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应用领域中国申请中

A metal composite hybrid fuselage structure

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申请人江西洪都航空工业集团有限责任公司
发明人张勇
公开号CN119551176A
申请日2024-11-11
公开日2025-03-04

摘要

A metal-composite hybrid fuselage structure comprises a metal skeleton structure and a composite outer shape structure embedded in the metal skeleton structure. Based on the stress characteristics of the fuselage structure of a new basic trainer aircraft, the main load-bearing structure adopts a …

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