SELECTIVELY THRUSTING PROPULSION UNITS FOR AERIAL VEHICLES

    公开(公告)号:US20190135412A1

    公开(公告)日:2019-05-09

    申请号:US16236247

    申请日:2018-12-28

    Abstract: Aerial vehicles may include propulsion units having motors with drive shafts that may be aligned at a variety of orientations, propellers with variable pitch blades, and common operators for aligning the drive shafts at one or more orientations and for varying the pitch angles of the blades. The common operators may include plate elements to which a propeller hub is rotatably joined, and which may be supported by one or more linear actuators that may extend or retract to vary both the orientations of the drive shafts and the pitch angles of the blades. Operating the motors and propellers at varying speeds, gimbal angles or pitch angles enables the motors to generate forces in any number of directions and at any magnitudes. Attributes of the propulsion units may be selected in order to shape or control the noise generated thereby.

    Unmanned aerial vehicle with center mounted fuselage and closed wing

    公开(公告)号:US09815552B1

    公开(公告)日:2017-11-14

    申请号:US14860377

    申请日:2015-09-21

    Inventor: Ricky Dean Welsh

    CPC classification number: B64C27/20 B64C27/10 B64C27/26 B64C39/12

    Abstract: This disclosure describes a configuration of an unmanned aerial vehicle (“UAV”) in which the fuselage of the UAV is center mounted and at least some of the motors are configured to encompass at least a portion of the fuselage. In such a configuration, the stator and rotor of the motor extend around a perimeter of the fuselage, the propellers are coupled to an outer perimeter of the rotor, and the propellers extend radially outward away from the fuselage. Likewise, a closed wing may be coupled to the fuselage and positioned to encompass the radially extending propellers and at least a portion of the fuselage.

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