Title:
翼構造体、翼構造体の制御方法及び航空機
Document Type and Number:
Japanese Patent JP7096698
Kind Code:
B2
Abstract:
A wing structure for an aircraft includes a stationary wing, a movable wing and at least one plasma actuator. The movable wing is configured to have a slot between the movable wing and the stationary wing. The at least one plasma actuator is configured to control air flow through the slot.
Inventors:
Hiroki Kato
Maki Kikuchi
Kentaro Yoshida
Nobuyuki Nakazato
Tomofumi Iwamoto
Maki Kikuchi
Kentaro Yoshida
Nobuyuki Nakazato
Tomofumi Iwamoto
Application Number:
JP2018082348A
Publication Date:
July 06, 2022
Filing Date:
April 23, 2018
Export Citation:
Assignee:
Subaru corporation
International Classes:
B64C9/16; B64C21/10; H05H1/24
Domestic Patent References:
| JP2008290710A | ||||
| JP2012249510A |
Foreign References:
| US3724784 | ||||
| US20090173837 |
Other References:
浅田健吾ほか,DBDプラズマアクチュエータを用いた翼剥離制御におけるバースト発振周波数効果,第24回数値流体力学シンポジウム,JSFM,2010年,p.1-10
Attorney, Agent or Firm:
Takehiko Yamada