发明名称 Hinge device of a nacelle cowling of an aircraft engine on a supporting structure
摘要 A hinge device of a nacelle cowling of an aircraft engine on a supporting structure is disclosed. The hinge device includes two fittings and a link rod connected thereto and mounted on the fitting by an end connection. The link rod is further mounted on the fitting by an intermediate connection including a pivot pin slidably housed in a hole, and the end connection includes a guide pin slidably housed in a guide ramp. The connections are designed so as to create, upon rotation of the link rod about the pin, a relative movement of the axis in the ramp, simultaneously causing a relative movement of the pin in the hole.
申请公布号 US7959107(B2) 申请公布日期 2011.06.14
申请号 US20070765065 申请日期 2007.06.19
申请人 AIRBUS FRANCE 发明人 BEAUFORT JACQUES
分类号 B64C1/14 主分类号 B64C1/14
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