发明名称 TURBINE BLADE DAMPER SEAL
摘要 A damper seal received in a cavity of a turbine blade located between a platform and a retention shelf damper seal according to an exemplary aspect of the present disclosure includes, among other things, a central body portion having a first end region, an opposing second end region, and a width. The damper seal further includes a first portion extending from the first end region of the central body portion, and a first end region of the first portion includes first outwardly extending tabs that define a first enlarged portion that has a first width greater than the width of the central body portion and a second portion extending from the opposing second end region of the central body portion.
申请公布号 WO2013154657(A2) 申请公布日期 2013.10.17
申请号 WO2013US23132 申请日期 2013.01.25
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 SNYDER, DANIEL A.;LANA, KYLE, CHARLES;SANDOVAL, JONATHAN, PERRY;VIRKLER, SCOTT, DANIEL;TARASKEVICH, JAIMIE;OTERO, EDWIN
分类号 F01D11/00;F01D5/14 主分类号 F01D11/00
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