Give step-by-step solution with explanation and final answer:
Act like a helpful tutor and exlain me :
A pair of
2
0
°
full depth involute bevel gears is used to connect two shafts at right angles having a velocity ratio
2
.
5
:
1
.
The gear is made from cast steel and the pinion is from the forged steel. Pinion transmits
3
7
.
5
kW at
7
5
0
rpm Design the gear drive and check the design for dynamic and wear loads.
Question:
Give step-by-step solution with explanation and final answer:
Act like a helpful tutor and exlain me :
A pair of
2
0
°
full depth involute bevel gears is used to connect two shafts at right angles having a velocity ratio
2
.
5
:
1
.
The gear is made from cast steel and the pinion is from the forged steel. Pinion transmits
3
7
.
5
kW at
7
5
0
rpm Design the gear drive and check the design for dynamic and wear loads.
This is AI generated Response.
Asked by: manish kumar
Created at: 2025-09-23 10:13:21
Final Answer:
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# Bevel Gear Design Problem: Step-by-Step Solution
## Problem Summary
- **Type:** 20° full-depth involute bevel gears
- **Shafts:** Connect at right angles (90°)
- **Velocity Ratio:** 2.5:1 (Pinion : Gear)
- **Materials:**
- Pinion: Forged steel
- Gear: Cast steel
- **Power Transmitted:** 37.5 kW
- **Pinion Speed (N₁):** 750 rpm
- **Tasks:**
1. Design the gear drive (determine main dimensions, module, teeth, etc.)
2. Check for dynamic and wear loads.
---
## 1. **Find the Number of Teeth and Gear Ratio**
### a. **Velocity Ratio**
\[
\text{Velocity Ratio (VR)} = \frac{\text{Speed of Pinion}}{\text{Speed of Gear}} = \frac{N_1}{N_2} = 2.5:1
\]
\[
N_1 = 750 \text{ rpm} \implies N_2 = \frac{750}{2.5} = 300 \text{ rpm}
\]
### b. **Number of Teeth**
Let \( z_1 \) = Number of pinion teeth
Let \( z_2 \) = Number of gear teeth
\[
\frac{z_2}{z_1} = \text{Gear Ratio} = 2.5
\implies z_2 = 2.5 \, z_1
\]
Select \( z_1 \) to avoid undercutting. For 20° full-depth teeth, minimum \( z_1 = 18 \) (practical, can use 20 or more).
Let’s **choose \( z_1 = 20 \):**
\[
z_2 = 2.5 \times 20 = 50
\]
---
## 2. **Pitch Cone Angles (Bevel Gears at 90°)**
\[
\text{For shafts at 90°:}
\]
\[
\theta_1 = \tan^{-1} \left( \frac{z_1}{z_2} \right) = \tan^{-1} \left( \frac{20}{50} \right) = \tan^{-1} (0.4) \approx 21.8^\circ
\]
\[
\theta_2 = \tan^{-1} \left( \frac{z_2}{z_1} \right) = \tan^{-1} (2.5) \approx 68.2^\circ
\]
---
## 3. **Calculate Pitch Diameters**
\[
\text{Let } m = \text{module}
\]
\[
d_1 = m \cdot z_1
\]
\[
d_2 = m \cdot z_2
\]
---
## 4. **Power and Tangential Force**
### a. **Torque on Pinion**
\[
P = 2\pi N_1 T_1 / 60
\implies T_1 = \frac{P \times 60}{2\pi N_1}
\]
\[
T_1 = \frac{37,500 \times 60}{2\pi \times 750}
= \frac{2,250,000}{4712.39}
\approx 477.73 \text{ Nm}
\]
### b. **Tangential Force at Pinion Pitch Circle**
\[
F_t = \frac{2T_1}{d_1}
\]
But \( d_1 = m \times 20 \).
So,
\[
F_t = \frac{2 \times 477,730}{m \times 20}
= \frac{955,460}{20m}
= \frac{47,773}{m} \text{ N}
\]
---
## 5. **Module Selection (Strength Equation)**
For bevel gears, the **Lewis equation** (approximate for external gears):
\[
F_t = \sigma_d \cdot b \cdot Y \cdot m \cdot K_v
\]
Where:
- \( \sigma_d \) = allowable bending stress (based on weaker material)
- \( b \) = face width (\( b = 10m \) recommended for bevel gears; max \( b = 1/3 \) of cone distance)
- \( Y \) = Lewis form factor (for 20 teeth, 20°: \( Y \approx 0.322 \))
- \( K_v \) = velocity factor
#### a. **Allowable Stress**
Assume allowable bending stress (\( \sigma_{d} \)) for **cast steel** (gear) = 140 MPa (from data books)
For **forged steel** (pinion) = 200 MPa
Pinion is stronger. **Gear is weaker** → use gear's value.
#### b. **Cone Distance (Mean Pitch Diameter)**
\[
\text{Cone distance } (L) = \sqrt{(d_1/2)^2 + (d_2/2)^2}
= \frac{m}{2} \sqrt{z_1^2 + z_2^2}
\]
\[
= \frac{m}{2} \sqrt{20^2 + 50^2}
= \frac{m}{2} \sqrt{400 + 2500}
= \frac{m}{2} \sqrt{2900}
= \frac{m}{2} \times 53.85
= 26.93 m
\]
#### c. **Face Width**
\[
b = 10m \qquad (\text{but } b \leq \frac{1}{3} L = \frac{1}{3} \times 26.93m = 8.98m)
\]
So, **limit \( b \) to \( 8m \)** (rounded).
#### d. **Lewis Form Factor \( Y \)**
For 20° pressure angle and \( z = 20 \):
\[
Y = 0.154 - \frac{0.912}{z}
= 0.154 - \frac{0.912}{20}
= 0.154 - 0.0456 = 0.1084
\]
#### e. **Velocity Factor \( K_v \)**
Pitch line velocity,
\[
v = \frac{\pi d_1 N_1}{60 \times 1000} \quad \text{(in m/s)}
= \frac{\pi \cdot (m \cdot 20) \cdot 750}{60 \times 1000}
= \frac{\pi \cdot m \cdot 15,000}{60,000}
= \frac{\pi m \cdot 15,000}{60,000}
= \frac{\pi m \cdot 15}{60}
= \frac{\pi m}{4}
\]
Let’s try \( m = 5 \) mm first:
\[
v = \frac{\pi \cdot 5}{4} \approx 3.93 \text{ m/s}
\]
Velocity factor (Barth’s formula):
\[
K_v = \frac{3}{3 + v}
\]
\[
K_v = \frac{3}{3 + 3.93} = \frac{3}{6.93} = 0.433
\]
#### f. **Calculate Required Module**
Rewriting Lewis equation:
\[
F_t = \sigma_d \cdot b \cdot Y \cdot m \cdot K_v
\]
\[
\frac{47,773}{m} = 140 \times 8m \times 0.1084 \times 0.433
\]
\[
= 140 \times 8 \times 0.1084 \times 0.433 \times m
\]
\[
= 140 \times 8 = 1,120
\]
\[
1,120 \times 0.1084 = 121.408
\]
\[
121.408 \times 0.433 = 52.56
\]
So,
\[
\frac{47,773}{m} = 52.56 m
\]
\[
\Rightarrow 47,773 = 52.56 m^2
\]
\[
m^2 = \frac{47,773}{52.56} = 909.76
\]
\[
m = \sqrt{909.76} \approx 30.2 \text{ mm}
\]
This is **very large**. Let's check calculations.
#### g. **Check for Calculation Error**
Let’s check face width:
- \( b = 8m \), so for \( m = 5 \) mm, \( b = 40 \) mm, which is less than \( 1/3 \) of cone distance (26.93m ≈ 134 mm). OK.
Let’s try \( m = 8 \) mm:
\[
v = \frac{\pi \cdot 8}{4} = 6.28 \text{ m/s}
\]
\[
K_v = \frac{3}{3 + 6.28} = \frac{3}{9.28} = 0.323
\]
\[
F_t = 140 \times 64 \times 0.1084 \times 0.323 \times 8
\]
But \( b = 8m = 64 \) mm.
\[
\sigma_d = 140 \text{ MPa}
\]
\[
b = 64 \text{ mm}
\]
\[
Y = 0.1084
\]
\[
K_v = 0.323
\]
\[
m = 8 \text{ mm}
\]
\[
F_t = 140 \times 64 \times 0.1084 \times 0.323
= 8,960 \times 0.1084 \times 0.323
= 971.264 \times 0.323
= 313.77
\]
Multiply by \( m \):
\[
313.77 \times 8 = 2,510 \text{ N}
\]
\[
F_t = \frac{47,773}{8} = 5,972 \text{ N}
\]
**Required \( F_t \) (power) is much higher than strength.**
Try **larger module**:
Let’s try \( m = 15 \) mm:
- \( d_1 = 300 \text{ mm} \)
- \( b = 8m = 120 \text{ mm} \)
- \( v = \frac{\pi \cdot 15}{4} = 11.78 \text{ m/s} \)
- \( K_v = \frac{3}{3 + 11.78} = 0.203 \)
\[
F_t = 140 \times 120 \times 0.1084 \times 0.203 = 16,800 \times 0.1084 \times 0.203
= 1,822.12 \times 0.203 = 370 \text{ N}
\]
\[
370 \times 15 = 5,550 \text{ N}
\]
\[
F_t = \frac{47,773}{15} = 3,185 \text{ N}
\]
Still not matching; perhaps our face width is too small.
Let’s use the **maximum face width** (\( b = 1/3 L \)):
\[
L = 26.93 m
\]
For \( m = 15 \) mm:
\[
L = 26.93 \times 15 = 404 \text{ mm}
\]
\[
b = \frac{404}{3} = 134.7 \text{ mm}
\]
Now,
\[
F_t = 140 \times 134.7 \times 0.1084 \times 0.203 \times 15
= (18,858 \times 0.1084 \times 0.203) \times 15
= (2,044.5 \times 0.203) \times 15
= (415 \times 15) = 6,225 \text{ N}
\]
Now,
\[
F_t = \frac{47,773}{15} = 3,185 \text{ N}
\]
**Now, strength is sufficient.**
---
## 6. **Summary of Gear Dimensions**
- **Module \( m \):** 15 mm
- **Pinion Teeth \( z_1 \):** 20
- **Gear Teeth \( z_2 \):** 50
- **Pitch Diameters:**
- \( d_1 = 15 \times 20 = 300 \) mm
- \( d_2 = 15 \times 50 = 750 \) mm
- **Face Width \( b \):** Max \( = \frac{1}{3} L = 134.7 \) mm
- **Pitch Cone Angles:**
- Pinion: \( 21.8^\circ \)
- Gear: \( 68.2^\circ \)
- **Cone Distance:** \( L = 404 \) mm
---
## 7. **Dynamic Load Check**
**Dynamic load (Buckingham’s equation):**
\[
F_d = F_t + \frac{21 v (F_t + b C)}{21 v + \sqrt{F_t + b C}}
\]
Where:
- \( C \) = deformation factor (from tables, for steel, \( C \approx 118 \) N/mm for cut gears)
- \( v \) = pitch line velocity at pinion
\
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