发明名称 Gasket, e.g. a metal gasket, for a gas turbine engine
摘要 A gasket assembly (50) for a gas turbine engine includes a seal portion (52) defining outer surfaces (62) for providing sealing contact and a bias portion (54) defining inner structures that are spaced apart from the seal portion (52) for biasing the outer surfaces (62) into sealing contact. The gasket further includes end portions (56) disposed at ends of the seal portion (52) that including a material thickness greater than a thickness of the bias portion (54).
申请公布号 EP2589757(A2) 申请公布日期 2013.05.08
申请号 EP20120190515 申请日期 2012.10.30
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 LUTJEN, PAUL M.;STEVENS, MICHAEL S.
分类号 F01D11/00;F16J15/08 主分类号 F01D11/00
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