发明名称 ATTACHMENT OF TURBOJET TO AIRCRAFT
摘要 FIELD: transport.SUBSTANCE: turbojet comprises front blower, intermediate housing with outer shell and hub arranged behind the blower and interconnected by radial arms, and outlet housing with outer shell on common axle. Proposed attachment comprises front fastener at intermediate housing, rear fastener with small links of rear fastener connected with outlet housing outer shell, two thrust transmission links attached to intermediate housing bush at its front. Plane formed by said two small links is inclined forward relative to outlet housing plane.EFFECT: decreased local flexures of housing.18 cl, 7 dwg
申请公布号 RU2487821(C2) 申请公布日期 2013.07.20
申请号 RU20080148085 申请日期 2008.12.05
申请人 SNEKMA 发明人 SHUAR P'ER-ALEN ZHAN-MARI FILIPP JUG;LEFOR GIJOM
分类号 B64D27/26 主分类号 B64D27/26
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