Woven preform, composite, and method of making thereof

摘要

A three dimensional woven preform, a fiber reinforced composite incorporating the preform, and methods of making thereof are disclosed. The woven preform includes one or more layers of a warp steered fabric. A portion of the warp steered fabric is compressed into a mold to form an upstanding leg. The preform includes the upstanding leg and a joggle in a body portion. The body portion and upstanding leg are integrally woven so there is continuous fiber across the preform. A portion of the warp steered fabric includes stretch broken carbon fibers in the warp direction, and another portion includes conventional carbon fibers. The warp steered fabric can be woven on a loom equipped with a differential take-up mechanism. The warp steered fabric can be a single or multilayer fabric. The preform or the composite can be a portion of an aircraft window frame.

主权项

1. A three dimensional woven preform comprising:
one or more layers of a warp steered fabric, at least one non-elongatable portion; and at least one elongatable portion of the warp steered fabric comprising a fiber in the warp direction of the warp steered fabric which will allow the fabric to elongate as needed in a substantially circumferential direction, wherein the one or more layers of the warp steered fabric are not darted or cut to shape the preform, wherein said preform comprises an upstanding leg and a joggle in a body portion, the body portion comprising the at least one non-elongatable portion comprising conventional carbon fibers and wherein the elongatable portion of said warp steered fabric is configured such that the upstanding leg or the joggle or both are formed in a mold, and wherein the preform includes a first distinct portion of the warp steered fabric including a plurality of stretch broken carbon fibers or discontinuous tows; a second distinct portion of the warp steered fabric including the conventional carbon fibers and not the stretch broken carbon fibers or discontinuous tows, and a third distinct portion of the warp steered fabric including the stretch broken carbon fibers; and wherein the preform is configured to be an aircraft window frame.