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1. 发明授权

US5570859A Aerodynamic braking device 失效
标题翻译：气动制动装置
公开(公告)号：US5570859A
公开(公告)日：1996-11-05
申请号：US370371
申请日：1995-01-09
申请人： Gene A. Quandt
发明人： Gene A. Quandt
IPC分类号： B64C9/18 , F03D7/02 , B64C27/72
CPC分类号： F03D7/0252 , B64C9/18 , Y02E10/723
摘要： A spoiler flap is pivotably mounted to the rearward portion of a wind turbine blade or wing to control or influence air flow over the surface of the blade or wing. The spoiler flap has forward and rearward edges. The spoiler flap can be pivoted to simultaneously raise the forward edge (into low pressure flow) and lower the rearward edge of the spoiler flap (into high pressure flow). The extent to which the spoiler flap is pivoted determines the extent to which the air flow over the surface of the blade or wing is influenced. When the spoiler flap is fully deployed or pivoted, it serves as a braking device. When it is only partially pivoted, it serves the function of power modulation.
摘要翻译：扰流板可枢转地安装到风力涡轮机叶片或机翼的后部，以控制或影响叶片或机翼表面上的空气流动。扰流板具有前后边缘。扰流板可以枢转，同时将前缘（低压流动）提升并降低扰流板的后边缘（进入高压流）。扰流板折叠的程度决定了叶片或机翼表面上的气流如何受到影响。当扰流板完全展开或枢转时，它用作制动装置。当它仅部分转动时，它起到功率调制功能。

2. 发明申请

US20140077038A1 AIRCRAFT FLAP SYSTEM AND ASSOCIATED METHOD 有权
标题翻译：飞机襟翼系统及相关方法
公开(公告)号：US20140077038A1
公开(公告)日：2014-03-20
申请号：US13623533
申请日：2012-09-20
申请人： Bruce A. Dahl , Gene A. Quandt
发明人： Bruce A. Dahl , Gene A. Quandt
IPC分类号： B64C9/20
CPC分类号： B64C9/20 , B64C9/323 , B64C2009/143 , Y02T50/32
摘要： An aircraft flap system and an associated method are provided to facilitate ground roll breaking without compromising in-flight performance. The aircraft flap system includes a first flap and a panel pivotally attached to the first flap, such as to a rearward portion of the first flap. The aircraft flap system also includes an actuator configured to controllably position the panel in a stowed position and in a deployed position. In the stowed position, the panel serves as a continuation of the first flap, thereby contributing to the lift provided by the first flap during flight. Conversely, in the deployed position, a panel is articulated relative to the first flap, thereby reducing or eliminating the lift otherwise provided by the flap, following landing of the aircraft.
摘要翻译：提供飞行器翼片系统和相关联的方法以便于地面滚动破碎而不损害飞行性能。飞行器翼片系统包括第一翼片和枢转地附接到第一翼片的面板，例如到第一翼片的后部。飞行器翼片系统还包括致动器，该致动器被配置为将面板可控地定位在收起位置和展开位置。在收起位置，面板作为第一挡板的延续部，从而有助于在飞行期间由第一挡板提供的升力。相反，在展开位置，面板相对于第一挡板铰接，从而减少或消除由飞行器着陆后由挡板提供的电梯。

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