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    AIRCRAFT LANDING GEAR INCLUDING A FAIRING
    1.
    发明公开
    AIRCRAFT LANDING GEAR INCLUDING A FAIRING 有权
    有盖的空气悬架

    公开(公告)号：EP2509863A1

    公开(公告)日：2012-10-17

    申请号：EP10718678.5

    申请日：2010-04-30

    申请人： Messier-Dowty Limited

    发明人： SIMONNEAUX, Yann

    IPC分类号： B64C25/00

    CPC分类号： B64C25/001 ,  B64C2025/003

    摘要： An aircraft landing gear including a fairing (12) arranged to be moveable between first and second configurations, wherein in the first configuration the fairing shields an element of the landing gear from an incident airflow, the fairing being arranged to be in the first configuration when the landing gear is deployed but unloaded, and wherein in the second configuration the fairing exposes the landing gear element to the incident airflow, the fairing being arranged to be in the second configuration when the landing gear is deployed and loaded.

    AIRCRAFT LANDING GEAR WITH A HOLLOW STRUCTURAL ELEMENT
    3.
    发明公开
    AIRCRAFT LANDING GEAR WITH A HOLLOW STRUCTURAL ELEMENT 有权
    具有中空结构元素空气悬架

    公开(公告)号：EP2490937A1

    公开(公告)日：2012-08-29

    申请号：EP10718674.4

    申请日：2010-04-30

    申请人： Messier-Dowty Limited

    发明人： SIMONNEAUX, Yann

    IPC分类号： B64C25/02

    CPC分类号： B64C25/02

    摘要： Aircraft landing gear including at least one load bearing longitudinal structural element (116) wherein said longitudinal structural element is hollow and is arranged to have at least one non-structural element (118) located inside.

    A LANDING GEAR ASSEMBLY
    5.
    发明公开
    A LANDING GEAR ASSEMBLY 有权
    悬挂装置

    公开(公告)号：EP2663490A1

    公开(公告)日：2013-11-20

    申请号：EP11804766.1

    申请日：2011-12-21

    申请人： Messier-Dowty Limited

    发明人： LACY, Stuart ,  SIMONNEAUX, Yann

    IPC分类号： B64C25/36 ,  B64C25/50

    CPC分类号： B64C25/50 ,  B64C25/34 ,  B64C25/36 ,  B64C2025/345

    摘要： A landing gear assembly for an aircraft, the landing gear assembly 10 comprises an elongate bogie beam 12 and a first axle bearing 16a having an outer part 16aâ rotatably coupled to an inner part of bogie socket 14 by, for example, an interference fit. An inner part 16aâ â of the bearing 16a has a mounting aperture 18a and has a bearing axis B which is offset from a longitudinal axis A of a steerable axle. This offset configuration is such that rotation of the inner part 16aâ â causes a change in the orientation of the steerable axle relative to the bogie beam 12. An actuator causes rotation of the inner part 16aâ â and of an intermediate part so that an angular position of these parts is changed. The actuator receives a signal transmitted by a processing device, e.g. micro controller (42, fig 8), which receives input signals from an input device such as a joy stick (44).