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.
摘要飞机发动机防冰飞行安全具有十分重要的意,热气防冰系统,前缘防冰器的构型式防冰的效果影响很。
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.
摘要飞机发动机防冰飞行安全具有十分重要的意,热气防冰系统,前缘防冰器的构型式防冰的效果影响很。
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