Spectrum Editing for a Full-Scale Fatigue Test of a Fighter Aircraft Wing with Buffet Loading

2008 ◽  
pp. 113-113-14 ◽  
Author(s):  
RL Hewitt ◽  
JP Weiss ◽  
PK Nor
Keyword(s):  
Fatigue Test ◽  
Full Scale ◽  
Aircraft Wing ◽  
Fighter Aircraft

SIMULTANEOUS ULTRASONIC MONITORING OF CRACK GROWTH AND DYNAMIC LOADS DURING A FULL SCALE FATIGUE TEST OF AN AIRCRAFT WING

2009 ◽  
Author(s):  
Thomas E. Michaels ◽  
Jennifer E. Michaels ◽  
Adam C. Cobb ◽  
Donald O. Thompson ◽  
Dale E. Chimenti
Keyword(s):  
Crack Growth ◽  
Fatigue Test ◽  
Full Scale ◽  
Dynamic Loads ◽  
Ultrasonic Monitoring ◽  
Aircraft Wing

Health Monitoring of the Aircraft Structure during a Full Scale Fatigue Test with Use of an Active Piezoelectric Sensor Network

2015 ◽  
Vol 220-221 ◽  
pp. 328-332
Author(s):  
Michal Dziendzikowski ◽  
Krzysztof Dragan ◽  
Artur Kurnyta ◽  
Sylwester Klysz ◽  
Andrzej Leski
Keyword(s):  
Signal Processing ◽  
Damage Detection ◽  
Crack Growth ◽  
Fatigue Test ◽  
Piezoelectric Sensor ◽  
Full Scale ◽  
Growth Monitoring ◽  
Aircraft Structure ◽  
System Functioning ◽  
Signal Processing Methods

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.

The Swiss F/A-18 Full Scale Fatigue Test - Modern and Efficient Testing

2004 ◽  
Author(s):  
Michel Guillaume ◽  
Georges Mandanis ◽  
Ignaz Pfiffner ◽  
Lukas Schmid
Keyword(s):  
Fatigue Test ◽  
Full Scale

scholarly journals Full Scale Fatigue Test of New Undercarriage for Commuter Aircraft

2012 ◽  
Vol 2012 (4) ◽  
Author(s):  
Józef Brzęczek ◽  
Henryk Gruszecki ◽  
Leszek Pieróg ◽  
Janusz Pietruszka
Keyword(s):  
Fatigue Test ◽  
Full Scale

AE monitoring of airframe structure during full scale fatigue test

1992 ◽  
Vol 25 (6) ◽  
pp. 301
Author(s):  
D. Bozzetti ◽  
A. Sala ◽  
G. Borzacchiello ◽  
C. Sabatino
Keyword(s):  
Fatigue Test ◽  
Full Scale

Fatigue and Damage Tolerance Substantiation Approach for a Regional Jet

2014 ◽  
Vol 891-892 ◽  
pp. 1688-1693
Author(s):  
Toshiyasu Fukuoka ◽  
Kaoru Tsukigase ◽  
Keisuke Kumagai
Keyword(s):  
Fatigue Test ◽  
Fatigue Damage ◽  
Material Properties ◽  
Damage Tolerance ◽  
Full Scale ◽  
Structural Configuration ◽  
Component Level ◽  
Regulatory Requirement ◽  
Analysis Methodology ◽  
Structural Tests

The overview of the fatigue and damage tolerance substantiation approach for a 70-90 seat class regional aircraft named Mitsubishi Regional Jet, which is now under development by Mitsubishi Aircraft Corporation, is presented. To comply with the new regulatory requirement for prevention from widespread fatigue damage, full-scale airplane fatigue test will be performed with simulating actual airplane structural configuration and typical loading spectra expected in service. In addition to widespread fatigue damage, damage tolerance evaluations assuming manufacturing defect or in-service damage are being performed. Hundreds of structural tests from coupon level to sub-component level are to be used to verify the material properties and analysis methodology.

Fatigue Performance of Grade R4 and R5 Mooring Chains in Seawater

2014 ◽  
Author(s):  
Jonathan Fernández ◽  
Walther Storesund ◽  
Jesús Navas
Keyword(s):  
Fatigue Test ◽  
Fatigue Damage ◽  
Fatigue Tests ◽  
Design Methods ◽  
Full Scale ◽  
Fatigue Performance ◽  
Test Program ◽  
Gas Industry ◽  
Fatigue Design ◽  
Cumulative Fatigue Damage

With more than 50.000 tons in service to date, the Oil&Gas Industry has the need to understand the tension fatigue performance of grade R5 chains in straight tension, and corroborate the validity of the existing design methods. The chain fatigue design curves in API and DNV are based on fatigue tests obtained in the nineties and early two thousands. However the tests were performed on lower grades such as ORQ, R3 and R4, and small chains, 76 mm diameter being the largest studless chain tested. The industry has moved towards the use of large studless chains, especially in permanent units, where chain diameters above 150 mm are not unusual. This paper gathers information from a full scale fatigue test program on grade R4 and R5 studless chains, performed in seawater and with diameters between 70 mm and 171 mm. The chains being tested are actual production chains supplied for different drilling units and large permanently moored production floating units. The paper analyses the data and determines tension-tension fatigue curves based on API and DNV methods for computation of cumulative fatigue damage, regardless of other damaging mechanisms. Improved fatigue capacity is obtained with respect to the above recommended design methods.

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