This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Integrated Aircraft Fuel Thermal Management
Annotation ability available
Sector:
Language:
English
Abstract
Advanced military aircraft have separate airframe and engine fuel thermal management systems resulting in less than maximum use of the onboard fuel heat sink (FHS). In response, the proposed integrated configuration combines airframe and engine FHS systems, and optimizes control of engine burn fuel to nozzle temperature limits. This approach results in lower main tank fuel temperatures, less fuel boiloff, smaller environmental control systems (ECS) increased capacity at mission completion, and less supplemental ram air cooling. Three FHS systems are parametrically compared as a function of mission, heat loads, fuel control temperatures, and component performance.
Recommended Content
Technical Paper | Flexible Heat Pipe Cold Plates for Aircraft Thermal Control |
Aerospace Standard | Animal Environment in Cargo Compartments |
Authors
Topic
Citation
Hudson, W. and Levin, M., "Integrated Aircraft Fuel Thermal Management," SAE Technical Paper 860911, 1986, https://doi.org/10.4271/860911.Also In
References
- AFAPL-TR-71-79 Johnston, R. K. Monita, C. M. Kemper, W. A. “Physical and Chemical Properties of JP-4 Jet Fuel for 1970,” Southwest Research Institute 1971
- Coordinating Research Council, Inc. “Volatility Characteristics of Aircraft Fuels at Elevated Temperatures,” New York 1955
- AFAPL-TR-73-51 Gray C. N. Shayeson, M. W. “Aircraft Fuel Heat Sink Utilization,” General Electric 1973
- REP-F33615-83-R-3411 Air Force Request for Proposal - Integrated Closed Loop Environmental Control System 1983
- T.O. IF-15A-1, F-15A/B Flight Manual, U. S. Air Force 1978
- T.O. IF-16A-1, F-16A/B Flight Manual, U. S. Air Force 1984
- DPM 01-F18AAA-1, F/TF-18A Flight Manual, U. S. Navy 1979
- NASA CR-174752 Study of Advanced Fuel System Concepts for Commercial Aircraft and Engines Versaw E. F. et al Lockheed California Company 1983