Means for reducing the gap between rotor-backing plate interface

Brakes – Position adjusters – Release mechanism

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Details

188 715, 188 723, F16D 5548, F16D 6522

Patent

active

041179129

ABSTRACT:
In an aircraft multiple disc brake assembly utilizing carbon composite rotors and stators, an excessive gap occurs at the rotor-backing plate interface during brake depressurization. This gap allows oxidation of the carbon material at the interface thereby reducing friction performance and increasing wear. A spring is disposed between the backing plate and its friction surface thereby axially moving the friction surface closer to the surface of the adjacent rotor to reduce this gap.

REFERENCES:
patent: 2756847 (1956-07-01), Puse et al.
patent: 3018852 (1962-01-01), Stanton
patent: 3692150 (1972-09-01), Ruppe, Jr.
patent: 3958833 (1976-05-01), Stanton

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