Give step-by-step solution with explanation and final answer:o a ETE Ee tac wt eo Se es At eed ane Blam TO0 TA Sea TA Bre | | wr Gq | ; ww IY ) | l1ag I hl | | | J ft i) ee mw ri iad SE Ene
Question:
Give step-by-step solution with explanation and final answer:
o a
ETE
Ee tac wt eo Se es At eed ane
Blam TO0 TA Sea TA Bre |
| wr Gq |
; ww IY
) |
l1ag I
hl
|
| | J
ft i)
ee mw ri iad SE
Ene
This is AI generated Response.
Asked by: Rahul
Created at: 2026-01-24 06:48:37
Asked by: Rahul
Created at: 2026-01-24 06:48:37
Final Answer:
Rendered
Raw Text
Did you like this answer?
Let's break down the problem step by step:
---
## **Given Data**
- Pulleys A and B transmit forces at different points.
- Tension in the belts:
- \( T_1(A) = 560 \) lb
- \( T_2(A) = 93.3 \) lb
- \( T_1(B) = 700 \) lb
- \( T_2(B) = 60 \) lb
- Distances:
- \( a = 9 \) in
- \( b = 12 \) in
- \( c = 6 \) in
- \( d = 18 \) in
- Shaft diameter \( d_{shaft} = 2 \) in
---
## **Step 1: Find Forces at Each Pulley**
### Pulley A
- Net force at A:
\[
F_A = T_1(A) - T_2(A) = 560 - 93.3 = 466.7 \text{ lb (downward)}
\]
(Assume direction per figure.)
### Pulley B
- Net force at B:
\[
F_B = T_1(B) - T_2(B) = 700 - 60 = 640 \text{ lb (upward)}
\]
---
## **Step 2: Find Reactions at Bearings**
Let’s denote:
- Left bearing = O
- Right bearing = C
Sum of vertical forces:
\[
R_O + R_C - F_A + F_B =
\]
\[
R_O + R_C - 466.7 + 640 =
\]
\[
R_O + R_C = -173.3 \text{ lb}
\]
Take moments about O:
- \( F_A \) acts at \( a = 9 \) in from O
- \( F_B \) acts at \( a + b = 9 + 12 = 21 \) in from O
- \( R_C \) acts at \( a + b + c + d = 9 + 12 + 6 + 18 = 45 \) in from O
\[
\text{Sum of moments about O:}
\]
\[
- F_A \cdot 9 + F_B \cdot 21 - R_C \cdot 45 =
\]
\[
-466.7 \cdot 9 + 640 \cdot 21 - R_C \cdot 45 =
\]
\[
-4,200.3 + 13,440 - 45R_C =
\]
\[
9,239.7 = 45R_C
\]
\[
R_C = \frac{9,239.7}{45} = 205.33 \text{ lb}
\]
Now back to force equilibrium:
\[
R_O + 205.33 = -173.3
\]
\[
R_O = -173.3 - 205.33 = -378.63 \text{ lb}
\]
---
## **Step 3: Shear and Bending Moment Diagrams**
Key points:
- O (x=)
- A (x=9 in)
- B (x=21 in)
- C (x=45 in)
### Shear at each point:
- \( V_O = R_O = -378.63 \) lb
- At A: \( V_A = V_O - F_A = -378.63 - 466.7 = -845.33 \) lb
- At B: \( V_B = V_A + F_B = -845.33 + 640 = -205.33 \) lb
- At C: \( V_C = V_B + R_C = -205.33 + 205.33 = \) lb
### Bending Moment at each section:
- At O: \( M_O = \)
- At A: \( M_A = R_O \cdot a = -378.63 \cdot 9 = -3,407.67 \) in-lb
- Between A and B (at B, x=21 in):
\[
M_B = R_O \cdot 21 - F_A \cdot (21-9)
\]
\[
= -378.63 \cdot 21 - 466.7 \cdot 12
\]
\[
= -7,951.23 - 5,600.4 = -13,551.63 \text{ in-lb}
\]
- At C: \( M_C = \)
**Maximum moment is at B: \( M_{max} = |M_B| = 13,551.63 \) in-lb**
---
## **Step 4: Find Torsional Moment at B**
Torsional moment at B is due to the net belt tensions at B:
\[
T_B = (T_1(B) - T_2(B)) \cdot r_B
\]
But since the shaft transmits the torque, the **torque at B** is:
\[
T = (T_1(B) - T_2(B)) \cdot r_B = 640 \cdot 9 = 5,760 \text{ in-lb}
\]
(Assuming pulley B radius is 9 in per diagram.)
---
## **Step 5: Calculate Bending and Shear Stresses**
### **Bending Stress \(\sigma_b\):**
\[
\sigma_b = \frac{M_{max} \cdot c}{I}
\]
Where:
- \( M_{max} = 13,551.63 \) in-lb \( = 162,619.56 \) lb-in (\(1 \text{ ft-lb} = 12 \text{ in-lb}\))
- \( c = \frac{d}{2} = 1 \) in
- \( I = \frac{\pi d^4}{64} \) for a circular shaft, \( d = 2 \) in
Calculate \( I \):
\[
I = \frac{\pi (2)^4}{64} = \frac{\pi \cdot 16}{64} = \frac{\pi}{4} = .785 \text{ in}^4
\]
\[
\sigma_b = \frac{13,551.63 \cdot 1}{.785} = 17,273 \text{ psi}
\]
---
### **Torsional Shear Stress \(\tau_{max}\):**
\[
\tau_{max} = \frac{T \cdot c}{J}
\]
Where:
- \( T = 5,760 \) in-lb
- \( c = 1 \) in
- \( J = \frac{\pi d^4}{32} = \frac{\pi (2)^4}{32} = \frac{\pi \cdot 16}{32} = \frac{\pi}{2} = 1.57 \) in\(^4\)
\[
\tau_{max} = \frac{5,760 \cdot 1}{1.57} = 3,668 \text{ psi}
\]
---
## **Summary Table**
| Quantity | Value | Unit |
|-------------------------------|-----------|------|
| Max bending moment (\(M_{max}\)) | 13,551.63 | in-lb |
| Max bending stress (\(\sigma_b\)) | 17,273 | psi |
| Max torsional shear (\(\tau_{max}\))| 3,668 | psi |
---
## **Final Answers**
\[
\boxed{
\begin{aligned}
\text{The bending stress at the point of maximum bending moment is:} \quad & 17,273~\text{psi} \\
\text{The torsional shear stress at the point of maximum bending moment is:} \quad & 3,668~\text{psi}
\end{aligned}
}
\]
---
**Let me know if you need a combined stress analysis or have further questions!**
📢 Instructions:
- Ask anything relatd to above question only.
- For new Question goto :
VIPSolutions