A STUDY OF THE METHOD FOR CALCULATING FATIGUE DAMAGE OF AIRCRAFT BY USING RECORDED LOAD FACTORS

机译：利用记录的载荷因子计算飞机疲劳损伤的方法研究。

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A study of the method for calculating fatiguedamage of aircraft by using recorded loadfactors is presented in this paper. Through asystematical calculation by using 35000 hoursof flight data recorded from two types ofaircraft, each consisting 30 aircraft, it has beenprove that this method is a powerful tool tomonitor aircraft fatigue damage consumptions.

机译：本文对利用记录的载荷系数计算飞机疲劳损伤的方法进行了研究。通过使用两种类型的飞机（每架由30架飞机组成）记录的35000个小时的飞行数据进行系统计算，已证明该方法是监控飞机疲劳损伤消耗的有力工具。

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《Congress of the International Council of the Aeronautical Sciences;ICAS 2010》|2010年|p.1-7|共7页
会议地点 Nice(FR);Nice(FR)
作者
Wang Zhi; Wang YuYa;
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作者单位

Beijing Aeronautical Technology Research Center China;

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关键词
fatigue damage; ; aircraft load; ; fatigue calculation; ; structural life monitoring;

机译：疲劳损伤;飞机负载;疲劳计算； ;结构寿命监测;

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专利

1. Advanced damage tolerance and risk analysis methodologies and tools for aircraft structures containing multiple-site and multiple-element fatigue damages [J] . M Liao, Y Bombardier, G Renaud, Proceedings of the Institution of Mechanical Engineers . 2012,第G11期

机译：包含多点和多元素疲劳损伤的飞机结构的高级损伤承受能力和风险分析方法和工具
2. A critical review of available composite damage growth test data under fatigue loading and implications for aircraft sustainment [J] . Molent L., Haddad A. Composite Structures . 2020,第Jana期

机译：在疲劳载荷下对可用复合材料损伤增长测试数据的严格审查及其对飞机维持性的影响
3. Damage-tolerant composite design principles for aircraft components under fatigue service loading using multi-scale progressive failure analysis [J] . DorMohammdi Saber, Godines Cody, Abdi Frank, Journal of Composite Materials . 2017,第15期

机译：使用多尺度逐行故障分析疲劳服务负荷下飞机组件损坏复合设计原理
4. A STUDY OF THE METHOD FOR CALCULATING FATIGUE DAMAGE OF AIRCRAFT BY USING RECORDED LOAD FACTORS [C] . Wang Zhi, Wang YuYa Congress of the International Council of the Aeronautical Sciences . 2010

机译：用记录的负载因子计算飞机疲劳损伤的方法研究
5. Nonlinear fatigue damage accumulation in aircraft engine alloys under multiaxial loading. [D] . Suman, Sandip Kumar. 2013

机译：多轴载荷下飞机发动机合金中的非线性疲劳损伤累积。
6. Study on Damage Accumulation and Life Prediction with Loads below Fatigue Limit Based on a Modified Nonlinear Model [O] . Junhong Zhang, Xi Fu, Jiewei Lin, 2018

机译：基于修正非线性模型的疲劳极限以下载荷累积损伤与寿命预测研究
7. Method of Calculating Life-Cycle Fatigue Damage of Orthotropic Steel Bridge Decks under the Combined Actions of Vehicle Loads and Pavement Temperature [O] . Gaoxin Wang, Youliang Ding, Zhijun Liu, 2020

机译：在车载和路面温度综合作用下计算正交钢桥甲板生命周期疲劳损伤的方法

A STUDY OF THE METHOD FOR CALCULATING FATIGUE DAMAGE OF AIRCRAFT BY USING RECORDED LOAD FACTORS

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