risk analysis
DESCRIPTION
Risk Analysis of aircraftTRANSCRIPT
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Southwest Research Institute (SwRI) structural engineering specialists use probabi-listic methods to perform risk assessments to quantify the safety and useful service life of aircraft structures in terms of probability of failure and hazard rate. These analyses evalu-ate alternative usage, maintenance and inspec-tion scenarios in terms of safety-of-flight risk and can be used to make planning decisions by balancing safety, cost and readiness of the aircraft system.
SwRI engineers use analysis tools such as the USAF probability of fracture (PROF) software and other advanced probabilistic methods contained in SwRIs NESSUS and DARWIN software to assess the effects of variabilities and uncertainties in loadings, material properties, fatigue and fracture models, flaw sizes, and inspection methods on the risk of structural failure.
Aircraft Risk Analysis
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KEYWORDS
Risk Assessment
Probability of Fracture
Fatigue
Fracture
Failure
Damage Tolerance
Inspection Interval
PROF
POD
EIFS
Crack Growth
Aircraft Usage
Random Variables
Sensitivity Studies
Economic Life
Hazard Rate
MIL-STD-882D
JSSG-2006
Training/Short Course
SouthwestResearchInstitute
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Single-flight probability of failure (SFPOF) results with and without recurring inspections
0 1,000 2,000 3,000 4,000 5,000
Initial Inspection at 4.250 hrsRecurring Inspection at 1,500 hrs
Flight Hours
SFPO
F
6,000 7,000 8,000 9,000 10,000
With Recurring Inspections at 1,500 hrs
Without Inspections
Capabilities n Risk evaluations of in-service cracking
n Evaluation of safety and economic impacts of service life extensions
n Risk-based evaluations of inspection, repair and/or modification plans
n Single aircraft and fleet-wide risk analyses
n Development of random variable proba- bilistic distributions for risk analyses
n Probabilistic fatigue and fracture analyses
n Equivalent Initial Flaw Size (EIFS) distribution development using in-service cracking and teardown data
n Probability of Detection (POD) curve development for nondestructive inspection method
n Interpretation of risk analysis results in terms of MIL-STD-882D and JSSG-2006
n Economic life evaluations
n Sensitivity studies
n Risk assessment workshops and training
SwRI performs risk analyses of in-service cracking detected in aircraft structures
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Southwest Research Institute is an independent, nonprofit, applied engineering and physical sciences research and development organi-zation using multidisciplinary approaches to problem solving. The Institute occupies 1,200 acres in San Antonio, Texas, and provides more than 2 million square feet of laboratories, test facilities, work-shops and offices for more than 3,100 employees who perform contract work for industry and government clients.
Benefiting government, industry and the public
through innovative science and technology
Joseph W. Cardinal, P.E., Staff EngineerStructural Integrity Analysis(210) [email protected]
Structural Engineering DepartmentMechanical Engineering DivisionSouthwest Research Institute6220 Culebra Road (78238-5166)P.O. Drawer 28510 (78228-0510)San Antonio, Texas
www.swri.orgwww.structural-engr.swri.orgAn Equal Opportunity Employer M/F/D/V
Committed to Diversity in the Workplace
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We welcome your inquiries.
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SFPOF for recurring inspections and different detectable flaw sizes
1,0001.E-15
1.E-14
1.E-13
1.E-12
1.E-11
1.E-10
1.E-09
1.E-08
1.E-07
1.E-06
1.E-05
1,200 1,400 1,600 1,800
Flight Hours (IFF)
SFPO
F
2,000 2,200 2,400
Median Defectable = 0.05 inchesMedian Defectable = 0.10 inchesMedian Defectable = 0.15 inches
Experience n Damage Tolerance Risk Assessment of T-38 Wing Skin Cracks n Risk Assessment of T-37B Fatigue Critical Locations
n Risk Assessment of the A-10 Wing Aft Lower Cover at Rear Spar Cap (WS 23)
n Risk and Economic Implications of DADTA for F-5 Foreign Operators
n Probabilistic Structural Analyses of Fatigue and Fracture
n Advanced Probabilistic Fracture Mechanics and Life Evaluations of Turbine Rotor Blade Attachments
Analysis Tools for Risk Assessment
n PROF
n DARWIN
n NESSUS
n Weibull Analyses
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