发明名称 Device for attachment of an engine onto an aircraft nacelle stub
摘要 This device is designed to transmit lateral and vertical forces generated by the engine to the nacelle stub (10), together with the engine torque, and comprises a main attachment structure and an emergency attachment structure (38). The main attachment structure includes two half-fittings (18a, 18b), connecting rods (20a, 20c) connecting the two half-fittings to the engine and attachment devices for the half-fittings on the nacelle stub. The emergency attachment structure transmits forces between one of the two half-fittings and the nacelle stub when the other half-fitting or its devices for attachment to the nacelle stub are defective. For example, it comprises a hinge pin (42) supported by the nacelle stub and passing through a hole (44) formed in the half-fittings with a clearance.
申请公布号 US2002104924(A1) 申请公布日期 2002.08.08
申请号 US20020052439 申请日期 2002.01.23
申请人 ROSZAK SEBASTIEN 发明人 ROSZAK SEBASTIEN
分类号 B64D27/26;(IPC1-7):B64D27/00 主分类号 B64D27/26
代理机构 代理人
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