Design aspects in small aircraft gas turbine fuel injectors

K Mccaldon; L. A. Prociw; P. Sampath

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NASA NTRS · 19940024761

Design aspects in small aircraft gas turbine fuel injectors

K Mccaldon·L. A. Prociw·P. Sampath

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Abstract

The 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.

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K Mccaldon, L. A. Prociw, P. Sampath. 1993-09-01. Design aspects in small aircraft gas turbine fuel injectors. https://ntrs.nasa.gov/citations/19940024761

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