Conference
Thermal Modeling of a Rotating Heat Pipe Aero-Engine Nose Cone Anti-Icing System
Abstract
A new aero-engine nose cone anti-icing system using a rotating heat pipe has been proposed to replace the current method of blowing hot compressor bleed air over the nose cone surface. Here, the heat is transferred from a hot source within the engine to the nose cone through a rotating heat pipe along the central fan shaft. A compact evaporator is used at the evaporator end due to space constraints in the engine. The system is modeled as a …
Authors
Gilchrist S; Ewing D; Ching C; Brand J; Dowhan M
Volume
1
Publisher
SAE International
DOI
10.4271/2004-01-1817
Name of conference
SAE Technical Paper Series
Conference proceedings
SAE Technical Papers
ISSN
0148-7191