Combined with existing software and hardware resources
integrative simulation platform for aero-engine digital electronic control system
which mainly includes aeroengine model subsystem
signal simulation and processing subsystem
controller rapid prototyping subsystem was designed with modular approach.Aero-engine model subsystem acts as a numerical simulation platform that calls aero-engine mathematical model library and mechanical hydraulic actuator mathematical model library.Rapid prototyping subsystem for controller runs in Matlab/Simulink environment
in which control code encapsulated into S-Function module.As key techniques in platform software design
mixed programming and WINDOWS timer programming method were described in detail.Applying the platform to a turbofan control system researchment
numerical simulation
semi-physical simulation and bed test results are consistent.It shows the platform is feasible and effective in engineering.
Development path and future trend of carrier-based advanced trainer engine
Thermal protection effectiveness of thermal barrier coatings in turbine blade applications
Aero-engine cycle design approach for multiple operating conditions performance reliability
Relationship between rotor/vanes blade number andnodal diameter number of bladed-disk coupling vibration
ptimum design of rotor structure layout and its mechanical properties
Related Author
PENG Yunlong
WU Xiong
DING Ting
ZHU Jianqin
ZHAO Chaofan
QIU Lu
曹大录
白广忱
Related Institution
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics