SINGLE SLOTTED FLAP WITH SLIDING DEFLECTOR FLAP AND LOWERABLE SPOILER
    1.
    发明申请
    SINGLE SLOTTED FLAP WITH SLIDING DEFLECTOR FLAP AND LOWERABLE SPOILER 审中-公开
    单滑块与滑动偏转片和可更换的球面

    公开(公告)号:WO2006108579A1

    公开(公告)日:2006-10-19

    申请号:PCT/EP2006/003212

    申请日:2006-04-07

    CPC classification number: B64C9/20 B64C9/02 B64C9/18 B64C2009/143 Y02T50/44

    Abstract: The present invention relates to a device for adjusting the lift characteristics of an aircraft with a high lift device (2) that is movably attachable to a wing element (1) and that comprises at least one slot covering device (3; 4), wherein the at least one slot covering device (3; 4), is movably attachable to the wing element (1). The slot covering device (3; 4) is designed to regulate the size of a slot (7) between the wing element (1) and the high lift device (2).

    Abstract translation: 本发明涉及一种用于通过具有可移动地附接到翼元件(1)并且包括至少一个狭槽覆盖装置(3; 4)的高升降装置(2)来调节飞行器的提升特性的装置,其中 所述至少一个狭槽覆盖装置(3; 4)可移动地附接到所述翼元件(1)。 狭槽覆盖装置(3; 4)被设计成调节翼元件(1)和高升降装置(2)之间的狭槽(7)的尺寸。

    SINGLE SLOTTED FLAP WITH SLIDING DEFLECTOR FLAP AND LOWERABLE SPOILER
    2.
    发明申请
    SINGLE SLOTTED FLAP WITH SLIDING DEFLECTOR FLAP AND LOWERABLE SPOILER 审中-公开
    单滑块与滑动偏转片和可更换的球面

    公开(公告)号:WO2006108579B1

    公开(公告)日:2007-01-11

    申请号:PCT/EP2006003212

    申请日:2006-04-07

    CPC classification number: B64C9/20 B64C9/02 B64C9/18 B64C2009/143 Y02T50/44

    Abstract: The present invention relates to a device for adjusting the lift characteristics of an aircraft with a high lift device (2) that is movably attachable to a wing element (1) and that comprises at least one slot covering device (3; 4), wherein the at least one slot covering device (3; 4), is movably attachable to the wing element (1). The slot covering device (3; 4) is designed to regulate the size of a slot (7) between the wing element (1) and the high lift device (2).

    Abstract translation: 本发明涉及一种用于通过具有可移动地附接到翼元件(1)并且包括至少一个狭槽覆盖装置(3; 4)的高升降装置(2)来调节飞行器的提升特性的装置,其中 所述至少一个狭槽覆盖装置(3; 4)可移动地附接到所述翼元件(1)。 狭槽覆盖装置(3; 4)被设计成调节翼元件(1)和高升降装置(2)之间的狭槽(7)的尺寸。

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