Skip to Main Content
Skip Nav Destination
ASME Press Select Proceedings
International Conference on Mechanical and Electrical Technology, 3rd, (ICMET-China 2011), Volumes 1–3
By
Yi Xie
Yi Xie
Search for other works by this author on:
ISBN:
9780791859810
No. of Pages:
906
Publisher:
ASME Press
Publication date:
2011

An air cycle refrigeration system that transferred large heat to environment was proposed, which was on account of more and more heat produced by avionics. It used fuel as main heat sink, and enhanced heat transfer of liquid-cooled heat exchanger by reduced turbine inlet temperature. Dynamic characteristics of system were investigated on Flowmaster simulation platform, meanwhile, fuel penalty was calculated with the method of take-off gross weight. The results show that this new system satisfies requirements of aircraft and decreases ratio of fuel penalty caused by engine bleed air. It makes sense to guide the development of traditional air cycle refrigeration system.

Abstract
Key Words
1 Introduction
2. Mathematical Model
3 Results and Discussion
4. Summaries
References
This content is only available via PDF.
You do not currently have access to this chapter.
Close Modal

or Create an Account

Close Modal
Close Modal