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NASA NTRS ยท 19900000112

Liquid-Flow Controller Responds To Pressure

Abstract

Mechanism controls flow of liquid in fuel-spraying head in combustion chamber responds nonlinearly to pressure of liquid. Shell of spraybar expands or contracts laterally as its internal pressure rises or falls, forcing collar down or up on entry tube. Area of window formed by slots in collar and entry tube thus increases or decreases. Drop in pressure through variable-area orifice increases much more with flow through orifice than does corresponding drop in pressure with flow through fixed-area orifice. In practical terms, lower pump pressure needed with variable orifice for given flow of liquid. Principle of operation applicable to spraying heads for other fluids.

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BibTeXRIS

Cox, George B., Jr.. 1990-03-01. Liquid-Flow Controller Responds To Pressure. https://ntrs.nasa.gov/citations/19900000112

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