Static Force Analysis - Computer-Aided Analysis of Machine Dynamics - Lecture Notes, Study notes of Computer-Aided Analysis of Machine Dynamics

Main objectives of this course are: 1. Recognize constrained kinematic chains embedded in larger engineering systems 2. Identify forward and inverse dynamic problems 3. Use numerical integration methods and other numerical solution techniques 4. Communicate well using verbal, written and electronic methods. Key points for this lecture are: Static Force Analysis for Skid Loader, Virtual Work, Trunnion Mount Hydraulic Cylinder, Sewing Machine, Crank Torque, Velocity Solution, Static Force Analysi

Typology: Study notes

2012/2013

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Static Force Analysis for Skid Loader - Scalar
A trunnion mount hydraulic cylinder actuates the arm of a skid steer loader as shown below. At
this position, e = 40 inches, = 61.131°, e
= -12 ips,
= -0.3625 rad/s.
Determine the force on the hydraulic cylinder required to lower an 800 lbf payload attached to
point D by a cable. The payload moves with constant velocity at the position shown. You may
neglect the effects of friction. The weight of the arm and cylinder are small compared to the
payload. Show your work.
FCYLINDER __________________________
What corresponding hydraulic pressure would be required for a cylinder with a 3 inch DIA bore?
PCYLINDER __________________________
Is this value reasonable? Why?
If you include friction between the piston and cylinder wall, will it increase or decrease your
computation for pressure.
increase decrease Why?
What value would you use for the coefficient of friction between the piston and cylinder wall?
_________________________________ Why?
Should your analysis be different if the cylinder were retracting at constant velocity instead of
the payload moving at constant velocity?
yes no Why?
A
B
C
e
Not to scale
AB = 36 inches
AC = 42 inches
AD = 96 inches
= 16°

D 
Payload

sin / AB = sin / e
= 52.01°
 = 77.131°
4
M on 4 about A CCW+
-(FC sin ) AC +(P sin() AD = 0
FC = 2261.9 lbf
2261.9 lbf up/left
320 psi A = D2 / 4 = 7.069 in2
OK, industrial hydraulics often go to 3000 psi
pressure pushes up
friction force will be up opposing piston motion
0.1 lubricated
constant e
means
will not be constant means velocity of the payload will
not be constant, therefore must account for acceleration of payload mass
P
D
C
F14y
F14x
A
FC

4

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Static Force Analysis for Skid Loader - Scalar

A trunnion mount hydraulic cylinder actuates the arm of a skid steer loader as shown below. At this position, e = 40 inches,  = 61.131°, e = -12 ips, ^ = -0.3625 rad/s.

Determine the force on the hydraulic cylinder required to lower an 800 lbf payload attached to point D by a cable. The payload moves with constant velocity at the position shown. You may neglect the effects of friction. The weight of the arm and cylinder are small compared to the payload. Show your work.

FCYLINDER __________________________

What corresponding hydraulic pressure would be required for a cylinder with a 3 inch DIA bore?

PCYLINDER __________________________

Is this value reasonable? Why?

If you include friction between the piston and cylinder wall, will it increase or decrease your computation for pressure.

increase decrease Why?

What value would you use for the coefficient of friction between the piston and cylinder wall?

 _________________________________ Why?

Should your analysis be different if the cylinder were retracting at constant velocity instead of the payload moving at constant velocity?

yes no Why?

A

B

C

e

Not to scale AB = 36 inches AC = 42 inches AD = 96 inches = 16°

D 

Payload

sin  / AB = sin  / e  = 52.01°  = 77.131°

∑M on 4 about A CCW+ -(FC sin ) AC +(P sin() AD = 0 FC = 2261.9 lbf

2261.9 lbf up/left

320 psi A =  D^2 / 4 = 7.069 in^2

OK, industrial hydraulics often go to 3000 psi

pressure pushes up friction force will be up opposing piston motion

0.1 lubricated

constant e^ means ^ will not be constant means velocity of the payload will not be constant, therefore must account for acceleration of payload mass

P

D

C

F 14 y F 14 x

A

FC

Static Force Analysis for Four Bar - Scalar

M on 4 about D CCW+

  • F 34 x^ (CD) sin 65.173- F 34 y^ (CD) sin 24.827 + FQ (DQ) sin 77 = 0 40.842 F 34 x^ + 18.895 F 34 y^ = 4676.98 N

M on 3 about B CCW+

  • F 43 x^ (BC) sin 13.151 + F 43 y^ (BC) sin 76.849 + FP (BP) sin 60 = 0
  • 13.651 F 43 x^ + 58.426 F 43 y^ = -2987.78 N

F on 4 right + F 34 x^ - FQ cos 37.827 + F 14 x^ = 0 F 14 x^ = 75.980 N  F on 4 up + F 34 y^ - FQ sin 37.827 + F 14 y^ = 0 F 14 y^ = 52.360 N   F on 3 right + F 43 x^ - FP cos 46.849 + F 23 x^ = 0 F 23 x^ = 184.580 N  F on 3 up + F 43 y^ + FP sin 46.849 + F 23 y^ = 0 F 23 y^ = -39.138 N

M on 2 about A CCW+ - F 32 x^ (AB) sin 65 + F 32 y^ (AB) sin 25 + T 12 = 0 T 12 = - 5514.8 N.cm   F on 2 right + F 12 x^ + F 32 x^ = 0 F 12 x^ = 184.580 N  F on 2 up F 12 y^ + F 32 y^ = 0 F 12 y^ = -39.138 N

F (^) Q = 200 N F 34 x

F 34 y

24.827

65.173

F 14 y

F 14 x

65.173

24.827

77 

D

C

CD = 45 cm DQ = 24 cm CQ = 21 cm

Q

37.827

F 43 y

F 43 x F 23 x

76.849 F 23 y

13.151

46.849

B

C

F (^) P = 150 N

BC = 60 cm BP = 23 cm CP = 37 cm

P

13.151 60 

76.849

  70.295N

81.993N

F

F

2987.78N

4676.98N

F

F

y 34

x 34 y 34

x 34

F 12 x

AB = 30 cm

F 32 y

F 32 x

F 12 y 65 

25 

A

B

T 12 25 

65 

A 65 

T 12

D

77 

60 

C B P

Q

F (^) Q = 200 N

F (^) P = 150 N AB = 30 cm BC = 60 cm CD = 45 cm AD = 90 cm BP = 23 cm DQ = 24 cm

3 4

2

1 D 1

13.151

65.173

Static Force Analysis for Four Bar - Matrix

F on 2 right + F 12 x^ + F 32 x^ = 0  F on 2 up + F 12 y^ + F 32 y^ = 0  M on 2 about A CCW + - F 32 x^ r (^) B/Ay^ + F 32 y^ r (^) B/Ax^ + T 12 = 0   F on 3 right + F 23 x^ + F 43 x^ + FPx^ = 0  F on 3 up + F 23 y^ + F 43 y^ + FPy= 0  M on 3 about P CCW + - F 23 x^ r (^) B/Py^ + F 23 y^ r (^) B/Px^ - F 43 x^ r (^) C/Py^ + F 43 y^ r (^) C/Px^ = 0

F on 4 right + F 34 x^ + F 14 x^ + FQx^ = 0  F on 4 up + F 34 y^ + F 14 y^ + FQx^ = 0  M on 4 about Q CCW + - F 34 x^ r (^) C/Qy^ + F 34 y^ r (^) C/Qx^ - F 14 x^ r (^) D/Qy^ + F 14 y^ r (^) D/Qx^ = 0

F

F

F

F

T

F

F

F

F

F

F

F

F

0 0 0 0 r r r r 0

0 0 r r r r 0 0 0

0 0 r r 0 0 0 0 1

y Q

x Q

y P

x P

12

14 y

14 x

34 y

34 x

23 y

23 x

12 y

12 x

x D/Q

y D/Q

x C/Q

y C/Q

x C/P

y C/P

x B/P

y B/P

x B/A

y B/A

FP

= 150 N @ 133.151 = - 102.589 + j 109.433 N FQ

= 200 N @ 217.827 = - 157.973 - j 122.656 N B/A = 30 cm @ 65 = 12.678 + j 27.189 cm B/P = 23 cm @ 193.151 = -22.396 - j 5.233 cm C/P = 37 cm @ 13.151 = 36.030 + j 8.418 cm C/Q = 21 cm @ 114.827 = -8.817 + j 19.059 cm D/Q = 24 cm @ -65.173 = 10.077 - j 21.782 cm

F 12 x

F 32 y

F 32 x

F 12 y 65  A

B T 12

F 43 y

F 43 x F 23 x

F 23 y

B

C

F (^) P = 150 N

P 13.151

60  46.849

F 14 y

F (^) Q = 200 N F 34 x

F 34 y

F 14 x

65.173

77 

D

C

Q

37.827

T

F

F

F

F

F

F

F

F

12

y 14

x 14

x 34

34 x

23 y

23 x

12 y

12 x

  • 5514.89N.cm

52.36N

75. 98 N

70.29N

82.00N

- 39.14N

184.59N

- 39.14N

184.59N

T

F

F

F

F

F

F

F

F

12

y 14

x 14

x 34

x 34

y 23

x 23

y 12

x 12

F on 2 right + F 12 x^ + F 32 x^ = 0  F on 2 up + F 12 y^ + F 32 y^ = 0  M on 2 about A CCW + - (F 32 x^ sin 45°) AB + (F 32 y^ sin 45°) AB + T 32 = 0   F on 3 right + F 23 x^ + F 43 x^ = 0  F on 3 up + F 23 y^ + F 43 y^ = 0  M on 3 about B CCW + - (F 43 x^ sin 30.86°) BC - (F 43 y^ sin 59.14°) BC + T 23 = 0

F on 4 right + F 34 x^ + F 14 x^ = 0  F on 4 up + F 34 y^ + F 14 y^ - W 4 = 0  M on 4 about D CCW + - (F 34 x^ sin 15.76°) CD - (F 34 y^ sin 74.24°) CD + (W 4 sin 74.24°) DG 4 = 0         

F 12 x

F 12 y

45 

A

F 32 y

B F^32 x

T 32

45 

45 

45 

F 43 y F 43 x

F 23 x

F 23 y

B

C (^) 30.86

30.86

59.14

59.14 T 23

F 14 y

F 34 x

F 34 y

74.24 F^14 x

D

C (^) G (^4)

15.76

15.76

74.24

W (^4)

74.24

4

4

4

x 12 y 12 x 23 y 23 x 34 y 34 x 14 y 14 32

DG)

sin W(

0000000 W

F F F F F F F F T

sin CD

sin CD

sin BC

sin BC

sin AB

sin AB 0 0

F F F F F F F F T

x 12 y 12 x 23 y 23 x 34 y 34 x 14 y 14 32

lbf. in 1 . 1351

lbf 1 . 50

lbf 3 . 29

lbf (^9). 129

lbf (^3). 29

lbf (^9). 129

lbf (^3). 29

lbf (^9). 129

lbf (^3). 29

xF 12 yF 12 xF 23 yF 23 xF 34 yF 34 xF 14 yF (^14) T 32

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Static Force Analysis for Slider Crank - Matrix

F on 2 right + F 12 x^ + F 32 x^ = 0  F on 2 up + F 12 y^ + F 32 y^ = 0  M on 2 about A CCW + - (F 32 x^ sin) AB + (F 32 y^ cos) AB + T 12 = 0   F on 3 right + F 23 x^ + F 43 x^ + FQx^ = 0  F on 3 up + F 23 y^ + F 43 y^ + FQy^ = 0  M on 3 about Q CCW + -(F 23 x^ sin) BQ -(F 23 y^ cos) BQ +(F 43 x^ sin) CQ +(F 43 y^ cos) CQ = 0

F on 4 right + F 14 x^ + F 34 x^ + P = 0  F on 4 up + F 14 y^ + F 34 y^ = 0 friction F 14 x^ = -  F 14 y^ sign(VC )

P

F

F

T

F

F

F

F

F

F

F

F

0 0 0 0 0 0 1 sign(V ) 0

0 0 BQsin BQcos CQsin CQcos 0 0 0

0 0 ABsin ABcos 0 0 0 0 1

Qy

Qx

12

14 y

14 x

34 y

34 x

23 y

23 x

12 y

12 x

C

2 A

B



T 12^ 

F 32 y

F 12 y

F 12 x

F 32 x

F 23 y

1 1

2

3

A^4

B

  P

T 12 Q Q

 C

B^ 

3

F 23 x

C

FQy FQx F 43 y Q  F 43 x 

(^4) P

F 14 x F 14 y

  • direction for impending V (^) C to right F 34 y C F^34 x

(^121223233434141412)

F F F F F F F F T

x y x y x y x y

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