LOW-THRUST LIQUID-PROPELLANT ROCKET ENGINE SPRAY ATOMISER Russian patent published in 2016 - IPC F02K9/62 

Abstract RU 2576765 C2

FIELD: engines and pumps.

SUBSTANCE: claimed jet atomiser consists of a body, a working fluid feed channel and a nozzle. The turbulence promoter composed by a cylindrical wire spiral is arranged in the working fluid channel, immediately ahead of the nozzle. The said spiral features the pitch equal to the wire diameter.

EFFECT: reduced jet range and reliable mixing of fuel components.

2 cl, 1 dwg

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RU 2 576 765 C2

Authors

Andreev Jurij Zakharovich

Dates

2016-03-10Published

2013-03-29Filed