发明名称 Bypass engine with means for limiting gas leakage
摘要 A bypass engine including a fan which has its blades disposed in both the primary gas flow path and the secondary gas flow path of the engine is provided with an annular intermediate gas flow path in the space between the primary and secondary flow paths, and gas take-off means is connected to a compressor of the engine and arranged to direct a flow of gas longitudinally along the intermediate flow path to prevent leakage of hot gas to the secondary flow path via the gaps existing between the platforms of the fan blades and the adjacent annular members of the primary and secondary flow paths.
申请公布号 US5822975(A) 申请公布日期 1998.10.20
申请号 US19970834877 申请日期 1997.04.10
申请人 SOCIETE NATIONAL D'ETUDE ET DE AUCTION DE MOTEURS D'AVIATION "SNECMA" 发明人 GUYONNET, XAVIER JEAN-MICHEL ANDRE;WURNIESKY, PASCAL CLAUDE
分类号 F01D5/02;F02K3/04;(IPC1-7):F02C7/28 主分类号 F01D5/02
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