Notes_06_01 1 of 11 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. sin / AB = sin / e = 52.01° 2261.9 lbf up/left FCYLINDER __________________________ = 77.131° A C 4 D Payload e Not to scale AB = 36 inches AC = 42 inches AD = 96 inches = 16° F14y A D 4 P C F14x FC ∑M on 4 about A CCW+ -(FC sin ) AC +(P sin() AD = 0 FC = 2261.9 lbf B What corresponding hydraulic pressure would be required for a cylinder with a 3 inch DIA bore? 320 psi PCYLINDER __________________________ A = D2 / 4 = 7.069 in2 Is this value reasonable? Why? OK, industrial hydraulics often go to 3000 psi If you include friction between the piston and cylinder wall, will it increase or decrease your computation for pressure. pressure pushes up increase decrease Why? friction force will be up opposing piston motion What value would you use for the coefficient of friction between the piston and cylinder wall? 0.1 lubricated _________________________________ 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? constant e means will not be constant means velocity of the payload will not be constant, therefore must account for acceleration of payload mass Notes_06_01 2 of 11 Static Force Analysis for Four Bar - Scalar FP = 150 N B FQ = 200 N P 60 13.151 4 2 T12 A C 3 77 Q D 65.173 65 AB = 30 cm BC = 60 cm CD = 45 cm AD = 90 cm BP = 23 cm DQ = 24 cm D 1 1 24.827 F34y F32x 65 F43y B 13.151 F32y T12 60 25 25 F12y A AB = 30 cm 65 F12 x 65.173 76.849 FP = 150 N 46.849 F23x 13.151 76.849 B F23y C 77 F43x CD = 45 cm DQ = 24 cm CQ = 21 cm P BC = 60 cm BP = 23 cm CP = 37 cm M on 3 about B CCW+ - F43x (BC) sin 13.151 + F43y (BC) sin 76.849 + FP (BP) sin 60 = 0 - 13.651 F43x + 58.426 F43y = -2987.78 N F on 4 up + F34 x 81.993 N y F34 70.295 N F34x - FQ cos 37.827 + F14x = 0 F34y - FQ sin 37.827 + F14y = 0 F14x = 75.980 N F14y = 52.360 N F43x - FP cos 46.849 + F23x = 0 F43y + FP sin 46.849 + F23y = 0 F23x = 184.580 N F23y = -39.138 N F on 3 right + F on 3 up + M on 2 about A CCW+ - F32x (AB) sin 65 + F32y (AB) sin 25 + T12 = 0 T12 = - 5514.8 N.cm F on 2 right + F on 2 up F12x + F32x = 0 F12y + F32y = 0 D F14x - F34x (CD) sin 65.173- F34y (CD) sin 24.827 + FQ (DQ) sin 77 = 0 40.842 F34x + 18.895 F34y = 4676.98 N F on 4 right + 37.827 Q 65.173 M on 4 about D CCW+ 18.895 F34 x 4676.98 N 40.842 13.651 58.426 y 2987.78 N F34 FQ = 200 N C F34x F12x = 184.580 N F12y = -39.138 N F14y 24.827 Notes_06_01 3 of 11 Static Force Analysis for Four Bar - Superposition FP = 150 N B 60 3 C FQ = 200 N P 13.151 4 2 T12 A AB = 30 cm BC = 60 cm CD = 45 cm AD = 90 cm BP = 23 cm DQ = 24 cm 77 Q 65.173 65 D 1 1 P T12 CASE I Q T12 CASE I - F34 parallel to BC CASE II F32 C M on 4 about D CCW + F34 B 101.676 - F34 sin 101.676º CD + FQ sin 77 º DQ = 0 F34 = 106.129 N = F32 77 Q M on 2 about A CCW + F14y + F32 sin 128.151º AB + T12 = 0 T12 = -2503.75 N.cm F12y A D M on 3 about B CCW + - F43 sin 101.676º BC + FP sin 60 º BP = 0 F43 = 50.849 N FP = 150 N P 60 13.151 F32//BC C 3 78.324 F43 B F on 3 //BC right + + F43 cos 78.324º - FP cos 60 º + F32//BC = 0 F32//BC = 64.709 N - F43 sin 78.324º + FP cos 60 º - F32 F32┴BC = 80.107 N F12x F14x CASE II – F43 parallel to CD F on 3 ┴BC up + 128.151 T12 FQ ┴BC F32┴BC 38.151 F32┴BC =0 B T12 M on 2 about A CCW + + F32//BC sin 51.849º AB + F32┴BC sin 38.151º AB + T12 = 0 T12 = -3011.14 N.cm T12 = T12(Case I) + T12(Case II) = -5514.89 N.cm F12y F12x A 51.849 F32//BC Notes_06_01 4 of 11 Static Force Analysis for Four Bar - Matrix F32x B FP = 150 N F32 T12 46.849 A M on 2 about A CCW + F on 3 right + F on 3 up + M on 3 about P CCW + F on 4 right + F on 4 up + M on 4 about Q CCW + 1 0 0 0 0 0 0 0 0 0 1 1 0 y 0 rB / A 0 1 0 0 0 rBy / P 0 0 0 0 0 0 0 1 rBx / A 0 1 rBx / P 0 0 0 F43x 13.151 77 37.827 Q F14y F23y F12x F on 2 up + C F34x B 65 F on 2 right + P FQ = 200 N C 60 y F23x F12y F34y F43y 65.173 F12x + F32x = 0 F12y + F32y = 0 - F32x rB/Ay + F32y rB/Ax + T12 = 0 F23x + F43x + FPx= 0 F23y + F43y + FPy= 0 - F23x rB/Py + F23y rB/Px - F43x rC/Py + F43y rC/Px = 0 F34x + F14x + FQx = 0 F34y + F14y + FQx = 0 - F34x rC/Qy + F34y rC/Qx - F14x rD/Qy + F14y rD/Qx = 0 0 0 0 1 0 rCy / P 1 0 rCy / Q 0 0 0 0 1 rCx / P 0 1 x rC / Q 0 0 0 0 0 0 1 0 rDy / Q 0 0 0 0 0 0 0 1 rDx / Q 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 0 F12x 0 0 F12y 0 1 F23x 0 0 F23y FPx 0 F34x FPy 0 F34y 0 0 F14x FQx 0 F14y FQy 0 T12 0 F14x D Notes_06_01 1 0 0 0 0 0 0 0 0 0 1 0 0 0 0 0 1 0 1 0 0 0 0 0 27.189 12.678 0 0 0 0 0 1 0 1 0 0 0 0 0 1 0 1 0 0 0 5.233 22.396 8.418 36.030 0 0 0 0 0 1 0 1 0 0 0 0 0 1 0 1 0 0 0 19.059 8.817 21.782 10.077 F12x 184.59 N y F12 - 39.14 N F23x 184.59 N y F23 - 39.14 N x F34 82.00 N F x 70.29 N 34 F14x 75.98 N y F14 52.36 N T12 - 5514.89 N.cm 5 of 11 0 F12x 0 y 0 F12 0 1 F23x 0 y 0 F23 102.589 0 F34x 109.433 0 F34x 0 0 F14x 157.973 0 F14y 122.656 0 T12 0 Notes_06_01 6 of 11 Static Force Analysis for Pushups - Matrix A person doing pushups is represented with wrists A, elbows B, shoulders C, and toes D. Mass of the torso/legs is 180 lbm. Use the additional assumptions: a) All muscular effort is provided by triceps as torque T32 across the elbows. b) Angular velocity of link 4 is constant at this position c) Weight of the arms is negligible compared to weight of the torso/legs. d) Friction is negligible at A, B, C and D. e) No muscular torque is generated at A, C and D. AD = 52 inch AB = 12 in BC = 14 in CD = 57.7 in DG4 = 39 in 2 = 45° 3 = 149.14° 4 = 164.24° 2 = 0.5 rad/sec 3 = -1.435 rad/sec 4 = -0.387 rad/sec C C 3 G4 B 3 2 A 4 B 2 4 D Determine angular velocity across the elbows 2/3 for the position and velocity provided above. 2/3 = 2 - 3 = +1.935 rad/sec Determine elbow torque T32 for the position and velocity provided above. T32 = 1351.1 in.lbf CCW Do the magnitude and direction for your answer seem reasonable? Why? direction seems OK approximate solution W4 (DG4) ~ F34y (CD), F34y ~ 122 lbf ~ F12y F12y (AB) ~ T32 ~ 1464 in.lbf Rate the last four assumptions and state your reasoning. b) constant 4 1=poor 2=acceptable for an approximation c) weight of arms is negligible d) friction is negligible 1=poor 1=poor e) no muscle force at A, C, D 3=very good 2=acceptable for an approximation 2=acceptable for an approximation 1=poor 3=very good 3=very good 2=acceptable for an approximation 3=very good Determine 4 of the torso/legs when the forearm is aligned with the upper arms (2 = 3). 4 = F43y 59.14 F43x F23y 30.86 59.14 C T23 B F23x 30.86 Notes_06_01 7 of 11 F34y 74.24 15.76 F34x C y F32 T32 G4 45 45 74.24 W4 y 74.24 F14 B F32x F14x 45 F12y A 45 D 15.76 F12x F on 2 right + F on 2 up + M on 2 about A CCW + F on 3 right + F on 3 up + M on 3 about B CCW + F on 4 right + F on 4 up + M on 4 about D CCW + F12x + F32x = 0 F12y + F32y = 0 - (F32x sin 45°) AB + (F32y sin 45°) AB + T32 = 0 F23x + F43x = 0 F23y + F43y = 0 - (F43x sin 30.86°) BC - (F43y sin 59.14°) BC + T23 = 0 F34x + F14x = 0 F34y + F14y - W4 = 0 - (F34x sin 15.76°) CD - (F34y sin 74.24°) CD + (W4 sin 74.24°) DG4 = 0 Notes_06_01 1 0 0 0 0 0 0 0 0 0 1 0 0 0 1 0 1 0 0 0 AB sin 45 AB sin 45 0 0 0 1 0 1 0 0 0 1 0 1 0 0 0 BC sin 30.86 BC sin 59.14 0 0 0 1 0 0 0 0 0 1 0 0 0 CD sin 15.76 CD sin 74.24 1 0 0 0 0 0 0 0 0 0 1 0 0 0 1 0 1 0 0 0 8.4853 8.4853 0 0 0 1 0 1 0 0 0 1 0 1 0 0 0 7.1812 12.0179 0 0 0 1 0 0 0 0 0 1 0 0 0 15.6718 55.5309 0 0 0 0 0 0 1 0 0 8 of 11 0 0 0 0 0 0 1 0 0 0 0 0 F12x y 0 0 0 F12 0 0 1 F23x y 0 0 0 F23 0 0 0 F34x y 0 0 1 F34 0 0 0 F14x y W4 1 0 F14 0 0 T32 ( W4 sin 74.24)DG 4 0 0 F12x 0 0 0 F12y 0 0 1 F23x 0 0 0 F23y 0 0 0 F34x 0 0 1 F34y 0 0 0 F14x 0 1 0 F14y 180 0 0 T32 6756.1 F12x 29.3 lbf y F12 129.9 lbf F23x 29.3 lbf y F23 129.9 lbf x F34 29.3 lbf F y 129.9 lbf 34 F14x 29.3 lbf y F14 50.1 lbf T32 1351.1 in .lbf Notes_06_01 9 of 11 Static Force Analysis for Slider Crank - Scalar B T12 R = AB L = BC 3 2 C A 4 1 1 B T12 + direction for impending VC to right B 2 A F23 3 F32 F34 C F14x F12x F43 y F12 F on 4 right + + P - F14x sign(VC) - F34 cos = 0 F on 4 up + + F34 sin - F14y = 0 M on 3 F23 = F43 M on 2 about A CCW + + T12 - ( F32 sin() ) R = 0 friction F14x = F14y F34 P cos sign (VC ) sin F14 P sin P tan for 0 cos sign (VC ) sin F14 P sin cos sign (VC ) sin y x F12 x F12 y T12 P P cos P for 0 cos sign (VC ) sin P sin P tan for 0 cos sign (VC ) sin P R sin( ) cos sign (VC ) sin C 4 F14y P Notes_06_01 10 of 11 Static Force Analysis for Slider Crank - Matrix B T12 2 A Q 3 Q C 4 1 1 F32y T12 B A y F23 F Qy F23x F32x 2 B Q F on 2 up + M on 2 about A CCW + F on 3 right + F on 3 up + M on 3 about Q CCW + F on 4 right + F on 4 up + friction 1 0 0 0 0 0 0 0 0 F43y C 4 F34x F43x 3 C F12y + direction for impending VC to right F34y FQx F12x F on 2 right + P F14x F14y F12x + F32x = 0 F12y + F32y = 0 - (F32x sin) AB + (F32y cos) AB + T12 = 0 F23x + F43x + FQx = 0 F23y + F43y + FQy = 0 -(F23x sin) BQ -(F23y cos) BQ +(F43x sin) CQ +(F43y cos) CQ = 0 F14x + F34x + P = 0 F14y + F34y = 0 F14x = - abs(F14y) sign(VC) 0 1 0 0 0 1 0 1 0 0 0 AB sin AB cos 0 0 0 1 0 1 0 0 0 1 0 1 0 BQ sin BQ cos CQ sin CQ cos 0 0 0 1 0 0 0 0 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 0 0 1 1 sign (VC ) 0 F12x 0 0 F12y 0 1 F23x 0 0 F23y FQx 0 F34x FQy 0 F34y 0 0 F14x P 0 F14y 0 0 T12 0 P Notes_06_01 11 of 11 F12x y F12 F23x y F23 x F34 y F34 F x 14y F14 T 12