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1. 发明公开

EP4197921A1 END EFFECTORS WITH MULTI-AXIS ROLLER WHEELS, SYSTEMS INCLUDING THE SAME, AND RELATED METHODS 审中-实审
公开(公告)号：EP4197921A1
公开(公告)日：2023-06-21
申请号：EP22212930.6
申请日：2022-12-12
申请人： The Boeing Company
发明人： TROY, James J. , DE OLIVEIRA, Daniel M. , GEORGESON, Gary E. , HAFENRICHTER, Joseph Lawrence
IPC分类号： B64G1/64 , B64G4/00 , B64U70/20 , B64D1/22 , B64U70/00 , B25J15/00
摘要： End effectors and systems may capture, release, and/or create a mating engagement between the end effector and a target object. Said end effectors are tolerant of positional and rotational misalignment of the target object, and include a plurality of roller wheels (14, 16, 18), one or more of which is arranged in a non-parallel plane with respect to one or more other roller wheels (14, 16, 18). A first roller wheel (14) configured to rotate in a first plane (118), a second roller wheel (16) configured to rotate in a second plane (120), and a third roller wheel (18) configured to rotate in a third plane (122) may be arranged such that the end effector (10) is configured to engage a passive receptacle of the target object, to capture the target object. Rotating the roller wheels in the opposite direction may cause the target object to be released or launched, by urging the passive receptacle off of or away from the roller wheels.

2. 发明公开

EP4194347A1 AIRCRAFT DEPLOYMENT AND RETRIEVAL OF UNMANNED AERIAL VEHICLES 审中-实审
公开(公告)号：EP4194347A1
公开(公告)日：2023-06-14
申请号：EP23152650.0
申请日：2013-10-23
申请人： The Boeing Company
发明人： HANNA, Mark , POLING, David R
IPC分类号： B64U80/40 , B64U80/30 , B64U80/10 , B64U70/90 , B64U70/20 , B64U70/30 , B64U80/82
摘要： An aircraft system incorporates a first aircraft having a grappling device including a first gripper with a first actuator and a second gripper with a second actuator. The first gripper and the second gripper are movable between an open and a closed position to engage a hooking device and pivot together to change a capture angle. A first controller receives a command and operates the actuators in response to open and close the first and second grippers of the grappling device. The controller also receives a second command and operates the first and second actuators to pivot the grippers and provide grappling at a range of capture angles. A second aircraft, which may be a UAV, incorporates the hooking device. The hooking device includes a ring rotatable from the surface and a third actuator to rotate the ring between a stowed and an extended position.

3. 发明授权

EP3812271B1 SYSTEME DE RECUPERATION D'UN AERONEF A PORTER 有权
公开(公告)号：EP3812271B1
公开(公告)日：2023-09-27
申请号：EP20186917.9
申请日：2020-07-21
发明人： THOMASSEY, Lionel
IPC分类号： B64U70/20 , B64D1/22 , B64D5/00 , B64D1/12 , B64U10/13

4. 发明公开

EP4155034A1 AUSGLEICHSMECHANISMUS UND DAMIT AUSGERÜSTETES TRÄGER-FLUGOBJEKT 审中-实审
公开(公告)号：EP4155034A1
公开(公告)日：2023-03-29
申请号：EP22195756.6
申请日：2022-09-15
申请人： Schuhmacher, Leo
发明人： Schuhmacher, Leo
IPC分类号： B25J9/00 , B64U70/20 , B64U70/92 , B64U80/80 , B64U80/25 , B64D39/00
摘要： Die vorliegende Erfindung betrifft einen Ausgleichsmechanismus (1) und ein damit ausgerüstetes Träger-Flugobjekt (2). Ein solcher Ausgleichsmechanismus (1) dient dem Zwecke, eine positionelle Inkongruenz zwischen dem Träger-Flugobjekt (2), insbesondere einer Drohne, im Flugzustand und einem weiteren Flugobjekt oder einer Bodenstation auszugleichen. Zur Erfüllung dieses Zweckes umfasst dieser Ausgleichsmechanismus (1):
- mindestens zwei kinematische Ketten (3, 4, 5), wobei jede kinematische Kette aus mindestens einem Glied (3a, 3b, 4a, 4b, 5a, 5b) besteht;
- einen Endeffektor (6), mit dem alle kinematischen Ketten (3, 4, 5) mit jeweils einem ersten ihrer Enden verbunden sind;
- erste Gelenke (7, 8, 9), die jeweils an einem zweiten Ende der kinematischen Ketten (3, 4, 5) angeordnet sind, um eine gelenkige Verbindung zwischen der jeweiligen kinematischen Kette (3, 4, 5) und dem Träger-Flugobjekt (2) herzustellen;
- zweite Gelenke (10, 11, 12), die jeweils an dem ersten Ende der kinematischen Ketten (3, 4, 5) angeordnet sind, um eine gelenkige Verbindung zwischen der jeweiligen kinematischen Kette und dem Endeffektor (6) herzustellen; und
- mindestens einen ersten Aktuator, der an einem ersten und/oder zweiten Gelenk (7, 8, 9, 10, 11, 12) vorgesehen ist, um eine translatorische und/oder rotatorische Bewegung der jeweiligen kinematischen Kette (3, 4, 5) am und/oder um das jeweilige erste und/oder zweite Gelenk (7, 8, 9, 10, 11, 12) zu erzeugen.

5. 发明授权

EP3976467B1 AIRCRAFT WING CONTROL 有权
公开(公告)号：EP3976467B1
公开(公告)日：2024-03-13
申请号：EP20731176.2
申请日：2020-05-28
发明人： NEWSAM, Michael
IPC分类号： B64C3/42 , B64C3/54 , B63G8/18 , B64U30/12 , B64U70/20 , B64U70/70 , B64U101/15

6. 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.

7. 发明授权

EP3638585B1 SYSTEM AND METHOD FOR LAUNCHING AN UNMANNED AERIAL VEHICLE 有权
公开(公告)号：EP3638585B1
公开(公告)日：2024-05-15
申请号：EP18818609.2
申请日：2018-06-06
IPC分类号： B64U10/13 , B64U70/20 , F42B12/36 , B60L53/80 , B60L50/64 , B64C39/02 , B64D5/00
CPC分类号： Y02T10/70 , Y02T10/7072 , B64D5/00 , F42B12/36 , B60L53/80 , B60L50/64 , B60L2200/1020130101 , B64U70/20 , B64U10/13 , B64U20/50 , B64U50/30

8. 发明公开

EP4342794A1 VEHICLE, TRANSPORT SYSTEM (VARIANTS) AND METHOD OF MOVING VEHICLE 审中-公开
公开(公告)号：EP4342794A1
公开(公告)日：2024-03-27
申请号：EP23195276.3
申请日：2023-09-05
申请人： Andreev, Pavel Ruslanovich
发明人： Andreev, Pavel Ruslanovich
IPC分类号： B64C37/02 , B64D5/00 , B64U20/40 , B64U30/20 , B64U30/292 , B64U30/296 , B64U50/37 , B64U70/20 , B64U80/25 , B64U80/30 , B64U80/40 , B64U80/82 , B64D3/00
摘要： Provided is a vehicle comprising a fuselage provided with at least one storage module configured each to accommodate therein unmanned aerial systems and at least one docking module configured each to detachably interact with at least one of said unmanned aerial systems so as to enable connection thereof to the fuselage for movement of said a vehicle, and a control module configured to present control commands to at least one of said unmanned aerial systems so as to enable release thereof from the storage module for interaction with one of said docking modules. Furthermore, provided are variants of the transport system, each of which variants comprises the subject vehicle, and a method of moving the subject vehicle.

9. 发明授权

EP3883852B1 RECOVERING AN UNMANNED VEHICLE 有权
公开(公告)号：EP3883852B1
公开(公告)日：2024-03-13
申请号：EP19797778.8
申请日：2019-10-30
发明人： HAMILTON, Alexander Samson
IPC分类号： B64U70/20 , B64U80/70 , B64U80/82 , B64D5/00

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