发明名称 Lift-flap mechanism
摘要 Lift flap mechanism for adjusting a lift flap assigned to an airplane wing by means of a driving system, the lift flap mechanism comprising a main connection mechanism and a secondary connection mechanism in the form of a guide lever disposed in an articulated manner on the lift flap and the flap track, the main connection mechanism having a steering lever arrangement with at least one steering lever which has a first steering lever joint and a second steering lever joint, the at least one steering lever by way of a pendulum coupled to the first steering lever joint being connected with the flap track, and the second steering lever joint being guided such that, by means of a defined angular position of the at least one steering lever, the positions of the main connection joint and of the secondary connection joint are unambiguously determined.
申请公布号 US2005040294(A1) 申请公布日期 2005.02.24
申请号 US20040483380 申请日期 2004.09.13
申请人 PEREZ-SANCHEZ JUAN;BECHHEIM CLAUDIA;VOGLSINGER MARTIN 发明人 PEREZ-SANCHEZ JUAN;BECHHEIM CLAUDIA;VOGLSINGER MARTIN
分类号 B64C9/16;B64C9/22;(IPC1-7):B64C3/50 主分类号 B64C9/16
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