Combustion chamber of a turbomachine

Combustion chamber of a turbomachine

The turbomachine has an annular combustion chamber (48) with internal and external radial rotation walls (24, 26) connected at their upstream ends by an annular chamber bottom (28) that supports fuel injectors (38). Suspension units suspend an upstream end of the chamber to an external case (18), an...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: VUILLEMENOT, YANN, FRANÇOIS, JEAN-CLAUDE, HERNANDEZ, DIDIER, HIPPOLYTE, DUVAL, SYLVAIN, COMMARET, PATRICE, ANDRÉ
Format: Patent
Sprache:eng ; fre ; ger
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 turbomachine has an annular combustion chamber (48) with internal and external radial rotation walls (24, 26) connected at their upstream ends by an annular chamber bottom (28) that supports fuel injectors (38). Suspension units suspend an upstream end of the chamber to an external case (18), and include a connecting rod (50) whose ends are articulated on the wall (26) of the chamber and on the external case. Downstream ends of the walls are respectively connected to an internal case (14) and the external case by two annular flanges.