Dynamometer test apparatus for aircraft brakes

Measuring and testing – Brake testing – Roller or belt wheel support

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7386229, G01L 302

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active

059455985

ABSTRACT:
The invention is in the field of dynamometer testing of aircraft wheel and brake assemblies and, more particularly, relates to the simulation of brake and landing gear vibration dynamics on a dynamometer. The test apparatus and method according to the invention employ a pitch beam that simulates bogie pitch motion, and a walk beam that simulates landing gear walk.

REFERENCES:
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patent: 4182166 (1980-01-01), Herr, Jr.
patent: 4593557 (1986-06-01), Oblizajek et al.
patent: 4753110 (1988-06-01), Burchett et al.
patent: 4753116 (1988-06-01), Burchett
patent: 4958512 (1990-09-01), Johnsen
patent: 5003829 (1991-04-01), DeConti et al.
patent: 5398545 (1995-03-01), Blazic et al.
Realistic Evaluation of Airplane Brake Vibration by Laboratory Test and Analysis, by Raymond J. Black, Aircraft Landing Systems, AlliedSignal, Inc. DE-vol. 84-1, 1995 Design Engineering Technical Conferences, vol. 3-Part A, ASME 1995. pp. 1197-1207.
Laboratory Simulation of Landing Gear Pitch-Plane Dynamics (#851937), by John J. Enright, Aerospace Division, BFGoodrich Co., SAE Technical Paper Series, Aerospace Technology Conference & Exposition, Long Beach, CA, Oct. 14-17, 1985, Pp. 1-10.
Brake Dynamics, Aerospace Information Report, AIR 1064, Society of Automotive Engineers, Inc., Mar. 30, 1988. pp. 1-21.
Exhibit E, telefax to The Boeing Company, dated Apr. 11, 1994.

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