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Damage Tolerance Methodology Composites @ Airbus
Damage Tolerance Methodology - ESAC - Ref. X029PR0608046 - Issue 1
Damage Tolerance
Methodology
Chicago, IL
Prepared by Emilie MORTEAU, Chantal FUALDES
Presented by
Chantal FUALDES
Airbus
Head of Composite stress analysis
Composite Senior Expert
FAA Workshop for Composite Damage Tolerance and Maintenance
July 19-21, 2006
Composites @ Airbus
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Main principles in Damage tolerance methodology
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ANALYSIS-
FATIGUE
DAMAGE
TOLERANCE
EVALUATIONS
IN-SERVICE
EXPERIENCE
TEST RESULTS –
BUILDING BLOCK APPROACH
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CONTENT
1. AIRBUS Damage tolerance philosophy
1. Damage Detectability
2. Impact threat
3. Large Damage
4. Hail
5. Manufacturing defects
6. No-growth / Fatigue
2. Test Pyramid
3. Analysis
4. Key messages
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CONTENT
1. AIRBUS Damage tolerance philosophy
1. Damage Detectability
2. Impact threat
3. Large Damage
4. Hail
5. Manufacturing defects
6. No-growth / Fatigue
2. Test Pyramid
3. Analysis
4. Key messages
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1- AIRBUS Damage tolerance philosophy
DT Philosophy to answer to requirement and means of compliance
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