GAS TURBINE ENGINE FUEL FEED SYSTEM Russian patent published in 2013 - IPC F02C9/26 

Abstract RU 2476702 C2

FIELD: engines and pumps.

SUBSTANCE: proposed system comprises electrically driven fuel pump fuel feed main line communicated with pump outlet with booster-shutoff valve or means to distribute fuel among atomiser manifold, and additional line communicating pump inlet with its outlet. Proposed fuel pump is a displacement pump with fuel feed amount varied by varying electric drive rpm. Extra pipeline is provided with fuel constant flow valve composed of jet arranged in said line and spring-loaded control slide valve. Jet inlet and outlet are communicated with slide valve free and spring-loaded chambers. Slide valve groove edge and slide valve sleeve orifice make variable-section channel in said extra line.

EFFECT: higher accuracy of fuel proportioning, fuel bleeding for engine fuel system components.

2 cl, 2 dwg

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RU 2 476 702 C2

Authors

Pavljuk Evgenij Viktorovich

Kravchenko Jurij Ignat'Evich

Matusevich Vladimir Anatol'Evich

Popov Viktor Vasil'Evich

Kononykhin Aleksandr Vladimirovich

Dates

2013-02-27Published

2011-01-13Filed