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Integrated Electrical and Thermal Management Sub-system Optimization
Technical Paper
2010-01-1812
ISSN: 0148-7191, e-ISSN: 2688-3627
Annotation ability available
Sector:
Event:
Power Systems Conference
Language:
English
Abstract
Air vehicle subsystems are moving towards more electric actuation and more electric architectures. This has resulted in transient electrical power demands that require high fidelity simulations to accurately predict the peak system electrical loads. In addition, the high power electronics necessary to drive more electric system devices are generating additional heat loads, resulting in increasing demands on thermal management system performance. Consequently, integrated system simulations and the capability to optimize integrated electrical / thermal management systems are becoming necessary at earlier stages in the design cycle. LM Aeronautics has developed a MATLAB / Simulink / SimPowerSystems based toolbox for rapid modeling of thermal and electrical subsystems. Use of this toolbox for simulating and optimizing an integrated thermal / electrical subsystem is demonstrated.
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Authors
Topic
Citation
Bodden, D., Eller, B., and Clements, S., "Integrated Electrical and Thermal Management Sub-system Optimization," SAE Technical Paper 2010-01-1812, 2010, https://doi.org/10.4271/2010-01-1812.Also In
References
- Mil-E-7016F Military Specification: Electrical Load and Power Source Capacity Aircraft 20 July 1976
- Ueda, J. Daniszewski, D. Monroe, J. Masrur, A. et.al. “Electrical Modeling and Simulation with MATLAB/Simulink and Graphical User Interface Software,” SAE Technical Paper 2006-01-3039 2006 10.4271/2006-01-3039
- Amrhein, M. Wells, J. Walters, E. Matasso, A. et.al. “Integrated Electrical System Model of a More Electric Aircraft Architecture,” SAE Technical Paper 2008-01-2899 2008 10.4271/2008-01-2899
- “Simulink Design Optimization 1.1.1.” MathWorks 11 August 2010 http://www.mathworks.com/products/sl-design-optimization/index.html