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1. 发明专利

JP2020524106A 垂直離着陸機体审中-公开
公开(公告)号：JP2020524106A
公开(公告)日：2020-08-13
申请号：JP2019559092
申请日：2018-03-16
申请人：プテロダイナミクス・インコーポレイテッド , PTERODYNAMICS INC.
发明人：ペトロフ,ヴァル
IPC分类号： B64D27/24 , B64D27/06 , B64D27/12 , B64C3/56 , B64C27/28
摘要：本願明細書には、前方飛行と垂直離着陸との間の安定した飛行中移行のために構成された機体が記載されている。一つの実施形態において、航空機は、胴体と、該胴体の両側から延びている対向する翼と、複数のエンジンとを含むことができる。少なくとも一つのエンジンを、該対向する翼の各々に取付けることができ、また、該複数のエンジンのうちの少なくとも一つを含む各対向する翼の少なくとも一部は、該胴体の長手方向軸に対して垂直ではなく、横断している回転軸周りで、該胴体に対して回転することができる。該複数のエンジンのうちの少なくとも一つを含む該翼の一部を、記載した方法で回転させることは、垂直飛行と前方飛行との間の安定した円滑な移行を実行することができる。

2. 发明专利

IL298177A Control of aircraft with vertical take-off and landing capabilities 未知
公开(公告)号：IL298177A
公开(公告)日：2023-01-01
申请号：IL29817722
申请日：2022-11-13
申请人： PTERODYNAMICS INC
IPC分类号： B64C29/00
摘要： Provided are computer-implemented methods for autonomously controlling an aircraft with vertical take-off and landing capabilities and folding wings that includes controlling a plurality of thrust producing components of an aircraft to cause the aircraft to rise vertically when wings of the aircraft are in a first folded configuration, where when the wings of the aircraft are in the first folded configuration, a leading edge of each wing is oriented in a vertical direction setting motor controller gains based on the wings of the aircraft being in the first folded configuration, and causing the aircraft to align with a direction of airflow when the wings of the aircraft are in the first folded configuration, and controlling thrust producing components and control surfaces and internal articulation mechanisms of the aircraft to cause the aircraft to transition from folded wing configuration to unfolded wing configuration. Systems and computer program products are also provided.

3. 发明申请

US20190225333A1 Vertical Takeoff and Landing Airframe 审中-公开
公开(公告)号：US20190225333A1
公开(公告)日：2019-07-25
申请号：US16373003
申请日：2019-04-02
申请人： PteroDynamics, Inc.
发明人： Val Petrov
IPC分类号： B64C29/00 , B64C3/42 , B64D27/24 , B64C3/38 , B64D27/12 , B64C25/54 , B64C25/34
CPC分类号： B64C29/0033 , B64C3/38 , B64C3/42 , B64C3/56 , B64C25/34 , B64C25/54 , B64C27/26 , B64C27/28 , B64C37/00 , B64D27/12 , B64D27/24
摘要： Airframes configured for stable in-flight transition between forward flight and vertical takeoff and landing are described herein. In one embodiment, an aircraft can include a fuselage, opposed wings extending from opposed sides of the fuselage, and a plurality of engines. At least one engine can be mounted to each of the opposed wings and at least a portion of each opposed wing including at least one of the plurality of engines can rotate relative to the fuselage around a rotation axis that is non-perpendicular and transverse to a longitudinal axis of the fuselage. Rotating portions of the wings including at least one of the plurality of engines in the described manner can provide a stable and smooth transition between vertical and forward flight.

4. 发明授权

US10967969B2 Vertical takeoff and landing airframe 有权
公开(公告)号：US10967969B2
公开(公告)日：2021-04-06
申请号：US16725042
申请日：2019-12-23
申请人： PteroDynamics, Inc.
发明人： Val Petrov
IPC分类号： B64C29/00 , B64C3/38 , B64C27/26 , B64C3/42 , B64C27/28 , B64C25/54 , B64D27/12 , B64C25/34 , B64C37/00 , B64D27/24 , B64C3/56
摘要： Airframes configured for stable in-flight transition between forward flight and vertical takeoff and landing are described herein. In one embodiment, an aircraft can include a fuselage, opposed wings extending from opposed sides of the fuselage, and a plurality of engines. At least one engine can be mounted to each of the opposed wings and at least a portion of each opposed wing including at least one of the plurality of engines can rotate relative to the fuselage around a rotation axis that is non-perpendicular and transverse to a longitudinal axis of the fuselage. Rotating portions of the wings including at least one of the plurality of engines in the described manner can provide a stable and smooth transition between vertical and forward flight.

5. 发明授权

US10556679B2 Vertical takeoff and landing airframe 有权
公开(公告)号：US10556679B2
公开(公告)日：2020-02-11
申请号：US16373003
申请日：2019-04-02
申请人： PteroDynamics, Inc.
发明人： Val Petrov
IPC分类号： B64C3/38 , B64C3/42 , B64C29/00 , B64C25/54 , B64D27/12 , B64C25/34 , B64D27/24 , B64C3/56 , B64C27/28 , B64C37/00 , B64C27/26
摘要： Airframes configured for stable in-flight transition between forward flight and vertical takeoff and landing are described herein. In one embodiment, an aircraft can include a fuselage, opposed wings extending from opposed sides of the fuselage, and a plurality of engines. At least one engine can be mounted to each of the opposed wings and at least a portion of each opposed wing including at least one of the plurality of engines can rotate relative to the fuselage around a rotation axis that is non-perpendicular and transverse to a longitudinal axis of the fuselage. Rotating portions of the wings including at least one of the plurality of engines in the described manner can provide a stable and smooth transition between vertical and forward flight.

6. 发明申请

US20200277051A1 Vertical Takeoff and Landing Airframe 审中-公开
公开(公告)号：US20200277051A1
公开(公告)日：2020-09-03
申请号：US16725042
申请日：2019-12-23
申请人： PteroDynamics, Inc.
发明人： Val Petrov
IPC分类号： B64C29/00 , B64C3/38 , B64C25/54 , B64D27/12 , B64C25/34 , B64D27/24 , B64C3/42 , B64C3/56 , B64C27/28 , B64C37/00 , B64C27/26
摘要： Airframes configured for stable in-flight transition between forward flight and vertical takeoff and landing are described herein. In one embodiment, an aircraft can include a fuselage, opposed wings extending from opposed sides of the fuselage, and a plurality of engines. At least one engine can be mounted to each of the opposed wings and at least a portion of each opposed wing including at least one of the plurality of engines can rotate relative to the fuselage around a rotation axis that is non-perpendicular and transverse to a longitudinal axis of the fuselage. Rotating portions of the wings including at least one of the plurality of engines in the described manner can provide a stable and smooth transition between vertical and forward flight.

7. 发明申请

WO2021242535A2 CONTROL OF AIRCRAFT WITH VERTICAL TAKE-OFF AND LANDING CAPABILITIES 审中-公开
公开(公告)号：WO2021242535A2
公开(公告)日：2021-12-02
申请号：PCT/US2021/032258
申请日：2021-05-13
申请人： PTERODYNAMICS INC.
发明人： PETROV, Val
IPC分类号： B64C29/00 , B64C29/02 , B64C27/26 , B64C3/56 , B64C27/28 , B64C29/0033 , G05D1/102
摘要： Provided are computer-implemented methods for autonomously controlling an aircraft with vertical take-off and landing capabilities and folding wings that includes controlling a plurality of thrust producing components of an aircraft to cause the aircraft to rise vertically when wings of the aircraft are in a first folded configuration, where when the wings of the aircraft are in the first folded configuration, a leading edge of each wing is oriented in a vertical direction setting motor controller gains based on the wings of the aircraft being in the first folded configuration, and causing the aircraft to align with a direction of airflow when the wings of the aircraft are in the first folded configuration, and controlling thrust producing components and control surfaces and internal articulation mechanisms of the aircraft to cause the aircraft to transition from folded wing configuration to unfolded wing configuration. Systems and computer program products are also provided.

8. 发明公开

EP4149835A2 CONTROL OF AIRCRAFT WITH VERTICAL TAKE-OFF AND LANDING CAPABILITIES 审中-公开
公开(公告)号：EP4149835A2
公开(公告)日：2023-03-22
申请号：EP21814018.4
申请日：2021-05-13
申请人： Pterodynamics Inc.
发明人： PETROV, Val
IPC分类号： B64C29/00 , B64C29/02 , B64C27/26 , B64C3/56 , B64C27/28

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