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Reducing Aircraft Brake Squeal with a Damped Brake-Rod BFGoodrich Aerospace Wheel and Brake Systems Division
- Format:
- Conference/Event
- Author/Creator:
- Enright, John J., author.
- Conference Name:
- World Aviation Congress & Exposition (2000-10-10 : San Diego, California, United States)
- Language:
- English
- Physical Description:
- 1 online resource
- Place of Publication:
- Warrendale, PA SAE International 2000
- Summary:
- In multi-brake aircraft landing gear systems, it is common for brake rod bending to participate in brake squeal vibration modes. Experiments have proven that damping the bending mode of the rod can reduce brake vibration. A patented method of doing so with a simple, lightweight, split-tube insert for tubular brake rods is described. Equations for sizing the insert for a given interference pressure are presented, results of bench tests are summarized, and further development is discussed
- Notes:
- Vendor supplied data
- Publisher Number:
- 2000-01-5599
- Access Restriction:
- Restricted for use by site license
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