Fuel and oil heat management system for a gas turbine engine

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

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F02C 7/06 (2006.01) F01D 25/18 (2006.01) F02C 7/14 (2006.01) F02C 7/22 (2006.01) F02C 7/224 (2006.01)

Patent

CA 1273212

ABSTRACT FUEL AND OIL HEAT MANAGEMENT SYSTEM FOR A GAS TURBINE ENGINE A heat management system is provided for a gas turbine engine (10) having first and second oil cooling loops (14, 16). The system distributes excess fuel flow from a main fuel pump (44) among a plurality of upstream locations (58, 60, 68) for managing the transfer of heat between the oil loops (14, 16) and the flowing fuel. A diverter valve (62) regulates the distribution of the bypass fuel responsive to engine heat generation, oil temperature, and/or fuel temperature. A passive fuel distribution configuration using one or more fuel flow restrictors (72, 74, 76) is also disclosed.

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