GASEOUS HYDROGEN AND OXYGEN THRUSTER WITH SLOT NOZZLE Russian patent published in 2017 - IPC F02K9/62 

Abstract RU 2624419 C1

FIELD: engines and pumps.

SUBSTANCE: gaseous hydrogen and oxygen thruster consisting of an engine head, a fuel spark plug, a system of fuel supply to a combustion chamber and of internal combustion chamber cooling, while the slot nozzle is installed to supply an oxidizer into the combustion chamber and direct the oxidizer to the motor axis.

EFFECT: invention promotes intensive mixing of hydrogen and oxygen and their more complete combustion.

1 dwg

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RU 2 624 419 C1

Authors

Gradov Vitalij Nikolaevich

Ryzhkov Vladimir Vasilevich

Dates

2017-07-03Published

2016-10-03Filed