专利内容由知识产权出版社提供
专利名称：Flow sleeve with tabbed direct combustion
liner cooling air
发明人：Tu, John S.,Chokshi, Jaisukhlal V.,Brdar,
Christopher R.,McKinney, Randal G.,Ramos,Shakira A.
申请号：EP09250781.3申请日：20090320公开号：EP2144002B1公开日：20160914
摘要：A combustion duct for a gas turbine engine has a combustion liner (3 1) toreceive products of combustion, and deliver the products of combustion downstreamtoward a turbine rotor. An outer housing (22) is positioned radially outwardly of thecombustion liner (31). A flow sleeve (32) is positioned radially intermediate the outerhousing (22) and the combustion liner (31). A chamber (30) radially outwardly of the flowsleeve (32) receives cooling air. A plurality of holes (35) through the flow sleeve delivercooling air from the chamber (30) against an outer periphery of the combustion liner (31).A plurality of tabs (40) are associated with at least some of the holes (35) in the flowsleeve (32). The tabs (40) are positioned to extend radially inwardly on a downstream sideof the holes (35).
申请人：UNITED TECHNOLOGIES CORP
地址：US
国籍：US
代理机构：Leckey, David Herbert
更多信息请下载全文后查看
