发明名称 AIRCRAFT ENGINE WITH SUSPENSION APPLIANCES
摘要 FIELD: aircraft engineering. ^ SUBSTANCE: invention relates to aircraft engines, particular by to engine suspensions. Engine suspension appliances allow transmitting forces between engine crankcase and airplane frame and comprise safety emergency device. The latter consists of safety yoke with two ears (31, 32) and long tab, or similar device arranged between aforesaid two ears. Aforesaid yoke or long tab is rigidly attached to engine crankcase element, while the other element is attached to safety emergency device. Note here that both aforesaid elements pass through safety pins (35), perpendicular to engine axis, while both ears (31, 32) and long tab are arranged parallel to aforesaid engine axis. ^ EFFECT: possibility to transmit front suspension traction force in case transmission gear fails. ^ 8 cl, 3 dwg
申请公布号 RU2372256(C2) 申请公布日期 2009.11.10
申请号 RU20050113388 申请日期 2005.05.03
申请人 SNEKMA 发明人 DRON SEBAST'JAN
分类号 B64D27/16;B64D27/20;B64D27/26;F02C7/20 主分类号 B64D27/16
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