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Aircraft landing gear having axle to brake plate integration

  • US 6,149,100 A
  • Filed: 08/26/1998
  • Issued: 11/21/2000
  • Est. Priority Date: 04/10/1996
  • Status: Expired due to Fees
First Claim
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1. In combination in a landing gear system, having a main shock absorber piston:

  • a structure disposed between adjacent wheel brakes for joining a right hand brake stator (27) to a left hand brake stator (29), said structure assembled to a landing gear truck beam (16); and

    ,said structure having rotational freedom concentric with the relevant brake rotation, and being connected to a fixed structure comprising the main shock absorber piston by a single brake rod, thereby enabling the reaction of loads due to brake application for all positions of the landing gear system including landing gear extended through landing gear retracted, and including gear at static during aircraft roll out and ground maneuvering.

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