ROCKET ELECTRIC ENGINE ANODE WITH CLOSED ELECTRON DRIFT Russian patent published in 2011 - IPC F03H1/00 

Abstract RU 2421630 C2

FIELD: engines and pumps.

SUBSTANCE: proposed anode comprises case, input and output commutators. Note here that input commutator is connected with isolated anode lines and has perforations to communicate it with output commutator provided with system of holes. Note also that input commutator is made up of two air-isolated commutators tightly connected with appropriate isolated anode lines. Mind that every input commutator incorporates holes to it to be communicated with output commutator.

EFFECT: reduced weight of propulsion unit, higher reliability and longer life.

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RU 2 421 630 C2

Authors

Ostrovskij Valerij Georgievich

Popov Aleksandr Nikolaevich

Dates

2011-06-20Published

2008-09-18Filed