发明名称 Combustion liner with open cell foam and acoustic damping layers
摘要 The disclosure is directed to a gas turbine engine combustion liner and a gas turbine engine. The gas turbine engine combustion liner may include a thermally cooled wall section, an acoustically damped wall section, or a thermally cooled and acoustically damped wall section. Open cell foam or honeycomb may be disposed between inner and outer combustion liner walls. The walls, open cell foam, or honeycomb may be made of a composite material.
申请公布号 US9310079(B2) 申请公布日期 2016.04.12
申请号 US201113162103 申请日期 2011.06.16
申请人 Rolls-Royce North American Technologies, Inc. 发明人 Uskert Richard Christopher
分类号 F23R3/06;F23R3/00;F23M20/00;F23M5/02 主分类号 F23R3/06
代理机构 Brinks Gilson & Lione 代理人 Brinks Gilson & Lione
主权项 1. A combustion liner, comprising: an outer combustion liner wall; an inner combustion liner wall; an open cell foam disposed between the outer combustion liner wall and the inner combustion liner wall, wherein at least one of the outer combustion liner wall and the inner combustion liner wall includes a plurality of openings extending therethrough; and a plurality of cells exposed to the plurality of openings; wherein the open cell foam is formed of a composite material, wherein the composite material of the open cell foam is a ceramic matrix composite.
地址 Indianapolis IN US