发明名称 GAS TURBINE ENGINE SEAL ASSEMBLY
摘要 <p>A seal assembly is positioned within a cavity that extends circumferentially about an axial centerline of a gas turbine engine. The cavity includes a cavity wall. The seal assembly includes a seal and a seal protector. The seal extends circumferentially within the cavity. The seal protector extends circumferentially within the cavity. The seal protector is positioned between the seal and the cavity wall. The seal protector includes a locating feature that is operative to contact the seal to aid in axially positioning the seal protector relative to the seal.</p>
申请公布号 WO2015002673(A2) 申请公布日期 2015.01.08
申请号 WO2014US17386 申请日期 2014.02.20
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 MCGARRAH, CRAIG R.
分类号 F01D11/08;F02C7/28;F04D29/08 主分类号 F01D11/08
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