发明名称 Suspension system for carrying an external load with an aircraft, and an aircraft
摘要 A suspension system (10) of an aircraft (1). The suspension system (10) comprises a fastener device (15) including a coupling member (20) suitable for carrying a load (5) with a sling (21). The suspension system (10) has a return device (30) that comprises a linkage (40) provided with a plurality of bars (41, 42, 43) hinged in pairs to apply a non-linear force to the coupling device (15), said linkage (40) being suitable for fastening to a load-carrier structure (2) of an aircraft (1). In addition, the return device (30) includes a tie (35) connecting said linkage (40) to the coupling device (15), as well as a spring member (36) fastened to a bar (41) of the linkage (40) and suitable for being connected to an aircraft (1).
申请公布号 US9340285(B2) 申请公布日期 2016.05.17
申请号 US201414325648 申请日期 2014.07.08
申请人 AIRBUS HELICOPTERS 发明人 Prud'homme-Lacroix Pierre;Garcin Patrice
分类号 B64D1/22;B64C1/22;B64C27/04 主分类号 B64D1/22
代理机构 Brooks Kushman P.C. 代理人 Brooks Kushman P.C.
主权项 1. A suspension system for carrying an external load with an aircraft, the suspension system comprising: a coupling device for carrying the external load, the coupling device comprising a coupling member suitable for carrying a sling; a return device tending to place the coupling device in a storage position while fastened to the aircraft absent the external load while allowing the coupling device to move towards a working position when the external load is present; wherein the return device comprises: a linkage provided with a plurality of rigid bars that are hinged so that two adjacent bars are hinged to each other in order to apply a non-linear force to the coupling device, the linkage being suitable for fastening to a load-carrier structure of the aircraft; a tie connecting the linkage to the coupling device; anda spring member fastened to a bar of the linkage and suitable for being connected to the aircraft.
地址 Marignane FR
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