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    HOVERING VEHICLE
    4.
    发明公开
    HOVERING VEHICLE 审中-公开

    公开(公告)号：EP3659915A1

    公开(公告)日：2020-06-03

    申请号：EP18837976.2

    申请日：2018-03-09

    申请人： Tatsumi Ryoki Co., Ltd

    发明人： KONDO Toyoshi

    IPC分类号： B64C29/00 ,  B60F5/02 ,  B64C3/56 ,  B64C37/00

    摘要： Provided is a floating type moving apparatus capable of safely moving while floating from the ground. A floating type moving apparatus 1 includes: six or more impellers 37 provided below an operator cab 10, for blasting, downward in a z direction, air taken in from the air intake space between the impellers and the operator cab 10; six or more motors for driving the six or more impellers 37; and an electricity storage unit for supplying power to the six or more motors. The floating type moving apparatus 1 is allowed to float from the ground by the air blasted from some or all of the six or more impellers 37, and the six or more impellers are arranged on the circumference of a circle with the center passing through an axis parallel to the z direction.

    AN AIR VEHICLE AND IMAGING APPARATUS THEREFOR
    9.
    发明公开
    AN AIR VEHICLE AND IMAGING APPARATUS THEREFOR 审中-公开

    公开(公告)号：EP3368412A1

    公开(公告)日：2018-09-05

    申请号：EP16788766.0

    申请日：2016-10-28

    申请人： BAE Systems PLC

    发明人： WRIGHT, Julian, David ,  COLOSIMO, Nicholas, Giacomo, Robert ,  WARSOP, Clyde

    IPC分类号： B64C29/02 ,  B64C37/00 ,  B64C39/02 ,  H04N5/232 ,  H04N7/18

    摘要： An air vehicle (10) comprising a main body (12) and a pair of opposing wing members (14a, 14b) extending substantially laterally from the main body (12) having a principal axis orthogonal to the longitudinal axis (20) of said wing members, at least a first propulsion device (16a) associated with a first of said wing members arranged and configured to generate a linear thrust relative to the main body in a first direction, and a second propulsion device (16b) associated with a second of said wing members arranged and configured to generate linear thrust relative to said main body in a second, substantially opposite, direction such that said wing members and said main body are caused to rotate about said principal axis, in use, the air vehicle further comprising an imaging system (100) configured to cover a substantially 360° imaging area about said principal axis and comprising at least one electro-optic sensor (102) mounted on a support member (104) and having a field of view (102a) covering a portion of said imaging area, said support member being mounted on said air vehicle, said imaging system (100) further comprising a control module (400) configured to define an object or region of interest in relation to said air vehicle, determine a nominal sensor field of view incorporating said object or region of interest, and obtain sequential image data from a sensor having a field of view matching said nominal field of view as said air vehicle completes a rotary cycle.

    AVION CONVERTIBLE A ROTORS DÉCOUVRABLES
    10.
    发明公开
    AVION CONVERTIBLE A ROTORS DÉCOUVRABLES 审中-公开

    公开(公告)号：EP3294624A1

    公开(公告)日：2018-03-21

    申请号：EP16724685

    申请日：2016-05-04

    申请人： DESLYPPER CHRISTIAN ROGER RENE

    发明人： DESLYPPER CHRISTIAN ROGER RENE

    IPC分类号： B64C29/00 ,  B64C3/54 ,  B64C37/00

    CPC分类号： B64C29/0025 ,  B64C3/54 ,  B64C39/12

    摘要： Convertible airplane capable of flying with the speed and economy of use of an airplane and of taking off/landing vertically and of flying/hovering like a helicopter. The craft that forms the subject of the invention takes the appearance of a conventional airplane, having a fuselage (1), a wing (2), a stabilizer (3) and a rudder (4), as well as one or more jet or turboprop engines (5) for propulsion, and comprises exposable rotors (6 and 7) installed in the wing and possibly in the stabilizer or in the fuselage and providing lift for vertical take off and landing and hovering flight. For horizontal flight and horizontal take off/landing, the rotors are completely encased inside the wing and possibly the stabilizer or the fuselage.