COMBUSTOR PANELS WITH DIRT TOLERANT PINS

A gas turbine engine component assembly including: a first component (600) having a first surface (610) and a second surface (620) opposite the first surface; and a second component (400) having a first surface (410), a second surface (420) opposite the first surface of the second component, and a p...

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Bibliographische Detailangaben
Hauptverfasser:	KRAMER, Stephen K, LUNDGREEN, Ryan, PRENTER, Robin
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:	A gas turbine engine component assembly including: a first component (600) having a first surface (610) and a second surface (620) opposite the first surface; and a second component (400) having a first surface (410), a second surface (420) opposite the first surface of the second component, and a plurality of pin fins (430) extending away from the second surface of the second component, the first surface of the first component and the second surface of the second component defining a cooling channel (390) therebetween, wherein the plurality of pin fins extend into the cooling channel, wherein each of the plurality of pin fins have a pointed ellipse shape.