Heat Sink Options for a More Electric Aircraft Thermal Management System

971244

06/18/1997

Event
SAE Aerospace Power Systems Conference
Authors Abstract
Content
The concept of a more electric aircraft has revolutionized the way aircraft and subsystems are being built. New components are also proving to be more efficient, resulting in the possibility of changing the way systems are cooled. Before these new concepts will be utilized, they must be evaluated to determine system level impacts. To aid in these evaluations, an engine model is developed, traditional cooling schemes system level impacts calculated, a boundary layer heat sink proposed, and several new technologies proposed for evaluation.
Meta TagsDetails
DOI
https://doi.org/10.4271/971244
Pages
5
Citation
Beam, J., "Heat Sink Options for a More Electric Aircraft Thermal Management System," SAE Technical Paper 971244, 1997, https://doi.org/10.4271/971244.
Additional Details
Publisher
Published
Jun 18, 1997
Product Code
971244
Content Type
Technical Paper
Language
English