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1. 发明公开

EP4267460A1 SYSTEM AND METHODS FOR MOBILE TOWING AND LIFTING PLATFORMS 审中-实审
公开(公告)号：EP4267460A1
公开(公告)日：2023-11-01
申请号：EP21908215.3
申请日：2021-12-23
申请人： Oqab Dietrich Induction Inc.
发明人： OQAB, Haroon B. , DIETRICH, George B.
IPC分类号： B64C37/02 , B64B1/00 , B64C39/02 , B64D1/00 , B64D3/00 , B66F19/00

2. 发明授权

EP3554945B1 AERIAL LAUNCH AND/OR RECOVERY FOR UNMANNED AIRCRAFT, AND ASSOCIATED SYSTEMS AND METHODS 有权
公开(公告)号：EP3554945B1
公开(公告)日：2023-02-01
申请号：EP17881921.5
申请日：2017-12-12
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

3. 发明公开

EP3887250A1 ARTICULATED MAGNET-BEARING LEGS FOR UAV LANDING ON CURVED SURFACES 审中-公开
公开(公告)号：EP3887250A1
公开(公告)日：2021-10-06
申请号：EP19827927.5
申请日：2019-11-26
申请人： Saudi Arabian Oil Company , King Abdullah University Of Science And Technology
发明人： ABDELLATIF, Fadl , ABDELKADER, Mohamed , SHAMMA, Jeff S.
IPC分类号： B64C25/32 , B64C37/02 , F17D5/00

4. 发明授权

EP3587260B1 SELF-ALIGNING DOCKING MECHANISM FOR AN UNMANNED AERIAL VEHICLE 有权
公开(公告)号：EP3587260B1
公开(公告)日：2021-05-05
申请号：EP19180057.2
申请日：2019-06-13
发明人： KIRKBRIDE, David W.
IPC分类号： B64C37/02 , B64C39/02 , B64C27/20 , G06Q10/04 , G06Q10/06 , G06Q10/08 , G06Q50/30

5. 发明公开

EP3599168A1 ASSISTED AIRCRAFT TAKE-OFF 审中-公开
公开(公告)号：EP3599168A1
公开(公告)日：2020-01-29
申请号：EP18185273.2
申请日：2018-07-24
申请人： ArianeGroup GmbH
发明人： Rinze, Andreas
IPC分类号： B64C37/02 , B64D5/00 , B64C39/02
摘要： Disclosed is a take-off assisting device (1) for aircrafts, comprising a connector system (10) for detachably coupling the take-off assisting device to a mating connection component of an aircraft, and at least one engine (20a, 20b) configured to provide thrust both in an coupled state, in which the take-off assisting device is coupled to an aircraft, and in a detached state. The take-off assisting device is constructed as a drone further comprising a steering system (30) and adapted to fly separately in the detached state.
Further disclosed is an aircraft comprising a connection component (140) configured to be releasably combined with a connector system (10) of a take-off assisting device (1).
Moreover, a method of assisting take-off of an aircraft (100) is disclosed.

6. 发明公开

EP3515818A1 VORRICHTUNG ZUM LUFTTRANSPORT EINES GEGENSTANDS 无效
公开(公告)号：EP3515818A1
公开(公告)日：2019-07-31
申请号：EP17772014.1
申请日：2017-09-15
申请人： Airrobot GmbH & Co. KG
发明人： WIGGERICH, Burkhard
IPC分类号： B64C39/02 , B64C37/02 , B64C39/00

7. 发明授权

EP2314508B1 UNMANNED AIRCRAFT SYSTEM AND METHOD OF OPERATING SAME 有权
标题翻译：维也纳爆炸品联合会制造的“联合国气候变化框架公约”
公开(公告)号：EP2314508B1
公开(公告)日：2017-05-24
申请号：EP09808231.6
申请日：2009-08-13
申请人： Mitsubishi Heavy Industries, Ltd.
发明人： SUZUKI Satoshi
IPC分类号： B64C37/02 , B64D5/00 , B64D47/08
CPC分类号： B64C39/024 , B64C37/02 , B64C2201/082 , B64C2201/206 , G05D1/104
摘要： An unmanned aircraft system includes a manned aircraft and an unmanned aircraft. The manned aircraft includes a manned aircraft main wing, a manned aircraft fuselage, a manned aircraft landing system, and a manned aircraft joining mechanism provided at a bottom portion of the manned aircraft fuselage. The unmanned aircraft includes an unmanned aircraft main wing, an unmanned aircraft fuselage, an unmanned aircraft landing system, and an unmanned aircraft joining mechanism provided at a roof portion of the unmanned aircraft fuselage. The manned aircraft joining mechanism and the unmanned aircraft joining mechanism are detachably joined. The unmanned aircraft system can take off or land in a state that the unmanned aircraft and the manned aircraft are joined.
摘要翻译：无人机系统包括载人飞机和无人飞机。载人飞机包括载人飞机主翼，载人飞机机身，载人飞机着陆系统，以及设置在载人飞机机身底部的载人飞机连接机构。无人机包括无人机主翼，无人飞机机身，无人飞机着陆系统，以及设在无人驾驶飞机机身顶部的无人飞机接合机构。载人飞机接合机构和无人飞行器接合机构可拆卸地接合。无人机系统可以无人驾驶飞机和载人飞机加入的状态起飞或着陆。

8. 发明公开

EP3036155A4 LONG ENDURANCE AIRSHIP OPERATIONS USING A FREE-FLYING TETHERED AIRSHIP SYSTEM 审中-公开
标题翻译： LUFTSCHIFFOPERATIONEN MIT LANGER DAUERHAFTIGKEIT UNTER VERWENDUNG EINES FREI FLIEGENDEN FESTGEBUNDENEN LUFTSCHIFFSYSTEMS
公开(公告)号：EP3036155A4
公开(公告)日：2017-05-10
申请号：EP14837201
申请日：2014-08-18
申请人： HEPPE STEPHEN B
发明人： HEPPE STEPHEN B
IPC分类号： B64B1/54 , B64B1/58 , B64B1/60 , B64C37/02
CPC分类号： B64B1/54 , B64B1/02 , B64B1/06 , B64B1/58 , B64B2201/00 , B64C37/02

9. 发明公开

EP2686238A1 SYSTEMS AND METHODS FOR LONG ENDURANCE AIRSHIP OPERATIONS 有权
标题翻译：系统和方法，持续时间长AIR船舶营运
公开(公告)号：EP2686238A1
公开(公告)日：2014-01-22
申请号：EP12712014.5
申请日：2012-03-13
申请人： Heppe, Stephen
发明人： Heppe, Stephen
IPC分类号： B64B1/06 , B64C37/02
CPC分类号： B64B1/32 , B64B1/06 , B64C37/02 , B64C2201/022 , B64C2201/063
摘要： In one example, a long endurance airship system includes a payload airship and a first logistics airship mechanically joined to the payload airship to form a first combined airship, the payload airship and the logistics airship having design capabilities differing by at least a factor of two with regard to at least one of: power generation capability, propulsion capability, endurance capability, and lift capability, in which the first combined airship is free flying, lighter-than-air, and configured to maintain stationkeeping for greater than 30 days. Illustrative methods for long endurance airship operations are also provided.

10. 发明授权

EP1628878B1 METHOD AND DEVICE FOR LAUNCHING AERIAL VEHICLES 有权转让
标题翻译：方法和装置启动的飞机
公开(公告)号：EP1628878B1
公开(公告)日：2007-03-07
申请号：EP04734053.4
申请日：2004-05-20
申请人： QinetiQ Limited
发明人： KELLEHER, Christopher C., Cody Technology Park
IPC分类号： B64C37/02 , B64D5/00
CPC分类号： B64C37/02 , B64C39/024 , B64C39/026 , B64C2201/021 , B64C2201/022 , B64C2201/042 , B64C2201/088 , B64C2201/101 , B64C2201/104 , B64C2201/123 , B64C2201/127 , B64C2201/128 , B64C2201/146 , B64C2201/148 , B64C2201/201 , B64D5/00
摘要： A heavier-than-air air vehicle (1), particularly a long endurance, solar powered, unmanned aerial vehicle (UAV) intended for 'perpetual' flight within the stratosphere, is carried to its operational altitude suspended on a tether (14) from a helium balloon (16). The tether is attached at or towards a tip of the UAV's wing (3) so that it is carried in effectively a 90° banked attitude. At the desired altitude the UAV's powerplant is started and it flies on its tether in an upwardly-spiralling path relative to the balloon until a level or near level attitude is attained, when the tether is released and the UAV is permitted to assume free flight.

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