The invention relates to a front engine attachment system (150) for an engine of an aircraft, where the front engine attachment system (150) has an engine pylon (12) having a front rib (62); a front engine attachment (50) having a first link (56) fixed directly to the front rib (62) by two connection points (60a-b), and a second link (70), a first end (72) of which is fixed to the first link (56) by a connection point (60e); and an engine housing (14) of the engine (10), in which the first connecting rod (56) is fixed directly to the engine housing (14) by at least two connection points (60c-d), and in which the second end (76) of the second connecting rod (70) is fixed to the engine housing (14) by a connection point (73). Such a front engine attachment system is simple, compact and easy to manufacture in which the first link is thus fastened directly to the front rib.
本发明涉及一种飞行器的发动机的前发动机附接系统(150),其中该前发动机附接系统(150)具有:发动机吊挂架(12),该发动机吊挂架具有前肋(62);前发动机附接件(50),前发动机附接件具有通过两个连接点(60a‑b)直接固定至所述前肋(62)的第一连杆(56),以及第二连杆(70),该第二连杆的第一端(72)通过连接点(60e)固定至所述第一连杆(56);以及所述发动机(10)的发动机壳体(14),其中第一连杆(56)通过至少两个连接点(60c‑d)直接固定至发动机壳体(14),并且其中第二连杆(70)的第二端(76)通过连接点(73)固定至发动机壳体(14)。这种前发动机附接系统简单、紧凑且易于制造,其中第一连杆因此直接紧固到前肋。
Front engine attachment system for aircraft engine having lightweight structure
具有轻质结构的飞行器发动机的前发动机附接系统
2022-07-08
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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