COMBUSTION CHAMBER FOR GAS TURBINE ENGINE

COMBUSTION CHAMBER FOR GAS TURBINE ENGINE

FIELD: gas turbine engine engineering. ^ SUBSTANCE: combustion chamber comprises housing provided with inner and outer ring shells, device for graduate change of the ratio of areas of the cross-sections of primary and secondary passages, and collector stabilizer. The reaction zone has shutters and i...

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Hauptverfasser: PERESLAVTSEV ANDREJ VIKTOROVICH, MAJATSKIJ SERGEJ ALEKSANDROVICH, PRONIN ALEKSEJ JUR'EVICH, SHAPKO IVAN VITAL'EVICH
Format: Patent
Sprache:eng ; rus
Schlagworte:
BLASTING
COMBUSTION APPARATUS
COMBUSTION PROCESSES
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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creator PERESLAVTSEV ANDREJ VIKTOROVICH
MAJATSKIJ SERGEJ ALEKSANDROVICH
PRONIN ALEKSEJ JUR'EVICH
SHAPKO IVAN VITAL'EVICH
description FIELD: gas turbine engine engineering. ^ SUBSTANCE: combustion chamber comprises housing provided with inner and outer ring shells, device for graduate change of the ratio of areas of the cross-sections of primary and secondary passages, and collector stabilizer. The reaction zone has shutters and inserts that define inner and outer rings. The shutters and inserts are pivotally interconnected for permitting change of the area of the cross-section in radial direction. The collector stabilizer is unmovable. ^ EFFECT: enhanced reliability. ^ 4 dwg
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language eng ; rus
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subjects BLASTING
COMBUSTION APPARATUS
COMBUSTION PROCESSES
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
title COMBUSTION CHAMBER FOR GAS TURBINE ENGINE
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