发明名称 Method of using an afterburner to reduce high velocity jet engine noise
摘要 A system and method of reducing noise caused by jet engines is provided. The method comprises the steps of using the afterburner to heat the exhaust gas flow while simultaneously reducing power to the core engine. Together these two operations reduce the pressure of the exhaust gas in the nozzle area while holding the exhaust gas velocity constant, which maintains engine thrust while decreasing engine noise. The method may be supplemented by altering the location of the afterburner flames to create an inverted exhaust velocity profile, thereby decreasing engine noise even further.
申请公布号 US9140214(B2) 申请公布日期 2015.09.22
申请号 US201213407018 申请日期 2012.02.28
申请人 United Technologies Corporation 发明人 Stern Alfred M.
分类号 F02K3/10 主分类号 F02K3/10
代理机构 Miller, Matthias & Hull LLP 代理人 Miller, Matthias & Hull LLP
主权项 1. A method of reducing noise from a turbofan jet engine equipped with an afterburner and a variable area nozzle, the nozzle having a cross sectional area, the method comprising the steps of: starting the engine to create exhaust gas flow through the variable area nozzle, the exhaust gas having a temperature, pressure and velocity at a base state level; increasing the cross sectional area of the variable area nozzle to increase exhaust gas flow through the variable area nozzle; lighting the afterburner to increase the exhaust gas temperature; and retarding engine throttle to lower the engine exhaust gas flow rate; wherein the afterburner lighting and engine throttle retarding steps reduce exhaust gas pressure to its base state level while holding exhaust gas velocity at a level above the base state, thereby maintaining engine thrust while reducing engine noise.
地址 Hartford CT US