Health monitoring of the aircraft structure during a full scale fatigue test with use of resistive ladder sensors

被引：1

作者：

Kurnyta, Artur ^{[1
,2
]}

Leski, Andrzej ^{[1
]}

Dragan, Krzysztof ^{[1
]}

Dziendzikowski, Michal ^{[1
]}

机构：

[1] Air Force Institute of Technology, ul. Ks. Boleslawa 6, Warszawa,PL-01-494, Poland

[2] Military University of Technology, ul. gen. Sylwestra Kaliskiego 2, Warszawa,PL-00-906, Poland

来源：

Solid State Phenomena | 2015年 / 220-221卷

关键词：

Aircraft structure - Fatigue cracks - FSFT - Full-scale fatigue test - Measurement system - Parametric transducers - Resistive ladders - Surface crack detection;

D O I：

10.4028/www.scientific.net/SSP.220-221.349

中图分类号：

学科分类号：

摘要：

The paper presents an application of resistive ladder sensors (or resistive crack gages) for health monitoring of an aircraft structure. An experiment was conducted during a Full Scale Fatigue Test (FSFT) of PZL 130 ORLIK TC II turbo-prop military trainer. The sensor can be successively used to detect and quantify fatigue cracks. It is a parametric transducer, similar to foil strain gages. Differences in shape of the measuring grid can be noticed. Principle of operation, sensor’s characteristics as well as block diagram of measurement system is presented in the paper. Also examples, both laboratory and FSFT data are delivered to prove surface crack detection capabilities. Simultaneously with new data collection, some investigation is carried out, connected with customize hardware elaboration, signal processing and structure-sensor integration method, what is briefly described. © (2015) Trans Tech Publications, Switzerland.

引用

页码：349 / 354

共 41 条

[1] Use of Resistive Ladder Sensors for Crack Monitoring During Full Scale Fatigue Test
Kurnyta, Artur
Dziendzikowski, Michal
Dragan, Krzysztof
2014 IEEE INTERNATIONAL WORKSHOP ON METROLOGY FOR AEROSPACE (METROAEROSPACE), 2014, : 196 - 200
[2] Health monitoring of the aircraft structure during a full scale fatigue test with use of an active piezoelectric sensor network
Dziendzikowski, Michal
Dragan, Krzysztof
Kurnyta, Artur
Klysz, Sylwester
Leski, Andrzej
Solid State Phenomena, 2015, 220-221 : 328 - 332
[3] Remote Monitoring of Fatigue Cracks Growth in the Aircraft Structure Based on Active Piezosensor Network During the Full Scale Fatigue Test
Dragan, Krzysztof
Dziendzikowski, Michal
Uhl, Tadeusz
Stepinski, Tadeusz
SMART DIAGNOSTICS V, 2014, 588 : 249 - +
[4] Acoustic emission monitoring technology for fatigue test of full-scale civil aircraft structure
Yang Y.
Wang B.
Qi X.
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2022, 43 (06):
[5] SIMULTANEOUS ULTRASONIC MONITORING OF CRACK GROWTH AND DYNAMIC LOADS DURING A FULL SCALE FATIGUE TEST OF AN AIRCRAFT WING
Michaels, Thomas E.
Michaels, Jennifer E.
Cobb, Adam C.
REVIEW OF PROGRESS IN QUANTITATIVE NONDESTRUCTIVE EVALUATION, VOLS 28A AND 28B, 2009, 1096 : 1458 - +
[6] Crack detection on a full scale aircraft fatigue test
Searle, I
Ziola, S
Seidel, B
SMART SENSING, PROCESSING, AND INSTRUMENTATION - SMART STRUCTURES AND MATERIALS 1997, 1997, 3042 : 267 - 277
[7] Monitoring the structural integrity of a flexible riser during a full-scale fatigue test
Clarke, T.
Jacques, R.
Bisognin, A.
Camerini, C.
Damasceno, S.
Strohaecker, T.
ENGINEERING STRUCTURES, 2011, 33 (04) : 1181 - 1186
[8] Structural health monitoring technology for a full-scale aircraft structure under changing temperature
State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, China
1600, Royal Aeronautical Society (118):
[9] Structural health monitoring technology for a full-scale aircraft structure under changing temperature
Gao, D.
Wang, Y.
Wu, Z.
Rahim, G.
AERONAUTICAL JOURNAL, 2014, 118 (1210): : 1519 - 1537
[10] Introduction of Developing Fatigue Load Spectrum for Full-Scale Fatigue Test of Composite Aircraft
Young-Sik Joo
Won-Jun Lee
Bo-Hwi Seo
Seung-Gyu Lim
International Journal of Aeronautical and Space Sciences, 2020, 21 : 681 - 692

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