发明名称 Device for sealing gas turbine stator blades
摘要 A sealing device for a gas turbine stator blade, in which an outer shroud (32) is mounted by heat insulating rings (32a,32b) on a blade ring (50). The blade ring (50) has a first air hole (1), which communicates with a space (53), and a second air hole (51), which communicates with a seal tube (2). The seal tube (2) is inserted into the second air hole (51), and a spring (6) is arranged between a projection (4) of the tube (2) and a retaining portion (5) of the air hole (51) to removably secure the seal tube (2). Cooling air (54) flows through the first air hole (1) to cool the shrouds and the inside of a stator blade (31) until it is released from the trailing edge of the blade. The cooling air also flows into a cavity (36) so that a high pressure can be maintained without a pressure loss because the tube (2) is independent of the space (53) in the blade ring.
申请公布号 US6217279(B1) 申请公布日期 2001.04.17
申请号 US19990230820 申请日期 1999.02.10
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 AI TOSHISHIGE;YURI MASANORI;TOMITA YASUOKI;SUENAGA KIYOSHI;AOKI SUNAO;FUKUNO HIROKI
分类号 F01D9/06;F01D11/04;F02C7/18;(IPC1-7):F01D5/18 主分类号 F01D9/06
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