Granted Patent B2

US 12,378,914 · App. 18/166,308 · Granted Aug 5, 2025

Inventor: Richard G Mochrie (Guildford, GB)

Assignee: ROLLS-ROYCE plc

F02C7/224F02C7/14F05D2260/213

Abstract

Claims (16)

1. A fuel management system for a gas turbine engine, the fuel management system comprising:

a fuel supply line configured to supply fuel from an inlet to a combustor of the gas turbine engine;

a recirculation line extending from a recirculation point on the fuel supply line and configured to recirculate excess fuel from the fuel supply line for resupply to the fuel supply line;

a heat exchanger configured to reject heat from a thermal load of the gas turbine engine to the excess fuel, wherein the heat exchanger is disposed on the recirculation line at a first position that is downstream of the recirculation point and upstream of the fuel supply line;

a fuel cooling device including an evaporator of a refrigerant circuit configured to receive heat from the excess fuel provided to the fuel cooling device, the fuel cooling device is disposed at a second position along the recirculation line, the second position being downstream of the first position and upstream of the fuel supply line such that the excess fuel within the recirculation line is first heated in the heat exchanger and is then cooled in the fuel cooling device before being returned to the fuel supply line; and

a fuel heating device including a condenser of the refrigerant circuit, wherein the condenser is configured to reject heat into the fuel provided to the fuel heating device, the fuel heating device is disposed on the fuel supply line between the recirculation point and the combustor.

2. The fuel management system according to claim 1 , further comprising:

a cooled fuel sensor configured to monitor a cooled fuel temperature parameter relating to a temperature of the excess fuel within the recirculation line downstream of the fuel cooling device; and

a refrigerant circuit controller configured to control the refrigerant circuit based on the monitored cooled fuel temperature parameter to maintain the temperature of the excess fuel downstream of the fuel cooling device within an excess fuel temperature target range.

3. The fuel management system according to claim 2 , wherein the excess fuel temperature target range is from 0° C. to 10° C.

4. The fuel management system according to claim 2 , further comprising a heated fuel sensor configured to monitor a heated fuel temperature parameter relating to a temperature of the fuel within the fuel supply line downstream of the fuel heating device, wherein the refrigerant circuit controller is configured to control the refrigerant circuit based on the monitored heated fuel temperature parameter to maintain the temperature of the fuel downstream of the fuel heating device below a fuel temperature threshold value.

5. The fuel management system according to claim 4 , wherein the fuel temperature threshold value is between 160° C. and 180° C.

6. The fuel management system according to claim 1 , wherein the recirculation line is configured to recirculate the excess fuel to an external reservoir via an outlet of the fuel management system, for subsequent resupply to the fuel supply line via the external reservoir.

7. The fuel management system according to claim 6 , comprising a fuel flow controller configured to:

receive an external reservoir signal relating to a temperature of fuel within the external reservoir; and

control fuel flow in the fuel management system based on the external reservoir signal.

Assignments (1)

Priority Claims (4)

Continuity (1)

References Cited (40)