航空器起落架及舱门结冰适航标准分析

陈启曦, 张丽芬, 邓文亮, 李斌, 刘振侠

装备环境工程 ›› 2026, Vol. 23 ›› Issue (7) : 204-217.

PDF(3270 KB)
PDF(3270 KB)
装备环境工程 ›› 2026, Vol. 23 ›› Issue (7) : 204-217. DOI: 10.7643/issn.1672-9242.2026.07.019
环境试验与观测

航空器起落架及舱门结冰适航标准分析

  • 陈启曦1, 张丽芬1, 邓文亮2,*, 李斌2, 刘振侠1
作者信息 +

Analysis of Airworthiness Standards for Aircraft Landing Gear and Door Icing

  • CHEN Qixi1, ZHANG Lifen1, DENG Wenliang2,*, LI Bin2, LIU Zhenxia1
Author information +
文章历史 +

摘要

对国内外航空器起落架及舱门结冰适航审定标准与实验室结冰试验要求进行了系统性分析,重点研究了FAA、中国民航局适航规章及北约、美国相关军用标准和中国相关军用标准,对当前国际主流结冰适航条款(如CCAR-25-R4附录C、FAR25部等)及实验室结冰环境试验标准(RTCA/DO-160G、MIL-STD-810H、GJB 150.22A等)的应用现状进行了分析。揭示了进行实验室结冰试验时各标准给定试验方法、试验条件的异同点。通过分析国内各军用、民用起落架与舱门性能标准并对比分析某型飞机适航审定案例,提出了适用于适航取证过程中起落架及舱门系统结冰防护性能的评估流程,为航空器型号开发阶段的结冰适航性审定提供了技术依据和操作规范。研究成果对完善我国航空器结冰适航审定体系具有参考价值。

Abstract

A systematic analysis was conducted on the domestic and international airworthiness certification standards for aircraft landing gear and door icing, as well as laboratory icing test requirements. With a focus on relevant regulations of the FAA and the Civil Aviation Administration of China (CAAC), along with the military standards of NATO, the United States, and China, the current application status of mainstream international icing airworthiness clauses (e.g., CCAR-25-R4 Appendix C, FAR Part 25, etc.) and laboratory icing environmental test standards (e.g., RTCA/DO-160G, MIL-STD-810H, GJB 150.22A, etc.) were examined. The similarities and differences in test methods and conditions prescribed by these standards for laboratory icing tests were identified. By analyzing domestic military and civil performance standards for landing gear and doors, and comparing them with a case study of the airworthiness certification process for a specific aircraft, an evaluation procedure for assessing the icing protection performance of landing gear and door systems during airworthiness certification was proposed. This procedure provides a technical basis and operational guidelines for icing airworthiness certification during the aircraft development phase. The research findings are of reference value for improving the aircraft icing airworthiness certification system in China.

关键词

适航审定 / 结冰试验 / 起落架 / 舱门 / 航标 / 国军标

Key words

airworthiness certification / icing test / landing gear / door / aviation standard / national military standard

引用本文

导出引用
陈启曦, 张丽芬, 邓文亮, 李斌, 刘振侠. 航空器起落架及舱门结冰适航标准分析[J]. 装备环境工程. 2026, 23(7): 204-217 https://doi.org/10.7643/issn.1672-9242.2026.07.019
CHEN Qixi, ZHANG Lifen, DENG Wenliang, LI Bin, LIU Zhenxia. Analysis of Airworthiness Standards for Aircraft Landing Gear and Door Icing[J]. Equipment Environmental Engineering. 2026, 23(7): 204-217 https://doi.org/10.7643/issn.1672-9242.2026.07.019
中图分类号: V216.5+7   

参考文献

[1] 桂业伟, 周志宏, 李颖晖, 等. 关于飞机结冰的多重安全边界问题[J]. 航空学报, 2017, 38(2): 6-17.
GUI Y W, ZHOU Z H, LI Y H, et al.Multiple Safety Boundaries Protection on Aircraft Icing[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(2): 6-17.
[2] 张丽芬, 刘振侠, 胡剑平. 机翼三维结冰数值模拟[J]. 航空计算技术, 2013, 43(1): 36-39.
ZHANG L F, LIU Z X, HU J P.Numerical Simulation of Three-Dimensional Ice Accretion on Airfoils[J]. Aeronautical Computing Technique, 2013, 43(1): 36-39.
[3] 张丽芬, 葛鑫, 张斐, 等. 旋转帽罩结冰相似准则的冰风洞试验研究[J]. 实验流体力学, 2021, 35(4): 52-59.
ZHANG L F, GE X, ZHANG F, et al.An Ice Wind Tunnel Test Study on the Scaling Law of a Rotating Cone[J]. Journal of Experiments in Fluid Mechanics, 2021, 35(4): 52-59.
[4] 张丽芬, 余邦拓, 徐弘历, 等. 直升机多管式分离器结冰及压降损失[J]. 航空学报, 2023, 44(S2): 323-332.
ZHANG L F, YU B T, XU H L, et al.Icing and Pressure Drop Loss on Helicopter Multi-Tube Separator[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 323-332.
[5] 丁军亮, 赵利利, 杨涛, 等. 自然结冰飞行试验技术综述[J]. 航空学报, 2023, 44(17): 50-65.
DING J L, ZHAO L L, YANG T, et al.Flight Test Technology of Natural Icing[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(17): 50-65.
[6] CHEN Q X, ZHANG L F, ZHOU C X, et al.Numerical Simulation Study on Predicting the Critical Icing Conditions of Aircraft Pitot Tubes[J]. Sensors, 2024, 24(22): 7410.
[7] 王洪伟, 李先哲, 宋展. 通用飞机结冰适航验证关键技术及工程应用[J]. 航空学报, 2016, 37(1): 335-350.
WANG H W, LI X Z, SONG Z.Key Airworthiness Validation Technologies for Icing of General Aviation Aircraft and Their Engineering Application[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(1): 335-350.
[8] 高郭池, 张波, 全敬泽, 等. 正常类飞机自然结冰试飞适航审定技术[J]. 航空学报, 2024, 45(1): 188-209.
GAO G C, ZHANG B, QUAN J Z, et al.Airworthiness Certification Technology of Normal Aircraft Natural Icing Flight Test[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(1): 188-209.
[9] 强国彦, 薛小锋, 冯蕴雯. 民机起落架机构破冰动力学仿真分析方法[J]. 航空科学技术, 2023, 34(8): 44-50.
QIANG G Y, XUE X F, FENG (W/Y)W. Dynamic Simulation Analysis Method for Icebreaking of Landing Gear Mechanism of Civil Aircraft[J]. Aeronautical Science and Technology, 2023, 34(8): 44-50.
[10] 朱晨辰, 王彬文, 刘小川, 等. 复杂环境下起落架动力学行为研究现状与展望[J]. 航空科学技术, 2023, 34(1): 1-11.
ZHU C C, WANG B W, LIU X C, et al.Research Status and Prospect of Landing Gear Dynamics in Complex Environment[J]. Aeronautical Science & Technology, 2023, 34(1): 1-11.
[11] 祝耀昌, 魏莱, 程丛高. GJB150/150A、GJB4239和MIL-STD-810F/G的特性和相互关系分析[J]. 航天器环境工程, 2012, 29(3): 243-249.
ZHU Y C, WEI L, CHENG C G.Characteristics and Relations among GJB 150/150A, GJB 4239 and MIL-STD-810F/G[J]. Spacecraft Environment Engineering, 2012, 29(3): 243-249.
[12] 张方. CCAR 25部条款适用性判定方法[J]. 科技视界, 2017, 7(7): 258-259.
ZHANG F.Method for Judging Applicability of CCAR 25 Clause[J]. Science & Technology Vision, 2017, 7(7): 258-259.
[13] 迟颖君, 刘敬党. 新版GJB150A标准浅析[J]. 飞机设计, 2015, 35(3): 74-80.
CHI Y J, LIU J D.Analysis of the New Edition of GJB150A[J]. Aircraft Design, 2015, 35(3): 74-80.
[14] 刘旭华. 飞机结冰适航验证和试飞技术[C]//第十六届中国航空测控技术年会论文集. 北京: 中国航空学会, 2019.
LIU X H.Airworthiness Verification and Flight Test Technology for Aircraft Icing[C]//Proceedings of the 16th China Aviation Measurementand Control Technology Annual Conference. Beijing: Chinese Society of Aeronautics and Astronautics, 2019.
[15] 傅耘, 祝耀昌, 陈丹明. 装备环境要求及其确定方法[J]. 装备环境工程, 2008, 5(6): 46-51.
FU Y, ZHU Y C, CHEN D M.Materiel Environmental Requirements and Their Determination Method[J]. Equipment Environmental Engineering, 2008, 5(6): 46-51.
[16] 林琳, 晏效锋, 张熙川. 民机机载产品环境试验技术解析[C]//2008年航空试验测试技术峰会. 北京: 中国航空学会, 2008.
LIN L, YAN XF, ZHANG XC.Analysis of Environmental Test Technology for Civil Aircraft Airborne Products[C]//Proceedings of the 2008 Aviation Test and Measurement Technology Summit. Beijing: Chinese Society of Aeronautics and Astronautics, 2008.
[17] 翟波, 蔡良续, 祝耀昌. 实验室环境试验条件及其剪裁技术[J]. 装备环境工程, 2014, 11(5): 87-91.
ZHAI B, CAI L X, ZHU Y C.The Conditions of Laboratory Environmental Tests and Its Tailoring Techniques[J]. Equipment Environmental Engineering, 2014, 11(5): 87-91.
[18] 中国民用航空总局. 运输类飞机适航标准: CCAR-25-R3—2001[S]. 北京: 中国标准出版社, 2001.
Civil Aviation Administration of China. Airworthiness Standards for Transport Category Aircraft: CCAR-25-R3—2001[S]. Beijing: China Standard Press, 2001
[19] 金海鹏, 叶雷, 刘世英, 等. 民机材料适航符合性验证方法和技术发展[J]. 航空材料学报, 2022, 42(3): 1-11.
JIN H P, YE L, LIU S Y, et al.Research Progress in Airworthiness Conformity Verification Method and Technology of Civil Aircraft Materials[J]. Journal of Aeronautical Materials, 2022, 42(3): 1-11.
[20] 敖文伟, 付双检, 辛勃, 等. 民机适航符合性方法研究[J]. 民用飞机设计与研究, 2024(2): 1-7.
AO W W, FU S J, XIN B, et al.Research on Means of Compliance for Airworthiness of Civil Aircraft[J]. Civil Aircraft Design & Research, 2024(2): 1-7.
[21] 中国民用航空局. 航空器型号合格审定程序: AP-21-AA-2023-14R2[S]. 北京: 中国民用航空局, 2023.
Civil Aviation Administration of China. Aircraft Type Certification Procedures: AP-21-AA-2023-14R2[S]. Beijing: CAAC, 2023.
[22] 中华人民共和国工业和信息化部. 民用飞机货舱舱门设计要求: HB 8490—2014[S]. 北京: 中国航空综合技术研究所, 2014.
Ministry of Industry and Information Technology of the PRC. Design Requirements for Civil Aircraft Cargo Compartment Doors: HB 8490—2014[S]. Beijing: AVIC CAPE, 2014.
[23] 中华人民共和国工业和信息化部. 民用飞机客舱舱门和应急出口设计要求: HB8493—2014[S]. 北京: 中国航空综合技术研究所, 2014.
Ministry of Industry and Information Technology of the PRC. Design Requirements for Civil Aircraft Cabin Doors and Emergency Exits[S]. Beijing: AVIC CAPE, 2014.
[24] 中华人民共和国工业和信息化部. 民用飞机起落架系统性能试验验证要求: HB8498—2014[S]. 北京: 中国航空综合技术研究所, 2014.
Ministry of Industry and Information Technology of the PRC. Test Requirements for Landing Gear System Performance of Civil Aircraft[S]. Beijing: AVIC CAPE, 2014.
[25] Federal Aviation Administration.Aircraft Ice Protection: AC 20-73A[S]. Washington: FAA, 2006.
[26] Federal Aviation Administration.Certification of Transport Category Airplanes for Flight in Icing Conditions: AC 25.1419-1A[S]. Washington: FAA, 2004.
[27] 罗琳胤, 舒龙珍, 吕继航, 等. 水陆两栖飞机起落架水环境适应性验证要求与方法[J]. 装备环境工程, 2023, 20(1): 37-42.
LUO L Y, SHU L Z, LYU J H, et al.Requirements and Methods for Water Environment Adaptability Verification of Landing Gear of Amphibious Aircraft[J]. Equipment Environmental Engineering, 2023, 20(1): 37-42.
[28] 中国人民解放军总装备部. 飞机起落架系统通用规范: GJB 3063A—2008[S]. 北京: 总装备部军标出版发行部, 2008.
General Armament Department of the PLA. General Specification for Aircraft Landing Gear Systems: GJB 3063A—2008[S]. Beijing: GAD, 2008.
[29] 中国人民解放军总装备部. 飞机起落架和舱门收放装置通用规范: GJB 3818—1999[S]. 北京: 总装备部, 1999.
General Armament Department of the PLA. General Specification for Aircraft Landing Gear and Door Retraction Devices: GJB 3818—1999[S]. Beijing: GAD, 1999.
[30] 中国人民解放军总装备部. 飞机舱门和座舱盖机械系统通用规范: GJB 3062—1997[S]. 北京: 总装备部, 1997.
General Armament Department of the PLA. General Specification for Mechanical Systems of Aircraft Doors and Canopies: GJB 3062—1997[S]. Beijing: GAD, 1997.
[31] 中国人民解放军总装备部. 装备环境工程通用要求: GJB 4239—2001[S]. 北京: 总装备部, 2001.
General Armament Department of the PLA. General Requirements for Equipment Environmental Engineering: GJB 4239—2001[S]. Beijing: GAD, 2001(in Chinese).
[32] 中国人民解放军总装备部. 军用设备气候极值[S]. 北京: 总装备部, 1992.
General Armament Department of the Chinese People's Liberation Army. Climatic Extremes for Military Equipment[S]. Beijing: GAD, 1992.
[33] Radio Technical Commission for Aeronautics. Environmental Conditions and Test Procedures for Airborne Equipment: RTCA DO-160G[S]. Washington: RTCA Inc, 2010.
[34] 中华人民共和国工业和信息化部. 民用飞机机载设备环境条件和试验方法第13部分: 结冰试验: HB 6167.13—2014[S]. 北京: 中国标准出版社, 2014.
Ministry of Industry and Information Technology of the PRC. Environmental Conditions and Test Procedures for Airborne Equipment of Civil Airplane — Part 13: Icing Test: HB 6167.13—2014[S]. Beijing: China Standard Press, 2014.
[35] NATO Standardisation Agency.Climatic Environmental Tests: AECTP-300 (STANAG 4370)[S]. Brussels: NATO, 2006.
[36] U.S.Department of Defense. Environmental Engineering Considerations and Laboratory Tests: MIL-STD-810H[S]. Washington: DoD, 2019.
[37] Ministry of Defence. Environmental Handbook for Defence Materiel—Part 3: Environmental Test Methods: DEF STAN 00-35[S]. London: MoD, 2006.
[38] 中国人民解放军总装备部. 军用装备实验室环境试验方法第22部分: 积冰/冻雨试验: GJB 150.22A— 2009[S]. 北京: 总装备部, 2009.
General Armament Department of the PLA. Laboratory Environmental Test Methods for Military Equipment — Part 22: Icing/Freezing Rain Test: GJB 150.22A— 2009[S]. Beijing: GAD, 2009.

PDF(3270 KB)

Accesses

Citation

Detail

段落导航
相关文章

/