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"Airbus Operations GmbH" Search Results: 66
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
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 Testing1272, Berlin, Germany
 DE  
DGZfP RT-2017
2017-09
2017-02 QIRT 2016 Vibrothermography
Phased matched guided wave excitation for ultrasonic thermography
M. Rahammer122, I. Solodov145, W. Bisle212, D. Scherling26, M. Kreutzbruck1127
1Institute for Polymer Technology (IKT); University of Stuttgart271, Stuttgart , Germany
2Airbus Operations GmbH66, Bremen, Germany
 
QIRT 2016
Session: Vibrothermography
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. Rahammer122, I. Solodov145, W. Bisle212, D. Scherling26, M. Kreutzbruck1127
1Institute for Polymer Technology (IKT); University of Stuttgart271, 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 Testing1272, 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 France29, 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)459, Saarbrücken, Germany
3Testing Technology; Airbus Operations GmbH66, Bremen, Germany
4PIMM, CNRS-ENSAM; ParisTech14, Paris, France
Other Methods, bond testing, kissing bond, carbon fiber composite, laser shock
 
AeroNDT 2012
Session: Laser / Optical
2013-02
2012-05 DGZfP 2011 Faserverbundwerkstoffe
ZfP von Flugzeug-CFK-Strukturenn der Wartung - Überblick über den aktuellen Stand bei Airbus
W. Bisle12, H. Hicken2, D. Scherling6
Airbus Operations GmbH66, Bremen, Germany
 DE  
DGZfP 2011
Session: Faserverbundwerkstoffe
2012-05
2012-05 DGZfP 2011 Materialcharakterisierung (Gefüge, Härte usw.)
Preliminary Tests for the Development of New NDT Techniques for the Quality of Adhesive Bond Assessment
B. Ehrhart17, B. Valeske126, M. SARAMBÉ22, N. Chobaut22, A. Gendard22, C. Bockenheimer212
1Fraunhofer-Institute for Non-Destructive Testing (IZFP)459, Saarbrücken, Germany
2aTesting Technology bEDSWNG Materials & Processes; Airbus Operations GmbH66, Bremen, Germany
 DE  
DGZfP 2011
Session: Materialcharakterisierung (Gefüge, Härte usw.)
2012-05
2012-05 DGZfP 2011 Zuverlässigkeit
Online Maintenance Assistance (OMA) zur Unterstützung von mobilen ZfPnspektoren
H. Speckmann6
NDT and Testing Technology; Airbus Operations GmbH66, Bremen, Germany
 DE  
DGZfP 2011
Session: Zuverlässigkeit
2012-05
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
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)459, Saarbrücken, Germany
2Institut Pprime, CNRS-ENSMA-Département Physique et Mécanique; Institut PPRIME6, Futuroscope Chasseneuil, France
3PIMM, CNRS-ENSAM; ParisTech14, 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
Approach to the Technical Qualification of a SHM System in terms of Damage Detection in Aerospace Industry
T. Hayo12, B. Frankenstein131, C. Boller278, C. Bockenheimer312
1Branch Lab Dresden; Fraunhofer Institute for Ceramic Technology and System (IKTS)217, Dresden, Germany
2Fraunhofer-Institute for Non-Destructive Testing (IZFP)459, 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
 
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