发明名称 Mounting of a gas turbine combustor with integrated turbine inlet guide conduit
摘要 <p>The turbine has a high pressure turbine nozzle (20), inner and outer connection ferrules (50, 60) connecting combustion chamber/nozzle assembly of the turbine to inner and outer metallic enclosures (30, 40). Catches (35) provided around nozzle axis with respect to the enclosures distribute the forces exerted on the nozzle blades by the gas stream from the chamber such that the ferrules recapture the exerted forces.</p>
申请公布号 EP1607582(A1) 申请公布日期 2005.12.21
申请号 EP20050291184 申请日期 2005.06.02
申请人 SNECMA 发明人 AUMONT, CAROLINE;CONETTE, ERIC;DE SOUSA, MARIO CESAR;HERNANDEZ, DIDIER HIPPOLYTE
分类号 F01D9/02;F01D9/04;F01D25/24;(IPC1-7):F01D9/04 主分类号 F01D9/02
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