Title:
垂直離着陸航空機の翼、ナセルおよび/または胴体への抵抗低減のためのプラズマアクチュエータ
Document Type and Number:
Japanese Patent JP2009511360
Kind Code:
A
Abstract:
An aircraft includes a surface over which an airflow passes. A plasma actuator (1) is configured to generate a plasma above the surface, the plasma coupling a directed momentum into the air surrounding the surface to reduce separation of the airflow from the surface. A method of reducing separation of an airflow from a surface of an aircraft includes generating a plasma in air surrounding the surface at a position where the airflow would separate from the surface in the absence of the plasma.
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Inventors:
Wood, Tommy
Cork, Thomas Sea.
Post, martica
Cork, Thomas Sea.
Post, martica
Application Number:
JP2008536572A
Publication Date:
March 19, 2009
Filing Date:
August 17, 2006
Export Citation:
Assignee:
Bell Helicopter Textron Incorporated
International Classes:
B64C23/00; B64C27/28; H05H1/24
Attorney, Agent or Firm:
Takehiko Suzue
Kurata Masatoshi
Satoshi Kono
Makoto Nakamura
Takashi Mine
Yoshihiro Fukuhara
Toshio Shirane
Sadao Muramatsu
Nobuhisa Nogawa
Katsu Sunagawa
Ryo Hashimoto
Tetsuya Kazama
Kurata Masatoshi
Satoshi Kono
Makoto Nakamura
Takashi Mine
Yoshihiro Fukuhara
Toshio Shirane
Sadao Muramatsu
Nobuhisa Nogawa
Katsu Sunagawa
Ryo Hashimoto
Tetsuya Kazama