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公开(公告)号：US20230234728A1
公开(公告)日：2023-07-27
申请号：US18003612
申请日：2020-11-25
申请人： Sang Hyun LEE
发明人： Sang Hyun LEE
摘要： Provided is a drone according to the present invention. The drone may include a fuselage in which a battery is mounted and a forward direction is set in an x-axis; a plurality of rotors disposed about the fuselage in four or more, each rotational axis of which is aligned in a z-axis direction; an x-axis tilting mechanism unit formed to tilt the plurality of rotors about an axis parallel to the x-axis; a y-axis tilting mechanism unit formed to tilt the plurality of rotors about an axis parallel to the y-axis; a first drive motor unit driving the y-axis tilting mechanism unit; a second drive motor unit driving the x-axis tilting mechanism unit; a control unit configured to implement a plurality of flight modes by controlling the first rotor, the second rotor, the third rotor, the fourth rotor, the first drive motor unit, and the second drive motor unit, and a wing part installed on an upper portion of the fuselage and formed in a form of an air foil to provide lift.
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公开(公告)号：US20240278943A1
公开(公告)日：2024-08-22
申请号：US18573267
申请日：2021-06-22
申请人： AERONEXT INC.
发明人： Yoichi SUZUKI
摘要： According to this invention, an aerial vehicle can be provided that reduces the effect of wind in a given direction striking its frame during flight of the aerial vehicle, thereby improving fuel consumption and stability. The aerial vehicle of this invention is equipped with a flight part including a frame to which a plurality of rotor blades including at least a propeller and a motor are connected, wherein the frame includes a right frame and a left frame extending side by side in the front-rear direction of the aerial vehicle, and at least one of the right frame and the left frame has a substantially wing-shaped portion with a leading edge located outside the aerial vehicle and a trailing edge located inside the aerial vehicle relative to a vertical center line in the frame. The substantially wing-shaped shape is a symmetrical wing shape.
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公开(公告)号：US20230227185A1
公开(公告)日：2023-07-20
申请号：US17780916
申请日：2020-12-09
申请人： GRIFF AVIATION AS
摘要： An aerial vehicle comprising: at least three support arms for interconnecting at least three motors; at least one battery module; at least one of the support arms is configured to support the at least one battery module such that the battery module forms a structural element of the support arm.
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公开(公告)号：US11964782B2
公开(公告)日：2024-04-23
申请号：US17861734
申请日：2022-07-11
申请人： WING Aviation LLC
发明人： André Prager
摘要： An unmanned aerial vehicle (UAV) includes a fuselage, a pair of wings attached to the fuselage, and a propulsion system mounted to the wings to provide propulsion to the UAV. The fuselage has an outer fuselage shell that is a first mechanical support structure for an airframe of the UAV. The pair of wings is attached to the fuselage and shaped to provide aerodynamic lift. The wings have outer wing shells that are second mechanical support structures for the airframe. The outer fuselage shell or the outer wing shells comprise one or more formed-metal sheets.
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公开(公告)号：US11932427B1
公开(公告)日：2024-03-19
申请号：US17753444
申请日：2021-08-16
申请人： ACSL Ltd. , NJS Co., Ltd.
发明人： Soki Kuga , Yusuke Inagaki , Patrik Ken Takeuchi
摘要： Provided is an unmanned aircraft which is capable of stably taking off. In one example, the unmanned aircraft has an aircraft body which includes an information acquisition device, a plurality of rotary wings, and a protective member disposed around the rotary wings. Each of the rotary wings has a rotation axis which is tilted with respect to a vertical direction by a given angle, such that the rotary wings generate a forward thrust force. The aircraft body has a lower edge which includes a middle lower edge and a forward lower edge, wherein the protective member has a lower edge including the forward lower edge. The forward lower edge is located above the middle lower edge, and the forward lower edge has a rear end located backward of a rear end of the rotary wing.
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公开(公告)号：US20240169718A1
公开(公告)日：2024-05-23
申请号：US18057661
申请日：2022-11-21
申请人： Wing Aviation LLC
发明人： Kyle Krafka , Trevor Shannon
摘要： Systems, apparatus, and methods are presented for testing a device. One method includes activating an actuator device to cause a carriage, coupled to a device, to be moved in one or more directions along a guide rail, wherein the device includes at least one processing device and one or more sensor devices. The method may also comprise receiving, by the device, one or more input commands and executing, by the device based on the one or more input commands, a software application to generate an output while the device is moving in the one or more directions. Further, the method may comprise verifying the execution of the software application on the device based on the output.
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公开(公告)号：US20240076068A1
公开(公告)日：2024-03-07
申请号：US17753444
申请日：2021-08-16
申请人： ACSL Ltd. , NJS Co., Ltd.
发明人： Soki Kuga , Yusuke Inagaki , Patrik Ken Takeuchi
摘要： Provided is an unmanned aircraft which is capable of stably taking off. In one example, the unmanned aircraft has an aircraft body which includes an information acquisition device, a plurality of rotary wings, and a protective member disposed around the rotary wings. Each of the rotary wings has a rotation axis which is tilted with respect to a vertical direction by a given angle, such that the rotary wings generate a forward thrust force. The aircraft body has a lower edge which includes a middle lower edge and a forward lower edge, wherein the protective member has a lower edge including the forward lower edge. The forward lower edge is located above the middle lower edge, and the forward lower edge has a rear end located backward of a rear end of the rotary wing.
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公开(公告)号：US20240010367A1
公开(公告)日：2024-01-11
申请号：US17861734
申请日：2022-07-11
申请人： WING Aviation LLC
发明人： André Prager
IPC分类号： B64C15/00
摘要： An unmanned aerial vehicle (UAV) includes a fuselage, a pair of wings attached to the fuselage, and a propulsion system mounted to the wings to provide propulsion to the UAV. The fuselage has an outer fuselage shell that is a first mechanical support structure for an airframe of the UAV. The pair of wings is attached to the fuselage and shaped to provide aerodynamic lift. The wings have outer wing shells that are second mechanical support structures for the airframe. The outer fuselage shell or the outer wing shells comprise one or more formed-metal sheets.
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