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    • 1. 发明授权
    • Flying-wing aircraft
    • 飞翼飞机
    • US08602348B2
    • 2013-12-10
    • US12865429
    • 2009-02-02
    • Ashley Christopher Bryant
    • Ashley Christopher Bryant
    • B64C15/12B64C29/00B64C39/10
    • B64C29/0033B64C39/024B64C39/10B64C2201/028B64C2201/088B64C2201/162B64C2201/165
    • A vertical take-off and landing flying-wing aircraft has a pair of thrust-vectoring propulsion units mounted fore and aft of the aircraft pitch axis on strakes at opposite extremities of the wing-structure, with the fore unit below, and the aft unit above, the wing-structure. The propulsion units are pivoted to the strakes, either directly or via arms, for individual angular displacement for thrust-vectored maneuvering of the aircraft in yaw, pitch and roll and for hover and forward and backward flight. When arms are employed, the arms of fore and aft propulsion units are intercoupled via chain drives or linkages. The wing-structure may have fins, slats and flaps and other aerodynamic control-surfaces, and enlarged strakes may incorporate rudder surfaces. Only one propulsion unit may be mounted at each extremity and additional fan units may be used.
    • 垂直起飞和着陆的飞翼飞机具有一对推力矢量推进装置,其在机翼结构的相对两端的前翼和后部单元的前后悬架的飞机俯仰轴上前后安装 以上,翼结构。 推进单元直接或经由臂枢转到斜面,用于单独的角位移,用于以偏航,俯仰和滚动以及用于悬停和向前和向后飞行的推力向导操纵飞行器。 当使用武器时,前后推进单元的臂通过链条驱动器或连杆相互联接。 机翼结构可以具有翅片,板条和翼片以及其它空气动力学控制表面,并且扩大的履带可以包括舵面。 每个末端只能安装一个推进装置,也可以使用额外的风扇装置。
    • 2. 发明申请
    • FLYING-WING AIRCRAFT
    • 飞行飞机
    • US20110001001A1
    • 2011-01-06
    • US12865429
    • 2009-02-02
    • Ashley Christopher Bryant
    • Ashley Christopher Bryant
    • B64C29/00B64C39/10
    • B64C29/0033B64C39/024B64C39/10B64C2201/028B64C2201/088B64C2201/162B64C2201/165
    • A vertical take-off and landing (VTOL) flying-wing aircraft has a pair of thrust-vectoring propulsion units (2, 3; 4, 5) mounted fore and aft of the aircraft pitch axis (PA) on strakes (6, 7) at opposite extremities of the wing-structure (1), with the fore unit (2; 4) below, and the aft unit (3; 5) above, the wing-structure (1). The propulsion units (2-5) are pivoted to the strakes (6, 7), either directly or via arms (56), for individual angular displacement for thrust-vectored maneuvering of the aircraft in yaw, pitch and roll and for hover and forward and backward flight. When arms (56) are employed, the arms (56) of fore and aft propulsion units (52,54; 53,55) are intercoupled via chain drives (57-60) or linkages (61). The wing-structure (1; 51 ; 78) may have fins (47;84), slats (81) and flaps (82) and other aerodynamic control-surfaces, and enlarged strakes (84) may incorporate rudder surfaces (80). Only one propulsion unit (21) may be mounted at each extremity and additional fan units (48,83) may be used.
    • 垂直起降(VTOL)飞翼飞机具有一对推进矢量推进单元(2,3; 4,5),其安装在飞行器俯仰轴线(PA)的前后,位于横梁(6,7) )在机翼结构(1)的相对两端,前部单元(2; 4)和下方的后部单元(3; 5),机翼结构(1)。 推进单元(2-5)直接地或经由臂(56)枢转到斜面(6,7),用于单独的角位移,用于偏航,俯仰和滚动中的推进向导操纵的飞行器,并且用于悬停和 向前和向后飞行 当使用臂(56)时,前后推进单元(52,54; 53,55)的臂(56)通过链条驱动器(57-60)或连杆(61)相互配合。 机翼结构(1; 51; 78)可以具有翅片(47; 84),板条(81)和翼片(82)和其它空气动力学控制表面,并且扩大的横条(84)可以包括舵表面(80)。 每个末端只安装一个推进单元(21),并且可以使用附加的风扇单元(48,83)。