The damage distribution of the same type of aircraft in similar service environments should be similar. Based on this assumption, to perform the maintenance and repair of aircraft composite structures, the damage of c...The damage distribution of the same type of aircraft in similar service environments should be similar. Based on this assumption, to perform the maintenance and repair of aircraft composite structures, the damage of composite structures in a certain type of aircraft were investigated. The time-varying damage distribution model was established and verified based on the damage of a 16-aircraft fleet. The results show that the quantitative proportions of structural damage are 74% for skin delamination, 22% for stringer delamination and 3% for stringer-skin interface debonding. The amount of structural damages increases linearly with service time while the proportion of different damages does not change. As the service time increases, the geometric parameter distribution of damage for the same type of aircraft gradually converges, which can be approximated using the same function. There are certain differences in the proportion and geometric parameter distribution of damages among different components and locations, and the differences do not change over time.展开更多
Dear Colleagues,It is my distinct honor to serve as the Honorary Chief Editor of AMEM,an international open-access journal,dedicated to serve as a platform for international exchange,and the translation of research ou...Dear Colleagues,It is my distinct honor to serve as the Honorary Chief Editor of AMEM,an international open-access journal,dedicated to serve as a platform for international exchange,and the translation of research outcomes in the field of life sciences.AMEM strives to establish itself as a high-level international academic exchange platform that brings together scientific wisdom from around the world and offers a prestigious journal for presenting research findings,and disseminating state of the art knowledge in the vibrant fields of life sciences.展开更多
文摘The damage distribution of the same type of aircraft in similar service environments should be similar. Based on this assumption, to perform the maintenance and repair of aircraft composite structures, the damage of composite structures in a certain type of aircraft were investigated. The time-varying damage distribution model was established and verified based on the damage of a 16-aircraft fleet. The results show that the quantitative proportions of structural damage are 74% for skin delamination, 22% for stringer delamination and 3% for stringer-skin interface debonding. The amount of structural damages increases linearly with service time while the proportion of different damages does not change. As the service time increases, the geometric parameter distribution of damage for the same type of aircraft gradually converges, which can be approximated using the same function. There are certain differences in the proportion and geometric parameter distribution of damages among different components and locations, and the differences do not change over time.
文摘Dear Colleagues,It is my distinct honor to serve as the Honorary Chief Editor of AMEM,an international open-access journal,dedicated to serve as a platform for international exchange,and the translation of research outcomes in the field of life sciences.AMEM strives to establish itself as a high-level international academic exchange platform that brings together scientific wisdom from around the world and offers a prestigious journal for presenting research findings,and disseminating state of the art knowledge in the vibrant fields of life sciences.
