Research on Auxiliary Design for Repair of Aircraft Composite Structures
The development of repair program is the first part of the repair work carried out by the force repair personnel,however,the laminate material components,complex structural forms,so in the repair of pavement design,sanding size design need to have a solid theoretical basis of mechanics,material science,design complexity,theoretical analysis of the difficulty of the problem has been restricting the force of the new aircraft repair capacity of the generation and development,therefore,this dissertation is based on the structure of the laminate as the object of study,focusing on the structure of the laminate,and the repair of the new aircraft,and the repair of the new aircraft.Therefore,this thesis takes the laminate structure as the research object,focuses on the laminate structure repair rapid analysis technology,designs a set of repair program auxiliary design algorithm program,and provides strong technical support for the troops to carry out the laminate structure repair work on various types of aircraft and weapons and equipment independently.
composite structural repairrepair aid designaircraft repairrepair programme