Simulation of Aircraft Brake Vibration Using Flexible Multibody and Finite Element Methods to Guide Component Testing Goodrich Corporation, Aircraft Wheels and Brakes

Format:

Conference/Event

Author/Creator:

Rook, Todd E., author.

Conference Name:

19th Annual Brake Colloquium And Exhibition (2001-10-28 : New Orleans, Louisiana, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 2001

Summary:

Brake-induced vibration often involves strong coupling with the aircraft structure, thereby necessitating a system level understanding. However, testing a full system is both costly and impossible until late in the development cycle. To overcome these issues, it becomes necessary to utilize simulation tools to assess the system behavior at an earlier stage. This paper demonstrates a methodology which implements such simulations to guide appropriate brake component tests that are more tractable for the brake supplier. As a result of this combined simulation and testing, a reduction in actual testing can be achieved

Notes:

Vendor supplied data

Publisher Number:

2001-01-3142

Access Restriction:

Restricted for use by site license