02 - Systems Engineering and Integration
APPLICATION OF MBSE IN AERO-ENGINE STRUCTURAL PARAMETER CALCULATING SYSTEM
Y.X. Che, Liaoning, China
Because of the high complexity of aero-engine structural parameters calculation system, the traditional text-based system engineering method can not fully meet the development of aero-engine structural parameters calculation system. A model-based system engineering method is introduced into the development of aero-engine structural parameters calculation system. In order to improve R&D efficiency, reduce R&D cost and shorten R&D cycle, the requirements are fully analyzed in the concept stage of the project, and the software tools are used for modeling, simulation and design analysis to verify and confirm the requirements. The application of model-based system engineering method in an aero-engine structural parameter calculation system is experimented. The necessity and feasibility of applying model-based system engineering theory to aero-engine structural parameter calculation system are proved.