发明名称 Layered composite component
摘要 A layered composite component is disclosed, the component including: a plurality of stacked layers defining a component thickness between opposed component surfaces and at least one reinforcing element extending from each of the opposed component surfaces the reinforcing elements extending at least partially through the component thickness. Another layered composite component is also disclosed, the component including: a plurality of stacked layers defining a plane and having a primary in-plane axis, wherein the at least one block array of reinforcing elements extends into the component along a reinforcing direction that is angled with respect to the plane of the stacked layers, and wherein the at least one block array is angled in the plane of the stacked layers with respect to the primary axis.
申请公布号 US8808847(B2) 申请公布日期 2014.08.19
申请号 US201213525821 申请日期 2012.06.18
申请人 Rolls-Royce PLC 发明人 Jevons Matthew P.;Backhouse Robert
分类号 B32B3/00;B32B3/02;B32B3/06;B32B3/08;B32B5/00;F01D5/00;F01D5/28 主分类号 B32B3/00
代理机构 Oliff PLC 代理人 Oliff PLC
主权项 1. A layered composite component for a gas turbine engine, comprising: a plurality of stacked layers defining a component thickness between opposed component surfaces; and block arrays of reinforcing elements extending from each of the opposed component surfaces, the reinforcing elements of each block extending only partially through the component thickness, wherein adjacent block arrays extend from opposing sides of the component surfaces, and the block arrays of reinforcing elements form a herringbone pattern.
地址 London GB