发明名称 |
Active Aircraft Pylon Noise Control System |
摘要 |
An active pylon noise control system for an aircraft includes a pylon structure connecting an engine system with an airframe surface of the aircraft and having at least one aperture to supply a gas or fluid therethrough, an intake portion attached to the pylon structure to intake a gas or fluid, a regulator connected with the intake portion via a plurality of pipes, to regulate a pressure of the gas or fluid, a plenum chamber formed within the pylon structure and connected with the regulator, and configured to receive the gas or fluid as regulated by the regulator, and a plurality of injectors in communication with the plenum chamber to actively inject the gas or fluid through the plurality of apertures of the pylon structure. |
申请公布号 |
US2015232170(A1) |
申请公布日期 |
2015.08.20 |
申请号 |
US201514703288 |
申请日期 |
2015.05.04 |
申请人 |
USA as represented by the Administrator of the National Aeronautics & Space Administration |
发明人 |
Thomas Russell H.;Czech Michael J.;Elmiligui Alaa A. |
分类号 |
B64C7/02;B64C21/04;B64D27/26 |
主分类号 |
B64C7/02 |
代理机构 |
|
代理人 |
|
主权项 |
1. A method for injecting a gas or fluid into a pylon structure of an aircraft, the method comprising:
inputting a gas or fluid in the pylon structure; controlling a pressure of a flow of the gas or fluid input in the pylon structure; and selectively injecting the gas or fluid through at least one aperture formed on the pylon structure. |
地址 |
Washington DC US |