发明名称 Mounting for aircraft gas turbine flow guides has flow guide sectors bolted directly in place on carrier and with sealing sectors to cover impingement surfaces
摘要 The mounting for the sectors of a flow guide in an aircraft gas turbine has the sectors (11) provided with ribs (13) which engage directly on the carrier (14) and are bolted (16) to them. The suspension hooks (21) on the opposite side is movable on the carrier. The sealing sectors (17) adjacent to the guide sectors can completely cover the impingement faces of the guide sectors.
申请公布号 FR2846997(A1) 申请公布日期 2004.05.14
申请号 FR20020013913 申请日期 2002.11.07
申请人 SNECMA MOTEURS 发明人 GIRARD PATRICK JOSEPH MARIE;IMBOURG SEBASTIEN ALAIN;PABION PHILIPPE JEAN PIERRE;SOUPIZON JEAN LUC
分类号 F01D9/04;(IPC1-7):F01D25/28;F01D25/24 主分类号 F01D9/04
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