杨嘉勤,许光群,管宇,季国梁.某型飞机4号油箱结构损伤分析及修复评估[J].装备环境工程,2019,16(1):129-136. YANG Jia-qin,XU Guang-qun,GUAN Yu,JI Guo-liang.Structure Damage Analysis and Repair Assessment for No.4 Fuel Tank of an Aircraft[J].Equipment Environmental Engineering,2019,16(1):129-136.
某型飞机4号油箱结构损伤分析及修复评估
Structure Damage Analysis and Repair Assessment for No.4 Fuel Tank of an Aircraft
投稿时间:2018-08-29  修订日期:2019-01-25
DOI:10.7643/ issn.1672-9242.2019.01.025
中文关键词:  飞机  油箱  损伤  补强  修理
英文关键词:aircraft  fuel tank  damage  reinforce  repair
基金项目:
作者单位
杨嘉勤 1.国营芜湖机械厂,安徽 芜湖 241000 
许光群 1.国营芜湖机械厂,安徽 芜湖 241000 
管宇 2.沈阳飞机设计研究所,沈阳 110000 
季国梁 1.国营芜湖机械厂,安徽 芜湖 241000 
AuthorInstitution
YANG Jia-qin 1. Wuhu State-owned Factory of Machining, Wuhu 241000, China 
XU Guang-qun 1. Wuhu State-owned Factory of Machining, Wuhu 241000, China 
GUAN Yu 2. Shenyang Aircraft Design and Research Institute, Shenyang 110000, China 
JI Guo-liang 1. Wuhu State-owned Factory of Machining, Wuhu 241000, China 
摘要点击次数:
全文下载次数:
中文摘要:
      目的 某型双座机使用中发现4号油箱存在不同程度结构损伤,分析其损伤原因和制定修理方案。方法 对4号油箱结构状态进行深入检查评估后,从结构损伤过程、载荷情况、设计制造和外场使用等方面综合分析损伤原因。对实际损伤结构进行强度计算和评估,制定结构损伤补强修理方案,并提出修理改进建议。结果 通过分析得出,损伤原因主要是4号油箱局部存在设计制造缺陷,且飞机在作大过载飞行时,4号油箱可能处于满油或大量余油的高负载状态。根据损伤原因制定的修理方案合理可行,通过了静强度校核和评估。结论 基于该损伤结构提出的修理方案通过实际修理验证,能够满足油箱结构强度设计要求,提出的改进建议能够改善飞机疲劳品质。
英文摘要:
      Objective To analyze causes and make repair procedures for structure damages at different levels of No.4 fuel tank found in the use of a two-seater aircraft. Methods After in-depth inspection and evaluation of the No.4 tank structure, the causes of damage were comprehensively analyzed from the structural damage process, load condition, design, manufacture and the use of cracks. The strength of the actual damage structure of the fuel tank was calculated and evaluated to formulate plans for repair of structural damage and propose suggestions on repair improvement. Results According to the analysis, the main cause of the damage was design and manufacturing defects in the No.4 fuel tank. And when the aircraft was in overload flight, the No.4 tank may be in a high-load state with full oil or a large amount of residual oil. The repair producers formulated based on the causes of damage passed the static strength check and evaluation and were verified of feasibility. Conclusion The repair producers formulated on this basis are verified in actual repairs and can satisfy the strength design requirements on the fuel tank structure. The proposed improvements can improve the fatigue quality of aircraft.
查看全文  查看/发表评论  下载PDF阅读器
关闭

关于我们 | 联系我们 | 投诉建议 | 隐私保护 | 用户协议

您是第11985470位访问者    渝ICP备15012534号-5

版权所有:《装备环境工程》编辑部 2014 All Rights Reserved

邮编:400039     电话:023-68792835    Email: zbhjgc@163.com

视频号 公众号