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Evaluation and Control of an Integrated Closed Environmental Control System (ICECS) Allied-Signal Aerospace Company, AiResearchLos Angeles Div

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Edgar, Jon M., author.
Conference Name:
International Conference On Environmental Systems (1990-07-09 : Williamsburg, Virginia, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1990
Summary:
The Integrated Closed Environmental Control System (ICECS) Program included design, analysis, fabrication and testing of an advanced environmental control system concept for military aircraft. Fuel was utilized as the primary heat sink of a vapor-cycle system with ram air augmentation. Through the use of closed-loop avionics cooling and maximum use of fuel as a heat sink, reductions in bleed air use reduced environmental control system (ECS)-related fuel penalties and, as a result, reduced life-cycle costs (LCC). Additionally, by providing a drier, more stable environment for avionics, significant reliability gains have been demonstrated when compared to the baseline open-loop ECS. The overall emphasis was to verify through test the benefits of an ICECS using primarily off-the-shelf hardware
Notes:
Vendor supplied data
Publisher Number:
901237
Access Restriction:
Restricted for use by site license

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