发明名称 REDUNDANT DE-ICING/ANTI-ICING SYSTEM FOR AIRCRAFT
摘要 A redundant ice management system and method to de-ice and anti-ice an aircraft member (150) is provided. The system comprising a primary ice management sub-system (154) for providing thermal ice management to the aircraft member and a secondary ice management sub-system (172) for providing back-up thermal ice management to the aircraft member (150) in the event of a failure by the primary ice management sub-system (154). The system provides primary and secondary de-ice and anti-ice capabilities to the aircraft member (150) before and during airborne operation.
申请公布号 WO0110713(A1) 申请公布日期 2001.02.15
申请号 WO2000US21350 申请日期 2000.08.04
申请人 BELL HELICOPTER TEXTRON INC. 发明人 SCHELLHASE, ERNST, CALVIN;EISENHAUER, MARK, P.;MILLER, RICHARD, DEAN;PAPPAS, JOHN, PETER;FROMAN, GARY, SCOTT;AUBERT, ROGER, JACQUES, MICHEL
分类号 B64D15/12;B64D15/14;(IPC1-7):B64D15/12 主分类号 B64D15/12
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