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    Tragflügel
    11.
    发明公开
    Tragflügel 失效
    Tragflügel。

    公开(公告)号：EP0260586A2

    公开(公告)日：1988-03-23

    申请号：EP87113154.6

    申请日：1987-09-09

    申请人： Riedelsheimer, Hans-Joachim

    发明人： Riedelsheimer, Hans-Joachim

    IPC分类号： B64C3/50 ,  B64C3/58

    CPC分类号： B64C3/58 ,  B64C3/50

    摘要： Zur Vergrößerung des maximalen Anstellwinkels und damit verbunden des Auftriebes sowie zur Erhöhung der Sicherheit wird bei Tragflügeln 1 für Flugzeuge vor­geschlagen, an der Oberseite 2 eine Klappe 4 schwenk­bar zu befestigen, die im anliegenden Zustand von der Hinterkante 3 ausgeht und bei Verschwenkung an der Hinterkante 3 öffnet und deren Öffnungswinkel maximal 90 Grad beträgt.

    摘要翻译： 为了增加最大迎角和因此提升安全性，提出在机翼1的情况下，飞机能以可转动的方式附接到顶侧2，一个翼片4，其在后缘3处突出， 紧密配合，在后缘3旋转时开启，最大孔径角为90度。

    WING TIP DEVICE WITH WINGLETS
    14.
    发明授权
    WING TIP DEVICE WITH WINGLETS 有权

    公开(公告)号：EP2982600B1

    公开(公告)日：2018-06-13

    申请号：EP15184356.2

    申请日：2011-07-07

    申请人： Airbus Operations Limited ,  Airbus Operations GmbH ,  Deutsches Zentrum für Luft- und Raumfahrt e.V.

    发明人： Wright, Christopher ,  Chu, James, K. ,  Himisch, Jan

    IPC分类号： B64C23/06 ,  B64C3/58

    CPC分类号： B64C23/065 ,  B64C3/58 ,  B64C23/069 ,  Y02T50/164 ,  Y10T29/49716

    摘要： A wing tip device for fixing to the outboard end of a wing (401), the wing (401) defining a wing plane, the wing tip device comprising: an upper wing-like element (404) projecting upwardly with respect to the wing plane and having a trailing edge (416); and a lower wing-like element (407) fixed with respect to the upper wing-like element (404) and having a root chord and a trailing edge (417), the lower wing-like element (407) root chord intersecting with the upper wing-like element (404), and the lower wing-like element (407) projecting downwardly from the intersection, wherein the upper wing-like element (404) is larger than the lower wing-like element (407) and the trailing edge (417) of the lower wing-like element is adjacent the trailing edge (416) of the upper wing-like element at the intersection, and wherein an included angle between the upper and lower wing-like elements (404, 407) at the intersection is less than, or equal to, 160 degrees. Also, a wing with the wing tip device; an aircraft with the wing; a method of fitting, or retro-fitting, the wing tip device to a wing; a method of modifying an existing wing tip device; and a method of operating a wing with the wing tip device.

    AIRCRAFT WINGS, AIRCRAFT, AND RELATED METHODS
    15.
    发明公开
    AIRCRAFT WINGS, AIRCRAFT, AND RELATED METHODS 审中-公开
    飞机翼，飞机和相关方法

    公开(公告)号：EP3309059A1

    公开(公告)日：2018-04-18

    申请号：EP17195660.0

    申请日：2017-10-10

    申请人： The Boeing Company

    发明人： KORDEL, Jan A. ,  BALZER, Michael Albert ,  BURTON, Jeffrey ,  WALKER, Steven Paul ,  SAUNDERS, John Barry

    IPC分类号： B64C9/32

    CPC分类号： B64C3/58 ,  B33Y10/00 ,  B33Y80/00 ,  B64C3/187 ,  B64C3/22 ,  B64C9/18 ,  B64C9/323 ,  B64C9/34 ,  Y02T50/32

    摘要： The disclosure relates to aircraft wings, aircraft, and related methods. Aircraft wings include a spoiler constructed substantially of a monolithic structural body with an upper side that defines a portion of an airfoil surface of an aircraft wing. The monolithic structural body further includes a lower side, opposite the upper side, that includes a plurality of stiffening ribs that define a plurality of open voids. Methods of constructing a spoiler for an aircraft wing include forming a monolithic structural body of the spoiler.

    摘要翻译： 本公开涉及飞机机翼，飞机和相关方法。 飞机机翼包括基本上由整体结构体构成的扰流板，其具有限定飞机机翼的翼型表面的一部分的上侧。 整体结构体还包括与上侧相对的下侧，其包括限定多个开放空隙的多个加强肋。 构造用于飞机机翼的扰流器的方法包括形成扰流器的整体结构体。

    BLADE FLOW DEFLECTOR
    16.
    发明公开
    BLADE FLOW DEFLECTOR 审中-公开
    SCHAUFELSTRÖMUNGSDEFLEKTOR

    公开(公告)号：EP3080402A4

    公开(公告)日：2017-09-06

    申请号：EP14866425

    申请日：2014-11-26

    申请人： UNIV RUTGERS

    发明人： DIEZ-GARIAS FRANCISCO JAVIER ,  VAQUERO ARTURO VILLEGAS

    IPC分类号： F01D5/14 ,  B64C3/58 ,  B64C11/18 ,  B64C27/467 ,  F03D1/06

    CPC分类号： F03D1/0641 ,  B64C3/58 ,  B64C11/18 ,  B64C27/467 ,  F01D5/14 ,  F03B17/061 ,  F03D1/0683 ,  F05B2240/30 ,  F05B2240/301 ,  Y02E10/28 ,  Y02E10/721 ,  Y02T50/673

    摘要： An airfoil blade assembly including a blade which includes a lift generating section with a first profiled body defined between a pressure surface and a suction surface. The first profiled body extends from a first leading edge to a first trailing edge with a first chord extending form the first leading edge to the first trailing edge and being perpendicular to the radial direction. At least one flow deflector extends along either the pressure surface or the suction surface within the lift generating section of the blade. The at least one flow deflector defines a second profiled body extending between a second leading edge and a second trailing edge with a second chord extending between the second leading edge and the second trailing edge. The second profiled body defines an outer surface facing away from respective pressure surface or suction surface along which the flow deflector extends.

    摘要翻译： 一种翼型叶片组件，其包括叶片，所述叶片包括升力产生部分，所述升力产生部分具有限定在压力表面和吸力表面之间的第一成形主体。 第一成型体从第一前缘延伸到第一后缘，第一弦从第一前缘延伸到第一后缘并垂直于径向方向。 至少一个导流板沿着叶片的升程产生部分内的压力表面或吸力表面延伸。 所述至少一个导流板限定第二成形主体，所述第二成形主体在第二前缘与第二后缘之间延伸，并具有在所述第二前缘与所述第二后缘之间延伸的第二弦。 第二成形主体限定背离相应的压力表面或吸力表面的外表面，导流器沿着该相应的压力表面或吸力表面延伸。

    WING TIP DEVICE AND METHODS
    19.
    发明授权
    WING TIP DEVICE AND METHODS 有权
    翼尖装置及方法

    公开(公告)号：EP2593362B1

    公开(公告)日：2014-09-03

    申请号：EP11730015.2

    申请日：2011-07-07

    申请人： Airbus Operations Limited ,  Airbus Operations GmbH

    发明人： WRIGHT, Christopher ,  CHU, James, K. ,  HIMISCH, Jan

    IPC分类号： B64C23/06

    CPC分类号： B64C23/065 ,  B64C3/58 ,  B64C23/069 ,  Y02T50/164 ,  Y10T29/49716

    摘要： A wing tip device for fixing to the outboard end of a wing (401), the wing (401) defining a wing plane, the wing tip device comprising: an upper wing-like element (404) projecting upwardly with respect to the wing plane and having a trailing edge (416); and a lower wing-like element (407) fixed with respect to the upper wing-like element (404) and having a root chord and a trailing edge (417), the lower wing-like element (407) root chord intersecting with the upper wing-like element (404), and the lower wing-like element (407) projecting downwardly from the intersection, wherein the upper wing-like element (404) is larger than the lower wing-like element (407) and the trailing edge (417) of the lower wing-like element is adjacent the trailing edge (416) of the upper wing-like element at the intersection, and wherein an included angle between the upper and lower wing-like elements (404, 407) at the intersection is less than, or equal to, 160 degrees. Also, a wing with the wing tip device; an aircraft with the wing; a method of fitting, or retro-fitting, the wing tip device to a wing; a method of modifying an existing wing tip device; and a method of operating a wing with the wing tip device.

    Wing tip device
    20.
    发明公开
    Wing tip device 有权
    Flügelspitzenanordnung

    公开(公告)号：EP2610169A1

    公开(公告)日：2013-07-03

    申请号：EP13161204.6

    申请日：2011-07-07

    申请人： AIRBUS OPERATIONS LIMITED ,  Airbus Operations GmbH

    发明人： Wright, Christopher ,  Chu, James, K. ,  Himisch, Jan

    IPC分类号： B64C23/06

    CPC分类号： B64C23/065 ,  B64C3/58 ,  B64C23/069 ,  Y02T50/164 ,  Y10T29/49716

    摘要： A wing tip device for fixing to the outboard end of a wing (401), the wing (401) defining a wing plane, the wing tip device comprising: an upper wing-like element (404) projecting upwardly with respect to the wing plane and having a trailing edge (416); and a lower wing-like element (407) fixed with respect to the upper wing-like element (404) and having a root chord and a trailing edge (417), the lower wing-like element (407) root chord intersecting with the upper wing-like element (404), and the lower wing-like element (407) projecting downwardly from the intersection, wherein the upper wing-like element (404) is larger than the lower wing-like element (407) and the trailing edge (417) of the lower wing-like element is adjacent the trailing edge (416) of the upper wing-like element at the intersection, and wherein an included angle between the upper and lower wing-like elements (404, 407) at the intersection is less than, or equal to, 160 degrees. Also, a wing with the wing tip device; an aircraft with the wing; a method of fitting, or retro-fitting, the wing tip device to a wing; a method of modifying an existing wing tip device; and a method of operating a wing with the wing tip device.

    摘要翻译： 一种翼尖装置，用于固定到翼（401）的外侧端，所述翼（401）限定翼平面，所述翼尖装置包括：相对于翼平面向上突出的上翼形元件（404） 并具有后缘（416）; 和相对于上翼形元件（404）固定并具有根弦和后缘（417）的下翼形元件（407），所述下翼形元件（407）的根弦与 上翼状元件（404）和从交叉点向下突出的下翼形元件（407），其中上翼形元件（404）大于下翼状元件（407），并且尾翼 下翼形元件的边缘（417）在相交处邻近上翼形元件的后缘（416），并且其中上翼形元件（404,407）之间的夹角在 交叉点小于或等于160度。 另外，一翼与翼尖装置; 一架飞机与翼; 将翼尖装置装配或改装成翼的方法; 修改现有翼尖装置的方法; 以及用翼尖装置操作机翼的方法。