Turbine engine combustion chamber bottom

The invention relates to a bottom wall (118) of a gas turbomachine combustion chamber. This bottom wall comprises openings (119) for mounting combustion air supply systems and holes (128) for the passage of cooling air between at least one inlet (128a) and at least one outlet of said holes. The hole...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Lunel, Romain Nicolas, Guezel, Yvan Yoann, Chapelle, François Xavier
Format: Patent
Sprache:eng
Schlagworte:
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Beschreibung
Zusammenfassung:The invention relates to a bottom wall (118) of a gas turbomachine combustion chamber. This bottom wall comprises openings (119) for mounting combustion air supply systems and holes (128) for the passage of cooling air between at least one inlet (128a) and at least one outlet of said holes. The holes (128) extend inwardly along the bottom wall with the outlet port located closer to the opening (119) adjacent to it than the inlet hole.