发明名称 CERAMIC DUCT SYSTEM FOR TURBINE ENGINE
摘要 <p>D-4353 C-3278 CERAMIC DUCT SYSTEM FOR TURBINE ENGINE A gas turbine engine has a metal engine block which houses interconnected ceramic duct components defining the gas flow path between a combustor and turbine stages of a two spool gas turbine engine. The ceramic duct components are coupled to the engine block by support cages that accommodate thermal expansion of the duct components to prevent excessive stress levels within the ceramic components throughout a wide range of turbine engine operating conditions.</p>
申请公布号 CA1149181(A) 申请公布日期 1983.07.05
申请号 CA19810379323 申请日期 1981.06.09
申请人 GENERAL MOTORS CORPORATION 发明人 SMALE, CHARLES H.
分类号 F02B39/00;F02C3/10;F02C7/00;F02C7/24;(IPC1-7):F23R3/60 主分类号 F02B39/00
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