发明名称 Combustor liner cooling assembly
摘要 A combustor liner defining a combustor chamber is included. Also included is a cover sleeve spaced radially outwardly from and at least partially surrounding an aft end of the combustor liner, the cover sleeve and the combustor liner defining a cooling annulus. Further included is at least one aperture extending through the cover sleeve for routing a cooling flow to the cooling annulus. Yet further included is a perforated sleeve disposed between the cover sleeve and the combustor liner, wherein the perforated sleeve comprises a plurality of holes for impinging the cooling flow toward the combustor liner.
申请公布号 US9222672(B2) 申请公布日期 2015.12.29
申请号 US201213585548 申请日期 2012.08.14
申请人 General Electric Company 发明人 Kodukulla Sridhar Venkat;Gopalakrishna Sandeep
分类号 F23R3/06;F23R3/00;F23R3/60;F23R3/08;F23R3/46 主分类号 F23R3/06
代理机构 代理人 Cusick Ernest G.;Landgraff Frank A.
主权项 1. A combustor liner cooling assembly comprising: a combustor liner defining a combustion chamber; a cover sleeve spaced radially outwardly from and at least partially surrounding an aft end of the combustor liner, the cover sleeve and the combustor liner defining a cooling annulus therebetween; at least one aperture extending through the cover sleeve for routing a cooling flow to the cooling annulus for convective cooling along the combustor liner within the cooling annulus; a perforated sleeve disposed in the cooling annulus between the cover sleeve and the combustor liner, wherein the perforated sleeve comprises a plurality of holes for impinging the cooling flow toward the combustor liner; and an outer sleeve surrounding the cover sleeve, the outer sleeve comprising at least one of a flow sleeve and an impingement sleeve.
地址 Schenectady NY US