GAS TURBINE ENGINE COMPONENT WITH INTEGRATED HEAT PIPE

A heat transfer apparatus for a gas turbine engine includes: a component (40) having a wall structure defining a flow bounding surface; a chamber (60) formed in the component (40), the chamber (60) including a wicking structure (64), a vapor channel (66), and a working fluid.

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Bibliographische Detailangaben
Hauptverfasser:	GERSTLER, William Dwight, MOORES, John William, RAMBO, Jeffrey Douglas, KOSTKA, James Michael
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	A heat transfer apparatus for a gas turbine engine includes: a component (40) having a wall structure defining a flow bounding surface; a chamber (60) formed in the component (40), the chamber (60) including a wicking structure (64), a vapor channel (66), and a working fluid.