9.24% 5

26

27 Datum A of Block to head deck dowel hole + 206.5 0.12 1.33 206.5 0.12 0.00814065 1.31% 9 4990454_page4_E2 11

28

29 Datum A/B of head to exhuast face + 49.5 0.25 49.5 0.25 0.0625 10.03% 4 5309649_page3_D3 8

30

31 Gasket total thickness + 1.5508 0.284 1.5508 0.284 0.080656 12.94% 3 5266422

32

33

Manifold mounting face to turbo mounting

face + 143.206577 0.201025 143.206577 0.201025 0.04041105 6.48% 6 5396617 0

Projected distance measured in creo as

plane is in 3D

34

35 Turbo mounting plane to exhaust outlet center + 91.952365 0.40205 91.952365 0.40205 0.1616442 25.93% 1 5352931

Projected distance measured in creo as

plane is in 3D

36

37 exhuats outlet center to air outlet center - 12.7324 0.040205 12.7324 0.040205 0.00161644 0.26% 11 5366563 0

Projected distance measured in creo as

plane is in 3D

38

39 Airoutlet center on Turbo to pipe outlet center + 25.3924 0.08 25.3924 0.08 0.0064 1.03% 10 5366563 0

Projected distance measured in creo as

plane is in 3D

40

41 Bonus 0.25 0.125 0.015625 2.51% 8

42

56

Output Distribution Results: Std. Dev. Nominal Total ± Min Max Output Distribution Using MRSS

Worst Case N/A 342.3697 2.3473 340.0225 344.7170 None None

RSS (± 3 Std. Dev.) 0.2632 342.3697 0.7896 341.5802 343.1593 LSL Lower Upper USL

X MRSS (± 3 Std. Dev.) 0.2961 342.3697 0.8883 341.4815 343.2580 Design PPK = =Design PPK

Monte-Carlo (± 3 Std. Dev.) Or Desired PPK=

N=1: Linear Stack-Up (Worst Case)

Place an "X" Next To Method N=2: .92 x Worst Case (Gilson) 99.7300%

N=3: .80 x Worst Case (Gilson)Y or Blank (Gaussian) (per QSP 3-15-01) N=4: .72 x Worst Case (Gilson) 0.13499% 0.13499%

6 N=5 or greater: 1.5 x RSS (Bender)

N (Uniform) Std. Dev. % in 1 Side out 1 Side out PPK MC Output 341.4815 342.3697 343.2580

± 3 99.7300% 0.135% 1350 PPM 1 Decimal Places 3 MIN @ 3 Std. Dev. 3 3 MAX @ 3 Std. Dev.

WC (Discrete Uniform) ± 4 99.9937% 0.00317% 32 PPM 1.33 Std. Dev. = 0.2961

CC (Discrete Uniform; only 1 Feature @ a Time) ± 4.5 99.9997% 0.00034% 3.4PPM 1.5 Σ WC = 0 Output = 342.369 ± 0.888

ST Statistical Tolerance Column

Distance from flywheel

housing datum B to Charge

Air pipe in X-direction

Sravanthi K

ISB6.7L - Keb Program

PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT PRIOR APPROVAL IN ACCORDANCE WITH TFE-CTC-0271

9/9/2016 Page 2 dva_flywheel&chargeairpipe_rev1.xlsm

Page 25: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential19

DVA Loop - Results

Flywheel housing to Charge Air Pipe:

2. DVA is performed from Datum B of Flywheel housing to Charge Air pipe outlet center in both X&Y-directions

� Total distance from datum B of Flywheel housing to Charge Air pipe outlet center in X-

direction is ~342.4mm

� Total assembly variation observed is ~0.87mm for MRSS in X-direction

Page 26: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential20

DVA Loop - ResultsFlywheel housing to Charge Air Pipe:

2. DVA is performed from Datum B of Flywheel housing to Charge Air pipe outlet center in both X&Y-directions

1. Flywheel housing center (Scania dtm B)

to datum B (on drwg)

2. Flywheel house mounting hole on Block to

Datum C on Block

3. Datum C on Block to Datum C on cylinder

Head

4. Datum C on cylinder head to manifold

mounting hole datum b center

5. Manifold mounting hole center to intersect

point of ZE & ZD

6. Datum point of turbo mounting face to

turbo exhaust outlet center

7. Turbo exhaust outlet center to air outlet

center

8. Air outlet center to charge air pipe outlet

center

Page 27: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

Dimensional Variation Analysis Interface / Worksheet

DVA Objective: Assumptions: GUI Info DATE: Note: Do Not Modify or Type In Any Colored Cells.

Author : Output Units : OUTPUT SPEC. (If Known) Parameter Classification

CTR # : Default Input PPK: 1 USL:

Engine Model : MC Mean Shift = Cc: 0.25 LSL:(Enter a space if no SL) Selection

# Part Name - Feature Description + or -Drawing Nominal (Used in Formula)

Drawing Tol (Used in Formula)

Input Ppk ST Formula Nominal± Formula

ToleranceTolerance

Squared100.00% Rank % Cont Item/Part Number Rev No. Assumptions/Comments/Issues

1 Datum C(scania) to flywheel center + 0 0 0 5402303

2 position tol 0.08 0.04 0.0016 0.38% 11

3 Bonus 0.25 0.125 0.015625 3.76% 5

4 flywheel center to datum B of flywheel drwg + 75 75 0.00% 13 5402303_page2_D2 0

5 Position tol 0.08 0.04 0.0016 0.38% 11

6 datum shift of Flywheel datum B

7 Hole dai, tol 13.125 0.125

8 position tol 0.08 5402303_page2_C2 0

9 LMC 13.25 5402303_page2_C2 0

10 MMC 13 5402303_page2_C2 0

11 VC 12.92

12 Shift 0.165 0.165 0.027225 6.55% 4

13

14 Datum B(flywheel drwg), block mounting hole

to datum C of Block+ 15 15 0.00% 13

4990454_page3_C611

15 position tol of hole 0.8 0.4 0.16 38.50% 1

16

17Datum C of Block to top machining face of

block- 412.25 0.25 412.25 0.25 0.0625 15.04% 3 4990454_page8_E1 11

18

19 Installed thickness - 1.25 0.06 1.25 0.06 0.0036 0.87% 9

20

21 Datum C of Cylinder Head to Datum B Manifold - 95 95 0.00% 13 5396617 0

22 position tol 0.7 0.35 0.1225 29.48% 2

23

24 Manifold mounting face to turbo mounting face + 50 0.08041 50 0.08041 0.00646577 1.56% 6 5396617 0

25

26 Turbo mounting plane to exhaust outlet center + 25.2461 0.040205 25.2461 0.040205 0.00161644 0.39% 10 5352931

27

28 exhuats outlet center to air outlet center + 132.4203 0.08041 132.4203 0.08041 0.00646577 1.56% 6 5366563 0

29

30 Airoutlet center on Turbo to pipe outlet center + 94.7 0.08 94.7 0.08 0.0064 1.54% 8 5366563 0

31

32

33

34

35

36

37

51

Output Distribution Results: Std. Dev. Nominal Total ± Min Max Output Distribution Using MRSS

Worst Case N/A -116.1336 1.7110 -117.8446 -114.4226 None None

RSS (± 3 Std. Dev.) 0.2149 -116.1336 0.6447 -116.7783 -115.4889 LSL Lower Upper USL

X MRSS (± 3 Std. Dev.) 0.3080 -116.1336 0.9240 -117.0576 -115.2096 Design PPK = =Design PPK

Monte-Carlo (± 3 Std. Dev.) Or Desired PPK=

N=1: Linear Stack-Up (Worst Case)

Place an "X" Next To Method N=2: .92 x Worst Case (Gilson) 99.7300%

N=3: .80 x Worst Case (Gilson)Y or Blank (Gaussian) (per QSP 3-15-01) 4 N=4: .72 x Worst Case (Gilson) 0.13499% 0.13499%

N=5 or greater: 1.5 x RSS (Bender)N (Uniform) Std. Dev. % in 1 Side out 1 Side out PPK MC Output -117.0576 -116.1336 -115.2096

± 3 99.7300% 0.135% 1350 PPM 1 Decimal Places 3 MIN @ 3 Std. Dev. 3 3 MAX @ 3 Std. Dev.

WC (Discrete Uniform) ± 4 99.9937% 0.00317% 32 PPM 1.33 Std. Dev. = 0.3080

CC (Discrete Uniform; only 1 Feature @ a Time) ± 4.5 99.9997% 0.00034% 3.4PPM 1.5 Σ WC = 0 Output = -116.134 ± 0.923

ST Statistical Tolerance Column

Distance from flywheel housing

datum B to Charge Air pipe in

Y-direction

Sravanthi K

ISB6.7L - Keb Program

PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT PRIOR APPROVAL IN ACCORDANCE WITH TFE-CTC-0271

9/9/2016 Page 3 dva_flywheel&chargeairpipe_rev1.xlsm

Page 28: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential21

DVA Loop - Results

Flywheel housing to Charge Air Pipe:

2. DVA is performed from Datum B of Flywheel housing to Charge Air pipe outlet center in both X&Y-directions

� Total distance from datum B of Flywheel housing to Charge Air pipe outlet center in Y-

direction is ~116.13mm

� Total assembly variation observed is ~0.924mm for MRSS in Y-direction

Page 29: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential22

DVA Loop - Results

Flywheel housing to Charge Air Pipe:

3. DVA is performed from Datum C of Flywheel housing to Charge Air pipe outlet center in both X&Y-directions

1. Datum C of flywheel housing (Scania dtm) to

center of housing

2. Flywheel housing center to datum B of

housing (on drwg)

3. Flywheel house mounting hole on Block to

Datum A on Block

4. Datum A on Block to head deck dowel hole

center (Datum B/Datum A)

5. Datum A on Cylinder head to exhaust Manifold

mounting surface

6. Thickness of gasket

7. Manifold mounting face to intersect point of ZE

& ZD

8. Datum point of turbo mounting face to turbo

exhaust outlet center

9. Turbo exhaust outlet center to air outlet center

10.Air outlet center to charge air pipe outlet

center

Page 30: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

Dimensional Variation Analysis Interface / Worksheet

DVA Objective: Assumptions: GUI Info DATE: Note: Do Not Modify or Type In Any Colored Cells.

Author : Output Units : OUTPUT SPEC. (If Known) Parameter Classification

CTR # : Default Input PPK: 1 USL:

Engine Model : MC Mean Shift = Cc: 0.25 LSL:(Enter a space if no SL) Selection

# Part Name - Feature Description + or -Drawing Nominal (Used in Formula)

Drawing Tol (Used in Formula)

Input Ppk ST Formula Nominal± Formula

ToleranceTolerance Squared 100.00% Rank % Cont Item/Part Number Rev No. Assumptions/Comments/Issues

1

2

3

4

5

6

7

8

9

10 Flywheel B to dwg datum B - 147 0 147 0 0.00% 13 5402303_page2_G4 0

11 Position tol 0.08 0 0.04 0.0016 0.29% 12

12 Datum Shift of ZB datum, hole dia, tol 13.125 0.125

13 position tol 0.08 5402303_page2_C2 0

14 LMC 13.25 5402303_page2_C2 0

15 MMC 13 5402303_page2_C2 0

16 VC 12.92

17 Shift 0.165 0.165 0.027225 4.96% 8

18

19 Float neglected for interfernce fit 0

20 Float tol 0

21

22 Block mounting hole to Datum A of Block - 16 16 0.00% 13 4990454_page3_C6 11

23 Position tol 0.8 0.4 0.16 29.14% 1

24 Datum shift of Datum A 15.09 0.14

25 Hole dia, tol 0.2 4990454_page5_B8 11

26 LMC 15.23 4990454_page5_B8 11

27 MMC 14.95 4990454_page5_B8 11

28 VC 14.75

29 Shift 0.24 0.24 0.0576 10.49% 5

30

31 Datum A of Block to head deck dowel hole + 206.5 0.12 1.33 206.5 0.12 0.008140652 1.48% 9 4990454_page4_E2 11

32

33 Datum A/B of head to exhuast face + 49.5 0.25 49.5 0.25 0.0625 11.38% 3 5309649_page3_D3 8

34

35 Gasket total thickness + 1.5508 0.284 1.5508 0.284 0.080656 14.69% 2

36

37 Manifold mounting face to turbo mounting face + 143.206577 0.201025 143.206577 0.201025 0.040411051 7.36% 6 5396617 0

Projected distance measured in creo as plane

is in 3D

38

39 Turbo mounting plane to exhaust outlet center + 91.952365 0.201025 91.952365 0.201025 0.040411051 7.36% 6 5352931

Projected distance measured in creo as plane

is in 3D

40

41 exhuats outlet center to air outlet center - 12.7324 0.040205 12.7324 0.040205 0.001616442 0.29% 11 5366563 0

Projected distance measured in creo as plane

is in 3D

42

43 Airoutlet center on Turbo to pipe outlet center + 25.3924 0.08 25.3924 0.08 0.0064 1.17% 10 5366563 0

Projected distance measured in creo as plane

is in 3D

44

45

46 Datum C to center of Flywheel housing - 68.61551705 68.61551705 0.00% 13

47 Bonus 0.5 0.25 0.0625 11.38% 3

48

49

50

51

52

53

54

55

56

57

58

59

60

Output Distribution Results: Std. Dev. Nominal Total ± Min Max Output Distribution Using MRSS

Worst Case N/A 273.7542 2.2713 271.4830 276.0255 None None

RSS (± 3 Std. Dev.) 0.2470 273.7542 0.7410 273.0132 274.4952 LSL Lower Upper USL

X MRSS (± 3 Std. Dev.) 0.2779 273.7542 0.8336 272.9206 274.5878 Design PPK = =Design PPK

Monte-Carlo (± 3 Std. Dev.) Or Desired PPK=

N=1: Linear Stack-Up (Worst Case)

Place an "X" Next To Method N=2: .92 x Worst Case (Gilson) 99.7300%

N=3: .80 x Worst Case (Gilson)Y or Blank (Gaussian) (per QSP 3-15-01) N=4: .72 x Worst Case (Gilson) 0.13499% 0.13499%

7 N=5 or greater: 1.5 x RSS (Bender)N (Uniform) Std. Dev. % in 1 Side out 1 Side out PPK MC Output 272.9206 273.7542 274.5878

± 3 99.7300% 0.135% 1350 PPM 1 Decimal Places 3 MIN @ 3 Std. Dev. 3 3 MAX @ 3 Std. Dev.

WC (Discrete Uniform) ± 4 99.9937% 0.00317% 32 PPM 1.33 Std. Dev. = 0.2779

CC (Discrete Uniform; only 1 Feature @ a Time) ± 4.5 99.9997% 0.00034% 3.4PPM 1.5 Σ WC = 0 Output = 273.754 ± 0.833

ST Statistical Tolerance Column

Distance from flywheel housing

datum C to Charge Air pipe in X-

direction

Sravanthi K

ISB6.7L - Keb Program

PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT PRIOR APPROVAL IN ACCORDANCE WITH TFE-CTC-0271

9/9/2016 Page 4 dva_flywheel&chargeairpipe_rev1.xlsm

Page 31: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential23

DVA Loop - Results

Flywheel housing to Charge Air Pipe:

2. DVA is performed from Datum B of Flywheel housing to Charge Air pipe outlet center in both X&Y-directions

� Total distance from datum C of Flywheel housing to Charge Air pipe outlet center in X-

direction is ~273.75mm

� Total assembly variation observed is ~0.83mm for MRSS in X-direction

Page 32: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential24

DVA Loop - ResultsFlywheel housing to Charge Air Pipe:

3. DVA is performed from Datum C of Flywheel housing to Charge Air pipe outlet center in both X&Y-directions

1. Datum C of flywheel housing (Scania dtm)

to center of housing

2. Flywheel housing center to datum B of

housing (on drwg)

3. Flywheel house mounting hole on Block to

Datum C on Block

4. Datum C on Block to Datum C on cylinder

Head

5. Datum C on cylinder head to manifold

mounting hole datum b center

6. Manifold mounting hole center to intersect

point of ZE & ZD

7. Datum point of turbo mounting face to

turbo exhaust outlet center

8. Turbo exhaust outlet center to air outlet

center

9. Air outlet center to charge air pipe outlet

center

Page 33: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

Dimensional Variation Analysis Interface / Worksheet

DVA Objective: Assumptions: GUI Info DATE: Note: Do Not Modify or Type In Any Colored Cells.

Author : Output Units : OUTPUT SPEC. (If Known) Parameter Classification

CTR # : Default Input PPK: 1 USL:

Engine Model : MC Mean Shift = Cc: 0.25 LSL:(Enter a space if no SL) Selection

# Part Name - Feature Description + or - Drawing Nominal (Used in Formula)

Drawing Tol (Used in Formula)

Input Ppk ST Formula Nominal± Formula

ToleranceTolerance Squared 100.00% Rank % Cont Item/Part Number Rev No. Assumptions/Comments/Issues

1 Datum C(scania) to flywheel center [arc length] + 256.0765958 256.0765958 0 0.00% 13 5402303 0

2 position tol 0.5 0.25 0.0625 11.38% 3

3

7 Bonus 0.25 0.125 0.015625 2.84% 8

8 flywheel center to datum B of flywheel drwg + 75 75 0.00% 13 5402303_page2_D2 0

9 Position tol 0.08 0.04 0.0016 0.29% 12

10 datum shift of Flywheel datum B

11 Hole dai, tol 13.125 0.125

12 position tol 0.08 5402303_page2_C2 0

13 LMC 13.25 5402303_page2_C2 0

14 MMC 13 5402303_page2_C2 0

15 VC 12.92

16 Shift 0.165 0.165 0.027225 4.96% 7

17

18 Datum B(flywheel drwg), block mounting hole to

datum C of Block+ 15 15 0.00% 13

4990454_page3_C611

19 position tol of hole 0.8 0.4 0.16 29.13% 1

20

21 Datum C of Block to top machining face of block - 412.25 0.25 412.25 0.25 0.0625 11.38% 3 4990454_page8_E1 11

22

23 Installed thickness - 1.25 0.06 1.25 0.06 0.0036 0.66% 11

24

25 Datum C of Cylinder Head to Datum B Manifold - 95 95 0.00% 13

26 position tol 0.7 0.35 0.1225 22.30% 2

27

28 Manifold mounting face to turbo mounting face + 50 0.201025 50 0.201025 0.040411051 7.36% 5 5396617 0

29

30 Turbo mounting plane to exhaust outlet center + 25.2461 0.201025 25.2461 0.201025 0.040411051 7.36% 5 5352931

31

32 exhuats outlet center to air outlet center + 132.4203 0.08041 132.4203 0.08041 0.006465768 1.18% 9 5366563 0

33

34 Airoutlet center on Turbo to pipe outlet center + 94.7 0.08 94.7 0.08 0.0064 1.17% 10 5366563 0

35

36

37

38

39

40

41

55

Output Distribution Results: Std. Dev. Nominal Total ± Min Max Output Distribution Using MRSS

Worst Case N/A 139.9430 2.2025 137.7405 142.1455 None None

RSS (± 3 Std. Dev.) 0.2470 139.9430 0.7411 139.2019 140.6841 LSL Lower Upper USL

X MRSS (± 3 Std. Dev.) 0.2779 139.9430 0.8337 139.1093 140.7767 Design PPK = =Design PPK

Monte-Carlo (± 3 Std. Dev.) Or Desired PPK=

N=1: Linear Stack-Up (Worst Case)

Place an "X" Next To Method N=2: .92 x Worst Case (Gilson) 99.7300%

N=3: .80 x Worst Case (Gilson)Y or Blank (Gaussian) (per QSP 3-15-01) N=4: .72 x Worst Case (Gilson) 0.13499% 0.13499%

6 N=5 or greater: 1.5 x RSS (Bender)

N (Uniform) Std. Dev. % in 1 Side out 1 Side out PPK MC Output 139.1093 139.9430 140.7767

± 3 99.7300% 0.135% 1350 PPM 1 Decimal Places 3 MIN @ 3 Std. Dev. 3 3 MAX @ 3 Std. Dev.

WC (Discrete Uniform) ± 4 99.9937% 0.00317% 32 PPM 1.33 Std. Dev. = 0.2779

CC (Discrete Uniform; only 1 Feature @ a Time) ± 4.5 99.9997% 0.00034% 3.4PPM 1.5 Σ WC = 0 Output = 139.942 ± 0.833

ST Statistical Tolerance Column

Distance from flywheel housing

datum C to Charge Air pipe in Y-

direction

Sravanthi K

ISB6.7L - Keb Program

PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT PRIOR APPROVAL IN ACCORDANCE WITH TFE-CTC-0271

9/9/2016 Page 5 dva_flywheel&chargeairpipe_rev1.xlsm

Page 34: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential25

DVA Loop - Results

Flywheel housing to Charge Air Pipe:

2. DVA is performed from Datum B of Flywheel housing to Charge Air pipe outlet center in both X&Y-directions

� Total distance from datum C of Flywheel housing to Charge Air pipe outlet center in Y-

direction is ~139.94mm

� Total assembly variation observed is ~0.83mm for MRSS in Y-direction

Page 35: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

Dimensional Variation Analysis Interface / Worksheet

Fastener Clx for : Assumptions: DATE: Note: Do Not Modify or Type In Any Colored Cells.

Author : All Clearance Holes share specifications. Units (mm or in) : mm OUTPUT SPECIFICATIONS (If Known)

CTR # : All Threaded Holes share specifications. Default Input CPK: 1 USL: (Enter a space if no USL)

Engine Model : All hole sets concentrically located. LSL: 0 (Enter a space if no LSL)

# Part Name - Feature Description + or -Drawing

Nominal

± Drawing

ToleranceInput CPK ST

Formula

Nominal

± Formula

ToleranceTolerance Squared 100.00% Rank % Cont Item/Part Number Rev No. Assumptions/Comments/Issues

1 Clearance Hole Diameter + 11.1 0.25 5.55 0.125 0.015625 7.54% 5

2 Cap Screw Diameter (locating diameter) - 9.89 0.11 4.945 0.055 0.003025 1.46% 7

3 Pattern True Position of Clearance Holes 0

4 Feature True Position (if specified composite) 0

5 Max Material Modifier (Y for Yes, N for No) N 0 0 Y

6 + 11.1 0.25 0 Y 5.55 0.125 0.015625 7.54% 5

7 - 9.89 0.11 0 Y 4.945 0.055 0.003025 1.46% 7

8 0 0 Y 0

9 0 0 Y 0

10 0 0 Y

11 Pattern True Position of Threaded Holes 0.5 0.25 0.0625 30.15% 1

12 Feature True Position (if specified composite) 0

13 Max Material Modifier (Y for Yes, N for No) Y 0.3 Y 0.15 0.0225 10.85% 3 General Purpose Tap Drill Tolerance

14 0.5 0 Y 0.25 0.0625 30.15% 1

15 0 0 Y 0

16 0.3 Y 0.15 0.0225 10.85% 3

17 Number of Bolts in Pattern (n=2 min) 4

18 Threaded Hole Tap Drill Depth (Max.) 15

19

Output Distribution Results: Std. Dev. Nominal Total ± Min Max Output Distribution Using MC Estimate

Worst Case (n=2 float) N/A 1.2100 1.1600 0.0500 2.3700 0.0000 None

RSS (± 3 Std. Dev.) (n=2 float) 0.1518 1.2100 0.4553 0.7547 1.6653 LSL Lower Upper

MRSS (± 3 Std. Dev.) (n=2 float) 0.1707 1.2100 0.5122 0.6978 1.7222 Design CPK = 4.0822 =Design CPK

X MC Estimate. (± 3 Std. Dev.) (n=4) 0.0796 0.9747 0.2388 0.7359 1.2134 0.0000% Or Desired CPK= #VALUE!

N=1: Linear Stack-Up (Worst Case)

N=2: .92 x Worst Case (Gilson) 99.7300%

N=3: .80 x Worst Case (Gilson)

Y or Blank (Gausian) (per QSP 3-15-01) N=4: .72 x Worst Case (Gilson) 0.13499% 0.13499%

5 N=5 or greater: 1.5 x RSS (Bender)

N (Uniform) Std. Dev. % in 1 Side out 1 Side out CPK 0.7359 0.9747 1.2134

± 3 99.7300% 0.135% 1350 PPM 1 Decimal Places 3 MIN @ 3 Std. Dev. 3 3 MAX @ 3 Std. Dev.

WC (Discrete Uniform) ± 4 99.9937% 0.00317% 32 PPM 1.33 Std. Dev. = 0.0796

CC (Discrete Uniform; only 1 Feature @ a Time) ± 4.5 99.9997% 0.00034% 3.4PPM 1.5 Σ WC = 0 Output = 0.974 ± 0.238

#..........

ST Statistical Tolerance Column

PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT PRIOR APPROVAL IN ACCORDANCE WITH TFE-CTC-0271

M ?

M ?

9/9/2016 Page 6 dva_flywheel&chargeairpipe_rev1.xlsm

Page 36: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

Dimensional Variation Analysis Interface / Worksheet

Fastener Clx for : Assumptions: DATE: Note: Do Not Modify or Type In Any Colored Cells.

Author : All Clearance Holes share specifications. Units (mm or in) : mm OUTPUT SPECIFICATIONS (If Known)

CTR # : All Threaded Holes share specifications. Default Input CPK: 1 USL: (Enter a space if no USL)

Engine Model : All hole sets concentrically located. LSL: 0 (Enter a space if no LSL)

# Part Name - Feature Description + or -Drawing

Nominal

± Drawing

ToleranceInput CPK ST

Formula

Nominal

± Formula

ToleranceTolerance Squared 100.00% Rank % Cont Item/Part Number Rev No. Assumptions/Comments/Issues

1 Clearance Hole Diameter + 11.065 0.115 5.5325 0.0575 0.00330625 0.59% 7

2 Cap Screw Diameter (locating diameter) - 9.89 0.11 4.945 0.055 0.003025 0.54% 9

3 Pattern True Position of Clearance Holes 0.8 0

4 Feature True Position (if specified composite) 0.5 0.25 0.0625 11.18% 3

5 Max Material Modifier (Y for Yes, N for No) Y 0.23 0 Y Not included in WC, RSS, MRSS.

6 + 11.065 0.115 0 Y 5.5325 0.0575 0.00330625 0.59% 7

7 - 9.89 0.11 0 Y 4.945 0.055 0.003025 0.54% 9

8 0.8 0 Y 0

9 0.5 0 Y 0.25 0.0625 11.18% 3

10 0.23 0 Y

11 Pattern True Position of Threaded Holes 0.7 0

12 Feature True Position (if specified composite) 0.8 0.4 0.16 28.63% 1

13 Max Material Modifier (Y for Yes, N for No) Y 0.45 Y 0.225 0.050625 9.06% 5 General Purpose Tap Drill Tolerance

14 0.7 0 Y 0

15 0.8 0 Y 0.4 0.16 28.63% 1

16 0.45 Y 0.225 0.050625 9.06% 5

17 Number of Bolts in Pattern (n=2 min) 2

18 Threaded Hole Tap Drill Depth (Max.) 28

19

Output Distribution Results: Std. Dev. Nominal Total ± Min Max Output Distribution Using MC Estimate

Worst Case (n=2 float) N/A 1.1750 1.9750 -0.8000 3.1500 0.0000 None

RSS (± 3 Std. Dev.) (n=2 float) 0.2492 1.1750 0.7476 0.4274 1.9226 LSL Lower Upper

MRSS (± 3 Std. Dev.) (n=2 float) 0.2804 1.1750 0.8411 0.3339 2.0161 Design CPK = 1.1294 =Design CPK

X MC Estimate. (± 3 Std. Dev.) (n=2) 0.2135 0.7233 0.6404 0.0829 1.3637 0.0352% Or Desired CPK= #VALUE!

N=1: Linear Stack-Up (Worst Case)

N=2: .92 x Worst Case (Gilson) 99.7300%

N=3: .80 x Worst Case (Gilson)

Y or Blank (Gausian) (per QSP 3-15-01) N=4: .72 x Worst Case (Gilson) 0.13499% 0.13499%

5 N=5 or greater: 1.5 x RSS (Bender)

N (Uniform) Std. Dev. % in 1 Side out 1 Side out CPK 0.0829 0.7233 1.3637

± 3 99.7300% 0.135% 1350 PPM 1 Decimal Places 3 MIN @ 3 Std. Dev. 3 3 MAX @ 3 Std. Dev.

WC (Discrete Uniform) ± 4 99.9937% 0.00317% 32 PPM 1.33 Std. Dev. = 0.2135

CC (Discrete Uniform; only 1 Feature @ a Time) ± 4.5 99.9997% 0.00034% 3.4PPM 1.5 Σ WC = 0 Output = 0.723 ± 0.64

ST Statistical Tolerance Column

#..........

PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT PRIOR APPROVAL IN ACCORDANCE WITH TFE-CTC-0271

M ?

M ?

9/9/2016 Page 7 dva_flywheel&chargeairpipe_rev1.xlsm

Page 37: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential26

DVA Loop - Results

Flywheel housing to Fan Support:

1. DVA is performed from Datum A of Flywheel housing to Fan Support end face in Z-direction

1. Width of Flywheel housing

2. Width of rear gear housing

3. Rear face cylinder Block to thrust face datum D

of Block

4. Thrust face datum D to front face of Block

5. Fan support mounting face pulley mounting face

assembly

6. Pulley thickness

7. Width of clamping plate

Page 38: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

Dimensional Variation Analysis Interface / Worksheet

DVA Objective: Assumptions: GUI Info DATE: Note: Do Not Modify or Type In Any Colored Cells.

Author : Output Units : OUTPUT SPEC. (If Known) Parameter Classification

CTR # : Default Input PPK: 1 USL:

Engine Model : MC Mean Shift = Cc: 0.25 LSL:(Enter a space if no SL) Selection

# Part Name - Feature Description + or -Drawing Nominal (Used in Formula)

Drawing Tol (Used in Formula)

Input Ppk STFormula

Nominal

± Formula

ToleranceTolerance

Squared100.00% Rank % Cont Item/Part Number Rev No. Assumptions/Comments/Issues

1 Flywheel Datum A to gear housing face + 128.6 0.1 128.6 0.1 0.01 2.41% 4 5402303_Page3_H7 0

2Gear housing width from flywheel mounting

face to Block mounting face+ 47 0.2 47 0.2 0.04 9.64% 2 5311333_Sheet2_B2 4

3

4 Rear face Datum G to Datum D + 150.115 0.1 150.115 0.1 0.01 2.41% 4 5253196_page5_H7 13

5

6 Datum D to front face datum E of Block + 597.885 0.1 597.885 0.1 0.01 2.41% 4 5253196_page5_H3 13

7

8

9Block front face to fan support pulley

mounting face+ 119.95 0.55 119.95 0.55 0.3025 72.89% 1 5398796_B4 0

10

11 Pulley thickness + 3.04 3.04 0.00% 8 3914645 8

12

13Clamping plate pulley mounting face to fan

mounting face+ 19 0.2 19 0.2 0.04 9.64% 2 5340802_D4 2

14

15 Parallelism w.r.t to datum A 0.05 0.05 0.0025 0.60% 7

16

17

18

19

20

Output Distribution Results: Std. Dev. Nominal Total ± Min Max Output Distribution Using MRSS

Worst Case N/A 1065.5900 1.3000 1064.2900 1066.8900 None None

RSS (± 3 Std. Dev.) 0.2147 1065.5900 0.6442 1064.9458 1066.2342 LSL Lower Upper USL

X MRSS (± 3 Std. Dev.) 0.2600 1065.5900 0.7800 1064.8100 1066.3700 Design PPK = =Design PPK

Monte-Carlo (± 3 Std. Dev.) Or Desired PPK=

N=1: Linear Stack-Up (Worst Case)

Place an "X" Next To Method N=2: .92 x Worst Case (Gilson) 99.7300%

3 N=3: .80 x Worst Case (Gilson)Y or Blank (Gaussian) (per QSP 3-15-01) N=4: .72 x Worst Case (Gilson) 0.13499% 0.13499%

N=5 or greater: 1.5 x RSS (Bender)

N (Uniform) Std. Dev. % in 1 Side out 1 Side out PPK MC Output 1064.8100 1065.5900 1066.3700

± 3 99.7300% 0.135% 1350 PPM 1 Decimal Places 3 MIN @ 3 Std. Dev. 3 3 MAX @ 3 Std. Dev.

WC (Discrete Uniform) ± 4 99.9937% 0.00317% 32 PPM 1.33 Std. Dev. = 0.2600

CC (Discrete Uniform; only 1 Feature @ a Time) ± 4.5 99.9997% 0.00034% 3.4PPM 1.5 Σ WC = 0 Output = 1065.59 ± 0.78

Distance from flywheel

housing datum A to

Fansupport - fan mounting

Sravanthi K

ISB6.7L - Keb program

ST Statistical Tolerance Column

PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT PRIOR APPROVAL IN ACCORDANCE WITH TFE-CTC-0271

9/9/2016 Page 1 dva1.xlsm

Page 39: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential27

DVA Loop - Results

Flywheel housing to Fan Support:

1. DVA is performed from Datum A of Flywheel housing to Fan Support end face in Z-direction

� Total distance from datum A of Flywheel housing to Fan support end face in Z-direction

is ~1065.59mm

� Total assembly variation observed is ~0.78mm for MRSS in Z-direction

Page 40: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential28

DVA Loop - Results

Flywheel housing to Fan Support:

2. DVA is performed from Datum B of Flywheel housing to Fan Support center in both X&Y-directions

1. Flywheel housing center (Scania dtm B)

to datum B (on drwg)

2. Flywheel house mounting hole on Block

to Datum A on Block

3. Datum A on Block to fan support

mounting hole center

4. Fan support mounting hole center to fan

support center

Page 41: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

Dimensional Variation Analysis Interface / Worksheet

DVA Objective: Assumptions: GUI Info DATE: Note: Do Not Modify or Type In Any Colored Cells.

Author : Output Units : OUTPUT SPEC. (If Known) Parameter Classification

CTR # : Default Input PPK: 1 USL:

Engine Model : MC Mean Shift = Cc: 0.25 LSL:(Enter a space if no SL) Selection

# Part Name - Feature Description + or -Drawing Nominal (Used in Formula)

Drawing Tol (Used in Formula)

Input Ppk ST Formula Nominal± Formula

ToleranceTolerance Squared 100.00% Rank % Cont Item/Part Number Rev No. Assumptions/Comments/Issues

1 Axis of datum B(Scania) to center of Flywheel 0 0

2 Position tol 0.08 0.04 0.0016 0.20% 11

3

4 Bonus

5

6

7 Flywheel B to dwg datum B + 147 0 147 0 0.00% 15 5402303_page2_H4 0

8 Position tol 0.08 0 0.04 0.0016 0.20% 11 5402303_page2_C2 0

9 Datum Shift of ZB datum, hole dia, tol 13.125 0.125 5402303_page2_C2 0

10 position tol 0.08 5402303_page2_C2 0

11 LMC 13.25

12 MMC 13

13 VC 12.92

14 Shift 0.165 0.165 0.027225 3.35% 7

15

16 Float neglected - dowel interference fit 0

17 Float tol 0

18

19 Block mounting hole to Datum A of Block + 16 16 0.00% 15 4990454_Page2_C6 11

20 Position tol 0.8 0.4 0.16 19.68% 2 4990454

21 Datum shift of Datum A 15.09 0.14 4990454

22 Hole dia, tol 0.2

23 LMC 15.23

24 MMC 14.95

25 VC 14.75

26 Shift 0.24 0.24 0.0576 7.08% 5

27

28Datum A on Block to fan support mounting hole - 193 193

0.00% 15 4990454_Page2_G4 11

29 Position tol 0.8 0.4 0.16 19.68% 2 4990454_Page2_H3 11

30

31

mounting hole center to fan support brg hole

center+ 54 54

0.00% 15 5396552_page1_G4 0

32 Position tol 1 0.5 0.25 30.75% 1 5398795_G4 0

33 Bonus 0.43 0.215 0.046225 5.69% 6

34 Datum Shift of Datum A 5398795_C6 0

35 Nominal 62.947 0.009

36 LMC 62.956

37 MMC 62.938

38 VC 62.688

39 shift 0.134 0.134 0.017956 2.21% 8

40

41

42 #2. Axis of OD to axis of ID on bearing - 0

43 concentricity 0.02 0.02 0.0004 0.05% 12

44

45 #. Axis of ID of bearing to axis of OD of fan hub - 0 0

46 #3. axis of OD Fan Hub to axis of ID of fan hub - 0 0

47 Position tolerance 0.5 0.25 0.0625 7.69% 4

48 Bonus neglected for threaded hole

49

50 Float between adaptor and plate

51 Hole dia, tol 25.61 0.01 1.33 0.005 1.4133E-05 0.00% 14

52 shaft dia, tol 25.375 0.025 1.33 0.0125 8.8332E-05 0.01% 13

53 float 0.235 0.1175 0.01380625 1.70% 10

54

55 Bonus 0.25 0.125 0.015625 1.92% 9

56

57

58

Output Distribution Results: Std. Dev. Nominal Total ± Min Max Output Distribution Using MRSS

Worst Case N/A 24.0000 2.6240 21.3760 26.6240 None None

RSS (± 3 Std. Dev.) 0.3006 24.0000 0.9017 23.0983 24.9017 LSL Lower Upper USL

X MRSS (± 3 Std. Dev.) 0.3381 24.0000 1.0144 22.9856 25.0144 Design PPK = =Design PPK

Monte-Carlo (± 3 Std. Dev.) Or Desired PPK=

N=1: Linear Stack-Up (Worst Case)

Place an "X" Next To Method N=2: .92 x Worst Case (Gilson) 99.7300%

N=3: .80 x Worst Case (Gilson)Y or Blank (Gaussian) (per QSP 3-15-01) N=4: .72 x Worst Case (Gilson) 0.13499% 0.13499%

6 N=5 or greater: 1.5 x RSS (Bender)N (Uniform) Std. Dev. % in 1 Side out 1 Side out PPK MC Output 22.9856 24.0000 25.0144

± 3 99.7300% 0.135% 1350 PPM 1 Decimal Places 3 MIN @ 3 Std. Dev. 3 3 MAX @ 3 Std. Dev.

WC (Discrete Uniform) ± 4 99.9937% 0.00317% 32 PPM 1.33 Std. Dev. = 0.3381

CC (Discrete Uniform; only 1 Feature @ a Time) ± 4.5 99.9997% 0.00034% 3.4PPM 1.5 Σ WC = 0 Output = 24 ± 1.014

Distance from flywheel housing

datum B to Fan support center

in X-direction

Sravanthi K

ISB6.7L - Keb program

ST Statistical Tolerance Column

PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT PRIOR APPROVAL IN ACCORDANCE WITH TFE-CTC-0271

9/9/2016 Page 2 dva1.xlsm

Page 42: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential29

DVA Loop - Results

Flywheel housing to Fan Support:

2. DVA is performed from Datum B of Flywheel housing to Fan Support center in both X&Y-directions

� Total distance from datum B of Flywheel housing to Fan support center in X-direction is

~24mm

� Total assembly variation observed is ~1mm for MRSS in X-direction

Page 43: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential30

DVA Loop - Results

Flywheel housing to Fan Support:

2. DVA is performed from Datum B of Flywheel housing to Fan Support center in both X&Y-directions

1. Flywheel housing center (Scania dtm B) to datum B (on drwg)

2. Flywheel house mounting hole on Block to Datum A on Block

3. Datum A on Block to fan support mounting hole center

4. Fan support mounting hole center to fan support center

Page 44: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

Dimensional Variation Analysis Interface / Worksheet

DVA Objective: Assumptions: GUI Info DATE: Note: Do Not Modify or Type In Any Colored Cells.

Author : Output Units : OUTPUT SPEC. (If Known) Parameter Classification

CTR # : Default Input PPK: 1 USL:

Engine Model : MC Mean Shift = Cc: 0.25 LSL:(Enter a space if no SL) Selection

# Part Name - Feature Description + or -Drawing Nominal (Used in Formula)

Drawing Tol (Used in Formula)

Input Ppk ST Formula Nominal± Formula

ToleranceTolerance

Squared100.00% Rank % Cont Item/Part Number Rev No. Assumptions/Comments/Issues

1 Axis of datum B(Scania) to center of Flywheel 0 0 0

2 Position tol 0.08 0.04 0.0016 0.21% 10

3

4 flywheel center to datum B of flywheel drwg + 75 75 0.00% 15 5402303_Page2-D2 0

5 Position tol 0.08 0.04 0.0016 0.21% 10 5402303_Page2-C2 0

6 datum shift of Flywheel datum B

7 Hole dai, tol 13.125 0.125

8 position tol 0.08

9 LMC 13.25

10 MMC 13

11 VC 12.92

12 Shift 0.165 0.165 0.027225 3.60% 6

13 Bonus 0.25 0.125 0.015625 2.06% 8

14

15

16 Datum B(flywheel drwg), block mounting hole to datum

C of Block+ 15 15 0.00% 15 4990454_Page3_C6 11

17 position tol of hole 0.8 0.4 0.16 21.13% 2 4990454_Page3_B8

18

19 Datum C of Block to fan support mounting hole - 404 404 0.00% 15 4990454_Page2_E1 11

20 position tol 0.8 0.4 0.16 21.13% 2 4990454_Page2_H3 11

21

22 fan support mounting holw to center + 88 88 0.00% 15 5398795_F2 0

23 position tol 1 0.5 0.25 33.02% 1

24 Bonus 0.43 0.215 0.046225 6.11% 5

25 Datum Shift of Datum A

26 Nominal 62.947 0.009

27 LMC 62.956

28 MMC 62.938

29 VC 62.688

30 shift 0.134 0.134 0.017956 2.37% 7

31

32 #2. Axis of OD to axis of ID on bearing - 0

33 concentricity 0.02 0.02 0.0004 0.05% 12

34

35 #. Axis of ID of bearing to axis of OD of fan hub - 0 0

36 #3. axis of OD Fan Hub to axis of ID of fan hub - 0 0

37 Position tolerance 0.5 0.25 0.0625 8.26% 4

38 Bonus neglected for threaded hole

39

40 Float between adaptor and plate

41 Hole dia, tol 25.61 0.01 1.33 0.005 1.4133E-05 0.00% 14

42 shaft dia, tol 25.375 0.025 1.33 0.0125 8.8332E-05 0.01% 13

43 float 0.235 0.1175 0.01380625 1.82% 9

44

45

46

47

48

49

50

51

Output Distribution Results: Std. Dev. Nominal Total ± Min Max Output Distribution Using MRSS

Worst Case N/A -226.0000 2.4240 -228.4240 -223.5760 None None

RSS (± 3 Std. Dev.) 0.2900 -226.0000 0.8701 -226.8701 -225.1299 LSL Lower Upper USL

X MRSS (± 3 Std. Dev.) 0.3263 -226.0000 0.9788 -226.9788 -225.0212 Design PPK = =Design PPK

Monte-Carlo (± 3 Std. Dev.) Or Desired PPK=

N=1: Linear Stack-Up (Worst Case)

Place an "X" Next To Method N=2: .92 x Worst Case (Gilson) 99.7300%

N=3: .80 x Worst Case (Gilson)Y or Blank (Gaussian) (per QSP 3-15-01) N=4: .72 x Worst Case (Gilson) 0.13499% 0.13499%

5 N=5 or greater: 1.5 x RSS (Bender)

N (Uniform) Std. Dev. % in 1 Side out 1 Side out PPK MC Output -226.9788 -226.0000 -225.0212

± 3 99.7300% 0.135% 1350 PPM 1 Decimal Places 3 MIN @ 3 Std. Dev. 3 3 MAX @ 3 Std. Dev.

WC (Discrete Uniform) ± 4 99.9937% 0.00317% 32 PPM 1.33 Std. Dev. = 0.3263

CC (Discrete Uniform; only 1 Feature @ a Time) ± 4.5 99.9997% 0.00034% 3.4PPM 1.5 Σ WC = 0 Output = -226 ± 0.978

Distance from flywheel housing

datum B to Fan support center

in Y-direction

Sravanthi K

ISB6.7L - Keb Program

ST Statistical Tolerance Column

PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT PRIOR APPROVAL IN ACCORDANCE WITH TFE-CTC-0271

9/9/2016 Page 3 dva1.xlsm

Page 45: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential31

DVA Loop - Results

Flywheel housing to Fan Support:

2. DVA is performed from Datum B of Flywheel housing to Fan Support center in both X&Y-directions

� Total distance from datum B of Flywheel housing to Fan support center in Y-direction is

~226mm

� Total assembly variation observed is ~0.97mm for MRSS in Y-direction

Page 46: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential32

DVA Loop - Results

Flywheel housing to Fan Support:

3. DVA is performed from Datum C of Flywheel housing to Fan Support center in both X&Y-directions

1. Datum C of flywheel housing (Scania dtm) to center of

housing

2. Flywheel housing center to datum B of housing (on drwg)

3. Flywheel house mounting hole on Block to Datum A on

Block

4. Datum A on Block to fan support mounting hole center

5. Fan support mounting hole center to fan support center

Page 47: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

Dimensional Variation Analysis Interface / Worksheet

DVA Objective: Assumptions: GUI Info DATE: Note: Do Not Modify or Type In Any Colored Cells.

Author : Output Units : OUTPUT SPEC. (If Known) Parameter Classification

CTR # : Default Input PPK: 1 USL:

Engine Model : MC Mean Shift = Cc: 0.25 LSL:(Enter a space if no SL) Selection

# Part Name - Feature Description + or -Drawing Nominal (Used in Formula)

Drawing Tol (Used in Formula)

Input Ppk ST Formula Nominal± Formula

ToleranceTolerance Squared 100.00% Rank % Cont Item/Part Number Rev No. Assumptions/Comments/Issues

1

2

3

4

5

6

7 Flywheel B to dwg datum B + 147 0 147 0 0.00% 15 5402303_page2_H4 0

8 Position tol 0.08 0 0.04 0.0016 0.19% 11 5402303_page2_C2 0

9 Datum Shift of ZB datum, hole dia, tol 13.125 0.125 5402303_page2_C2 0

10 position tol 0.08 5402303_page2_C2 0

11 LMC 13.25

12 MMC 13

13 VC 12.92

14 Shift 0.165 0.165 0.027225 3.28% 7

15

16 Float neglected - dowel interference fit 0

17 Float tol 0

18

19 Block mounting hole to Datum A of Block + 16 16 0.00% 15 4990454_Page2_C6 11

20 Position tol 0.8 0.4 0.16 19.29% 2 4990454

21 Datum shift of Datum A 15.09 0.14 4990454

22 Hole dia, tol 0.2

23 LMC 15.23

24 MMC 14.95

25 VC 14.75

26 Shift 0.24 0.24 0.0576 6.95% 6

27

28Datum A on Block to fan support mounting hole - 193 193

0.00% 15 4990454_Page2_G4 11

29 Position tol 0.8 0.4 0.16 19.29% 2 4990454_Page2_H3 11

30

31

mounting hole center to fan support brg hole

center+ 54 54

0.00% 15 5398795_H3 0

32 Position tol 1 0.5 0.25 30.15% 1 5398795_G4 0

33 Bonus neglected for threaded holes

34 Datum Shift of Datum A 5398795_C6 0

35 Nominal 62.947 0.009

36 LMC 62.956

37 MMC 62.938

38 VC 62.688

39 shift 0.134 0.134 0.017956 2.17% 8

40

41

42 #2. Axis of OD to axis of ID on bearing - 0

43 concentricity 0.02 0.02 0.0004 0.05% 12

44

45 #. Axis of ID of bearing to axis of OD of fan hub - 0 0

46 #3. axis of OD Fan Hub to axis of ID of fan hub - 0 0

47 Position tolerance 0.5 0.25 0.0625 7.54% 4

48 Bonus neglected for threaded hole

49

50 Float between adaptor and plate

51 Hole dia, tol 25.61 0.01 1.33 0.005 1.4133E-05 0.00% 14

52 shaft dia, tol 25.375 0.025 1.33 0.0125 8.8332E-05 0.01% 13

53 float 0.235 0.1175 0.01380625 1.66% 10

54

55 Datum C(scania) to flywheel center [arc length] + 68.61551705 68.61551705 0.00% 15 5402303

56 Position tol 0.5 0.25 0.0625 7.54% 4

57 Bonus 0.25 0.125 0.015625 1.88% 9

58

Output Distribution Results: Std. Dev. Nominal Total ± Min Max Output Distribution Using MRSS

Worst Case N/A 92.6155 2.6590 89.9565 95.2745 None None

RSS (± 3 Std. Dev.) 0.3036 92.6155 0.9107 91.7048 93.5262 LSL Lower Upper USL

X MRSS (± 3 Std. Dev.) 0.3415 92.6155 1.0245 91.5910 93.6400 Design PPK = =Design PPK

Monte-Carlo (± 3 Std. Dev.) Or Desired PPK=

N=1: Linear Stack-Up (Worst Case)

Place an "X" Next To Method N=2: .92 x Worst Case (Gilson) 99.7300%

N=3: .80 x Worst Case (Gilson)Y or Blank (Gaussian) (per QSP 3-15-01) N=4: .72 x Worst Case (Gilson) 0.13499% 0.13499%

6 N=5 or greater: 1.5 x RSS (Bender)N (Uniform) Std. Dev. % in 1 Side out 1 Side out PPK MC Output 91.5910 92.6155 93.6400

± 3 99.7300% 0.135% 1350 PPM 1 Decimal Places 3 MIN @ 3 Std. Dev. 3 3 MAX @ 3 Std. Dev.

WC (Discrete Uniform) ± 4 99.9937% 0.00317% 32 PPM 1.33 Std. Dev. = 0.3415

CC (Discrete Uniform; only 1 Feature @ a Time) ± 4.5 99.9997% 0.00034% 3.4PPM 1.5 Σ WC = 0 Output = 92.615 ± 1.024

Distance from flywheel housing

datum B to Fan support center

in X-direction

Sravanthi K

ISB6.7L - Keb program

ST Statistical Tolerance Column

PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT PRIOR APPROVAL IN ACCORDANCE WITH TFE-CTC-0271

9/9/2016 Page 4 dva1.xlsm

Page 48: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential33

DVA Loop - Results

Flywheel housing to Fan Support:

3. DVA is performed from Datum C of Flywheel housing to Fan Support center in both X&Y-directions

� Total distance from datum C of Flywheel housing to Fan support center in X-direction is

~92.6mm

� Total assembly variation observed is ~1.02mm for MRSS in X-direction

Page 49: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential34

DVA Loop - Results

Flywheel housing to Fan Support:

3. DVA is performed from Datum C of Flywheel housing to Fan Support center in both X&Y-directions

1. Datum C of flywheel housing (Scania dtm) to center of

housing

2. Flywheel housing center to datum B of housing (on drwg)

3. Flywheel house mounting hole on Block to Datum A on

Block

4. Datum A on Block to fan support mounting hole center

5. Fan support mounting hole center to fan support center

Page 50: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

Dimensional Variation Analysis Interface / Worksheet

DVA Objective: Assumptions: GUI Info DATE: Note: Do Not Modify or Type In Any Colored Cells.

Author : Output Units : OUTPUT SPEC. (If Known) Parameter Classification

CTR # : Default Input PPK: 1 USL:

Engine Model : MC Mean Shift = Cc: 0.25 LSL:(Enter a space if no SL) Selection

# Part Name - Feature Description + or -Drawing Nominal (Used in Formula)

Drawing Tol (Used in Formula)

Input Ppk ST Formula Nominal± Formula

ToleranceTolerance

Squared100.00% Rank % Cont Item/Part Number Rev No. Assumptions/Comments/Issues

1 Datum C(scania) to flywheel center [arc length] + 256.0765958 256.0765958 0 0.00% 15 5402303

2 position tol 0.5 0.25 0.0625 7.64% 4

3

4 flywheel center to datum B of flywheel drwg + 75 75 0.00% 15 5402303_Page2-D2 0

5 Position tol 0.08 0.04 0.0016 0.20% 11 5402303_Page2-C2 0

6 datum shift of Flywheel datum B

7 Hole dai, tol 13.125 0.125

8 position tol 0.08

9 LMC 13.25

10 MMC 13

11 VC 12.92

12 Shift 0.165 0.165 0.027225 3.33% 7

13 Bonus 0.25 0.125 0.015625 1.91% 9

14

15

16 Datum B(flywheel drwg), block mounting hole to datum

C of Block+ 15 15 0.00% 15 4990454_Page3_C6 11

17 position tol of hole 0.8 0.4 0.16 19.56% 2 4990454_Page3_B8

18

19 Datum C of Block to fan support mounting hole - 404 404 0.00% 15 4990454_Page2_E1 11

20 position tol 0.8 0.4 0.16 19.56% 2 4990454_Page2_H3 11

21

22 fan support mounting holw to center + 88 88 0.00% 15 5398795_F2 0

23 position tol 1 0.5 0.25 30.56% 1

24 Bonus 0.43 0.215 0.046225 5.65% 6

25 Datum Shift of Datum A

26 Nominal 62.947 0.009

27 LMC 62.956

28 MMC 62.938

29 VC 62.688

30 shift 0.134 0.134 0.017956 2.20% 8

31

32 #2. Axis of OD to axis of ID on bearing - 0

33 concentricity 0.02 0.02 0.0004 0.05% 12

34

35 #. Axis of ID of bearing to axis of OD of fan hub - 0 0

36 #3. axis of OD Fan Hub to axis of ID of fan hub - 0 0

37 Position tolerance 0.5 0.25 0.0625 7.64% 4

38 Bonus neglected for threaded hole

39

40 Float between adaptor and plate

41 Hole dia, tol 25.61 0.01 1.33 0.005 1.4133E-05 0.00% 14

42 shaft dia, tol 25.375 0.025 1.33 0.0125 8.8332E-05 0.01% 13

43 float 0.235 0.1175 0.01380625 1.69% 10

44

45

46

47

48

49

50

51

Output Distribution Results: Std. Dev. Nominal Total ± Min Max Output Distribution Using MRSS

Worst Case N/A 30.0766 2.6340 27.4426 32.7106 None None

RSS (± 3 Std. Dev.) 0.3015 30.0766 0.9044 29.1722 30.9810 LSL Lower Upper USL

X MRSS (± 3 Std. Dev.) 0.3392 30.0766 1.0175 29.0591 31.0940 Design PPK = =Design PPK

Monte-Carlo (± 3 Std. Dev.) Or Desired PPK=

N=1: Linear Stack-Up (Worst Case)

Place an "X" Next To Method N=2: .92 x Worst Case (Gilson) 99.7300%

N=3: .80 x Worst Case (Gilson)Y or Blank (Gaussian) (per QSP 3-15-01) N=4: .72 x Worst Case (Gilson) 0.13499% 0.13499%

6 N=5 or greater: 1.5 x RSS (Bender)

N (Uniform) Std. Dev. % in 1 Side out 1 Side out PPK MC Output 29.0591 30.0766 31.0940

± 3 99.7300% 0.135% 1350 PPM 1 Decimal Places 3 MIN @ 3 Std. Dev. 3 3 MAX @ 3 Std. Dev.

WC (Discrete Uniform) ± 4 99.9937% 0.00317% 32 PPM 1.33 Std. Dev. = 0.3392

CC (Discrete Uniform; only 1 Feature @ a Time) ± 4.5 99.9997% 0.00034% 3.4PPM 1.5 Σ WC = 0 Output = 30.076 ± 1.017

Distance from flywheel housing

datum B to Fan support center

in Y-direction

Sravanthi K

ISB6.7L - Keb Program

ST Statistical Tolerance Column

PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT PRIOR APPROVAL IN ACCORDANCE WITH TFE-CTC-0271

9/9/2016 Page 5 dva1.xlsm

Page 51: EWR19888 techreport page1...2017/02/24  · Sravanthi K ISB6.7L engine -Keb ST Statistical Tolerance Column PROPRIETARY - NOT TO BE RELEASED OUTSIDE CUMMINS OR ITS SUBSIDIARIES WITHOUT

9/3/2016 Cummins Confidential35

DVA Loop - Results

Flywheel housing to Fan Support:

3. DVA is performed from Datum C of Flywheel housing to Fan Support center in both X&Y-directions

� Total distance from datum C of Flywheel housing to Fan Support center in Y-direction is

~30.7mm

� Total assembly variation observed is ~1mm for MRSS in Y-direction