COMBUSTOR WALL ELEMENT AND METHOD FOR MANUFACTURING THE SAME

Disclosed is a combustor wall element (1). The combustor wall element comprises a wall (11), the wall comprising a front surface (12) and a back surface (13). The front surface is provided on a front side (14) of the wall and the back surface is provided on a back side (15) of the wall. A through op...

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Bibliographische Detailangaben
Hauptverfasser:	MIHELIC, Goran, CANKOVIC, Damir, MAURER, Michael, FURDEK, Stevica, VRANJIC, Nikola, MARKOVIC, Alen
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	Disclosed is a combustor wall element (1). The combustor wall element comprises a wall (11), the wall comprising a front surface (12) and a back surface (13). The front surface is provided on a front side (14) of the wall and the back surface is provided on a back side (15) of the wall. A through opening (2) penetrates the wall from the front surface to the back surface. A duct (21) is provided extending from the back surface and to a back end of the combustor wall element, and said duct (21) is in fluid communication with the through opening (2). At least one cooling channel (6, 6i, 6ii) is provided inside the wall, wherein said cooling channel extends between a first open end (61) and a second open end (62). At least a section of the cooling channel (6, 6i, 6ii) extends at least essentially parallel to the front surface (12).