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    DRAG NEUTRAL VEHICLE WINDOW
    4.
    发明授权
    DRAG NEUTRAL VEHICLE WINDOW 有权

    公开(公告)号：EP2794395B1

    公开(公告)日：2018-10-10

    申请号：EP12830870.7

    申请日：2012-12-18

    申请人： Bombardier Inc. ,  Short Brothers Plc

    发明人： DESROCHES, Alexandre ,  LENCZ, David ,  DERVAULT, Franck

    IPC分类号： B64C1/14 ,  B32B17/10

    CPC分类号： B64C1/1484 ,  B32B17/10055 ,  B32B17/10165 ,  B60J1/007 ,  B64C1/1492 ,  E06B3/66 ,  E06B7/16 ,  Y10T29/49764 ,  Y10T428/24628

    摘要： A window for a vehicle includes at least one transparent pane (30). The transparent pane comprises a deformable material. The transparent pane defines a first surface position h 1 when not subjected to a pressure differential thereacross and a second surface position h 2 when subject to the differential pressure thereacross. The first and second surface positions are defined with reference to an outside mold line. The first surface position h 1 defines a reverse curvature with respect to the outside mold line. In response to the differential pressure ”P, the second surface position h 2 includes bulging of the transparent pane by a predetermined distance ”h. The window is connected to a structural exterior surface of the pressurized vehicle without an intermediate frame.

    WINDOW OF AN AIRCRAFT
    6.
    发明授权
    WINDOW OF AN AIRCRAFT 有权

    公开(公告)号：EP2996938B1

    公开(公告)日：2018-06-13

    申请号：EP14797229.3

    申请日：2014-05-14

    申请人： Honda Patents & Technologies North America, LLC

    发明人： FUJINO, Michimasa ,  HOMMA, Yasuhiro

    IPC分类号： B64C1/14 ,  E06B5/12 ,  E06B9/24

    CPC分类号： B64C1/1484 ,  B64C1/1492 ,  B64D11/02

    摘要： An aircraft includes a fuselage including a plurality of frame members disposed at predetermined intervals in a longitudinal direction of the fuselage and a plurality of stringers extending substantially linearly in the longitudinal direction. The fuselage defines an aircraft interior. A compartment is located in the interior of the fuselage. The compartment defines an interior area. A first one window assembly is mounted to an upper portion of the fuselage for introducing daylight into the interior area. The first window assembly is flanked by adjacent frame members of the plurality of frame members and adjacent stringers of the plurality of stringers. The first window assembly includes a window pane, an inner cover and a retainer. The inner cover introduces daylight from the window pane into the interior area. The retainer secures the window pane and the inner cover to the fuselage.