Fluid system
OwnerMark J. Tumelty, Christopher J. Ellansinventors
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OwnerMark J. Tumelty, Christopher J. Ellansinventors
Estimating the term…
In a fluid system for a gas turbine engine, oil is supplied from an oil tank (10) by a constant displacement pump (12) to lubricate engine components (18). The oil is supplied to the components (18) via a heat exchanger (16) in which oil and fuel are placed in direct heat exchange relationship. The flow of oil to the components (18) is controlled by recirculating a proportion of the oil flow through a bypass (20). The bypass (20) regulates the flow of oil to the components (18) so that the amount of heat transferred to the fuel in the heat exchanger (16) is controlled. At low engine powers a greater proportion of the oil flows through the bypass (20) to reduce the oil flow to the components (18). This reduces the heat transferred to the fuel in the heat exchanger (16) and so prevents overheating of the fuel.
1-14. (canceled)
A fluid system for an engine which supplies a first and a second fluid to said engine, said fluid system comprising a heat exchanger, a pump, a valve and a pump bypass wherein said first and second fluids are placed in direct heat exchange relationship, said valve being configured to regulate recirculation of a portion of said first fluid through said pump bypass in dependence upon engine running conditions, and thereby controls the temperature of the first fluid in order to control the temperature of said second fluid, wherein the flow of said first fluid to the engine is reduced by said valve to reduce the amount of heat transferred from the first fluid to the second fluid in the heat exchanger wherein said first fluid flows in a closed circuit system.
A fluid system for an engine which supplies a first and a second fluid to said engine, said fluid system comprising a heat exchanger, a pump, a valve and a pump bypass wherein said first and said second fluids are placed in direct heat exchange relationship, said valve being configured to regulate recirculation of a portion of said first fluid through said pump bypass in dependence upon engine running conditions, and thereby controls the temperature of the first fluid in order to control the temperature of said second fluid, said pump being a constant displacement pump, the output of which is regulated by recirculation of a proportion of the first fluid flow upstream of the engine to reduce the flow of said first fluid to the engine and so control the amount of heat transferred from the first fluid to the second fluid in the heat exchanger wherein said first fluid flows in a closed circuit system.
A gas turbine engine oil system for regulating heat transferred from a lubrication oil to a fuel and regulate the temperature of the lubrication oil:
Dependencies are inferred from the claim text.