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 providin g 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 membe r (150) before and during airborne operation.
申请公布号
CA2379258(A1)
申请公布日期
2001.02.15
申请号
CA20002379258
申请日期
2000.08.04
申请人
BELL HELICOPTER TEXTRON INC.
发明人
EISENHAUER, MARK P.;PAPPAS, JOHN PETER;MILLER, RICHARD DEAN;FROMAN, GARY SCOTT;SCHELLHASE, ERNST CALVIN;AUBERT, ROGER JACQUES MICHEL