| 摘要 |
An aircraft brake piston housing ( 10 ) has a composite body ( 14 ) including a plurality of fibers embedded in a matrix, the body ( 14 ) including a central bore ( 18 ) and a plurality of circumferentially disposed openings ( 23 ) surrounding the bore ( 18 ), at least some of the circumferentially disposed openings ( 23 ) being configured to receive a brake piston ( 26 ), and a frame ( 12 ) embedded in the composite body ( 14 ) and formed from a material different than the matrix. Also a method of forming such a brake piston housing.
|
