GAS TURBINE ENGINE WITH FAN VARIABLE AREA NOZZLE, NACELLE ASSEMBLY AND METHOD OF VARYING AREA OF A FAN NOZZLE
摘要
<p>A turbofan engine includes a fan variable area nozzle, which includes a louver system having a multiple of slats generally transverse to the engine axis. Each of the louver slats are pivotally mounted to the fan nacelle to vary the effective area of the fan nozzle exit area and permit efficient engine operation at predefined pressure ratios.</p>
申请公布号
WO2008045050(A1)
申请公布日期
2008.04.17
申请号
WO2006US39796
申请日期
2006.10.12
申请人
UNITED TECHNOLOGIES CORPORATION;MIGLIARO, EDWARD, F., JR.