Designing Spur Gear Backlash Allowance

Backlash types (defined for each gear in a gear set)

Real gears must be manufactured with a specific backlash allowance. Designate the allowance by considering the machining and working conditions.

In spur and helical gearing, there are two alternate ways to obtain the appropriate amount of backlash. First, decrease tooth thickness by sinking the hob deeper into the blank than the theoretical standard depth is. Second, increase the center distance than theoretically computed.

When designing a backlash, consider following factors:

The amount of backlash must not be excessive for the requirements of the job. Ensure it is sufficient so that machining costs are not higher than necessary.

It is customary to make half of the allowance for backlash on the tooth thickness of each gear of a pair, although there are exceptions. For example, on pinions having low numbers of teeth, it provides all the allowance on the driven gear. It avoids weakening the pinion teeth.

Type of Gear Meshes The Relation between Circular Direction j t and Normal Direction j n The Relation between Circular Direction j t and Center Direction j r The Relation between Circular Direction j t and Angular Backlash j
Spur Gear j n = j t cos α
Helical Gear j nn = j tt cos α n cos β

Backlash of Helical Gear Mesh

The helical gear has two kinds of backlash when referring to the tooth space. There is a cross section in the normal direction of the tooth surface “n”, and a cross section in the transverse direction perpendicular to the axis “t”.

j nn

Backlash in the direction normal to the tooth surface

j nt

Backlash in the circular direction in the cross section normal to the tooth

j tn

Backlash in the direction normal to the tooth surface in the cross section perpendicular to the axis

j tt

Backlash in the circular direction perpendicular to the axis

In the plane normal to the tooth:

j nn = j nt cos α n

On the pitch surface:

j nt = j tt cos β

In the plane perpendicular to the axis

j tn = j tt cos α t

where:

α

Pressure angle

α n

Pressure angle in normal direction, α = α n

α t

Pressure angle in transverse direction

β

Helix angle

d

Pitch diameter