In double helical gear the helix angle is
![In double helical gear the helix angle is](http://storage.googleapis.com/tb-img/production/20/12/F1_Ashik_2.12.20_Pallavi_D2.1.png)
| In double helical gear the helix angle is
A. 90
B. 45
C. 75
D. 60
Please scroll down to see the correct answer and solution guide.
Right Answer is: B
SOLUTION
Explanation:
Helix angle:
- It is the angle between any helix and an axial line on its right, circular cylinder or cone.
- Helix angles are selected to obtain a minimum overlap ratio and to provide good load sharing.
- Helix angles vary from 5° to 45°.
- The helix angle for Single-helical gear falls between 12° and 20°, and for double-helical gears it falls between 20° and 45°.
- The thrust generated is also a function of the helix angle.
- An increase in the helix angle increases the thrust; thus, this increase is the main reason for the lower helix angles in single-helical gearing.
Double Helical Gear:
- A double helical gear is equivalent to a pair of helical gear secured together, one having a right-hand helix and the other has a left-hand helix. The teeth of the two rows are separated by a groove i.e. used for tool run out.
- In double helical gear the helix angle is 45°.
- Axial thrust occurs in the case of single helical gears eliminated in double helical gears. This is because the axial thrust of two rows of the teeth cancels each other.
- These gears can be run at high speeds with less noise and vibrations.
Helical Gear:
- They have curved teeth, each being helical in shape.
- Two mating gear have the same helix angle but have teeth of opposite hands.
- At the beginning of the engagement, contact occurs only at the point of the leading edge of the curved teeth. As the gear rotates, the contact extends along a diagonal line across the teeth. Thus load application is gradual, low impact stresses and reduction in noise.
- Helical gears have the disadvantages of having end thrust as there is a force component along the gear axis. The bearing and mounting must be able to withstand the thrust load.