Asymmetric Approach in Solving Aircraft Brake Vibration ALS, Honeywell

Format:

Conference/Event

Author/Creator:

Chang, Craig F., author.

Conference Name:

World Aviation Congress & Exposition (2002-11-05 : Phoenix, Arizona, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 2002

Summary:

The objective of this paper is to present an Aircraft Landing Systems' (ALS) approach to the solution of the whirl vibration problem of aircraft brakes. The developed method utilizes the concept of asymmetry to break two friction coupled symmetric modes into two distinct and separated modes. The analytical derivation of the whirl vibration will be first discussed. A method of creating asymmetry will then be presented. Finally, experimental results will be presented that confirm the effectiveness of the technique to reduce aircraft brake whirl vibration

Notes:

Vendor supplied data

Publisher Number:

2002-01-2948

Access Restriction:

Restricted for use by site license