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
