Aircraft landing gear having axle to brake plate integration

Aeronautics and astronautics – Landing gear – Wheel

Patent

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Details

244111, B64C 2502

Patent

active

061491004

ABSTRACT:
An aircraft landing gear brake arrangement wherein a landing gear stub axle and brake pressure plate are integrated. Each of the integrated assemblies is attached to a support fitting which pivots on the truck axle thereby causing the torque links to be unaffected by steering operations.

REFERENCES:
patent: 2943820 (1960-07-01), Westcott, Jr.
patent: 3027123 (1962-03-01), Westcott, Jr.
patent: 3134458 (1964-05-01), Westcott, Jr.
patent: 3164223 (1965-01-01), Kemp
patent: 3643898 (1972-02-01), Whitener et al.
patent: 5088662 (1992-02-01), Appleberry
patent: 5595359 (1997-01-01), Menghetti
patent: 5944147 (1999-08-01), Berwanger

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