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    • 3. 发明申请
    • ADAPTIVE COMPLIANT WING AND ROTOR SYSTEM
    • 自适应方式和转子系统
    • WO2004108525A1
    • 2004-12-16
    • PCT/US2004/006876
    • 2004-03-03
    • FLEXSYS, INC.KOTA, SridharHETRICK, Joel, A.
    • KOTA, SridharHETRICK, Joel, A.
    • B64C3/48
    • B63H25/38B63B1/285B63B1/32B63B39/06B63B2039/068B63G8/18B63G8/20B63G13/02B63G2013/027B63H1/26B63H3/002B63H25/382B64C3/48B64C27/001B64C27/615B64C2027/7222Y02T50/14Y02T50/34Y02T70/12
    • Variation in the contours of first and second compliant surfaces is produced by a compliant frame having a first resiliently variable frame element (120) having a corresponding first outer surface (122) and a first inner surface (124), and a second resiliently variable frame element (130) having a corresponding second outer surface (132) and a second inner surface (134). The first and second outer surfaces (122, 132) communicate with respective ones of the first and second compliant surfaces. A linkage element (141-144) having a predetermined resilience characteristic is coupled at a first end thereof to the first inner surface (124) and at a second end thereof to the second inner surface (134). A frame coupler (151) couples the first resiliently variable frame element (120) to a support element (150). An actuator (106) applies a force to the second resiliently variable frame element (130) with respect to the support element (150), resulting in a corresponding variation in the contour of the first and second compliant surfaces.
    • 第一和第二柔性表面的轮廓的变化由具有第一可弹性变化的框架元件(120)的柔性框架产生,所述第一可弹性变化的框架元件(120)具有对应的第一外表面(122)和第一内表面(124),以及第二弹性变量框架 元件(130)具有对应的第二外表面(132)和第二内表面(134)。 第一和第二外表面(122,132)与第一和第二顺应表面中的相应表面连通。 具有预定弹性特征的联动元件(141-144)在其第一端连接到第一内表面(124),并在其第二端连接到第二内表面(134)。 框架联接器(151)将第一弹性可变框架元件(120)联接到支撑元件(150)。 致动器(106)相对于支撑元件(150)向第二弹性可变框架元件(130)施加力,导致第一和第二顺应表面的轮廓的相应变化。
    • 5. 发明申请
    • SURFACE WIPER ARRANGEMENT
    • 表面刮水器布置
    • WO2013090626A1
    • 2013-06-20
    • PCT/US2012/069577
    • 2012-12-13
    • FLEXSYS, INC.
    • KOTA, SridharERVIN, Gregory, F.
    • B60S1/42
    • B60S1/42B60S1/3427B60S1/344B60S1/3459B60S1/3479B60S1/3801
    • A wiper has a wiper arm having first and second ends. A leaf spring urges the wiper arm and a compliant force distribution arrangement toward the surface, and a mounting arrangement couples the first end of the wiper arm and the leaf spring element to a source of motion. The wiper arm has a first end coupling the first end of the wiper arm member to a source of motion, and a compliant force distributor is coupled to the second end, having plural resilient beam members integrally formed with each other and adapted to engage a wiper blade. A wiper mount has a mounting element having a mounting portion coupled to a source of motion and a drive portion for engaging the wiper arm. The leaf spring element also has a mounting portion coupled to the source of motion, and has a drive portion for engaging the wiper arm.
    • 刮水器具有具有第一和第二端的刮水器臂。 板簧促使刮水器臂和朝向表面的柔顺力分配装置,并且安装装置将雨刷臂的第一端和板簧元件连接到运动源。 刮水器臂具有将雨刷臂构件的第一端连接到运动源的第一端,并且柔顺力分配器联接到第二端,其具有彼此一体地形成且适于接合雨刷的多个弹性梁构件 刀。 刮水器安装件具有安装元件,其具有联接到运动源的安装部分和用于接合雨刷臂的驱动部分。 板簧元件还具有联接到运动源的安装部分,并且具有用于接合雨刷臂的驱动部分。
    • 9. 发明申请
    • EDGE MORPHING ARRANGEMENT FOR AN AIRFOIL
    • 飞机的边缘变形安排
    • WO2017151580A1
    • 2017-09-08
    • PCT/US2017/019886
    • 2017-02-28
    • FLEXSYS, INC.
    • KOTA, SridharERVIN, Gregory F.LO, Jia-HsuanLU, Kerr-JiaMARIC, DraganTROST, Mark R.TSANG, Ruey-Khan K.
    • B64C3/48
    • An edge-morphing arrangement for an airfoil includes a compliant upper surface and a compliant lower surface that are joined together. An actuator is coupled to a driven surface and actuated to move the driven surface and change the shape thereof, with the non-driven surface changing its shape in response to actuation of the driven surface. The upper and lower surfaces can be part of a sub-flap mounted to a traditional flap of the fixed wing of an airplane. The upper and lower surfaces can be mounted to existing structure in the flap, or the flap components can be mounted to the sub-flap. The upper and lower surfaces can alternatively replace the traditional flap in the fixed wing of an aircraft. The upper and lower surfaces are continuous and can be deflected upward, downward, or twisted in a span-wise direction relative to the flap or wing.
    • 用于翼型的边缘变形布置包括连接在一起的柔性上表面和柔性下表面。 致动器联接到从动表面并被致动以移动从动表面并改变其形状,其中非从动表面响应于从动表面的致动而改变其形状。 上表面和下表面可以是安装在飞机固定翼的传统襟翼上的副翼的一部分。 上表面和下表面可以安装到襟翼中的现有结构上,或者襟翼部件可以安装到襟翼上。 上下表面可以替代飞机固定翼上的传统襟翼。 上表面和下表面是连续的,并且可以向上,向下偏转,或者相对于翼片或翼部沿翼展方向扭曲。