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Design aspects in small aircraft gas turbine fuel injectorsThe causes of fuel injector spray deterioration and the effects of this deterioration on engine durability and performance are discussed. Small aircraft gas turbine fuel injectors present special design challenges due to low fuel flow rates involved and the physical size limitations. The principal fuel injector performance requirements are discussed in relation to their effect on the hydraulic, aerodynamic, and thermal design of aerating fuel injectors.
Document ID
19940024761
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
External Source(s)
https://www.sto.nato.int/document/fuels-and-combustion-technology-for-advanced-aircraft-engines/
Authors
K Mccaldon (Pratt & Whitney Canada (Canada) Longueuil, Canada)
L. A. Prociw (Pratt & Whitney Canada (Canada) Longueuil, Canada)
P. Sampath (Pratt & Whitney Canada (Canada) Longueuil, Canada)
Date Acquired
August 16, 2013
Publication Date
September 1, 1993
Publication Information
Publication: AGARD, Fuels and Combustion Technology for Advanced Aircraft Engines
Publisher: North Atlantic Treaty Organization
ISBN: 92-835-0719-3
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AGARD-CP-536
AD-A275679
Meeting Information
Meeting: The Propulsion and Energetics Panel 81st Symposium
Location: Fiuggi
Country: IT
Start Date: May 10, 1993
End Date: May 14, 1993
Sponsors: North Atlantic Treaty Organization
Accession Number
94N29264
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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IDRelationTitle19940024743Collected WorksFuels and Combustion Technology for Advanced Aircraft Engines [Les Propergols et les Systèmes de Combustion pour les Moteurs d'Aéronefs]
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