Integrated Engine Inlet Thermal Anti-Icing and Environmental Control System (TAI/ECS)

760517

02/01/1976

Event
National Air Transportation Meeting
Authors Abstract
Content
The integrated engine inlet thermal anti-icing and environmental control system (TAI/ECS) for subsonic transport airplanes was conceived primarily for the efficient use of available energy and minimum engine bleed air extraction. The concept employs the engine inlet leading edge as the heat exchanger to provide ice protection for the engine inlet surfaces and to cool bleed air for the environmental control system. The results of a study conducted for a typical wide-body airplane using high bypass ratio engines show that the system concept will result in potential improvements in airplane operation and engine maintenance.
Meta TagsDetails
DOI
https://doi.org/10.4271/760517
Pages
6
Citation
Shah, A., "Integrated Engine Inlet Thermal Anti-Icing and Environmental Control System (TAI/ECS)," SAE Technical Paper 760517, 1976, https://doi.org/10.4271/760517.
Additional Details
Publisher
Published
Feb 1, 1976
Product Code
760517
Content Type
Technical Paper
Language
English