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"Airbus Operations GmbH" Search Results: 63
Title / Author(s) / Keywords PublicationDate
2018-11 EWSHM 2018, Aerospace
Virtual Product Life Cycle Management utilizing SHM Technologies
B. Eckstein18, M. Bach28, M. MOIX-BONET34, A. Weisser1, C. Bockenheimer112
1Testing Technology; Airbus Operations GmbH66, Bremen [Germany]
2Airbus Helicopters Deutschland GmbH11, Donauwörth [Germany]
3Institute of Composite Structures and Adaptive Systems (FA); Deutsches Zentrum für Luft- und Raumfahrt (DLR), German Aerospace Center34, Braunschweig [Germany]
Aerospace, Process control, Quality control, Smart materials

 
EWSHM 2018
Session: Aerospace
2018-11
2017-09 DGZfP RT-2017, Aerospace
Laminographische Prüfung großer CFK-Flugzeugbauteile bei Airbus
O. Bullinger15, U. Schnars29, D. Schulting12, B. Redmer361, M. Tschaikner32, U. Ewert3212
1Airbus Operations GmbH2, Stade [Germany]
2Airbus Operations GmbH66, Bremen [Germany]
3BAM Federal Institute for Materials Research and Testing1266, Berlin [Germany]
 DE  
DGZfP RT-2017
2017-09
2017-02 QIRT 2016, Aerospace
Phased matched guided wave excitation for ultrasonic thermography
M. Rahammer121, I. Solodov145, W. Bisle212, D. Scherling26, M. Kreutzbruck1126
1Institute for Polymer Technology (IKT); University of Stuttgart269, Stuttgart [Germany]
2Airbus Operations GmbH66, Bremen [Germany]
 
QIRT 2016
2017-02
2016-08 EWSHM 2016, Aerospace structures: Modeling, Verification & Validation
Probability-based damage assessment on a composite door surrounding structure
M. Moix Bonet12, B. Eckstein28, P. Wierach19
1Deutsches Zentrum für Luft- und Raumfahrt (DLR), German Aerospace Center34, Braunschweig [Germany]
2Airbus Operations GmbH66, Bremen [Germany]
aerospace, composite, guided waves (lamb waves), Feature Extraction, Piezoelectric sensors, SARISTU

 
EWSHM 2016
Session: Aerospace structures: Modeling, Verification & Validation
2016-08
2016-08 EWSHM 2016, Guided waves based methods for SHM-I
Reliability Aspects of Lamb Wave Interaction at Impact Damages in Complex Stiffened CFRP Structures
B. Eckstein18, M. Moix Bonet22, M. Bach18, N. Dobmann12
1Airbus Operations GmbH66, Bremen [Germany]
2Deutsches Zentrum für Luft- und Raumfahrt (DLR), German Aerospace Center34, Braunschweig [Germany]
aerospace, composite, Probability of Detection (POD), guided waves (lamb waves), reliability

 
EWSHM 2016
Session: Guided waves based methods for SHM-I
2016-08
2016-07 WCNDT 2016, Aviation
Thermosonic Testing with Phased Matched Guided Wave Excitation
M. Rahammer121, I. Solodov145, W. Bisle212, D. Scherling26, M. Kreutzbruck1126
1Institute for Polymer Technology (IKT); University of Stuttgart269, Stuttgart [Germany]
2Airbus Operations GmbH66, Bremen [Germany]
Aviation

 
WCNDT 2016
Session: Aviation
2016-07
2016-07 WCNDT 2016, CFRP Aircraft Structures
Laminographic Inspection of Large Carbon Fibre Composite Aircraft-Structures at Airbus
O. Bullinger15, U. Schnars29, D. Schulting12, B. Redmer361, M. Tschaikner32, U. Ewert3212
1Airbus Operations GmbH2, Stade [Germany]
2Airbus Operations GmbH66, Bremen [Germany]
38.3 Radiation Methods; BAM Federal Institute for Materials Research and Testing1266, Berlin [Germany]
Other Methods, Computed Tomography, X-ray computed tomography, CFRP Aircraft Structures

 
WCNDT 2016
Session: CFRP Aircraft Structures
2016-07
2016-07 WCNDT 2016, CFRP Aircraft Structures
Recurrence Quantification Analysis for Non-Destructive Evaluation with an Application in Aeronautic Industry
C. Brandt15, P. Maaß22
1Airbus Operations GmbH66, Bremen [Germany]
2Zentrum für Techno-mathematik (ZeTeM); University of Bremen14, Bremen [Germany]
Ultrasonic Testing (UT), aerospace, porosity, CFRP, Aircraft, stochastic, carbon fibre reinforced polymers (CFRP), periodic, back-wall echo, back-wall echo equivalent, Recurrence Plot, delay embedding, randomness, CFRP Aircraft Structures, Recurrence Quantification Analysis (RQA)

 
WCNDT 2016
Session: CFRP Aircraft Structures
2016-07
2016-04 AeroNDT 2015, Acoustic Methods for Composite Materials & Structures
A State Space Approach for the Non-Destructive Evaluation of CFRP with Ultrasonic Testing
C. Brandt15, P. Maaß22
1Airbus Operations GmbH66, Bremen [Germany]
2Zentrum für Techno-mathematik; University of Bremen14, Bremen [Germany]
Ultrasonic Testing (UT), aerospace, porosity, CFRP, Aircraft, stochastic, carbon fibre reinforced polymers (CFRP), periodic, back-wall echo, back-wall echo equivalent, Recurrence Plot, delay embedding, randomness, Recurrence Quantification Analysis (RQA)

 
AeroNDT 2015
Session: Acoustic Methods for Composite Materials & Structures
2016-04
2015-02 EWSHM 2014, Aeronautics
An Online System for Remote SHM Operation with Content Adaptive Signal Compression
C. Westerkamp1, A. Hennewig1, H. Speckmann26, W. Bisle312, N. Colin4, M. Rafrafi52
1University of Applied Sciences Osnabrück, Osnabrück [Germany]
2NDT and Testing Technology; TESTIA GmbH4, Bremen [Germany]
3Airbus Operations GmbH66, Bremen [Germany]
4Airbus France4, Bouguenais [France]
5TESTIA France28, Toulouse [France]
NDT-wide, signal processing, remote inspection, Sensors, Aerospace SHM applications

 
EWSHM 2014
Session: Aeronautics
2015-02
2015-02 EWSHM 2014, Aeronautics
Challenges of an Industrialized Acousto-Ultrasonic Sensor System Installation on Primary Aircraft Structure
N. Dobmann2, M. Bach8, B. Eckstein8
Airbus Operations GmbH66, Bremen [Germany]
Aircraft SHM applications

 
EWSHM 2014
Session: Aeronautics
2015-02
2015-02 EWSHM 2014, Environmental Effects
Analysis of Environmental and Operational Condition Effects on Guided Ultrasonic Waves in Stiffened CFRP Structures
B. Eckstein18, M. MOIX-BONET24, M. Bach18
1Airbus Operations GmbH66, Bremen [Germany]
2Deutsches Zentrum für Luft- und Raumfahrt (DLR), Bremen [Germany]
Guided waves, Aerospace SHM applications

 
EWSHM 2014
Session: Environmental Effects
2015-02
2013-02 AeroNDT 2012, Components Inspection
Non-Destructive Bond Quality Assessment of CFRP Structures … Status and Way Forward
C. Bockenheimer12
Testing Technology; Airbus Operations GmbH66, Bremen [Germany]
 
AeroNDT 2012
Session: Components Inspection
2013-02
2013-02 AeroNDT 2012, Laser / Optical
Laser Adhesion Test for Adhesive Bonded CFRP Structures
R. Ecault17, B. Ehrhart27, M. Boustie18, C. Bockenheimer312, B. Valeske226, F. Touchard14, L. Berthe49
1Institut Pprime, CNRS-ENSMA-Département Physique et Mécanique; Institut PPRIME6, Futuroscope Chasseneuil [France]
2Fraunhofer-Institute for Non-Destructive Testing (IZFP)454, Saarbrücken [Germany]
3Testing Technology; Airbus Operations GmbH66, Bremen [Germany]
4PIMM, CNRS-ENSAM; ParisTech13, Paris [France]
Other Methods, bond testing, kissing bond, carbon fiber composite, laser shock
 
AeroNDT 2012
Session: Laser / Optical
2013-02
2012-02 NDT Canada 2011, Laser / Optical
Remote NDT as a new possibility to perform NDT on In-Service aircraft by using the Online Maintenance Assistance (OMA) tool
H. Speckmann6
NDT and Testing Technology; Airbus Operations GmbH66, Bremen [Germany]
NDT-wide, NDT-wide, Ultrasonic Testing (UT), Other Methods, remote inspection, maintenance, Remote in-service inspection, Remote NDT inspector, In-Service, Online Maintenance Assistance (OMA)

 
NDT Canada 2011
2012-02
2012-02 NDT Canada 2011, Laser / Optical
Extended NDT for the quality assessment of adhesive bonded CFRP structures
B. Ehrhart17, B. Valeske126, R. Ecault27, M. Boustie28, L. Berthe39, C. Bockenheimer412
1Fraunhofer-Institute for Non-Destructive Testing (IZFP)454, Saarbrücken [Germany]
2Institut Pprime, CNRS-ENSMA-Département Physique et Mécanique; Institut PPRIME6, Futuroscope Chasseneuil [France]
3PIMM, CNRS-ENSAM; ParisTech13, Paris [France]
4Airbus Operations GmbH66, Bremen [Germany]
NDT-wide, Infrared Testing (IRT), Other Methods, aerospace, composite, quality, Laser, Adhesive Bond

 
NDT Canada 2011
2012-02
2012-02 NDT Canada 2011, Laser / Optical
Approach to the Technical Qualification of a SHM System in terms of Damage Detection in Aerospace Industry
T. Hayo12, B. Frankenstein131, C. Boller277, C. Bockenheimer312
1Branch Lab Dresden; Fraunhofer Institute for Ceramic Technology and System (IKTS)217, Dresden [Germany]
2Fraunhofer-Institute for Non-Destructive Testing (IZFP)454, Saarbrücken [Germany]
3Airbus Operations GmbH66, Bremen [Germany]
Ultrasonic Testing (UT), aerospace, reliability, Probability of Detection (POD), SHM, damage detection, Structural Health Monitoring, Lamb-wave

 
NDT Canada 2011
2012-02
2011-03 AeroNDT 2010, Advanced Aero Structures Assessment
The Airbus SHM Development Process
C. Bockenheimer12
Testing Technology; Airbus Operations GmbH66, Bremen [Germany]

 
AeroNDT 2010
Session: Advanced Aero Structures Assessment
2011-03
2011-03 AeroNDT 2010, Materials Characterization
Methods for the Quality Assessment of Adhesive Bonded CFRP Structures - A Resumé
B. Ehrhart17, B. Valeske126, C. Muller2, C. Bockenheimer212
1Fraunhofer-Institute for Non-Destructive Testing (IZFP)454, Saarbrücken [Germany]
2Airbus Operations GmbH66, Bremen [Germany]

 
AeroNDT 2010
Session: Materials Characterization
2011-03
2011-03 AeroNDT 2010, Poster
Heat Damage Detection and Assessment in CFRP by Means of Extended-NDT
N. Chobaut12, C. Bockenheimer112, C. Boller177, B. Valeske226, B. Ehrhart27
1EDSWNG Materials & Processes; Airbus Operations GmbH66, Bremen [Germany]
2Fraunhofer-Institute for Non-Destructive Testing (IZFP)454, Saarbrücken [Germany]
Infrared Testing (IRT), Ultrasonic Testing (UT), aerospace, composite, fibre reinforced materials, flaw detection

 
AeroNDT 2010
Session: Poster
2011-03
 
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