Helicopter Cooling, Air Cycle/Vapor Cycle Trade-Offs

840942

07/01/1984

Authors
Abstract
Content
Lift and flight capabilities of high performance helicopters are severely impaired when engine bleed air is extracted for the environmental cooling system. Current high fuel costs have necessitated fuel consumption efficiency improvement. Passenger helicopter owners have expressed need of improved ground cooling and pulldown performance. State-of-the-art cooling systems (air cycle machines and vapor cycle systems) are compared as to: (1) cooling performance, (2) installed shaft horsepower, (3) specific fuel consumption, (4) thermal diagrams, (5) psychrometrics, and (6) coefficient of performance.
These types are described by schematics, thermal diagrams and psychrometric plots. Since vapor cycle systems do not use engine bleed air, all helicopter performance is improved; flexibility of power source is also an advantage.
Meta TagsDetails
DOI
https://doi.org/10.4271/840942
Pages
14
Citation
Buckingham, R., "Helicopter Cooling, Air Cycle/Vapor Cycle Trade-Offs," SAE Technical Paper 840942, 1984, https://doi.org/10.4271/840942.
Additional Details
Publisher
Published
Jul 1, 1984
Product Code
840942
Content Type
Technical Paper
Language
English