发明授权
US5131812A Aircraft engine propulsor blade deicing 失效
飞机发动机推进器叶片检测

Aircraft engine propulsor blade deicing
摘要:
A blade heater (10) for an aircraft engine propulsor blade (14) has a foil pattern (18) which is comprised of a plurality of elements (25-56). The resistance of the elements (25-56) varies according to the distance between the elements (25-56) and the leading edge (12) of the blade (14).
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