초록 ▼

A fuel conveying member in a fuel system of a gas turbine engine includes a heat pipe disposed in heat transfer communication with a fuel flow passage of the fuel conveying member, such that heat is transferred by the heat pipe from a high temperature region to a lower temperature region of the fuel

A fuel conveying member in a fuel system of a gas turbine engine includes a heat pipe disposed in heat transfer communication with a fuel flow passage of the fuel conveying member, such that heat is transferred by the heat pipe from a high temperature region to a lower temperature region of the fuel flow passage. The heat pipe has a constant mass or working fluid enclosed within a sealed chamber in heat transfer communication with fuel in said fuel flow passage, said working fluid being self-circulating in a fluid flow having a liquid portion and a vapor portion, said working fluid passively boiling, flowing and condensing to transfer heat from said high temperature region to said lower temperature region.

대표청구항 ▼

The invention claimed is: 1. A gas turbine engine internal fuel manifold comprising at least one fuel flow passage and at least one heat pipe mounted to the fuel manifold, the heat pipe being adapted to transfer heat from a high temperature region of said fuel flow passage to a lower temperature re

The invention claimed is: 1. A gas turbine engine internal fuel manifold comprising at least one fuel flow passage and at least one heat pipe mounted to the fuel manifold, the heat pipe being adapted to transfer heat from a high temperature region of said fuel flow passage to a lower temperature region of the engine, said heat pipe comprising a constant mass of working fluid enclosed within a sealed chamber in heat transfer communication with fuel in said fuel flow passage, said working fluid being self-circulating in a fluid flow having a liquid portion and a vapour portion, the said working fluid passively boiling, flowing and condensing to transfer heat from said high temperature region to said lower temperature region. 2. The gas turbine engine internal fuel manifold as defined in claim 1, wherein said lower temperature region is a lower temperature region of the manifold. 3. The gas turbine engine internal fuel manifold as defined in claim 1, wherein said heat pipe is annular and has an evaporator portion and a condenser portion defined at diametrically opposed portions of the manifold. 4. The gas turbine engine internal fuel manifold as defined in claim 1, wherein the heat pipe includes a wicking member disposed along at least one inner surface of a working fluid chamber defined in the heat pipe, said wicking member being adapted to transport said working fluid in a liquid phase from a condenser portion to a evaporator portion of said heat pipe. 5. The gas turbine engine internal fuel manifold as defined in claim 1, wherein said heat pipe is disposed within said manifold. 6. A fuel conveying member in a gas turbine engine, the fuel conveying member comprising at least one fuel flow passage having a high temperature region and a lower temperature region thereof, and a heat pipe being disposed in heat transfer communication with said fuel flow passage and extending between said high and low temperature regions said heat pipe containing working fluid enclosed within a sealed chamber in heat transfer communication with fuel in said fuel flow passage, said working fluid being self-circulating in a fluid flow having a liquid portion and a vapour portion, said working fluid passively boiling, flowing and condensing to transfer heat from said high temperature region to said lower temperature region. 7. The fuel conveying member as defined in claim 6, wherein said heat pipe includes an internal wicking member extending from a portion of the heat pipe at which the working fluid pools to an evaporator portion of the heat pipe. 8. The fuel conveying member as defined in claim 6, wherein said fuel conveying member includes at least one of a fuel manifold and a fuel nozzle. 9. The fuel conveying member as defined in claim 6, wherein said heat pipe is annular.