公开(公告)号：EP3945020B1

公开(公告)日：2023-08-16

申请号：EP21186540.7

申请日：2021-07-20

发明人： Kim, Jaemo

IPC分类号： B64U30/20 ,  B64U50/13 ,  B64U50/19 ,  B64U50/34 ,  B64U101/60 ,  B64C39/02 ,  B64D1/12 ,  B64D1/22 ,  B64D9/00

公开(公告)号：EP4328130A1

公开(公告)日：2024-02-28

申请号：EP23192975.3

申请日：2023-08-23

申请人： Airbus Operations Limited ,  Imperial College Innovations Limited

发明人： MUIR, Martin ,  HEWSON, Robert W ,  SANTER, Matthew ,  NIGHTINGALE, Morgan D

IPC分类号： B64C3/18 ,  B33Y10/00 ,  B64C3/22 ,  B64D41/00 ,  B64D45/00 ,  B64U50/34 ,  F16F7/00 ,  H02N2/18 ,  B64C1/00

摘要： An aircraft arrangement (1) is provided, the aircraft arrangement comprising a first aircraft component (2) for converting at least one input vibration into an output vibration suitable for driving an energy harvester (3), and an energy harvester (3) coupled to the first aircraft component (2) and configured to generate electrical energy in response to the output vibration of the first aircraft component (3), the first aircraft component (3) comprising a three-dimensional lattice structure (4) comprising a multiplicity of unit cells, the unit cells comprising multiple lattice-forming members, the unit cells having a mean greatest dimension of at least 10nm.

公开(公告)号：EP3853970B1

公开(公告)日：2024-10-09

申请号：EP19861751.6

申请日：2019-09-20

IPC分类号： H02J50/00 ,  H02J50/05 ,  H02J50/12 ,  B64U10/13 ,  B64U30/20 ,  B64U50/19 ,  B64U50/34

CPC分类号： H02J50/05 ,  H02J50/12 ,  H02J50/005 ,  B64U10/13 ,  B64U50/34 ,  B64U50/19 ,  B64U30/20 ,  Y02T10/70

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

公开(公告)号：EP4395117A1

公开(公告)日：2024-07-03

申请号：EP22383308.8

申请日：2022-12-28

申请人： Airbus Operations, S.L.U.

发明人： CASADO MONTERO, Carlos

IPC分类号： H02J7/14 ,  H02J7/34 ,  B64U50/19 ,  B64U50/36 ,  B64D27/24 ,  B64U50/34 ,  H02J7/00

CPC分类号： H02J7/14 ,  H02J2310/4420200101 ,  H02J7/34 ,  H02J7/0042 ,  B64D27/24 ,  B64D41/007 ,  B64D41/00

摘要： In-flight electrical charging system and method for a battery-powered aircraft located in a charging aircraft and comprising:
- an electrical generation module (1) comprising:
o a turbine (1.1),
o an electric generator (1.2) in electrical connection to the turbine (1.1) for generating electricity,
o a turbine control unit in connection with the turbine (1.1) and controlling it (1.1), and
o an electric generator control unit in connection with the electric generator (1.2) and controlling it (1.2),

- a deployable power supply module (3), in electrical connection to the electrical generation module (1) and comprising at least a cable configured for the electrical connection of the electrical generation module (1) to the battery-powered aircraft to be charged,
- a pod (2) configured to be applied to the charging aircraft, wherein the electrical generation module (1) and the deployable power supply module (3) are located within the pod (2).