Health monitoring of the aircraft structure during a full scale fatigue test with use of an active piezoelectric sensor network

被引：0

作者：

Dziendzikowski, Michal ^{[1
]}

Dragan, Krzysztof ^{[1
]}

Kurnyta, Artur ^{[1
]}

Klysz, Sylwester ^{[1
,2
]}

Leski, Andrzej ^{[1
]}

机构：

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

[2] University of Warmia and Mazury, ul. Oczapowskiego 2, Olsztyn,10-719, Poland

来源：

Solid State Phenomena | 2015年 / 220-221卷

关键词：

Aircraft structure - Detection capability - Elastic waves propagation - Fatigue cracks - Full-scale fatigue test - Growth estimation - Piezoelectric sensor networks - Piezoelectric sensors;

D O I：

10.4028/www.scientific.net/SSP.220-221.328

中图分类号：

学科分类号：

摘要：

The paper presents an approach to develop a system for fatigue crack growth monitoring and early damage detection in the PZL – 130 ORLIK TC II turbo-prop military trainer aircraft structure. The system functioning is based on elastic waves propagation excited in the structure by piezoelectric PZT transducers. In the paper, a built block approach for the system design, signal processing as well as damage detection is presented. Description of damage detection capabilities are delivered in the paper and some issues concerning the proposed signal processing methods and their application to crack growth estimation models are discussed. Selected preliminary results obtained during the Full Scale Fatigue Test thus far are also presented. © (2015) Trans Tech Publications, Switzerland.

引用

页码：328 / 332

共 50 条

[31] BILBO Network: a proposal for communications in aircraft Structural Health Monitoring sensor networks
Monje, Pedro M.
Aranguren, Gerardo
STRUCTURAL MONITORING AND MAINTENANCE, 2014, 1 (03): : 293 - 308
[32] Static test technology for C919 full-scale aircraft structure
Zheng J.
Tang J.
Wang B.
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2019, 40 (01):
[33] Research and application of virtual test technology for static strength of full scale aircraft structure
Wang B.
Nie X.
Wan C.
Wu C.
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2022, 43 (06):
[34] Ultrasonic monitoring of structural "Hot Spots" during full scale fatigue tests
Michaels, J. E.
Michaels, T. E.
Cobb, A. C.
STRUCTURAL HEALTH MONITORING 2007: QUANTIFICATION, VALIDATION, AND IMPLEMENTATION, VOLS 1 AND 2, 2007, : 1576 - 1583
[35] Monitoring of a Wind Turbine Rotor Blade with Acousto Ultrasonics and Acoustic Emission Techniques During a Full Scale Fatigue Test
Schulze, E.
Schubert, L.
Frankenstein, B.
STRUCTURAL HEALTH MONITORING 2010, 2010, : 1229 - 1234
[36] Non-destructive inspection of L410 NG aircraft structure during full-scale fatigue tests
Podstawka, Michal
Belsky, Petr
EXPERIMENTAL STRESS ANALYSIS (EAN 2019), 2019, : 420 - 425
[37] On the Use of a Compact Optical Fiber Sensor System in Aircraft Structural Health Monitoring
Mrad, Nezih
Guo, Honglei
Xiao, Gaozhi
Rocha, Bruno
Sun, Zhigang
PHOTONIC APPLICATIONS FOR AEROSPACE, TRANSPORTATION, AND HARSH ENVIRONMENT III, 2012, 8368
[38] CHARACTERIZATION OF PIEZOELECTRIC NANOFIBER COMPOSITES ACOUSTIC EMISSION SENSOR FOR STRUCTURE HEALTH MONITORING
Chen, Xi
Shi, Yong
PROCEEDINGS OF THE ASME INTERNATIONAL DESIGN ENGINEERING TECHNICAL CONFERENCES AND COMPUTERS AND INFORMATION IN ENGINEERING CONFERENCE, VOL 5, 2012, : 247 - 251
[39] Hybrid Wireless Smart Sensor Network for Full-scale Structural Health Monitoring of a Cable-stayed Bridge
Jo, Hongki
Sim, Sung-Han
Mechitov, Kirill A.
Kim, Robin
Li, Jian
Moinzadeh, Parya
Spencer, B. F., Jr.
Park, Jong Woong
Cho, Soojin
Jung, Hyung-Jo
Yun, Chung-Bang
Rice, Jennifer A.
Nagayama, Tomonori
SENSORS AND SMART STRUCTURES TECHNOLOGIES FOR CIVIL, MECHANICAL, AND AEROSPACE SYSTEMS 2011, 2011, 7981
[40] A built-in active sensor network for health monitoring of composite structures
Su, Zhongqing
Wang, Xiaoming
Chen, Zhiping
Ye, Lin
Wang, Dong
SMART MATERIALS & STRUCTURES, 2006, 15 (06): : 1939 - 1949

← 1 2 3 4 5 →