The effects of a number of metals and alloys on the thermal stability of Avtur 50 have been evaluated from ASTM‐CRC and high temperature coker tests. The materials tested are used in current aircraft fuel systems or are possible alternatives for fuel systems of supersonic aircraft where they will be in contact with hot fuel. The alloys currently used in aircraft fuel systems have been classified and their probable effects on the stability of hot fuel listed. A number of the materials affected stability adversely, particularly alloys containing significant amounts of copper, and the use of these should be avoided. The pick‐up of copper by Avtur 50 at ambient temperature from alloys such as brass and gun‐metal has also been investigated. The results indicated that sufficient copper to affect thermal stability adversely is readily picked up from these alloys.
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Review Article|
April 01 1967
The Effect of Metals and Alloys on the Thermal Stability of Avtur 50: An evaluation of the effects of the materials used in fuel distribution systems on the thermal stability of the fuel and their importance in relation to supersonic transport requirements
J.D. Smith
J.D. Smith
“Shell” Research Ltd., Thornton Research Centre, Chester
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Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1967
Aircraft Engineering (1967) 39 (4): 19–26.
Citation
Smith J (1967), "The Effect of Metals and Alloys on the Thermal Stability of Avtur 50: An evaluation of the effects of the materials used in fuel distribution systems on the thermal stability of the fuel and their importance in relation to supersonic transport requirements". Aircraft Engineering, Vol. 39 No. 4 pp. 19–26, doi: https://doi.org/10.1108/eb034253
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