Regenerative engine analysis program. Final study report Oct 1979-Jul 1980
Technical Report
·
OSTI ID:6014802
A parametric cycle analysis and a preliminary recuperator design study were conducted for a 500-hp intermediate rated power (IRP) recuperative helicopter engine. The U-tube recuperator with airflow inside the tubes and single cross flow gas path was found to be the lightest design in the .6 - .8 effectiveness range considered for the cycle analysis.
- Research Organization:
- Avco/Lycoming, Stratford, CT (USA)
- OSTI ID:
- 6014802
- Report Number(s):
- AD-A-095144
- Country of Publication:
- United States
- Language:
- English
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Related Subjects
32 ENERGY CONSERVATION, CONSUMPTION, AND UTILIZATION
320201 -- Energy Conservation
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33 ADVANCED PROPULSION SYSTEMS
330103* -- Internal Combustion Engines-- Turbine
AIRCRAFT
DESIGN
EFFICIENCY
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320201 -- Energy Conservation
Consumption
& Utilization-- Transportation-- Air & Aerospace
33 ADVANCED PROPULSION SYSTEMS
330103* -- Internal Combustion Engines-- Turbine
AIRCRAFT
DESIGN
EFFICIENCY
ENERGY CONSUMPTION
ENGINES
FUEL CONSUMPTION
HEAT EXCHANGERS
PARAMETRIC ANALYSIS
PERFORMANCE
WEIGHT