Working depth
Clearance
Backlash
Face width
C. Backlash
20 to 30%
10 to 20%
30 to 40%
40 to 50%
2WD3n/Gd⁴
4WD3n/Gd⁴
8WD3n/Gd⁴
16WD3n/Gd⁴
Ductile materials
Brittle materials
Elastic materials
All of the above
Module
Tooth profile
Both module and pitch line velocity
Pitch line velocity
Brinell
Rockwell
Vickers
None of the above
Hot piercing
Extrusion
Cold peening
Cold heading
Ductile materials
Brittle materials
Equally serious in both cases
Depends on other factors
Increases the fatigue strength
Decreases the fatigue strength
Has no influence on fatigue strength
Alone has no influence on fatigue strength
0.2
0.25
0.50
0.6
Eutectoid steel
Hypereutectoid steel
Hypo-eutectoid steel
None of these
Bevel gearing
Helical gearing
Worm gearing
None of these
Metal strength by cycling
Metal hardness by surface treatment
Metal resistance to corrosion by coating
Fatigue limit by overstressing the metal by successively increasing loadings
It is subjected to a higher cyclic loading than the outer side
It is subjected to a higher stress than the outer side
It is more stretched than the outer side during the manufacturing process
It has a lower curvature than the outer side
Power transmitted increases
Power transmitted decreases
Power transmitted increases to a maximum value and then decreases
Power transmitted remains the same
Twice
Four times
Eight times
Sixteen times
0.5 times
Equal to
2 times
Double
1 in 24 to 1 in 20
1 in 15 to 1 in 10
1 in 32 to 1 in 24
1 in 48 to 1 in 24
Muff coupling
Compression coupling
Flange coupling
All of these
Rectangular
Elliptical
I-section
Any one of these
45 to 60 %
63 to 70 %
70 to 83 %
80 to 90 %
Centroidal axis
Neutral axis
Inside fibre
Outside fibre
Intersecting and the teeth are curved
Non-intersecting and nonparallel and the teeth are curved
Non-intersecting and non-parallel and the teeth are straight
None of the above
p.d.σc
p.t.σc
n.d.t.σc
(p - d) t.σc
7.5 kN
10.6 kN
15 kN
22.5 kN
Single
Double
Triple share
None of these
P1 - P2
P1 + P2
2 × (P1 + P2)
[2 × (P1 + P2)] + Pc Where Pc is centrifugal tension
Does not change
Increases
Decreases
None of the Above
8
4
2
6
Axial load plus stress due to bending
Acceleration/retardation of masses plus stress due to bending
Axial load plus stress due to acceleration/retardation
Bending plus stress due to acceleration/retardation
Bushed pin type coupling
Universal coupling
Oldham coupling
All of these