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对飞行安全具有十分重要
意义，对于热气防冰系统，前
防冰器结构型式对防冰效果影响很大。
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;，末端;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对飞行安全具有十分重要意义，对于热气防冰系统，前防冰器结构型式对防冰效果影响很大。
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