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用代表中值损伤的“飞行大纲”编排飞机载荷谱的方法 被引量:9

METHOD OF DEVELOPING AIRCRAFT SPECTRUM BASED ON THE FLIGHT TRAINING PROGRAM WITH MEDIAN DAMAGE
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摘要 通过对飞机使用情况的统计分析 ,在“用中值寿命 (损伤 )代表起落编制飞机载荷谱方法”的基础上 ,提出用代表中值损伤的飞机实用“飞行大纲”来编排各代表起落的编谱方法。按这种方法编出的载荷谱 。 It is prerequisite to develop a spectrum representing the average usage of an aircraft fleet in fatigue life determination process, however, a statistic analysis of aircraft usage in service has been made here which shows that the spectrum developed by a common method can not reach this request. One method of developing F by F spectrum for aircraft has now been well accepted and used in fatigue life determination practice for several types of aircraft. The spectrum developed by this method consist of various flight missions which each of those missoins is chosen from real recorded flight lading data with median damage. Based on this method, a modification is presented here, which various flight missions are arranged according to a specific training program with median damage instead of the training program specified for polit which used in all other spectrum developing method. Moreover, a way of calculating fatigue damage by using Load Factor parameters is suggested for selecting flight mission and training program which having medium damage. It can be proven that the spectrum developed by this modified method can be more close to the average usage for aircraft fleet.
出处 《机械强度》 CAS CSCD 北大核心 2004年第5期517-521,共5页 Journal of Mechanical Strength
关键词 载荷谱 疲劳损伤 飞机寿命 Spectrum Fatigue damage Aircraft life
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参考文献5

  • 1张福泽.飞机载荷谱编制的新方法研究[J].航空学报,1998,19(5):518-524. 被引量:29
  • 2高志成.歼×飞机单机寿命指标的监控[A]..见:飞机结构定寿文集,第四集[C].沈阳:航空工业中科学技术委员会,.526-542.
  • 3Heuler P, Schütz W. Fatigue life prediction on the crack initiation and crack propagation stage. 13th ICAF, Italy, 1985. 35 ~ 69.
  • 4张福泽.裂纹形成寿命的类比计算方法.航空学报,1982,3(2):51-60.
  • 5王智 陈志伟 刘文琦.飞机载荷谱不同编制方法的对比研究[A]..见:第五届全国疲劳会议文集[C].威海,1991..

二级参考文献2

  • 1张福泽,航空学报,1982年,3卷,2期,51页
  • 2高镇同,航空学报,1980年,2期,36页

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