Heat Sink Options for a More Electric Aircraft Thermal Management System

Document Number: 971244

Date Published: June 1997

Author(s):
Dr Jerry E Beam - Wright Laboratory

Abstract:
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.

File Size: 576K
Product Status: In Stock

See other papers presented at SAE Aerospace Power Systems Conference, April 1997, Williamsburg, VA, USA, Session: Aircraft Thermal Management Issues

Purchase more technical papers and save! With TechSelect, you decide what SAE Technical Papers you need, when you need them, and how much you want to pay. Learn more >