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应用领域中国已授权

Variable camber wing leading edge structure

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申请人中国飞机强度研究所
发明人王志刚
公开号CN111409816B
授权号CN111409816B
申请日2020-04-22
公开日2023-02-28
授权日2023-02-28

摘要

The application belongs to aircraft wing leading edge structure flap, slat design field, in particular to become camber wing leading edge structure, includes: a wing front spar; the flexible skin is fixed to the top and the top of the front beam of the wing; the fixed support is fixed on one side …

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