Fuel conveying member with heat pipe

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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Details

F02C 7/224 (2006.01) F23R 3/28 (2006.01)

Patent

CA 2603410

A fuel conveying member (22, 26) in a gas turbine engine (10) includes a heat pipe (50) disposed in heat transfer communication with a fuel flow passage (40) thereof, such that heat is transferred by the heat pipe (50) from a high temperature region to a lower temperature region of the fuel flow passage (40).

L~élément de transport de carburant (22, 26) d~une turbine à gaz (10), selon l~invention, inclut un caloduc (50) installé pour transférer la chaleur vers un passage de carburant (40), de telle sorte que la chaleur est transférée par le caloduc (50) depuis une zone à température élevée vers une zone à température inférieure du passage de carburant (40).

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