发明名称 Side wall cooling of a gas turbine nozzle segment
摘要 <p>A nozzle vane segment includes outer (12) and inner band portions with a vane extending therebetween and defining first and second cavities (26, 28) separated by an impingement plate (22) for flowing cooling medium for impingement cooling of nozzle side walls. The side wall (34) of each nozzle segment has an undercut region (44). The impingement plate has an inturned flange (46) with a plurality of openings. Cooling inserts or receptacles (48) having an open end are received in the openings and the base and side walls (53, 51) of the receptacles have apertures (54, 52) for receiving cooling medium from the first cavity and directing the cooling medium for impingement cooling of the side wall of the nozzle segment and a portion of the nozzle wall. <IMAGE></p>
申请公布号 CZ20003835(A3) 申请公布日期 2001.11.14
申请号 CZ20000003835 申请日期 2000.10.17
申请人 GENERAL ELECTRIC COMPANY 发明人 BURDGICK STEVEN SEBASTIAN
分类号 F01D9/02;F01D5/18;F01D25/12;F02C7/12;(IPC1-7):F01D25/12 主分类号 F01D9/02
代理机构 代理人
主权项
地址