A flow control system includes a movable wing attachable to a wing of an aircraft, and a plasma actuator mountable on a surface of the movable wing. The flow control system is configured to control air flow around the wing by having the changing of the steering angle of the movable wing work in conjunction with the operation of the plasma actuator.
FLOW CONTROL SYSTEM, FLOW CONTROL METHOD, AND AIRCRAFT
2019-10-03
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Flow control system, flow control method, and aircraft
Europäisches Patentamt | 2022
|FLOW CONTROL SYSTEM, FLOW CONTROL METHOD AND AIRCRAFT
Europäisches Patentamt | 2019
|FLOW CONTROL APPARATUS, FLOW CONTROL METHOD, AND AIRCRAFT
Europäisches Patentamt | 2019
|Flow control apparatus, flow control method, and aircraft
Europäisches Patentamt | 2021
|Aircraft environmental control system inlet flow control
Europäisches Patentamt | 2016
|