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公开(公告)号：US12162592B2
公开(公告)日：2024-12-10
申请号：US17609348
申请日：2019-09-17
Applicant: AERONEXT INC.
Inventor： Yoichi Suzuki
IPC: B64C3/48 , B64C3/38 , B64C9/08 , B64C27/28 , B64C29/00 , B64C39/08 , B64U10/25 , B64U30/10 , B64U50/13
Abstract: An aircraft that enables an efficient and safe transition from hovering to level-flight. The aircraft according to the present invention includes a lift generating part, a thrust generating part capable of flying and hovering, a connecting part that displaceably connects the lift generating part and the thrust generating part so that the lift generating part can maintain a positive angle of attack with respect to the flying direction at least at the time of ascending. The lift generating part is a wing part having a main surface, and at least at the time of hovering, a propulsion direction by the thrust generating part is along a direction obliquely intersecting the vertical direction. At least at the time of hovering, the propulsion direction and the main surface form an obtuse angle. At least at the time of hovering, the propulsion direction is along the vertical direction.
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公开(公告)号：US12084209B2
公开(公告)日：2024-09-10
申请号：US16754635
申请日：2017-10-10
Applicant: AERONEXT INC.
Inventor： Yoichi Suzuki
Abstract: To provide a rotorcraft capable of improving flight efficiency. The rotorcraft according to the present invention is capable of moving forward along at least a first direction and comprises an arm part, a plurality of motors mounted on the arm part, and a rotary blade mounted on each of the motors. The rotorcraft is configured to have one or more motors one or more front motors located at a front side and one or more rear motors located at a rear side, wherein the output characteristics of a motor included in the front motor and the output characteristics of a motor included in the rear motor are different.
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公开(公告)号：US12017796B2
公开(公告)日：2024-06-25
申请号：US17282298
申请日：2018-10-01
Applicant: AERONEXT INC.
Inventor： Yoichi Suzuki
Abstract: An easy extention of a telescopic rod. The telescopic rod extends in the axial direction by a gas forcibly fed to the inside and is provided with a posture control means.
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4.发明授权公开(公告)号：US11774832B2
公开(公告)日：2023-10-03
申请号：US17935829
申请日：2022-09-27
Applicant: AERONEXT INC.
Inventor： Yoichi Suzuki
CPC classification number: G03B17/561 , B64B1/44 , B64B1/54 , B64C27/00 , B64D47/08 , B64F3/00 , G03B15/006
Abstract: A high-place observation device for stably performing a fixed-point observation of a target object from a high place is provided. The high-place observation device provides [Solution] Provides a long pole which is formed to extend and contract freely and which stands on the installation surface, a rotorcraft for positioning the pole to a desirable height position by extending and contracting the pole by a floating force in a connected state, a winding mechanism which fixes and maintains the height position of the pole to the height position set by the rotorcraft, and a camera attached to the rotorcraft.
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公开(公告)号：US11565810B2
公开(公告)日：2023-01-31
申请号：US16754230
申请日：2017-10-10
Applicant: AERONEXT INC.
Inventor： Yoichi Suzuki
Abstract: [Problem] To provide a flying body having a new structure capable of improving flight efficiency. [Solution] The problem is addressed by a flying body capable of traveling along at least a first direction and comprising an airframe part and an auxiliary part wherein the airframe part has a body part and a lift generating part, the body part having a right part and a left part extending along the first direction and a connecting part whereby the ends of the right part and the left part in a second direction opposing to the first direction are connected. The flying body is thus configured so as to create a surrounded space surrounded by the left part, the right part, and the connecting part when seen from a third direction perpendicular to the first direction.
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Patent Agency Ranking
公开(公告)号：US12208920B2
公开(公告)日：2025-01-28
申请号：US18253372
申请日：2020-12-16
Applicant: AERONEXT INC.
Inventor： Yoichi Suzuki
Abstract: A landing facility that enables flight vehicles to land safely even in strong winds. The landing system of the invention includes a first area for landing a flight vehicle, a windbreak part having a predetermined height and cover part at least a portion of the perimeter of the first area, and a second area located away from the windbreak part, where the flight vehicle descends to a predetermined flight altitude. The flight altitude is lower than the predetermined height of the windbreak part. The second area is an area selected from a plurality of permitted areas where vertical descent is permitted. A portion of the windbreak part comprises a net.
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公开(公告)号：US11820506B2
公开(公告)日：2023-11-21
申请号：US17501720
申请日：2021-10-14
Applicant: AERONEXT INC.
Inventor： Yoichi Suzuki
CPC classification number: B64C39/024 , B64C17/04 , B64C27/08 , B64U10/13 , B64U50/19 , B64U2101/60
Abstract: An aerial vehicle has a loading section whereon a payload and the like can be loaded. The aerial vehicle is capable of traveling at least forward and backward, is provided with lift generation sections, arm sections for holding the lift generation sections, a loading section disposed on the arm sections and positioned posterior to the center of gravity of the aerial vehicle, and a maintaining means for maintaining the aerial vehicle at least in the horizontal attitude, and the loading section has a first connection part for maintaining a loaded object at least in the horizontal attitude. On the basis of the above mentioned, the payload can be prevented from entering slipstream regions created by propellers, improving flight efficiency.
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公开(公告)号：US11524768B2
公开(公告)日：2022-12-13
申请号：US16634074
申请日：2017-07-27
Applicant: AERONEXT INC.
Inventor： Yoichi Suzuki
Abstract: [Object] To provide a rotary wing aircraft capable of self-leveling and ensuring a stable landing state. [Solution] The rotary wing aircraft according to the present disclosure comprises a plurality of rotary blades, an arm part for supporting the plurality of rotary blades, a mounting part for mounting an object, and a connecting part for connecting the mounting part to the arm part in a state where the mounting part is movable within a predetermined range. The position of the connecting part of the rotary wing aircraft of the present disclosure is above the center of gravity of the arm part. Thereby, self-leveling is made possible and a stable landing state can be ensured.
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公开(公告)号：US11148806B2
公开(公告)日：2021-10-19
申请号：US16619066
申请日：2017-06-04
Applicant: AERONEXT INC.
Inventor： Yoichi Suzuki
Abstract: [Problem] To provide an aerial vehicle wherein the flight efficiency can be improved. [Solution] An aerial vehicle according to the present invention relates in particular to a aerial vehicle having a loading section whereon a payload and the like can be loaded. The aerial vehicle is capable of traveling at least forward and backward, is provided with lift generation sections, arm sections for holding the lift generation sections, a loading section disposed on the arm sections and positioned posterior to the center of gravity of the aerial vehicle, and a maintaining means for maintaining the aerial vehicle at least in the horizontal attitude, and the loading section has a first connection part for maintaining a loaded object at least in the horizontal attitude. On the basis of the above mentioned, the payload can be prevented from entering slipstream regions created by propellers, improving flight efficiency.
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公开(公告)号：US20210149279A1
公开(公告)日：2021-05-20
申请号：US16630426
申请日：2017-07-12
Applicant: AERONEXT INC.
Inventor： Yoichi Suzuki
Abstract: [Object] To provide a high-place observation device for stably performing a fixed-point observation of a target object from a high place. [Solution] Provides a long pole 30 which is formed to extend and contract freely and which stands on the installation surface E, a rotorcraft 40 for positioning the pole 30 to a desirable height position by extending and contracting the pole 30 by a floating force in a connected state, a winding mechanism 22 which fixes and maintains the height position of the pole 30 to the height position set by the rotorcraft 40, and a camera 50 attached to the rotorcraft 40.
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