《ICAF 2009, Bridging the Gap between Theory and Operational Practice》2009

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《ICAF 2009, Bridging the Gap between Theory and Operational Practice: Proceedings of the 25th Symposium of the International Committee on Aeronautical Fatigue, Rotterdam, The Netherlands,27–29 May 2009》
ICAF 2009，弥合理论与实践之间的差距：第二十五届国际航空疲劳委员会专题讨论会，鹿特丹，荷兰，27 - 2009年5月29日
编者：
M.J. Bos
National Aerospace Laboratory NLR
出版社：Springer
出版时间：2009年

《ICAF 2009, Bridging the Gap between Theory and Operational Practice: Proceedings of the 25th Sympo ...

《ICAF 2009, Bridging the Gap between Theory and Operational Practice: Proceedings of the 25th Sympo ...

《ICAF 2009, Bridging the Gap between Theory and Operational Practice: Proceedings of the 25th Sympo ...

《ICAF 2009, Bridging the Gap between Theory and Operational Practice: Proceedings of the 25th Sympo ...

目录
Preface ................................................................................................................. xiii
ICAF General Secretary & National Delegates ................................................. xvii
FULL-SCALE FATIGUE TESTING OF AIRCRAFT AND
AIRCRAFT STRUCTURAL COMPONENTS
A test concept for future aircraft fuselage panels
R. Best, Th. Fleischer, M. Götze, M. Sachse and M. Semsch ................................. 3
Marker loads for quantitative fractography of fatigue cracks in aerospace alloys
S.A. Barter, L. Molent and R.J.H. Wanhill ........................................................... 15
Substantiations of an airborne composite radome mounted on an aircraft dome
I. Kressel, U. Ben-Simon, M. Elyahu, D. Peled, A. David, T. Nachshhon,
Y. Gary, M. Interator, G. Ghilai and A. Simon .................................................... 55
AIRWORTHINESS CONSIDERATIONS
Development of a “low stress criterion” that eliminate a large portion of the
aircraft from damage tolerance based maintenance program for structural
repairs required by the new part 26 federal regulation
Girindra K. Das and Matthew Miller ................................................................... 61
Damage tolerance philosophy for bonded aircraft structures
C.D. Rans and R.C. Alderliesten ........................................................................... 73
First diamond: ‘Damage tolerance’ for the structural honeymoon
Steve Swift ............................................................................................................. 91
Survey of structural repairs and alterations in transport category airplanes
Michel D. Bode, Walter Sippel and John G. Bakuckas ...................................... 109
Enhanced teardown of ex-service F/A-18A/B/C/D centre fuselages
L. Molent, B. Dixon, S. Barter, P. White, T. Mills, K. Maxfield,
G. Swanton and B. Main .................................................................................... 123
NDI, INSPECTIONS AND MAINTENANCE
Glare teardowns from the MegaLiner Barrel (MLB) fatigue test
R.J.H. Wanhill, D.J. Platenkamp, T. Hattenberg, A.F. Bosch and
P.H. de Haan ...................................................................................................... 143
v
vi Table of Contents
30 Years of damage tolerance – Have we got it right?
Robert G. Eastin and Jon B. Mowery ................................................................. 169
Compilation of damage findings from multiple recent teardown analysis
programs
Gregory A. Shoales, Scott A. Fawaz and Molly R. Walters ............................... 187
Detection of arrested crack for foam core sandwich structures using
optical fiber sensors embedded in a crack arrester
Shu Minakuchi, Ippei Yamauchi, Nobuo Takeda and Yasuo Hirose .................. 209
LIFE EXTENSION AND MANAGEMENT OF AGEING FLEETS
Concept of the new A320 fatigue test
N. Rößler, C. Peters, O. Tusch, G. Hilfer and C. Herrmann ............................. 225
The use of composite material strips to extend the damage-tolerance life of
integrally stiffened aluminium panels
A. Brot, Y. Peleg-Wolfin, I. Kressel and Z. Yosef ............................................... 237
Structural integrity of a wing upper skin with exfoliation corrosion
Andreas Uebersax, Cyril Huber, Guillaume Renaud and Min Liao .................. 245
Helicopter structural integrity program of Polish Mi-24 Hind helicopters
Sławomir Klimaszewski, Andrzej Leski, Krzysztof Dragan, Marcin Kurdelski
and Mirosław Wrona ......................................................................................... 263
Airframe life extension by optimised shape reworking – Overview of
DSTO developments
M. Heller, M. Burchill, R. Westcott, W. Waldman, R. Kaye, R. Evans
and M. McDonald .............................................................................................. 279
Evaluation, modification and damage tolerance of an in-service aircraft
critical area
R.S. Rutledge, D.S. Backman and R.J. Hiscocks ................................................ 301
Procedures for aircraft structural teardown analysis: Development of a
best practices handbook
Gregory A. Shoales ............................................................................................ 329
Fatigue lifetime improvement of arrestment hook shanks by application of laser
peening
Mike Leap, Jon Rankin, Jim Harrison, Serena Marley, Lloyd Hackel
and Joe Nemeth .................................................................................................. 355
Table of Contents vii
ADVANCED MATERIALS AND INNOVATIVE STRUCTURAL
CONCEPTS
Design and testing of advanced composite load introduction structure for
aircraft high lift devices
Tamas Havar and Eckart Stuible ....................................................................... 365
Hybrid structure solution for the A400M wing attachment frames
Matthijs Plokker, Derk Daverschot and Thomas Beumler.................................. 375
Control of crack growth rates and crack trajectories for enhanced fail
safety and damage tolerance in welded aircraft structures
Phil Irving, Yu E Ma, Xiang Zhang, Guido Servetti, Stewart Williams,
Gary Moore, Jorge dos Santos and Marco Pacchione ...................................... 387
Durability and damage tolerance of bonded repairs to metallic fuselage
structure
John G. Bakuckas, Jr., Keith McIver and Ching Hsu ........................................ 407
Investigation on the design of bonded structures for increased damage
tolerance
Ivan Meneghin, Marco Pacchione and Pascal Vermeer .................................... 427
An experimental investigation on the fatigue performance of riveted lap
joints
M. Skorupa, A. Skorupa, T. Machniewicz and A. Korbel ................................... 449
Improving the fatigue life of aeronautical single lap bolted joints thanks
to the hybrid (bolted/bonded) joining technology
E. Paroissien, C.T. Hoang Ngoc, H. Bhugaloo and D. Ducher ......................... 475
An experimental approach to investigate detailed failure mechanisms in
fibre metal laminates
Riccardo Rodi, René Alderliesten and Rinze Benedictus ................................... 493
Experimental determination of energy release rate of CFRP structures by
means of transverse crack tension tests
Ll. Llopart Prieto, G. Spenninger and H. Wagner .............................................. 513
Central material concept: towards aircraft wing structure insensitive to
fatigue
Mohamed A.A. Attia ........................................................................................... 529
Practical applications of improvements in FML crack bridging theory
Greg Wilson, René Alderliesten, Riccardo Rodi and H.J.K. Lemmen ................ 539
viii Table of Contents
Simulation of the stress distribution on fuselage structures for the preand
post analysis of curved panel tests
Matthias Ziegenhorn, Frank Schulze, Holger Sparr, Karsten Wenke and
Thomas Fleischer ............................................................................................... 559
Low cycle lifetime prediction of AL2024 alloy
A. Vyshnevskyy, S. Khan and J. Mosler .............................................................. 569
Fatigue and damage tolerance aspects of metal laminates
J. Sinke and S.A.H. Johansson ........................................................................... 585
Arall and Glare FML’s: Three decades of bridging the gap between
theory and operational practice
Cees van Hengel and Peter Kortbeek ................................................................ 601
FATIGUE CRACK GROWTH AND LIFE PREDICTION
METHODS
Detailed strain field analyses of fatigue cracks in friction stir welded
joints
H.J.K. Lemmen, R.C. Alderliesten and R. Benedictus......................................... 619
A study of interaction and coalescence of micro surface fatigue cracks in
aluminium 7050
W. Hu, Q. Liu and S. Barter ............................................................................... 643
Fracture behaviour of skin materials of civil airplane structures
Boris Nesterenko, Grirory I. Nesterenko and Valentin N. Basov ...................... 661
Fatigue life prediction of small notched TI-6AL-4V based on the theory
of critical distance
Yoichi Yamashita, Masaharu Shinozaki, Hiroshi Kuroki and
Yusuke Ueda ....................................................................................................... 685
A case study of multiple-site fatigue crack growth in the F-18 Hornet
bulkhead
B. Andersson, A.F. Blom, U. Falk, G.S. Wang, K. Koski, A. Siljander,
J. Linna, A. Miettinen, K. Vaaraniemi and R. Lahtinen ..................................... 707
Experimental and theoretical comparison of some multiaxial fatigue
design criteria in the context of life assessment of rotating parts in
turboengines
V. Bonnand, J.L. Chaboche, H. Cherouali, P. Gomez, P. Kanouté, D. Pacou,
P. Paulmier, E. Ostoja-Kuczynski and F. Vogel ................................................ 743
Table of Contents ix
A contribution of environmental investigations for Glare riveted joint sizing
Thomas Beumler, Bob Borgonje and Jos Sinke ................................................. 765
Advances in crack growth modelling of 3D aircraft structures
S.C. Mellings, J.M.W. Baynham and R.A. Adey ................................................. 789
Development of advanced risk assessment methodologies for aircraft
structures containing MSD/MED
Min Liao, Yan Bombardier, Guillaume Renaud, Nick Bellinger and
Terence Cheung ................................................................................................. 811
Crack growth in fiber metal laminates under variable amplitude loading
S.U. Khan, R.C. Alderliesten and R. Benedictus ................................................ 839
Effect of residual stresses from shot peening on fatigue strength and
threshold to crack propagation of AL 7475 alloy components
G. Ratti, U. Mariani, M. Giglio and M. Guagliano ........................................... 859
Experimental validation of stress intensity factor solutions for the pin
loaded lug
D.R. Child, N.J. Moyle and A.F. Grandt ............................................................ 871
Properties of fatigue crack propagation in friction stir welded 2024-T3
aluminum alloy
T. Okada, K. Kuwayama, S. Fujita, M. Asakawa, T. Nakamura.
and S. Machida ................................................................................................... 899
Fatigue crack growth in thick plate 7050 aluminum
Joel Schubbe ...................................................................................................... 909
Fatigue life evaluation on tension type fitting
Nicolas Baréa and Marie Massé ........................................................................ 921
Accelerated fatigue testing on hydraulic shaker
M. Fressinet, M. Panis and C. Bordes ............................................................... 931
Methods for FEM analysis of riveted joints of thin-walled aircraft structures
within the Imperja project
Jerzy Kaniowski, Wojciech Wronicz, Jerzy Jachimowicz and
E. Szymczyk ........................................................................................................ 939
On the crack growth behaviour under simple compressive loads of
2024-T3 aluminium alloy
M. Krkoška, R.C. Alderliesten and R. Benedictus .............................................. 969
x Table of Contents
An analytical model for load transfer in a mechanically fastened,
double-lap joint
Ligieja Paletti, Calvin Rans and Rinze Benedictus ............................................ 987
Simulation of fatigue crack growth in the high speed machined panel
under the constant amplitude and spectrum loading
Petr Augustin ................................................................................................... 1005
Bonded composite patch to repair metallic structures: Disbond
propagation testing and modelling
P. Madelpech, S. Juaneda and M. Pradels ...................................................... 1019
Three dimensional crack growth prediction
Sarah E. Galyon, Saravanan R. Arunachalam, James Greer,
Matthew Hammond and Scott A. Fawaz .......................................................... 1035
Hybrid structures for concentrated load transmission in fibre composites:
Initial experiments
Pascal Vermeer, René Alderliesten and Rinze Benedictus ............................... 1069
STRUCTURAL HEALTH AND STRUCTURAL LOADS
MONITORING
Pilatus PC-21 – A damage tolerant aircraft
Lukas Schmid ................................................................................................... 1085
Introduction to service of an artificial neural network based fatigue
monitoring system
Steve Reed, Brian McCoubrey and Andy Mountfort ........................................ 1093
Towards automated flight-maneuver-specific fatigue analysis
Juha Jylhä, Marja Ruotsalainen, Tuomo Salonen, Harri Janhunen,
Tomi Viitanen, Juho Vihonen and Ari Visa ...................................................... 1121
Service history analysis and teardown evidence – Key elements for
structural usage monitoring of an ageing fleet
K.A. Lucas and M.J. Duffield ........................................................................... 1135
Development of fatigue life monitoring of RMAF fighter airplanes
Wahyu Kuntjoro, M. Suhaimi Ashari, M. Yazid Ahmad and
Assanah M. Mydin ............................................................................................ 1155
Table of Contents xi
Research and development of impact damage detection system for
airframe structures using optical fiber sensors
Hiroaki Tsutsui, Noriyoshi Hirano, Junichi Kimoto, Takahiko Akatsuka,
Hirofumi Sashikuma, Nobuo Takeda and Naoyuki Tajima .............................. 1165
Load factors (N/Z) / roll rate: First comparisons between design and inflight
recorded data on Eurofighter typhoon Italian fleet
Tommaso Giacobbe and Fabio Sardo .............................................................. 1177
Development of a structural health monitoring system to evaluate debonding
in composite adhesive structures
Hideki Soejima, Noritsugu Nakamura, Toshimichi Ogisu, Hiroshi Wakai,
Yoji Okabe, Nobuo Takeda and Yoshihiro Koshioka ......................................... 1187
OLM: A hands-on approach
Stephen Willis ................................................................................................... 1199
F-35 Joint strike fighter structural prognosis and health management: An
overview
Timothy Fallon, Devinder Mahal and Iain Hebden ......................................... 1215
FATIGUE LIFE ENHANCEMENT METHODS AND REPAIR SOLUTIONS
Bonded repair for fuselage damage: An overall benefit to commercial
aviation
D. Furfari, H.J.M. Woerden, R. Benedictus and A. Kwakernaak .................... 1219
Fatigue & damage tolerance of hybrid materials & structures – Some
myths, facts & fairytales
R.C. Alderliesten .............................................................................................. 1245
High cycle fatigue of laser beam deposited Ti-6Al-4V and inconel 718
E. Amsterdam and G.A. Kool............................................................................ 1261
The variable expansion process – A new cost efficient method for cold
working fastener holes in aluminium aircraft structures
Eggert D. Reese, Anthony L. Dowson and Timothy G.B. Jones........................ 1275
Stress measurements with x-ray diffractometry on aluminium alloys.
Determination of the most optimized parameters of the measurement
Elżbieta Gadalińska, Jerzy Kaniowski and Andrzej Wojtas.............................. 1285
Delamination growth at interfaces in hybrid materials and structures
under various opening modes
G. Delgrange, R.C. Alderliesten and R. Benedictus.......................................... 1305
xii Table of Contents
Developments in metal bonding
Jarkko J. Aakkula , Kari Lumppio, Olli Saarela and Tapani Haikola ............. 1321
ENVIRONMENTAL EFFECTS
On separating the effect of corrosion on inter-lamellar fatigue on thin sheet
AA7079-T6
Sandeep R. Shah and S.A. Fawaz...................................................................... 1345
Authors Index.................................................................................................... 1365

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