Rear engine fastener for aircraft and aircraft

• Main Authors: BERJOT MICHAEL, CAYSSIALS JULIEN
• Format: Patent
• Language: Chinese; English
• Published: 25.09.2020
• Subjects: AIRCRAFT; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; AVIATION; COSMONAUTICS; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; PERFORMING OPERATIONS; TRANSPORTING

The invention relates to a rear engine fastener for an aircraft and an aircraft. The rear engine fastener is used to connect a main structure (56) of the aircraft and an engine (58). The rear engine fastener comprises: a support (62) configured to be connected to the main structure (56); at least one main lifting lug (70) connected to said support (62) by a first support link pin (72.1) and a second support link pin (72.2), wherein the support link pins are symmetrical with respect to a vertical longitudinal plane and are connected to the engine (58) by a first lateral engine link pin (76.1) and a central engine link pin (74); at least one secondary lifting lug (78) connected to the engine by means of a second lateral engine link pin (76.2) and to the main lifting lug (70) by means of a secondary link pin (80). 本发明的主题是一种飞行器的后部发动机紧固件和飞行器，该后部发动机紧固件用于连接飞行器的主结构(56)和发动机(58)，所述后部发动机紧固件包括：-支撑件(62)，所述支撑件被配置成连接至所述主结构(56)；-至少一个主吊耳(70)，该至少一个主吊耳通过第一支撑链接销(72.1)和第二支撑链接销(72.2)连接至所述支撑件(62)，这些支撑链接销相对于竖直纵向平面对称，并且通过第一侧向发动机链接销(7