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m odel no. G eom etry B oundary condition in FE M odel 1st 2nd 3rd 4th (A nsys) 3 A ssem bly R ig only -no bracing or stiffeners added A llnodes on upperm ostsurface FULLY CO N STR A IN E D 35 - - - Longitud inal(x) Transverse (y) 1sttorsio nal 4 A ddition of2 x sm lcross braces,1 x strap,1 x large X-brace A llnodes on upperm ostsurface FULLY CO N STR A IN E D 93 100 150 185 Longitud inal(x) Transverse (y) 1sttorsio nal 5 A ddition ofm em bers to approxim ate a sim ilargeom etry used by Tim H ayler (N ov04) A llnodes on upperm ostsurface FULLY CO N STR A IN E D 62 96 103 185 Longitud inal(x) Transverse (y) 1sttorsio nal 6 A ddition ofthe 2 x sm lcross braces (as used in 4),to the geom etry used in 5 A llnodes on upperm ostsurface FULLY CO N STR A IN E D 92 100 140 185 Longitud inal(x) Transverse (y) 1sttorsio nal 7 B racing added from im plem entation ring dow n to ~ penultim ate m ass in longitudinaldirection A llnodes on upperm ostsurface FULLY CO N STR A IN E D 94 132 176 188 Transverse (y) Longitudinal(x) 1sttorsio nal M O DE FREQ U EN C IES FEA History: Lower Structure Table 1: Early results (from ANSYS Worbench 8.0)
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FEA History: Lower Structure

Jan 03, 2016

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FEA History: Lower Structure. Table 1: Early results (from ANSYS Worbench 8.0). Model 5. Model 6. Model 7. Model 4. 1 st mode = 93Hz. 1 st mode = 92Hz. 2 nd mode = 96Hz. 1 st mode = 94Hz. Bracing added in locations that mimic approach the approach used by Tim in November. - PowerPoint PPT Presentation
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Page 1: FEA History: Lower Structure

model no. Geometry Boundary condition in FE Model 1st 2nd 3rd 4th(Ansys)

3Assembly Rig only - no bracing or stiffeners added

All nodes on uppermost surface FULLY CONSTRAINED

35 - - -

Longitudinal (x) Transverse (y) 1st torsional

4Addition of 2 x sml cross braces, 1 x strap, 1 x large X-brace

All nodes on uppermost surface FULLY CONSTRAINED

93 100 150 185

Longitudinal (x) Transverse (y) 1st torsional

5

Addition of members to approximate a similar geometry used by Tim Hayler (Nov04)

All nodes on uppermost surface FULLY CONSTRAINED

62 96 103 185

Longitudinal (x) Transverse (y) 1st torsional

6Addition of the 2 x sml cross braces (as used in 4), to the geometry used in 5

All nodes on uppermost surface FULLY CONSTRAINED

92 100 140 185

Longitudinal (x) Transverse (y) 1st torsional

7

Bracing added from implementation ring down to ~ penultimate mass in longitudinal direction

All nodes on uppermost surface FULLY CONSTRAINED

94 132 176 188

Transverse (y) Longitudinal (x) 1st torsional

MODE FREQUENCIES

FEA History: Lower Structure

Table 1: Early results (from ANSYS Worbench 8.0)

Page 2: FEA History: Lower Structure

Model 4

1st mode= 93Hz

2nd mode= 100Hz

Model 5

2nd mode= 96Hz

Bracing added in locations that mimic approach the approach used by Tim in November

Model 6

1st mode= 92Hz

Addition of bracing as circled above (as was used in model 4)1st mode (longitudinal) increased by 30Hz2nd mode (transverse) of 100Hz

Model 7

1st mode= 94Hz

Quick addition of bracing as circled above 1st mode now in transverse direction

Graphical accompaniment to Table 1

Page 3: FEA History: Lower Structure

8 as in model 7All nodes round the edge fully constrained

90 128 172 186

Transverse (y) Longitudinal (x) 1st torsional

9

Moving the location of the bracing further down below the penultimate mass (lonitudinal only)

All nodes on uppermost surface FULLY CONSTRAINED

88 126 138.82 153

Transverse (y) Longitudinal (x) 1st torsionalcrossbraces

moving!

10

Bracing from implementation ring down to ~ penultimate mass in longitudinal and transverse directions

All nodes on uppermost surface FULLY CONSTRAINED

120 152 186 204

Transverse (y) Longitudinal (x) 1st torsional

11 As above see pic 94 115 154 192

Transverse (y) Longitudinal (x) 1st torsional

12 As above see pic 96 126 161 197

Transverse (y) Longitudinal (x) 1st torsional

13 Shortened structure!All nodes on uppermost surface FULLY CONSTRAINED

140 152 187 222

Transverse (y) Longitudinal (x) 1st torsional

FEA continued….

Table 2: further results from ANSYS

Page 4: FEA History: Lower Structure

Model 8

1st mode= 90Hz

Change in BC’s in model – constraining all nodes round edge of top surface1st mode goes down

Model 9

2nd mode= 126Hz

Quick change - lengthening of braces to support further down the structure1st mode still in transverse (88Hz)2nd, 3rd, and 4th modes all in the lengthened braces as shown above

Model 10

Addition of bracing to increase the Transverse modeThe following two models involved using the same geometry, changing the combinations of displacement constraints used at the top of the lower structure

1st mode= 120Hz

Model 13

Shortening of overall length of lower structure used in model, following assessment of overall structural dimension in SoildWorks

(Reduced height in location shown above! Initial numbers had stemmed from limitations set by )

1st mode= 140Hz

Graphical accompaniment to Table 2

Page 5: FEA History: Lower Structure

*Most recent Model of Lower Structure*

Boundary Conditions:

Uppermost surface of implementation ring fixed in all DOF

Mesh: (in Workbench 8.0)

Default setting: Global Control – basic, Relevance: -100

nodes:119 957, elements: 60 139

Page 6: FEA History: Lower Structure

*Results: Most recent model of Lower Structure*

(nodes:119 957, elements: 60 139)

1st Mode: 128 Hz (transverse - see pic below)

2nd Mode: 140 Hz (longitudinal)

3rd Mode: 166 Hz (1st Torsional)

4th Mode: 214 Hz (2nd Transverse)

Page 7: FEA History: Lower Structure

Model Geometry: Lower Structure….General comments/assumptions/

Limitation:

Model Geometry creates a ‘uniform transition’ between the basic structure and stiffening members at all joins (as highlighted opposite)

•consciously left in additional material in locations where further detailing is ongoing

•all bracing member as solid bars so far (for speed)

Page 8: FEA History: Lower Structure

Planned change/improvements: Lower structure

•Widening of footprint to improve improve access (in progress)

•Fcomplete the detail at all connection locations (I.e. with clamps/stiffeners etc) to mass