Noncircular transient fluid fuel injector control channels...

Power plants – Reaction motor – Liquid oxidizer

Reexamination Certificate

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C060S734000

Reexamination Certificate

active

07958719

ABSTRACT:
A fuel injector system for combustion engines and motors, such as pulsed bipropellant thrusters, includes noncircular fuel and oxidizer injectors at the ends of respective dribble channels for controlling the mixture ratio of the propellants passing into a combustion chambers for maintaining a desire or ideal mixture ratio as determined by the cross-sectional area of the injectors well suited for pulse combustion fuel injector systems.

REFERENCES:
patent: 2476185 (1949-07-01), Goddard
patent: 2709887 (1955-06-01), Goddard
patent: 3190070 (1965-06-01), Neu
patent: 3423942 (1969-01-01), Spindler
patent: 4894986 (1990-01-01), Etheridge
patent: 7640726 (2010-01-01), Fang et al.

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