Title:
エーロフォイル用能動抽気
Document Type and Number:
Japanese Patent JP6424042
Kind Code:
B2
Abstract:
An airfoil active bleed system and related method. A housing includes an induction wall (39), an exhaust wall (40a,b) having one or more exhaust ports (44), and a chamber (41) between the induction and exhaust walls. Zero-net-mass-flux actuators (48) are located in the chamber and configured and positioned to collectively induct fluid through the induction wall (39) and selectively exhaust fluid through the exhaust port(s) (44).
Inventors:
Dan Barzini
Neil David Domel
Jeffrey Gee Hakes
Daniel N Miller
Neil David Domel
Jeffrey Gee Hakes
Daniel N Miller
Application Number:
JP2014164919A
Publication Date:
November 14, 2018
Filing Date:
August 13, 2014
Export Citation:
Assignee:
Lockheed Martin Corporation
International Classes:
F15D1/02; B64C21/06; F03D80/00
Domestic Patent References:
| JP14004635B1 | ||||
| JP2011247419A | ||||
| JP2000513673A |
Foreign References:
| US20020195526 | ||||
| US20110309201 | ||||
| US6457654 |
Attorney, Agent or Firm:
Kenji Sugimura
Yoshihiro Uemura
Kenichiro Kataoka
Yoshihiro Uemura
Kenichiro Kataoka