Fatigue Life Supervision of Aircraft Structures under Corrosive Conditions

Yu Ting He; Chao Hua Fan; Heng Xi Zhang; Feng Li; Hong Peng Li

doi:10.4028/www.scientific.net/KEM.324-325.703

Paper Titles

The Reliability Analysis for Piezoelectric Truss Structure in Consideration of Electroelastic Damage
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Mechanical Properties and Fracture Analysis of Mn-Rich Ni-Mn-Ga Polycrystalline Alloys
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Mechanical Properties and Corrosion Behavior of a Beta Titanium Alloy
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Vibration Analyses of Cylindrical Hybrid Panel with Viscoelastic Layer Based on Layerwise Finite Elements
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Fatigue Life Supervision of Aircraft Structures under Corrosive Conditions
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Mechanics Characteristics and Failure Criteria of Concrete Confined by One-Way Lateral Stress after Suffering High Temperature
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Fatigue Assessment of High Loaded Bolted Bar Connection Using Strain-Life Approach
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Tensile Response and Fracture Process of High-Performance Hybrid Fiber-Reinforced Cement Composites
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Fatigue Test on a Full Scale Panel
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HomeKey Engineering MaterialsKey Engineering Materials Vols. 324-325Fatigue Life Supervision of Aircraft Structures...

Fatigue Life Supervision of Aircraft Structures under Corrosive Conditions

Abstract:

To consider the corrosive effects on aircraft structural life under natural environments, we have the calendric life to represent its impact. A new concept of Aircraft Structural Life Envelope (ASLE) to consider the combined effects of fatigue loads and corrosive conditions is developed and the sketch of ASLE is presented, then the basic determining methods of ASLE under different corrosive conditions are obtained too. Finally the linear damage cumulative rules are employed to analyze the usage of aircraft in different corrosive conditions, and the residual fatigue life and calendric life of aircraft structures can be predicted and supervised.