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
机发动机防
行安全具有十分重要的意义，于热气防系统，前缘防器的
构型式防的效果影响很大。
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.
摘要机发动机防行安全具有十分重要的意义，于热气防系统，前缘防器的构型式防的效果影响很大。
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