Determining and controlling a weight flow in an environmental control system

• US 11,703,890 B2
• Filed: 10/30/2018
• Issued: 07/18/2023
• Est. Priority Date: 10/30/2018
• Status: Active Grant

• Current Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Zywiak, Peter
• Primary Examiner(s): Satanovsky, Alexander
• Assistant Examiner(s): Zaykova-Feldman, Lyudmila
• Application Number:
  US16/175,268
• Publication Number:
  US 20200133314A1
• Time in Patent Office: 1,722 Days
• CPC Class Codes: B64D 13/06 the air being conditioned pressurising B64D13/02
• CPC Class Codes: G05B 15/02 electric
• CPC Class Codes: G05D 7/0623 characterised by the set value given to the control element
• CPC Class Codes: G05D 7/0635 by action on throttling means G05D7/0688, G05D7/0694 take precedence
• CPC Class Codes: Y02T 50/40 Weight reduction
• CPC Class Codes: Y02T 50/50 On board measures aiming to increase energy efficiency

Abstract

A method of determining and controlling a weight flow in an environmental control system includes sensing, using a turbine inlet temperature sensor, a turbine inlet temperature. A turbine inlet pressure is sensed using a turbine inlet pressure sensor. A turbine outlet pressure is sensed using a turbine outlet pressure sensor. A rotational shaft speed of a shaft is sensed using a rotational shaft speed sensor. The sensed turbine inlet temperature, the sensed turbine inlet pressure, the sensed turbine outlet pressure, and the sensed rotational shaft speed are received by a controller. A flow coefficient is determined by the controller using the turbine inlet pressure, the turbine outlet pressure, the shaft speed, and a Turbine Flow Coefficient Map. A weight flow through the turbine is determined by the controller using the flow coefficient, the turbine inlet temperature, a nozzle area, and the turbine inlet pressure.

Claims

1. A method of supplying conditioned air to an aircraft cabin of an aircraft, the method comprising:

receiving, with an air intake, compressed air;

cooling, with a primary heat exchanger and a secondary heat exchanger, the compressed air using ram air;

mixing, with a reheater which is fluidly connected to the secondary heat exchanger, the cooled air from the secondary heat exchanger with recirculated air from the aircraft cabin;

condensing, with a condenser, the cooled air;

sensing, by a turbine inlet sensor, a turbine inlet temperature of the condensed and cooled air at an inlet of a turbine for an aircraft, wherein the turbine is a component of an environmental control system and the turbine inlet sensor is upstream of and adjacent to the inlet of the turbine;

sensing, by a turbine inlet pressure sensor, a turbine inlet pressure of the condensed and cooled air at the inlet of the turbine;

sensing, by a turbine outlet pressure sensor, a turbine outlet pressure of the condensed and cooled air at an outlet of the turbine;

sensing, by a rotational speed sensor, a rotational speed of a rotor of the turbine;

receiving, by a controller including processing circuitry and computer-readable memory, the sensed turbine inlet temperature, the sensed turbine inlet pressure, the sensed turbine outlet pressure, and the sensed rotational shaft speed;

determining, by the controller, a flow coefficient using the turbine inlet pressure, the turbine outlet pressure, the rotational speed, and a turbine flow coefficient map, wherein the turbine flow coefficient map includes a set of empirically derived curves;

determining, by the controller, a weight flow through the turbine using the flow coefficient, the turbine inlet temperature, a turbine inlet nozzle area, and the turbine inlet pressure, wherein determining the weight flow through the turbine is according to the following equation;

2. The method of claim 1, wherein the control valve is located upstream of the turbine inlet temperature sensor and the turbine inlet pressure sensor.

3. The method of claim 1, wherein the control valve is located downstream of the turbine outlet pressure sensor.

4. The method of claim 1, further comprising:

opening the control valve when the weight flow through the turbine is below the target weight flow range.

5. The method of claim 1, further comprising:

closing the control valve when the weight flow through the turbine is above the target weight flow range.

6. The method of claim 1, further comprising:

communicating the output signal to a display which indicates the weight flow through the turbine to a user.

7. The method of claim 1, wherein the turbine flow coefficient map is plotted as a pressure ratio of the turbine outlet pressure over the turbine inlet pressure as a function of the rotational speed versus the flow coefficient.

8. The method of claim 7, wherein the pressure ratio of the turbine outlet pressure over the turbine inlet pressure is plotted on an x-axis as a function of the rotational speed and the flow coefficient is plotted on a y-axis.

9. The method of claim 7, wherein the flow coefficient is mapped based on the pressure ratio of the turbine outlet pressure over the turbine inlet pressure and the set of empirically defined curves.

10. An environmental control system for supplying conditioned air to an aircraft cabin of an aircraft, the environmental control system comprising:

an air intake which receives compressed air;

a primary heat exchanger which is fluidly connected to the air intake;

a secondary heat exchanger which is fluidly connected to the primary heat exchanger, wherein the primary heat exchanger and the secondary heat exchanger cool the compressed air received by the air intake using ram air;

a reheater which is fluidly connected to the secondary heat exchanger and which mixes the cooled air from the secondary heat exchanger with recirculated air from the aircraft cabin;

a condenser which condenses the cooled air;

a turbine for the aircraft that includes a turbine inlet, a turbine outlet, and a rotor, wherein the turbine inlet intakes the condensed and cooled air;

a turbine inlet temperature sensor located upstream of the turbine, which provides a signal representative of turbine inlet temperature, wherein the turbine inlet sensor is upstream of and adjacent to the turbine inlet;

a turbine inlet pressure sensor located upstream of the turbine, which provides a signal representative of turbine inlet pressure;

a turbine outlet pressure sensor located downstream of the turbine, which provides a signal representative of turbine outlet pressure;

a rotational speed sensor, which provides a signal representative of rotational speed of the rotor;

a controller that determines weight flow of the condensed and cooled air through the turbine as a function of a flow coefficient, a turbine inlet nozzle area, the turbine inlet pressure, and the turbine inlet temperature, according to the following equation;

11. The system of claim 10, wherein the control valve is located upstream of the turbine inlet temperature sensor and the turbine inlet pressure sensor.

12. The system of claim 10, wherein the control valve is located downstream of the turbine outlet pressure sensor.

13. The system of claim 10, and further comprising:

a display communicatively connected to the controller, wherein the display is configured to indicate the determined weight flow to a user based upon the output signal.

14. The system of claim 10, wherein the turbine flow coefficient map is plotted as a pressure ratio of the turbine outlet pressure over the turbine inlet pressure as a function of the rotational speed versus the flow coefficient.