Title:
ジェットエンジン排気混合タブおよび対応するジェットエンジンナセルの位置を制御するためのシステム、ならびに動作方法
Document Type and Number:
Japanese Patent JP4659836
Kind Code:
B2
Abstract:
A system for controlling a position of jet engine exhaust mixing tabs includes a plurality of exhaust mixing tabs spaced apart from one another and extending from a lip of an exhaust nozzle of a jet engine nacelle adjacent a flow path of an exhaust flow emitted from the exhaust nozzle. Each of the exhaust mixing tabs are constructed to be controllably deformable from a first position adjacent the flow path to a second position extending into the flow path of the exhaust flow in response to a control signal applied to each of the exhaust mixing tabs. In the first position, the exhaust mixing tabs either have no affect on the thrust produced, or increase the momentum (thrust) of the exhaust flow exiting from the exhaust nozzle. In the second position, that is, the "deployed" position, the exhaust mixing tabs are deformed to extend into the flow path. In this position the exhaust mixing tabs promote mixing of the exhaust flow with an adjacent air flow. This results in the attenuation of noise generated by the jet engine.
Inventors:
White, edward buoy
Application Number:
JP2007541292A
Publication Date:
March 30, 2011
Filing Date:
November 10, 2005
Export Citation:
Assignee:
The Boeing Company
International Classes:
F02K1/34; F02C7/24; F02K1/48; F02K3/04
Domestic Patent References:
| JP2005207422A | ||||
| JP2001289122A |
Foreign References:
| US20020125340 |
Attorney, Agent or Firm:
Sonoda Yoshitaka
Kobayashi Yoshinori
Kobayashi Yoshinori