1964-01-01

A Lightweight Universal Fuel Control for Aircraft Turbine Engines 640423

This paper examines some of the background that has led to the requirements for a lightweight universal fuel control for aircraft gas turbine engines. One design solution for this type of fuel control is reviewed with regard to function, adaptability, maintenance, and cost.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 18% off list price.
Login to see discount.
Special Offer: Download multiple Technical Papers each year? TechSelect is a cost-effective subscription option to select and download 12-100 full-text Technical Papers per year. Find more information here.

Due to current capacity constraints, printed versions of our publications - including standards, technical papers, EDGE Reports, scholarly journal articles, books, and paint chips - may experience shipping delays of up to four to six weeks. We apologize for any inconvenience.
We also recommend:
TECHNICAL PAPER

THE CASE FOR TURBINES IN SMALL AIRCRAFT

520149

View Details

TECHNICAL PAPER

Control System Requirements and Considerations for High Temperature Engines

700823

View Details

TECHNICAL PAPER

High Temperature Turbine Design Considerations

710462

View Details

X