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1. 发明授权

EP4156722B1 A CONSENSUS FOR A BLOCKCHAIN VALIDATION 有权
公开(公告)号：EP4156722B1
公开(公告)日：2024-03-20
申请号：EP21198597.3
申请日：2021-09-23
发明人： SIGNORINI, Matteo , PONTECORVI, Matteo
IPC分类号： H04W12/63 , H04W4/02 , H04W4/06 , H04L9/00 , H04L67/10 , B64U101/20

2. 发明授权

EP3682384B1 TECHNIQUE FOR SELECTING A UAV APPLICATION SERVER 有权
公开(公告)号：EP3682384B1
公开(公告)日：2023-11-22
申请号：EP17777498.1
申请日：2017-09-14
发明人： POSCHER, Jens , DETKE, Ralph , EICHINGER, Stefan , TERCERO, Pedro
IPC分类号： G06Q10/0631 , B64C39/02 , G05D1/00 , H04W4/02 , H04W4/029 , H04W4/50 , H04W24/02 , H04W60/04 , B64U101/20

3. 发明公开

EP4183681A1 COMBINED VERTICAL TAKEOFF AND LANDING UAVS 无效
公开(公告)号：EP4183681A1
公开(公告)日：2023-05-24
申请号：EP22208687.8
申请日：2022-11-22
申请人： Shanghai Autoflight Co., Ltd.
发明人： TIAN, Yu
IPC分类号： B64C39/02 , B64D5/00 , B64U80/82 , B64U10/20 , B64U70/20 , B64U101/20
摘要： The invention relates to the technical field of unmanned aerial vehicle (UAV), which discloses a combined vertical takeoff and landing UAV, comprising a large vertical takeoff and landing UAV (1), a connecting device (3), and a small vertical takeoff and landing UAV (2). The connecting device (3) comprises a clamping component (31) and an adsorption component (32). The clamping component (31) includes a clamping part (311), and a clamping groove (312) is arranged on the clamping part (311). The clamping component (31) comprises a snap-fitting part (313), and a snap-fitting groove (314) is arranged on the snap-fitting part (313). The clamping groove (312) and the snap-fitting groove (314) are correspondingly set. A first holding space (321) is arranged on the clamping part (311), and a second holding space (323) is arranged on the snap-fitting part (313). The adsorption component (32) comprises a first magnetic element (322) located in the first holding space (321), and the adsorption component (32) also comprises a second magnetic element (324), which is located in the second holding space (323). The invention relates to a connecting device (3) between large and small vertical takeoff and landing UAVs (1, 2), which is provided with a clamping component (31) and an adsorption component (32) at the same time. The configuration of double connecting parts makes the connection performance of the combined vertical takeoff and landing UAV more stable and reliable.

4. 发明授权

EP4013121B1 APPARATUS AND METHOD FOR DETERMINING NETWORK COVERAGE DATA FOR CONNECTING A MOBILE TERMINAL 有权
公开(公告)号：EP4013121B1
公开(公告)日：2024-05-22
申请号：EP22153470.4
申请日：2019-06-14
IPC分类号： H04W36/00 , H04W36/32 , B64C39/02 , B64U101/00 , B64U101/20
CPC分类号： H04W36/0083 , H04W36/32 , B64U2101/2020230101

5. 发明授权

EP3843443B1 CONTROL DEVICE, PROGRAM, CONTROL METHOD, AND FLIGHT VEHICLE 有权转让
公开(公告)号：EP3843443B1
公开(公告)日：2023-08-30
申请号：EP19863258.0
申请日：2019-07-24
发明人： HIRAI Ryoji , SAI, Jutatsu
IPC分类号： B64U101/20 , H04B7/185 , B64C39/02 , G05D1/00 , G05D1/10 , G08G5/00 , H04W16/18 , H04W84/06

6. 发明授权

EP3826424B1 CONTROL DEVICE, PROGRAM, CONTROL METHOD, AND FLYING OBJECT 有权转让
公开(公告)号：EP3826424B1
公开(公告)日：2023-11-15
申请号：EP19851929.0
申请日：2019-07-24
发明人： TAJIKA, Akihiko
IPC分类号： H04W84/06 , B64C39/10 , G08G5/00 , G05D1/10 , H04W52/02 , H04W16/24 , H04B7/185 , B64D27/24 , B64C39/02 , B64C13/18 , B64U50/19 , B64U101/20

7. 发明公开

EP4223637A1 SYSTEMS AND METHODS FOR PRECISE VEHICLE LOCATOR 审中-实审
公开(公告)号：EP4223637A1
公开(公告)日：2023-08-09
申请号：EP23154042.8
申请日：2023-01-30
申请人： Harris Global Communications, Inc.
发明人： Burke, Peter , Nink, Richard J. , Womack, Joel , Packer, Malcom , Howe, Thomas , Hendershot, Aaron
IPC分类号： B64C39/02 , B64U50/30 , B64D45/00 , B64U101/20 , B64U101/64
摘要： Systems and methods for locating UAV. The methods comprise: causing a physical joining of a payload with a fuselage of the UAV without any modification to the fuselage (where the payload comprises a communication relay configured to perform relay operations to extend a range between users of a communication relay link for voice and data communications and a first locator configured to perform location operations to determine and report a location of the UAV to the users of the communication relay link); using a power source to supply power to the payload that is independent from a main power source used to supply power to avionic electronics of the UAV; and continuing to perform the relay operations by the communication relay and the location operations by the first locator, when power is no longer being supplied to the avionic electronics by the main power source of the UAV.

8. 发明授权

EP3956220B1 A UAV CARRIER 有权
公开(公告)号：EP3956220B1
公开(公告)日：2023-08-02
申请号：EP20790713.0
申请日：2020-03-23
发明人： AMSILI, Shay , DORON, Eyal
IPC分类号： B64C39/02 , G05D1/10 , G05D1/00 , G05B19/418 , B64D27/02 , B64F3/02 , B64U50/19 , B64U50/34 , G06T7/73 , G06V20/17 , B64U80/82 , B64U101/30 , B64U101/20

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