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1. 发明授权

US06786451B2 Aircraft landing gear having an independent low-noise fairing system 有权
标题翻译：飞机起落架具有独立的低噪音整流罩系统
公开(公告)号：US06786451B2
公开(公告)日：2004-09-07
申请号：US10360638
申请日：2003-02-10
申请人： Maud Courtois , Dominique Ducos
发明人： Maud Courtois , Dominique Ducos
IPC分类号： B64C2516
CPC分类号： B64C25/16 , B64C7/00 , B64C2025/003
摘要： The invention relates to an aircraft landing gear having a retractable leg, in which the leg comprises a strut with a telescopic rod, the strut being hinged to a structure of the aircraft in order to pivot between a gear-up position and a gear-down position, said strut also being connected to the structure of the aircraft via hinged brace elements. According to an essential aspect of the invention, the landing gear includes an independent low-noise fairing system that serves, when the leg is in the gear-down position, to cover the front of at least a portion of the hinge between the brace elements, said low-noise fairing system comprising a hinged fairing of two complementary portions connected to each other via a hinge whose axis is parallel to the axis of the corresponding hinge portion of said brace elements.
摘要翻译：本发明涉及一种具有可伸缩腿部的飞机起落架，其中腿部包括具有伸缩杆的支柱，该支柱铰接到飞行器的结构上，以便在起落位置和减档之间枢转所述支柱还通过铰链支架元件连接到飞行器的结构。根据本发明的一个重要方面，起落架包括一个独立的低噪声整流装置系统，当腿部处于减速位置时，其用于覆盖支架元件之间铰链的至少一部分的前部所述低噪声整流罩系统包括通过铰链彼此连接的两个互补部分的铰接整流罩，所述铰链的轴线平行于所述支撑元件的相应铰链部分的轴线。

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