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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Bibliographische Detailangaben
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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Beschreibung
Zusammenfassung:	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.