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 US2013195665(A1) 申请公布日期 2013.08.01
申请号 US201213362552 申请日期 2012.01.31
申请人 SNYDER DANIEL A.;LANA KYLE CHARLES;SANDOVAL JONATHAN PERRY;VIRKLER SCOTT DANIEL;TARASKEVICH JAIMIE;OTERO EDWIN 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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