Aircraft brake wear limit indicator having integral configuratio

Details Aircraft brake wear limit indicator having integral configuratio Aircraft brake wear limit indicator having integral configuratio

1991-12-18

1993-07-20

Oberleitner, Robert J.

Brakes

With condition indicator

Electrical

116208, F16D 6602, G01D 2100

Patent

active

052285413

ABSTRACT:
A brake wear limit indicator which is matched to the brake energy capacity of the overhauled brake. A wear limit bushing is attached to the brake piston housing. The bushing length is chosen based on the brake energy capacity of the brake and is marked with a related part number. A wear pin is attached to the brake pressure plate and extends through a hole in the bushing. Brake overhaul is required when the brake wears such that the pin no longer protrudes from the bushing.

REFERENCES:
patent: 4013143 (1977-03-01), Juhasz
patent: 4279214 (1981-07-01), Thorn
patent: 4658936 (1987-04-01), Moseley
patent: 4989537 (1991-02-01), Hutchinson, Sr. et al.

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