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