发明名称 TAPERED GAS TURBINE SEGMENT SEALS
摘要 PROBLEM TO BE SOLVED: To provide gas turbine component sealing.SOLUTION: A gas turbine segment seal assembly 100 includes a first tapered segment seal 120 with a first tapered portion 140 having a first tapered surface and a first taper angle. The gas turbine segment seal assembly 100 includes a second tapered segment seal 150 with a second tapered portion 170 having a second tapered surface and a second taper angle. The gas turbine segment seal assembly 100 includes a seal pin 180 positioned in between the first tapered segment seal 120 and the second segment seal 150 and adjacent to the first tapered surface and the second tapered surface.SELECTED DRAWING: Figure 3
申请公布号 JP2016156375(A) 申请公布日期 2016.09.01
申请号 JP20160022309 申请日期 2016.02.09
申请人 GENERAL ELECTRIC CO <GE> 发明人 KIRTLEY KEVIN R;VICTOR JOHN MORGAN
分类号 F01D25/00;F01D11/00;F02C7/00;F02C7/28;F16J15/04 主分类号 F01D25/00
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