发明名称 Dilating fan duct nozzle
摘要 A turbofan engine includes an engine core and a ducted fan assembly, with the ducted fan assembly including an annular cowling and a dilating fan duct nozzle. The nozzle includes continuous nozzle sections with intermeshing tiles. The tiles include drive tiles that are pivotal between nominal and dilated positions and driven tiles that intermesh with the drive tiles and shift with the drive tiles between the positions. The intermeshing tiles cooperatively adjust an orifice size of the nozzle by shifting between the positions and thereby affect the thrust and noise developed by the ducted fan assembly.
申请公布号 US8677758(B2) 申请公布日期 2014.03.25
申请号 US20100750153 申请日期 2010.03.30
申请人 CORE ROBERT ARTHUR;SPIRIT AEROSYSTEMS, INC. 发明人 CORE ROBERT ARTHUR
分类号 F02K1/00;B05B12/00 主分类号 F02K1/00
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