A New Non-Destructive Testing Method Used in the Axle of Landing Gear

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The relations between stresses and leakage magnetic signal of concentration area of the airplane’s landing gear under varying load were studied. The finite element method was used to calculate the stress of axle under different conditions; An experiment was designed to simulate the stress status under the bending moment, the slight magnetic signals on specimen were measured, and the relation of the signals and stress was studied. The new testing method was explained with the theory of ferromagnetic and the significance of this technique for detecting defects of the airplane structural part was discussed. The safety of airplane’s main bearing parts plays an important role during its operation and it often comes to bad situation of fatigue damage for stress concentration [1, 2]. To prevent the breaking down of structural parts and get rid of big accidents, it becomes important and necessary to find out the early concentration and damage zone, and to make some certain examination of damage and stress status [3]. The method of magnetic memory testing would be effective for the confirming of stress concentration zone in the equipment or structural parts, and could lead the way ahead the matters of fatigue analysis, evaluation of equipment life and technological design. The method can detect the endurance failure of the airplane’s undercarriage shaft, which is composed of ferromagnetic materials, and that provides the experimental basis for the prevention of parts’ fatigue defects.

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1150-1154

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July 2011

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© 2011 Trans Tech Publications Ltd. All Rights Reserved

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[1] REN Jilin; Song Kai. Application of Magnetic Memory Testing To The Inspection of The Langing Gear of Airplane ,J. Nonde Structive Testing, 2002, 24(8): 346-351.

Google Scholar

[2] REN Jilin; SONG Kai. Application of Magnetic Memory Testing in Ferromagnetic Aero Structure ,J. Aeronautical Manufacturing Technology, 2005, (1): 80-83.

Google Scholar

[3] GENG Rongsheng. Magnetic Memory Inspection: Its Application To The Detection of Early Damages of Aircraft Main Stuctures ,J. Nonde Structive Testing, 2002, 24 (3): 118-122.

Google Scholar

[4] JI Qian. Research on Fatigue Reliability Analysis Method of Aircraft Landing Gear,D. Nanjing University of Aeronautics & Astronautics, (2007).

Google Scholar

[5] WU Hai-jun; YAO Wei. Experimental Study on Dynamic Mechanical Properties of Ultrahigh Strength 30CrMnSiNi2A Steel,J. Transactions of Beijing Institute of Technology, 2010, 3(30): 258-263.

Google Scholar

[6] A.A. Dubov. Metal magnetic memory method~ A new direction of the diagnostic of equipment and metal structure ,J. Detect and Diagnostics, 2000, (11): 157-162.

Google Scholar

[7] D.C. Jiles and D. L. Atherton, Theory of the magnetization process in ferromagnets and its application to the magnetomechanical effect. Appl. Phys. 6, 17 (1984).

DOI: 10.1088/0022-3727/17/12/516

Google Scholar

[8] DING Hui; ZHANG Han. The Theoretical Model for Detecting Cracks By Metal Magnetic Memory Technique ,J. Nonde Structive Testing, 2002, 24(2): 78-80.

Google Scholar