Two patterns of air plane engine inlet hot-air anti-icer are introduced in this paper, one is circumferential anti-icer, the other is double skin corrugated chord direction anti-icer.
摘飞机发动机防冰对飞行安全具有十义,对于热气防冰系统,前缘防冰器结构型式对防冰效果影响很大。
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