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DYNAMICS OF RECIPROCATING ENGINES
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DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

Mar 06, 2018

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Page 1: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

DYNAMICS OF RECIPROCATING ENGINES

Page 2: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

Indicator Diagrams

Page 3: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

In-Line Engines

Page 4: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

V Engines

Page 5: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

GAS FORCES

Binomial Theorem:

So,

Since in most engines,

is so small, and only the first two terms of the series may be taken with sufficient accuracy.

Therefore, and since

We can write and finally

Page 6: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

It is important to note that always angular velocity () is assumed constant. Therefore, acceleration of the piston may be obtained as, -------------------------------------------------------------------------------------------------------

Using Binomial theorem for the denominator of this ratio and taking only first two terms of the series,

Therefore, Similarly,

Page 7: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

T12k + xi X (F14j)=0

T12=-F14 x k =-P tan x k

T21=P tan x k F14

P

F12

T12

x

Making appropriate substitutions and neglecting higher order terms,

torque delivered by the crank to the shaft is obtained

Page 8: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

EQUIVALENT MASSES

• A A

• m3 = G3

• G3

• B

• IG3

• B

• 1) Total masses should be the same:

• 2) The mass center positions should be the same:

• (If , )

In practice,

for a connecting

rod

Page 9: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

EQUIVALENT MASSES

• The first two conditions is called STATIC EQIVALENCE.

• 3) The mass moment of inertias should be the same:

• The third condition is called DYNAMIC EQIVALENCE.

• For a connecting rod of a slider-crank mechanism, our aim is to divide the total mass into two masses; one, at point A (rotating) and the other one, at point B (reciprocating). The third condition does not conform our aim , therefore it is not satisfied throughout the analysis of connecting rod.

Page 10: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

Dividing the crank mass into two parts, at O2 and A, regarding the static

equivalence conditions.

+0

Page 11: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

INERTIA FORCES

Constant angular velocity assumption for crank gives the acceleration of point A as,

Inertia force at A

Acceleration of the piston has been found as,

Inertia force of the reciprocating parts

The components of total inertia force,

Secondary inertia force

Primary

İnertia

force

Page 12: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

Inertia Torque

T12

F12

F14=-mBaB tan

-mBaB

-mAaA T12k + xi X (- F14j)=0

T12=F14 x k =-mBaB tan x k

Making appropriate substitutions, neglecting higher

order terms and using trigonometric identities, inertia

torque exerted by the engine on the shaft is obtained ,

Inertia torque is a periodic function, including the first three harmonics.

x

Page 13: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

BEARING LOADS IN THE SINGLE-CYLINDER ENGINE

• The resultant bearing loads in a single-cylinder engine are made up of due to the following four forces:

• 1) Gas force (examined at the beginning).

• 2) Inertia force due to the mass of piston m4.

• 3) Inertia force due to the mass of connecting rod m3B at piston-pin end.

• 4) Inertia force due to the mass of connecting rod m3A at crank-pin end.

• (It is assumed that crank has been balanced.)

Page 14: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

2) Inertia force due to the mass of piston m4

F14’’

F34’’

Page 15: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

3) Inertia force due to the mass of connecting

rod m3B at piston-pin end

R

F43’’’

R

Page 16: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

4) Inertia force due to the mass of connecting rod m3A at crank-pin end

O2

r

r

A

If a counterweight of

m3A is added at point C,

O2

A

C

C

r

r

no bearing force

will act at O2.

Therefore shaking

force due to m3A

İs eliminated

FBD

Page 17: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

Superposition

Page 18: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

CRANKSHAFT TORQUE

• O2 1 B MO2=0 • T21

• F21

F41

The torque delivered by the crankshaft to the load.

Page 19: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

ENGINE SHAKING FORCES (due to only reciprocating masses)

Shaking Force: (Linear vibration in x direction)

Shaking Couple: (Torsional vibration about crank center)

Graphically, F21x = OA’+OB’

for

Page 20: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

PROBLEM Stroke=2r =90 mm r=45 mm

d=100 mm A=d2/4=1002/4=7853.98 mm2=7.854x10-3 m2

n=4400 rpm =4400(2)/60=460.767 r/s

m3A=0.8 kg m3B=0.38 kg m4=1.64 kg

Obtain cylinder pressure for the 30% expansion case.

p= 1.857 Mpa=1857000 Pa(N/m2)

P=1857000(7.854x10-3 ) = 14584.878 N

Page 21: DYNAMICS OF RECIPROCATING ENGINES - Kişisel …kisi.deu.edu.tr/saide.sarigul/Dyn_Rec_Eng.pdf · total mass into two masses; one, at point A (rotating) and the other one, at point

Force Calculations F41=-[(0.38+1.64)(-3578.663)+14584.878](0.1155)j

F41= -849.616j N

F41

F34=[1.64(-3578.663)+14584.878]i – 849.616j = 8715.87i-849.616j N