Title:
空気力学的流れのためのシステムおよび関連する方法
Document Type and Number:
Japanese Patent JP5344917
Kind Code:
B2
Abstract:
A system and method for controlling boundary layer flow over an aircraft wing are provided. The system includes at least one wing element, and a plurality of ports defined in the wing element and in fluid communication with one another. The system also includes at least one fluidic device operable to continuously ingest the fluid through at least one of the ports and eject the fluid out of at least one other port to control boundary layer flow of the fluid over the wing element.
Inventors:
Schmirovich, Irvine
Yadolin, yoram
Clark, Roger W
Manley, david jay
Yadolin, yoram
Clark, Roger W
Manley, david jay
Application Number:
JP2008526047A
Publication Date:
November 20, 2013
Filing Date:
July 26, 2006
Export Citation:
Assignee:
The Boeing Company
International Classes:
B64C21/02; B64C9/14
Domestic Patent References:
| JP58164499A | ||||
| JP5113102A | ||||
| JP2001520149A | ||||
| JP11079096A | ||||
| JP54151298A | ||||
| JP62225498A | ||||
| JP1132499U |
Foreign References:
| DE584585C2 | ||||
| US2517524 |
Attorney, Agent or Firm:
Sonoda Yoshitaka
Kobayashi Yoshinori
Kobayashi Yoshinori