记忆合金接头适航审查符合性方法研究
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1.中国民用航空沈阳航空器适航审定中心,沈阳 110043;2.航空工业哈尔滨飞机工业集团有限责任公司,哈尔滨 150066;3.沈阳航空航天大学安全工程学院,沈阳 110136

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TB332

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民航安全能力建设基金(AADSA2021018)


Study on Conformity of Airworthiness Examination of Memory Alloy Joints
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Affiliation:

1.Shenyang Aircraft Airworthiness Certification Center of Civil Aviation of China,Shenyang 110043;2.AVIC Harbin Aircraft Industry Group Co. LTD,Harbin 150066;3.School of Safety Engineering, Shenyang Aerospace University,Shenyang 110136

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    摘要:

    形状记忆合金已广泛应用于美国军机及空客、波音民用机型,并首次在国产运12F型机成功应用且通过适航审查。为突破进口管接头适航验证技术壁垒,建立自主适航审定标准,本文基于运12F进口产品适航验证经验,首次对国产形状记忆合金管接头开展系统性试验。结果表明:国产接头在火焰耐受性(5 min无失效)、爆破强度(临界值35 MPa)、耐压稳定性(21 MPa保压合格)及重复装配性能(8次拆装后密封达标)等核心指标上均达到进口产品水平,符合国际适航标准。确定了国产记忆合金管接头的主要失效模式及可采用的符合性方法,并依据相应符合性方法初步建立了适航验证方法,为建立国产记忆合金管接头适航审定方法和标准奠定了基础。

    Abstract:

    Shape memory alloys have been widely used in U.S.military aircraft and Airbus/Boeing civil aircraft models,and were first successfully applied in the domestic Yun12F aircraft with airworthiness certification approval.To break through the airworthiness verification technical barriers of imported pipe joints and establish independent airworthiness certification standards,this study conducted systematic tests on domestic shape memory alloy pipe joints for the first time,based on airworthiness verification experience with imported products from the Yun12F.Results demonstrate that domestic joints have reached imported product levels in core performance metrics:flame resistance (5min exposure without failure),burst strength (critical value 35 MPa),pressure stability(21 MPa pressure maintenance qualified),and repeated assembly performance (maintained sealing after 8 disassemblies),all complying with international airworthiness standards.The research identified primary failure modes of domestic memory alloy pipe joints and applicable compliance methods,preliminarily establishing airworthiness verification methodologies.This lays the foundation for developing domestic airworthiness certification methods and standards for shape memory alloy pipe joints.

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引用本文

徐海,王征,张磊,谷峰,盖迪.记忆合金接头适航审查符合性方法研究[J].宇航材料工艺,2025,55(3):106-113.

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  • 收稿日期:2023-07-07
  • 最后修改日期:2024-03-16
  • 录用日期:2024-03-18
  • 在线发布日期: 2025-06-27
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