Combustor swirler and method of manufacturing same

A combustor swirler for a gas turbine engine and method of manufacturing by injection moulding an inner component and an outer cylindrical component. Indentations are moulded in of the inner and outer component and sealed by the engagement of the components together to form a series of fluid flow pa...

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Bibliographische Detailangaben
Hauptverfasser: SHAFIQUE HARRIS, PROCIW LEV A, KOJOVIC ALEKSANDER
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A combustor swirler for a gas turbine engine and method of manufacturing by injection moulding an inner component and an outer cylindrical component. Indentations are moulded in of the inner and outer component and sealed by the engagement of the components together to form a series of fluid flow passages.