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    Unmanned aerial vehicle and control method of unmanned aerial vehicle
    3.
    发明授权
    Unmanned aerial vehicle and control method of unmanned aerial vehicle 有权

    公开(公告)号：US10817000B2

    公开(公告)日：2020-10-27

    申请号：US15653915

    申请日：2017-07-19

    Applicant: FUJITSU LIMITED

    Inventor： Moyuru Yamada ,  Yoshiro Hada

    IPC: G05D1/10 ,  B64C37/00 ,  B64C39/02 ,  G05D1/00 ,  B64C27/08

    Abstract: A flying device configured to communicate with a controller device operated by a user, the flying device includes: a memory; and a processor coupled to the memory and configured to: determine whether the flying device is in contact with an object based on a signal from a contact detector; and move the flying device in a direction corresponding to an operation command transmitted from the controller device while causing a thrust force to be produced so that a contact between the object and the flying device is maintained when it is determined that the flying device is in contact with the object.

    Flying machine and control method of flying machine
    5.
    发明授权
    Flying machine and control method of flying machine 有权

    公开(公告)号：US11142314B2

    公开(公告)日：2021-10-12

    申请号：US16364357

    申请日：2019-03-26

    Applicant: FUJITSU LIMITED

    Inventor： Yoshiro Hada

    IPC: B64C39/02 ,  B64C27/08

    Abstract: A flying machine includes a plurality of rotary blades arranged in the front and rear and on the left and right, a plurality of motors configured to respectively rotate the plurality of rotary blades, contact portions located in front of the plurality of rotary blades and configured to contact a wall surface, vertical blades arranged below the plurality of rotary blades and configured so as to be capable of inclining toward a rear side or toward a front side, and so as to be capable of sliding within a range in a direction toward the front side or the rear side in a rotation area of the plurality of rotary blades and driving units configured to incline the vertical blades toward the rear side or front side, and to slide the vertical blade in a direction toward the front side or rear side.

    FLYING MACHINE AND CONTROL METHOD OF FLYING MACHINE
    7.
    发明申请
    FLYING MACHINE AND CONTROL METHOD OF FLYING MACHINE 审中-公开

    公开(公告)号：US20190329884A1

    公开(公告)日：2019-10-31

    申请号：US16364357

    申请日：2019-03-26

    Applicant: FUJITSU LIMITED

    Inventor： Yoshiro Hada

    IPC: B64C39/02

    Abstract: A flying machine includes a plurality of rotary blades arranged in the front and rear and on the left and right, a plurality of motors configured to respectively rotate the plurality of rotary blades, contact portions located in front of the plurality of rotary blades and configured to contact a wall surface, vertical blades arranged below the plurality of rotary blades and configured so as to be capable of inclining toward a rear side or toward a front side, and so as to be capable of sliding within a range in a direction toward the front side or the rear side in a rotation area of the plurality of rotary blades and driving units configured to incline the vertical blades toward the rear side or front side, and to slide the vertical blade in a direction toward the front side or rear side.

    AIRCRAFT AND METHOD OF CONTROLLING THE SAME
    9.
    发明申请
    AIRCRAFT AND METHOD OF CONTROLLING THE SAME 审中-公开

    公开(公告)号：US20200023967A1

    公开(公告)日：2020-01-23

    申请号：US16376742

    申请日：2019-04-05

    Applicant: FUJITSU LIMITED

    Inventor： Yoshiro Hada

    IPC: B64C39/02 ,  B64D35/02 ,  B64D47/08 ,  B64C25/36

    Abstract: An aircraft includes: an aircraft body including rotating wings and motors that rotates the rotating wings; wheels arranged on both sides of the aircraft body and rotatably supported around an axis that extends in a left and right direction of the aircraft body; rollers that protrude forward and upward with respect to each of the wheels when the aircraft body is in a horizontal state, and are rotatably supported around an axis that extends in a tangential direction of each of the wheels; and a controller that controls a rotation speed of the motors such that, when the aircraft body is moved in the left and right direction along a vertical wall surface, the aircraft body is inclined forward to bring the rollers into contact with the vertical wall surface, and the aircraft body is inclined to a side where the aircraft body moves in the left and right direction.

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