NDLI: Study of advanced fuel system concepts for commercial aircraft and engines

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Study of advanced fuel system concepts for commercial aircraft and engines

Content Provider	NASA Technical Reports Server (NTRS)
Author	Hanks, D. E. Brewer, G. D. Chirivella, J. Byers, W. D. Versaw, E. F. Fogg, H. W.
Copyright Year	1983
Description	The impact on a commercial transport aircraft of using fuels which have relaxed property limits relative to current commercial jet fuel was assessed. The methodology of the study is outlined, fuel properties are discussed, and the effect of the relaxation of fuel properties analyzed. Advanced fuel system component designs that permit the satisfactory use of fuel with the candidate relaxed properties in the subject aircraft are described. The two fuel properties considered in detail are freezing point and thermal stability. Three candidate fuel system concepts were selected and evaluated in terms of performance, cost, weight, safety, and maintainability. A fuel system that incorporates insulation and electrical heating elements on fuel tank lower surfaces was found to be most cost effective for the long term.
File Size	6290920
Page Count	141
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19850010866
Archival Resource Key	ark:/13960/t6wx2756m
Language	English
Publisher Date	1983-01-01
Access Restriction	Open
Subject Keyword	Propellants And Fuels Viscosity Fuel Tanks Vapor Pressure Aircraft Performance Aircraft Design Aircraft Engines Commercial Aircraft Melting Points Thermal Stability Aircraft Fuel Systems Cost Effectiveness Electrical Resistivity Flash Point Jet Engine Fuels Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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