F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
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).
Prociw Lev Alexander
Shafique Harris
Ogilvy Renault Llp/s.e.n.c.r.l.,s.r.l.
Pratt & Whitney Canada Corp.
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