IP Library Granted Patent US 12,723,521
Granted Patent B2
US 12,723,521 · App. 19/448,816 · Granted Sep 1, 2026

Liquid fluid systems for turbine engines

Inventors: Arthur William Sibbach (Boxford, MA); Brandon Wayne Miller (Evendale, OH)
Assignee: GENERAL ELECTRIC COMPANY
F01D21/003F02C9/28H03H9/0009H03H9/0014F05D2270/3015F05D2270/303F05D2270/333F05D2270/804
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Quick Facts
Patent No.
US 12,723,521
App. No.
19/448,816
Granted
Sep 1, 2026
Kind
B2
Abstract

A method of operating a thermal management system associated with a turbine engine includes circulating a pericritical fluid through a cooling circuit; generating a sensor output using a phase detection sensor in fluid communication with the pericritical fluid, the sensor output including an impedance value; determining that the pericritical fluid has reached a bubble point based at least on a first characteristic change in the impedance value; determining that the pericritical fluid has reached a dew point based at least on a second characteristic change in the impedance value, the second characteristic change being different from the first characteristic change; and controlling at least one controllable component of the thermal management system based at least on the bubble point and the dew point.

Claims (37)

1 . A method of operating a thermal management system associated with a turbine engine, the method comprising:

circulating a pericritical fluid through a cooling circuit;

generating a sensor output using a phase detection sensor in fluid communication with the pericritical fluid, the sensor output including an impedance value;

determining that the pericritical fluid has reached a bubble point based at least on a first characteristic change in the impedance value;

determining that the pericritical fluid has reached a dew point based at least on a second characteristic change in the impedance value, the second characteristic change being different from the first characteristic change; and

controlling at least one controllable component of the thermal management system based at least on the bubble point and the dew point.

2 . The method of claim 1 , wherein the first characteristic change comprises an increase in the impedance value by a first amount, and wherein the second characteristic change comprises an increase in the impedance value by a second amount that is greater than the first amount.

3 . The method of claim 1 , further comprising determining that the impedance value is above an upper threshold value, below a lower threshold value, or within a range between the upper threshold value and the lower threshold value.

4 . The method of claim 1 , further comprising determining that a rate of change of the impedance value is above an upper threshold rate of change value or below a lower threshold rate of change value.

5 . The method of claim 1 , further comprising determining that the pericritical fluid has reached a critical point when the impedance value is about zero.

6 . The method of claim 1 , wherein the impedance value exhibits multiple inflection points, and wherein the multiple inflection points correspond to a component part of a bimodal fluid or a component part of a multimodal fluid.

7 . The method of claim 1 , further comprising determining one or more additional phase properties of the pericritical fluid based on the sensor output and at least one of a look-up table or a model.

8 . A pericritical fluid system for a thermal management system associated with a turbine engine, the pericritical fluid system comprising:

a cooling circuit configured to circulate a pericritical fluid;

a phase detection sensor configured to generate a sensor output including an impedance value corresponding to the pericritical fluid; and

a controller communicatively coupled to the phase detection sensor, the controller configured to:

determine that the pericritical fluid has reached a bubble point based at least on a first characteristic change in the impedance value;

determine that the pericritical fluid has reached a dew point based at least on a second characteristic change in the impedance value, the second characteristic change being different from the first characteristic change; and

control at least one controllable component of the thermal management system based at least on the bubble point and the dew point.

9 . The pericritical fluid system of claim 8 , wherein the controller is further configured to determine that the first characteristic change comprises an increase in the impedance value by a first amount and that the second characteristic change comprises an increase in the impedance value by a second amount that is greater than the first amount.

10 . The pericritical fluid system of claim 8 , wherein the controller is further configured to determine that the pericritical fluid has reached a critical point based at least on the impedance value being about zero.

11 . The pericritical fluid system of claim 8 , further comprising a second phase detection sensor configured to generate a second sensor output, wherein the controller is configured to determine a phase separation condition of the pericritical fluid based at least on a level of noise or a deviation in the second sensor output.

12 . The pericritical fluid system of claim 11 , wherein the second phase detection sensor comprises a fiber-optic reflectometer.

13 . The pericritical fluid system of claim 11 , wherein the controller is further configured to determine that the level of noise or the deviation increases as a result of phase separation.

14 . The pericritical fluid system of claim 8 , wherein the cooling circuit is configured as a thermal transport bus comprising a plurality of heat exchangers respectively configured to transfer heat from a plurality of fluid streams to the pericritical fluid.

15 . The pericritical fluid system of claim 14 , wherein the plurality of heat exchangers include at least one of: a fuel system heat exchanger, a lubrication system heat exchanger, a sump heat exchanger, a bleed air heat exchanger, a compressor cooling air heat exchanger, a thermal clearance control heat exchanger, an engine casing heat exchanger, an environmental control system heat exchanger, or an auxiliary systems heat exchanger.

16 . The pericritical fluid system of claim 8 , wherein the thermal management system comprises a primary cooling circuit and an intermediate cooling circuit with an intermediate heat exchanger configured to transfer heat from a primary cooling fluid to an intermediate cooling fluid, and wherein the intermediate cooling fluid is supplied in a supercritical phase state or a near-supercritical phase state.

17 . A non-transitory computer-readable medium storing instructions that, when executed by one or more processors of a controller for a thermal management system associated with a turbine engine, cause the controller to:

receive a sensor output from a phase detection sensor in fluid communication with a pericritical fluid circulating through a cooling circuit, the sensor output including an impedance value;

determine that the pericritical fluid has reached a bubble point based at least on a first characteristic change in the impedance value;

determine that the pericritical fluid has reached a dew point based at least on a second characteristic change in the impedance value, the second characteristic change being different from the first characteristic change; and

output a control signal to control at least one controllable component of the thermal management system based at least on the bubble point and the dew point.

18 . The non-transitory computer-readable medium of claim 17 , wherein the first characteristic change comprises an increase in the impedance value by a first amount, and wherein the second characteristic change comprises an increase in the impedance value by a second amount that is greater than the first amount.

19 . The non-transitory computer-readable medium of claim 17 , wherein the instructions, when executed by the one or more processors of the controller for the thermal management system associated with the turbine engine, further cause the controller to:

determine that the pericritical fluid has reached a critical point when the impedance value is about zero.

20 . The non-transitory computer-readable medium of claim 17 , wherein the instructions, when executed by the one or more processors of the controller for the thermal management system associated with the turbine engine, further cause the controller to:

determine a phase separation condition based at least on a level of noise or a deviation in a second sensor output from a second phase detection sensor.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 15, 2026
From: SIBBACH, ARTHUR WILLIAM; MILLER, BRANDON WAYNE
To: GENERAL ELECTRIC COMPANY
Reel/Frame 073477/0112 →
Continuity (3)
Continuation 19076054 · Mar 11, 2025
Continuation 17687976 · Mar 7, 2022
Related Publication 20260146545A1 · May 28, 2026
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