The Verification of the Technical Conditions of a Combat-Trainer Jet’s Airframe

Q4 Engineering
M. Kurdelski, M. Stefaniuk, Wojciech Zieliński, Tomasz Bartoszek
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引用次数: 0

Abstract

Abstract The combat-trainer jet aircraft is an important element in the process of fighter pilot training. This type of aircraft provides a means of transition from basic training on low-speed propeller trainers to piloting high-speed and highly maneuverable fighter aircraft. Nowadays, in Poland, the PZL TS-11 “ISKRA” jet trainers, designed in 1960s, are employed for training purposes. Because of financial considerations this trainer hasn’t been yet replaced by modern aircraft that conforms to current specifications and needs. As is the case with other aircraft in service of the PLAF, the TS-11 fleet has a large reserve of remaining Hourly Service Life (HSL). This opens an opportunity to extend the Calendar Service Life (CSL), so as it matches the HSL. To this end, a series of technical and research activities needed to be undertaken. The Air Force Institute of Technology is conducting the necessary verification of airframe structural conditions in cooperation with the Military Aviation Works No. 1 J.S.C. (branch in Dęblin) responsible for the overhaul and repair operations. The AFIT’s activities in this program include: deformation analysis of the selected surface areas of the wing and the fuselage; assessment of hidden corrosion in riveted joints; non-destructive testing of selected riveted joints. This paper describes the deformation analysis. As of today, the first stage of the deformation inspection has been completed. At this stage, baseline surface measurements were obtained. Further inspections shall be performed cyclically. The future measurements will be used to establish the areas that deform due to the aircraft operation.
某型战斗教练机机体技术条件的验证
摘要战斗教练机是战斗机飞行员训练过程中的重要组成部分。这种类型的飞机提供了从低速螺旋桨教练机的基本训练过渡到驾驶高速和高机动性战斗机的手段。现在,在波兰,PZL TS-11“ISKRA”喷气式教练机是在1960年设计的,用于训练目的。由于财政方面的考虑,这种教练机还没有被符合当前规格和需求的现代飞机所取代。与plaaf服役的其他飞机一样,TS-11机队有大量剩余小时使用寿命(HSL)储备。这为延长日历服务寿命(CSL)提供了机会,使其与HSL相匹配。为此目的,需要进行一系列技术和研究活动。空军技术学院正在与负责大修和维修作业的军事航空工厂第一J.S.C. (Dęblin分支机构)合作,对机身结构条件进行必要的核查。AFIT在该项目中的活动包括:机翼和机身选定表面积的变形分析;铆接接头隐性腐蚀评价选定铆接接头的无损检测。本文对其进行了变形分析。截至今天,第一阶段的变形检测已经完成。在此阶段,获得了基线表面测量值。进一步的检查应周期性地进行。未来的测量将用于确定由于飞机操作而变形的区域。
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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
自引率
0.00%
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0
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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