Landing gear door assembly
    1.
    发明授权
    Landing gear door assembly 有权
    起落架门总成

    公开(公告)号:US07458542B2

    公开(公告)日:2008-12-02

    申请号:US10504253

    申请日:2004-04-07

    IPC分类号: B64C25/10

    摘要: An aircraft landing gear door assembly (1, 2, 3, 4, 5) includes a door (1), which is moveable to an open position, in which an aperture (6) is exposed, the landing gear (10) being able to be deployed through said aperture (6), and moveable to a closed position, in which the door (1) is closed across the aperture (6). The door (1) is arranged for rotational movement of a first type, in which the door rotates about an axis that is substantially parallel to the length of the aircraft, between the closed position and the open position. The door (1) is also arranged for movement of a second type, different from the first type, in which the door (1) rotates, about an axis that is substantially transverse to the length of the aircraft, to a position in which it acts as a fairing to reduce the noise caused by the landing gear or a part thereof. In one embodiment, the second type of movement is rotational movement about an axis that is substantially parallel to the door when in the closed position and the door (1) forms a ramp type fairing. In another embodiment, the second type of movement is rotational movement about an axis that is substantially transverse to the door when in the closed position and the door (31) forms a V-shaped fairing (when viewed from above) with an opposite door (33).

    摘要翻译: 飞机起落架门组件(1,2,3,4,5)包括门(1),该门能够移动到打开位置,其中露着孔(6),起落架(10)能够 通过所述孔(6)部署,并且可移动到关闭位置,其中门(1)跨过孔(6)封闭。 门(1)布置成用于第一类型的旋转运动,其中门围绕基本上平行于飞行器的长度的轴线在关闭位置和打开位置之间旋转。 门(1)还布置成用于与第一类型不同的第二类型的移动,门(1)围绕基本横向飞行器的长度的轴线旋转到其中的位置 作为整流罩,以减少起落架或其一部分引起的噪音。 在一个实施例中,第二类型的运动是在处于关闭位置且门(1)形成斜坡式整流罩时围绕基本上平行于门的轴的旋转运动。 在另一个实施例中,第二类型的运动是在处于关闭位置时围绕基本上横向于门的轴线的旋转运动,并且门(31)形成V形整流罩(当从上方观察时)与相对的门 33)。

    Aircraft landing gear and door assembly
    2.
    发明授权
    Aircraft landing gear and door assembly 有权
    飞机起落架和门总成

    公开(公告)号:US08028956B2

    公开(公告)日:2011-10-04

    申请号:US12233229

    申请日:2008-09-18

    IPC分类号: B64C25/40

    CPC分类号: B64C25/16 B64C2025/003

    摘要: An aircraft landing gear door assembly includes a door, which is moveable to an open position, in which an aperture is exposed, the landing gear being able to be deployed through said aperture, and moveable to a closed position, in which the door is closed across the aperture. The door is arranged for rotational movement of a first type, in which the door rotates about an axis that is substantially parallel to the length of the aircraft, between the closed position and the open position. The door is also arranged for movement of a second type, different from the first type, in which the door rotates, about an axis that is substantially transverse to the length of the aircraft, to a position in which it acts as a fairing to reduce the noise caused by the landing gear or a part thereof. In one embodiment, the second type of movement is rotational movement about an axis that is substantially parallel to the door when in the closed position and the door forms a ramp type fairing. In another embodiment, the second type of movement is rotational movement about an axis that is substantially transverse to the door when in the closed position and the door forms a V-shaped fairing (when viewed from above) with an opposite door.

    摘要翻译: 飞机起落架门组件包括可移动到打开位置的门,其中孔被暴露,起落架能够通过所述孔展开,并且可移动到关闭位置,在该关闭位置,门被关闭 穿过光圈。 门被布置成第一类型的旋转运动,其中门围绕基本上平行于飞行器的长度的轴在关闭位置和打开位置之间旋转。 门还被布置成与第一类型不同的第二类型的运动,其中门围绕基本横向于飞机长度的轴旋转到其作为整流罩以减小的位置 由起落架或其一部分引起的噪音。 在一个实施例中,第二类型的运动是在处于关闭位置时围绕基本上平行于门的轴的旋转运动,并且门形成斜坡式整流罩。 在另一个实施例中,第二类型的运动是在处于关闭位置时围绕基本上横向于门的轴的旋转运动,并且门形成V形整流罩(当从上方观察时)与相对的门形成。

    LANDING GEAR
    3.
    发明申请
    LANDING GEAR 有权
    起落架

    公开(公告)号:US20090008501A1

    公开(公告)日:2009-01-08

    申请号:US12233229

    申请日:2008-09-18

    IPC分类号: B64C25/12

    CPC分类号: B64C25/16 B64C2025/003

    摘要: An aircraft landing gear door assembly includes a door, which is moveable to an open position, in which an aperture is exposed, the landing gear being able to be deployed through said aperture, and moveable to a closed position, in which the door is closed across the aperture. The door is arranged for rotational movement of a first type, in which the door rotates about an axis that is substantially parallel to the length of the aircraft, between the closed position and the open position. The door is also arranged for movement of a second type, different from the first type, in which the door rotates, about an axis that is substantially transverse to the length of the aircraft, to a position in which it acts as a fairing to reduce the noise caused by the landing gear or a part thereof. In one embodiment, the second type of movement is rotational movement about an axis that is substantially parallel to the door when in the closed position and the door forms a ramp type fairing. In another embodiment, the second type of movement is rotational movement about an axis that is substantially transverse to the door when in the closed position and the door forms a V-shaped fairing (when viewed from above) with an opposite door.

    摘要翻译: 飞机起落架门组件包括可移动到打开位置的门,其中孔被暴露,起落架能够通过所述孔展开,并且可移动到关闭位置,在该关闭位置,门被关闭 穿过光圈。 门被布置成第一类型的旋转运动,其中门围绕基本上平行于飞行器的长度的轴在关闭位置和打开位置之间旋转。 门还被布置成与第一类型不同的第二类型的运动,其中门围绕基本横向于飞机长度的轴旋转到其作为整流罩以减小的位置 由起落架或其一部分引起的噪音。 在一个实施例中,第二类型的运动是在处于关闭位置时围绕基本上平行于门的轴的旋转运动,并且门形成斜坡式整流罩。 在另一个实施例中,第二类型的运动是在处于关闭位置时围绕基本上横向于门的轴的旋转运动,并且门形成V形整流罩(当从上方观察时)与相对的门形成。