发明名称 Method and apparatus for aircraft inlet ice protection
摘要 An inlet ice protection system, and methods for making and using ice protection systems. In one embodiment, the inlet includes an acoustic liner positioned forward of the inlet throat and has a perforated face sheet a perforated back sheet, and an acoustic core between the face sheet and the back sheet. The perforations through the face sheet are sized to allow acoustic energy to be transmitted to and dissipated in the acoustic core, and the perforations in the back sheet are sized to transmit hot gas through the acoustic liner to the surface of the inlet to heat the inlet and prevent and/or restrict ice formation on the inlet. The face sheet can have a higher porosity than the back sheet, and both the sheets and the core can be formed from titanium to withstand high gas temperatures.
申请公布号 US6371411(B1) 申请公布日期 2002.04.16
申请号 US19990448524 申请日期 1999.11.23
申请人 THE BOEING COMPANY 发明人 BREER MARLIN D.;OLSEN RONALD F.;KUNZE, JR. ROBERT K.;RIEDEL BRIAN L.
分类号 B64C1/40;B64D15/04;B64D33/02;F02C7/047;(IPC1-7):B64D15/00;F02G3/00 主分类号 B64C1/40
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