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Dynamic Thermal Management System Modeling of a More Electric Aircraft
Technical Paper
2008-01-2886
ISSN: 0148-7191, e-ISSN: 2688-3627
Annotation ability available
Sector:
Event:
Power Systems Conference
Language:
English
Abstract
Advancements in electrical, mechanical, and structural design onboard modern more electric aircraft have added significant stress to the thermal management systems (TMS). A thermal management system level analysis tool has been created in MATLAB/Simulink to facilitate rapid system analysis and optimization to meet the growing demands of modern aircraft. It is anticipated that the tracking of thermal energy through numerical integration will lead to more accurate predictions of worst case TMS sizing conditions. In addition, the non-proprietary nature of the tool affords users the ability to modify component models and integrate advanced conceptual designs that can be evaluated over multiple missions to determine the impact at a system level.
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Authors
- K. McCarthy - P.C. Krause and Associates, Inc.
- E. Walters - P.C. Krause and Associates, Inc.
- A. Heltzel - P.C. Krause and Associates, Inc.
- R. Elangovan - Boeing
- G. Roe - Boeing
- W. Vannice - Boeing
- C. Schemm - Lockheed Martin
- J. Dalton - Avetec
- S. Iden - USAF
- P. Lamm - USAF
- C. Miller - USAF
- A. Susainathan - USAF
Topic
Citation
McCarthy, K., Walters, E., Heltzel, A., Elangovan, R. et al., "Dynamic Thermal Management System Modeling of a More Electric Aircraft," SAE Technical Paper 2008-01-2886, 2008, https://doi.org/10.4271/2008-01-2886.Also In
References
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