REAR BELT OF TURBOJET ENGINE-TO-AIRCRAFT FASTENING SYSTEM Russian patent published in 2002 - IPC

FIELD: aeronautical engineering. SUBSTANCE: invention relates to devices for fastening engines to aircraft, particularly, to single-engine aircraft. Rear belt of system fastening turbojet engine 2 to aircraft fuselage 1 has ring 3 installed around rear load-bearing belt of engine. Engine is installed in ring with ring radial compensating clearance 4. Ring space is made on inner side of ring which accommodates resilient member installed to thrust without clearance relative to engine. Invention prevents taking of torque load from engine by fuselage owing to provision of engine turning relative to fuselage. EFFECT: improved comfort owing to damping of dynamic loads by installed resilient member. 2 cl, 3 dwg