SYSTEME AERODYNAMIQUE A EFFERVESCENCE D'INJECTION AIR/CARBURANT DANS UNE CHAMBRE DE COMBUSTION DE TURBOMACHINE

SYSTEME AERODYNAMIQUE A EFFERVESCENCE D'INJECTION AIR/CARBURANT DANS UNE CHAMBRE DE COMBUSTION DE TURBOMACHINE

The aerodynamic injection system (2) has an air feed channel (6) to supply air to a tubular structure (4). A fuel passage (8) is connected to a fuel feed channel (10). A gas injection channel (12) injects gas into fuel feed channel at a pressure which is greater than pressure of air supplied to tubu...

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Hauptverfasser: PIKALOV VALERY, NOEL THOMAS, ORLOV VLADIMIR, ROLLIN GILLES, MANTCHENKOV IGOR, NOVIKOV ALEXANDER
Format: Patent
Sprache:fre
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 PIKALOV VALERY
NOEL THOMAS
ORLOV VLADIMIR
ROLLIN GILLES
MANTCHENKOV IGOR
NOVIKOV ALEXANDER
description The aerodynamic injection system (2) has an air feed channel (6) to supply air to a tubular structure (4). A fuel passage (8) is connected to a fuel feed channel (10). A gas injection channel (12) injects gas into fuel feed channel at a pressure which is greater than pressure of air supplied to tubular structure and greater than or equal to pressure of fuel flowing in fuel feed channel, to create effervescence in fuel. Independent claims are also included for the following: (1) turbomachine combustion chamber; and (2) turbomachine.
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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 SYSTEME AERODYNAMIQUE A EFFERVESCENCE D'INJECTION AIR/CARBURANT DANS UNE CHAMBRE DE COMBUSTION DE TURBOMACHINE
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