A test unit has been developed by Rolls-Royce for the U.S. Navy to use in evaluating fuel thermal deposition typically found in various aircraft engine components. Although the current Jet Fuel Thermal Oxidation Tester (JFTOT) provides a qualitative thermal stability evaluation, it may not be able to predict in-service problems. Conditioning and testing of the fuel under realistic conditions is crucial if one is to predict deposit formations accurately. Engine fuel deposit evaluations and evidence from unpublished Rolls-Royce laboratory rig tests were used to help design a test unit that would address fuel stability problems in current or future aircraft. The Aviation Fuel Thermal Stability (AFTS) test unit embodies test modules that were selected with extensive fuel systems experience to enable the evaluation of thermal deposition in various fuel components using properly conditioned fuel. The test modules are controlled and results are recorded by a computer. This paper includes a review of the AFTS test unit design and preliminary test results thereof.
Skip Nav Destination
Article navigation
July 1995
Research Papers
The Development of an Aviation Fuel Thermal Stability Test Unit
D. L. Daggett,
D. L. Daggett
Rolls-Royce Inc., Engineering, Atlanta, GA 30339
Search for other works by this author on:
A. Veninger,
A. Veninger
Rolls-Royce Inc., Engineering, Atlanta, GA 30339
Search for other works by this author on:
C. Lewis,
C. Lewis
Rolls-Royce PLC, Engineering, Derby, United Kingdom
Search for other works by this author on:
S. Bullock,
S. Bullock
Rolls-Royce PLC, Engineering, Derby, United Kingdom
Search for other works by this author on:
R. Kamin
R. Kamin
Aircraft Division, Naval Air Warfare Center, Trenton, NJ 08628
Search for other works by this author on:
D. L. Daggett
Rolls-Royce Inc., Engineering, Atlanta, GA 30339
A. Veninger
Rolls-Royce Inc., Engineering, Atlanta, GA 30339
C. Lewis
Rolls-Royce PLC, Engineering, Derby, United Kingdom
S. Bullock
Rolls-Royce PLC, Engineering, Derby, United Kingdom
R. Kamin
Aircraft Division, Naval Air Warfare Center, Trenton, NJ 08628
J. Eng. Gas Turbines Power. Jul 1995, 117(3): 468-474 (7 pages)
Published Online: July 1, 1995
Article history
Received:
March 8, 1994
Online:
November 19, 2007
Citation
Daggett, D. L., Veninger, A., Lewis, C., Bullock, S., and Kamin, R. (July 1, 1995). "The Development of an Aviation Fuel Thermal Stability Test Unit." ASME. J. Eng. Gas Turbines Power. July 1995; 117(3): 468–474. https://doi.org/10.1115/1.2814119
Download citation file:
Get Email Alerts
Cited By
Inter-Stage Pressure Drop of Multi-Stage Brush Seal With Differentiated Structure
J. Eng. Gas Turbines Power (July 2023)
Estimation of Wiebe Function Parameters for Syngas and Anode Off-Gas Combustion in Spark-Ignition Engines
J. Eng. Gas Turbines Power (July 2023)
Mixture Distribution in Spark Ignited Port Fuel Injection Engines: A Review
J. Eng. Gas Turbines Power (July 2023)
Related Articles
JP-8+100: The Development of High-Thermal-Stability Jet Fuel
J. Energy Resour. Technol (September,1996)
One-Dimensional Simulations of Jet Fuel Thermal-Oxidative Degradation and Deposit Formation Within Cylindrical Passages
J. Energy Resour. Technol (December,2000)
The Effects of Dissolved Oxygen Concentration, Fractional Oxygen Consumption, and Additives on JP-8 Thermal Stability
J. Eng. Gas Turbines Power (October,1997)
Fuel Deposit Characteristics at Low Velocity
J. Eng. Gas Turbines Power (July,1986)
Related Proceedings Papers
Related Chapters
Aviation Fuel Cavitation in a CD Nozzle: A Quantitative Experimental Characterization
Proceedings of the 10th International Symposium on Cavitation (CAV2018)
The Application of Computer Measurement and Control Technology in a Tester for Single-Jet Nozzles of Aero Engine
Proceedings of the International Conference on Technology Management and Innovation
Piston Aeroengines
Turbo/Supercharger Compressors and Turbines for Aircraft Propulsion in WWII: Theory, History and Practice—Guidance from the Past for Modern Engineers and Students