Introduction of an Individual Aircraft Tracking Program for the Polish SU-22

Q4 Engineering Fatigue of Aircraft Structures Pub Date : 2017-12-01 DOI:10.1515/fas-2017-0008
P. Reymer, M. Kurdelski, A. Leski, A. Leśniczak, M. Dziendzikowski
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引用次数: 1

Abstract

Abstract The Su-22 fighter-bomber is a military aircraft used in the Polish Air Force (PLAF) since the mid 1980’s. By decision of the Ministry of National Defence Republic of Poland, the assumed service life for this type of aircraft was prolonged up to 3200 flight hours based on the Full Scale Fatigue Test (FSFT) results. The FSFT was conducted using the real load profile defined during the Operational Load Monitoring Program (OLM) and the 3200 hour service life was also based on this load profile. In order to assure safe operation of all the 18 Su-22 aircraft, the Individual Aircraft Tracking program was introduced. The program was based on the results of the FSFT as well as the analysis of the flight parameters recorded by the THETYS onboard flight recorder. In this paper, the authors present the methodology, assumed fatigue hypothesis and preliminary results of the IAT program for the Polish Su-22.
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介绍了波兰SU-22的单个飞机跟踪程序
苏-22战斗轰炸机是波兰空军(PLAF)自20世纪80年代中期以来使用的军用飞机。根据波兰共和国国防部的决定,根据全尺寸疲劳试验(FSFT)结果,该型飞机的假定使用寿命延长至3200飞行小时。FSFT使用运行负载监控程序(OLM)中定义的实际负载剖面进行,3200小时的使用寿命也是基于该负载剖面。为了保证所有18架苏-22飞机的安全运行,引入了单机跟踪计划。该方案是基于FSFT的结果以及由THETYS机载飞行记录仪记录的飞行参数分析。在本文中,作者介绍了波兰苏-22的IAT程序的方法、假定疲劳假设和初步结果。
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来源期刊
Fatigue of Aircraft Structures
Fatigue of Aircraft Structures Engineering-Safety, Risk, Reliability and Quality
CiteScore
0.40
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0.00%
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期刊介绍: The publication focuses on problems of aeronautical fatigue and structural integrity. The preferred topics include: full-scale fatigue testing of aircraft and aircraft structural components, fatigue of materials and structures, advanced materials and innovative structural concepts, damage tolerant design of aircraft structure, life extension and management of ageing fleets, structural health monitoring and loads, fatigue crack growth and life prediction methods, NDT inspections, airworthiness considerations.
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