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1. 发明申请

WO2023027414A1 수직이착륙형 플라잉카 审中-公开
公开(公告)号：WO2023027414A1
公开(公告)日：2023-03-02
申请号：PCT/KR2022/012320
申请日：2022-08-18
申请人： 신용식
发明人： 신용식 SHIN, Yong Sik
IPC分类号： B60F5/02 , B60K17/04 , B64C37/00 , B64C27/12 , B64C27/08 , B64D27/24
摘要： 본 발명은 주행 및 비행 겸용의 수직이착륙형 플라잉카들의 다양한 구조에 대한 것으로서, 4륜 전기자동차를 베이스로 각 바퀴의 독립구동을 위한 모터를 배치함에 있어서 각 모터의 전후 양단에 주행용과 비행용으로서의 각각의 조건과 구조에 부합되는 클러치와 변속기의 세트가 결합되되, 차체 내측일 경우에는 주행용, 차체 외측일 경우에는 비행용이 결합되어 변속기, 클러치, 모터, 클러치, 변속기의 순으로 동축 직선상의 일체형으로 각각 동일하게 형성되는 4개소의 독립된 주행 및 비행 겸용의 동력계가 각 플라잉카의 유형에 따라 각각 설치되고 각 동력계의 클러치를 단속함으로써 동일한 하나의 모터를 주행용 또는 비행용으로 선택적으로 사용될 수 있도록 하는 구조가 확보되도록 하며, 상기 각 동력계의 주행용 출력부로 부터는 각 바퀴로의 주행용 구동계가 각각의 설치 조건에 따라 구비되고, 비행용 출력부로부터는 수직 기립형 로터, 수평 회전 전개식 동축반전형 이중 로터, 수직 3겹의 덕티드 팬형 로터, 수평 회전 전개식 단일 로터의 4가지 형태의 비행용 구동계 구조가 각각 구비되는 것에 대한 것이다.

2. 发明申请

WO2022271436A1 AIR AND ROAD VEHICLE SYSTEM 审中-公开
公开(公告)号：WO2022271436A1
公开(公告)日：2022-12-29
申请号：PCT/US2022/032341
申请日：2022-06-06
申请人： SATHYA, Santh
发明人： SATHYA, Santh
IPC分类号： B60F5/02 , B64C37/00 , B64C25/10 , B64D27/02
摘要： An air and road vehicle system includes a road vehicle having a chassis, a plurality of wheels, an engine, and a cabin area. A flight vehicle having a main body, wings, flight control surfaces, and a plurality of propulsion devices is removably coupled to the road vehicle by a plurality of docking mechanisms. In the connected orientation, the top end of the road vehicle is connected to the bottom surface of the wings, and the back end of the road vehicle is connected to the main body via an elongated catch tongue. Controllers on the flight vehicle and road vehicle are communicatively linked wirelessly or via hardwire receptacles. In the disconnected orientation, the road vehicle is functional as a road motor vehicle, and in the connected orientation, the flight vehicle and the road vehicle are functional for flight in a vertical or horizontal orientation.

3. 发明申请

WO2022153368A1 移動体审中-公开
公开(公告)号：WO2022153368A1
公开(公告)日：2022-07-21
申请号：PCT/JP2021/000708
申请日：2021-01-12
申请人：エバーブルーテクノロジーズ株式会社 , シンガポール国立大学
发明人：野間　恒毅 , 末田　航
IPC分类号： B63B41/00 , B64C35/00 , B64C37/00 , B63B3/38 , B63H25/38
摘要：本発明の課題は、目的水域まで速やかに到達可能とし、且つ、目的水域での航行に要するエネルギー量を抑制することである。移動体１００は、空中を飛行可能且つ水上を航行可能である。移動体１００は、船体部１と、船体部１の上側に設けられた帆装部２と、を備えている。帆装部２は、航行時に風を受けるセイル６０と、セイル６０を支持するマスト５０と、を有している。船体部１は、航行時における当該移動体１００の進行方向を調整する航行ラダー３２と、船体部１の下側に設けられたキール１１と、を有している。

4. 发明申请

WO2022121279A1 驱动机构和无人机审中-公开
公开(公告)号：WO2022121279A1
公开(公告)日：2022-06-16
申请号：PCT/CN2021/101929
申请日：2021-06-24
申请人：歌尔股份有限公司 GOERTEK INC. [CN]/[CN]
发明人：王爱良 WANG, Ailiang
IPC分类号： B64C27/08 , B64C27/12 , B64C27/20 , B64D27/26 , B64D27/24 , B60F5/02 , B64C37/00
摘要：一种驱动机构和无人机，驱动机构包括：连接组件（1）、活动组件（2）、圆环（5）及螺旋桨（6）。连接组件（1）用于连接无人机的机体（7），活动组件（2）与连接组件（1）转动连接，活动组件（2）上设置有第一马达（3）和第二马达（4），第一马达（3）与第二马达（4）间隔设置；圆环（5）与活动组件（2）活动连接，圆环（5）与第一马达（3）传动连接；螺旋桨（6）与第二马达（4）连接；其中，定义圆环（5）远离连接组件（1）的一端为第一远端，螺旋桨（6）远离连接组件（1）的一端为第二远端，第一远端至连接组件（1）的距离大于第二远端至连接组件（1）的距离。

5. 发明申请

WO2021216241A2 HUBLESS PROPULSION UNIT 审中-公开
公开(公告)号：WO2021216241A2
公开(公告)日：2021-10-28
申请号：PCT/US2021/023330
申请日：2021-03-19
申请人： EVERON CORPORATION
发明人： OPALINSKI, Lukasz
IPC分类号： B63H1/16 , B60F5/02 , B60B19/00 , B60B19/02 , B64C37/00 , B63H2001/165
摘要： The propulsion unit including a casing having an inner curved surface and an outer curved surface, at least one tire disposed within the casing within a duct defined by the inner curved surface and the outer curved surface, a first propeller and a second propeller having a plurality of blades extending from within the casing toward a center axis of the casing, and one or more motors housed within the casing, the one or motor being configured to operate the at least one tire, the first propeller, and the second propeller independently of one another. There is also provided a vehicle with one or more propulsion units of the present disclosure.

6. 发明申请

WO2021068010A2 MULTI-MODAL MOBILITY PLATFORM 审中-公开
公开(公告)号：WO2021068010A2
公开(公告)日：2021-04-08
申请号：PCT/ZA2020/050056
申请日：2020-10-02
申请人： CLAASSEN, Daniël Gerhardus
发明人： CLAASSEN, Daniël Gerhardus
IPC分类号： A61G5/00 , A61G5/04 , A61G5/10 , A61G2203/30 , A61G2203/70 , A61G5/006 , A61G5/045 , A61G5/1056 , A61G5/121 , A61G5/127 , A61G5/128 , A61G5/14 , B60F5/02 , B64C27/08 , B64C27/20 , B64C37/00
摘要： A multimodal mobility platform comprising a prime mover (not shown), wheels 12 and an enclosure (14) for an occupant user 16. The configuration of the wheels 12 and user enclosure 14 are variable to position the wheels 12 and user enclosure 14 in a number of operational modes, including a chair mode (illustrated) and (not illustrated) a standing travel mode, a powered gurney mode, a wheeled vehicle mode, a flying drone mode and a watercraft mode. The wheels 12 and the enclosure 14 are secured to one another in a mechanical linkage comprising rigid links or support bars 18 connected to one another by joints 20 that, in combination, make up a kinematic chain that, in effect, constitutes the chassis of the mobility platform 10. The wheels 12 are driven by the prime mover to propel the vehicle across a roadway, across or through water or through the air.

7. 发明申请

WO2020050189A1 ハイブリッド有人飛行体审中-公开
公开(公告)号：WO2020050189A1
公开(公告)日：2020-03-12
申请号：PCT/JP2019/034315
申请日：2019-08-31
申请人：株式会社A.L.I. Technologies
发明人：小松　周平
IPC分类号： B64C37/00 , B64C27/68 , B64D27/24
摘要：【課題】新たな移動手段としての有人飛行体を提供すること。【解決手段】本発明によるハイブリッド有人飛行体は、エンジン及びモータと、エンジンによって揚力を発生させる第１回転翼部と、モータによって少なくとも前後方向の推進力を発生させる第２回転翼部と、エンジン及びモータを制御する制御部と、を備えている。このように、浮上用の回転翼部と推進用の回転翼部とを分離したことから必要とされる力に応じた効率的な構造とすることができる。

8. 发明申请

WO2019022618A1 SHROUD 审中-公开
公开(公告)号：WO2019022618A1
公开(公告)日：2019-01-31
申请号：PCT/NZ2018/050101
申请日：2018-07-23
申请人： DOTTEREL TECHNOLOGIES LIMITED
发明人： ROWE, Samuel Seamus , ROWE, Matthew , CLARKE, Aidan
IPC分类号： B64C27/20 , B64C11/00 , B64C27/00 , B64C29/00 , B64C39/00 , B64C37/00 , B64C30/00
摘要： A shroud for an aircraft configured to at least partially surround a noise source including a propeller. The shroud includes an outer layer and two or more sound absorbing materials located inside the shroud. The outer layer is configured to transmit noise from the noise source into the inside of the shroud and/or includes a recess located and sized to partially surround at least a part of a tip of at least one blade

9. 发明申请

WO2018192868A1 SUSPENSION SYSTEM 审中-公开
公开(公告)号：WO2018192868A1
公开(公告)日：2018-10-25
申请号：PCT/EP2018/059645
申请日：2018-04-16
申请人： AEROMOBIL R&D, S. R. O.
发明人： MACANDREW, Kenneth Douglas Alexander , RANDLE, Steve , SNAPE, Jan
IPC分类号： B60G3/20 , B60G7/00 , B64C37/00 , B60F5/02
摘要： A wheel suspension system for mounting a wheel on a vehicle body, such as a flying car, the system comprising: an upright assembly for mounting the wheel; a lower arm assembly comprising: a lower control arm; and a storage arm; a mounting structure connecting the lower arm assembly to the upright assembly; an upper control arm; and an adjustable suspension assembly pivotally connected to the upright assembly or lower control arm assembly and pivotally connected to the body; wherein one end of the lower control arm is pivotally connected to the body, and the other end of the lower control arm is connected to the mounting structure to be pivotable about a first axis; the mounting structure is connected to the upright assembly to be pivotable about a second axis that is substantially perpendicular to the first axis; the storage arm is pivotally connected to the lower control arm at one end, and is moveably connected to the body under control of an actuator at the other end; and the upper control arm having a pivot connection to an upper part of the upright assembly at one and, and a pivot connection to the body at the other end; and wherein the lateral position of the upright assembly with respect to the body is adjustable by movement of the actuator of the storage arm with respect to the body, and the vertical position of the upright assembly with respect to the body is adjustable by operation of the adjustable suspension assembly.

10. 发明申请

WO2018111924A1 AERIAL LAUNCH AND/OR RECOVERY FOR UNMANNED AIRCRAFT, AND ASSOCIATED SYSTEMS AND METHODS 审中-公开
公开(公告)号：WO2018111924A1
公开(公告)日：2018-06-21
申请号：PCT/US2017/065890
申请日：2017-12-12
申请人： INSITU, INC.
发明人： MCGREW, James, Statelar , GRUBB, Matthew, David , DICKSON, Andrew, Keith , HAYES, Andrew, Royds
IPC分类号： B64C39/02 , B64C25/08 , B64C25/10 , B64C25/68 , B64C37/00 , B64C37/02
摘要： Aerial launch and/or recovery for unmanned aircraft, and associated systems and methods. A representative system includes a first, carrier aircraft having an airframe a propulsion system carried by the airframe and positioned to support the carrier aircraft in hover, and a capture line carried by the carrier aircraft and deployable to hang from the carrier aircraft. The capture line is sized to releasably engage with a capture device of a second, carried aircraft. The system further includes a retrieval device positioned to support the carried aircraft for detachment from the capture line..

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