发明名称 KNIFE EDGE SEAL FOR GAS TURBINE ENGINE
摘要 A seal for a gas turbine engine and a gas turbine engine employing such a seal are disclosed. More specifically, the engine includes a knife edge seal which is better able to withstand the extremely high temperatures and mechanical loads to which gas turbine engine components are increasingly subjected. By moving the knife edge seal to the aft hub and cantilevering its angle off of vertical, thermal and mechanical loads are balanced and thus thermal mechanical fatigue life is improved while low cycle fatigue is maintained.
申请公布号 EP2831380(A4) 申请公布日期 2015.12.23
申请号 EP20130778419 申请日期 2013.01.16
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 KNAUL, DAVID, A.;MAALOUF, FADI, S.;AIELLO, NICHOLAS;MORGAN, ORENTHRAL, T.;MALI, RAJI
分类号 F01D11/14 主分类号 F01D11/14
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