Mechanics Analysis and Optimized Design of Aircraft Skin Pass Damage Repair

Abstract:

Against the sticking patch design problems of pass damage of aircraft skin repair, by using the calculation method of mechanical analysis, the stress analysis of pass damage is completed. The calculation methods are used quantitatively to determine the sticking patch dimension of pass damage repair, which is compared with analysis sticking patch design method calculated by the repair empirical equation of aircraft skin of Airline Company. The reason of error is analyzed and the measure to correct empirical equation method is put forward. The optimization of the critical parameters of pass damage empirical equation is completed.

• Periodical: Advanced Materials Research (Volumes 945-949)
• Pages: 306-309
• DOI: https://doi.org/10.4028/www.scientific.net/AMR.945-949.306
• Online since: June 2014
• Authors: Ting Jian Dong, Jin Chen*, Hua Peng Ding
• Keywords: Aircraft, Analysis of Mechanics, Optimization Design, Pass Damage, Skin Repair

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