SYSTEMS AND METHODS FOR COMBUSTOR PANEL OF A GAS TURBINE

A combustor panel (110) of a combustor may include a combustion facing surface (112), a cooling surface (113) opposite the combustion facing surface (112), and heat transfer pins (116) extending from the cooling surface (113). A grouping (216B) of the heat transfer pins (216) may include a metallic...

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Bibliographische Detailangaben
Hauptverfasser:	QUACH, San, TU, John S, RUP JR., John J, VAN, Anthony, SELINSKY JR., Robert, SONNTAG, Robert M
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COMBUSTION APPARATUS COMBUSTION PROCESSES GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE WEAPONS
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Beschreibung
Zusammenfassung:	A combustor panel (110) of a combustor may include a combustion facing surface (112), a cooling surface (113) opposite the combustion facing surface (112), and heat transfer pins (116) extending from the cooling surface (113). A grouping (216B) of the heat transfer pins (216) may include a metallic coating (220).