Accession Number : AD0848566
Title : High Temperature Hydrocarbon Fuels Research in an Advanced Aircraft Fuel System Simulator on Fuel AFFB-10-67.
Descriptive Note : Fuel Series rept. no. 3, 3 Oct 67-19 Nov 68,
Corporate Author : NORTH AMERICAN ROCKWELL CORP LOS ANGELES CA LOS ANGELES DIV
Personal Author(s) : Goodman, Harold ; Bradley, Royce ; Sickles, Theodore
Report Date : FEB 1969
Pagination or Media Count : 177
Abstract : At elevated temperatures, hydrocarbon jet fuels tend to form deposits which decrease heat exchanger efficiency and plug screens and filter elements. In order to quantify this tendency so that it may be predicted, it is necessary to obtain comparative test results on a simulated aircraft fuel system and small-scale test devices. In this report, the thermal stability of a fuel tested in the Advanced Aircraft Fuel System Simulator is quantified in terms of the amount of deposit formed. The quantification of deposit formation is determined under cyclic conditions (mission profiles) and two types of steady state test conditions (steady-state and steady-state-varied flow). (Author)
Descriptors : (*JET ENGINE FUELS, DEPOSITS), HYDROCARBONS, FUEL CONTAMINATION, TEST METHODS, VIBRATION, CHEMICAL ANALYSIS, THERMAL STABILITY, CHEMICAL PRECIPITATION.
Subject Categories : Fuels
Distribution Statement : APPROVED FOR PUBLIC RELEASE