IP Library Granted Patent US 9,850,841
Granted Patent B2
US 9,850,841 · App. 14/102,615 · Granted Dec 26, 2017

System and program product for controlling exhaust gas temperature of engine system

Inventors: Julian R. Knudsen (Waukesha, WI); Troy Christopher Gosselin (Kenosha, WI); Yupeng Xiong (Milwaukee, WI); James Kristopher von der Ehe (Delafield, WI)
Assignee: General Electric Company
F02D41/1446F02D41/0007F02D41/0205F02D2200/101Y02T10/144
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Quick Facts
Patent No.
US 9,850,841
App. No.
14/102,615
Granted
Dec 26, 2017
Kind
B2
Abstract

Aspects of the disclosure include a system for controlling an exhaust gas communicated from an engine system to a turbine component of a turbocharger system. The system can include an engine having an operational speed; a turbocharger system including a turbine component, the exhaust gas being output from the engine in an exhaust line; a controller in communication with the engine; and a sensor disposed in the exhaust line being in communication with the controller, the system operating according to the following method: measuring the first temperature of the exhaust gas, determining if the measured first temperature of the exhaust gas is within a temperature safety window of the system; calculating an engine speed of the engine; and adjusting an engine speed setpoint and speed of the engine based on the measured first temperature and the calculated engine speed.

Claims (47)

1. A system for controlling an operational temperature of an exhaust gas, the system comprising:

an engine having an operational speed when the engine is in operation;

a turbocharger system including a turbine component, the exhaust gas being output from the engine in an exhaust line which is received at an input of the turbine component;

a controller in communication with the engine; and

a sensor disposed in the exhaust line being in communication with the controller, the sensor being configured to measure a first temperature and a second temperature of the exhaust gas disposed in the exhaust line;

the system operating according to the following method:

measuring the first temperature of the exhaust gas by the sensor,

determining via the controller if the measured first temperature of the exhaust gas is less than a minimum temperature value or greater than a maximum temperature value, the minimum temperature value and maximum temperature values defining a temperature safety window of the system;

calculating an engine speed of the engine via the controller;

if the measured first temperature of the exhaust gas is determined to be less than the minimum temperature value of the temperature safety window or greater than the maximum temperature value of the temperature safety window, adjusting a first speed setpoint of the engine by the calculated engine speed via the controller to produce a second speed setpoint of the engine;

changing the operational speed of the engine by the controller based on the second speed setpoint of the engine that results in the operational temperature of the exhaust gas in the exhaust line being altered so that when a second temperature of the exhaust gas is measured by the sensor at a later time period of operation of the system after the step of changing the operational speed, the measured second temperature of the exhaust gas is determined by the controller to be less than the maximum temperature value of the temperature safety window and greater than the minimum temperature value of the temperature safety window such that the operational temperature of the exhaust gas is controlled.

2. The system of claim 1 , wherein the step of adjusting the first speed setpoint includes an adjustment to produce the second speed setpoint that is decreased from the first speed setpoint when the measured first temperature of the exhaust gas is determined to be greater than the maximum temperature value, and the step of adjusting the first speed setpoint includes an adjustment to produce the second speed setpoint that is increased from the first speed setpoint when the measured first temperature of the exhaust gas is determined to be less than the minimum temperature value.

3. The system of claim 1 , wherein the calculated engine speed of the engine is calculated in a product, integral, derivative (PID) loop within the controller, is at least partially based on an input from a user of the engine, and is defined in revolutions per minute (RPM).

4. The system of claim 1 , wherein the maximum temperature value of the temperature safety window is a maximum safe temperature within a temperature safety operating range of the turbocharger system.

5. The system of claim 1 , wherein the temperature safety window includes a target exhaust gas temperature.

6. The system of claim 5 , wherein the target exhaust gas temperature prevents creep-effects from occurring within the turbocharger system.

7. The system of claim 1 , wherein the temperature safety window is based on an operational characteristic of the engine.

8. The system of claim 7 , wherein the operational characteristic of the engine system includes one of an engine size, a maximum power output, an engine model, and a fuel supply of the engine.

9. A program product stored on a computer readable storage medium, the program product operative to control an operational temperature of an exhaust gas yielded from an engine system to a turbocharger system when executed, the exhaust gas being output from the engine in an exhaust line which is received at an input of a turbine component of the turbocharger system, the computer readable storage medium comprising program code for:

reading the temperature of the exhaust gas from a temperature sensor positioned within the turbocharger system;

determining if the measured first temperature of the exhaust gas is less than a minimum temperature value or greater than a maximum temperature value, the minimum temperature value and maximum temperature values defining a temperature safety window of the system;

calculating an engine speed of an engine of the engine system;

if the measured first temperature of the exhaust gas is determined to be less than the minimum temperature value of the temperature safety window or greater than the maximum temperature value of the temperature safety window, adjusting a first speed setpoint of the engine by the calculated engine speed to produce a second speed setpoint of the engine;

changing the operational speed of the engine by based on the second speed setpoint of the engine that results in the operational temperature of the exhaust gas in the exhaust line being altered so that when a second temperature of the exhaust gas is measured by the sensor at a later time period of operation of the system after the step of changing the operational speed, the measured second temperature of the exhaust gas is determined to be less than the maximum temperature value of the temperature safety window and greater than the minimum temperature value of the temperature safety window such that the operational temperature of the exhaust gas is controlled.

10. The program product of claim 9 , wherein the step of adjusting the first speed setpoint includes an adjustment to produce the second speed setpoint that is decreased from the first speed setpoint when the measured first temperature of the exhaust gas is determined to be greater than the maximum temperature value, and the step of adjusting the first speed setpoint includes an adjustment to produce the second speed setpoint that is increased from the first speed setpoint when the measured first temperature of the exhaust gas is determined to be less than the minimum temperature value.

11. The program product of claim 9 , wherein the calculated engine speed of the engine is calculated in a product, integral, derivative (PID) loop, is at least partially based on an input from a user of the engine, and is defined in revolutions per minute (RPM).

12. The program product of claim 9 , wherein the maximum temperature value of the temperature safety window is a maximum safe temperature within a temperature safety operating range of the turbocharger system.

13. The program product of claim 9 , wherein the changing of the operational speed of the engine includes one of opening or closing a throttle of the engine system.

14. The program product of claim 9 , wherein the temperature safety window is based a composition of fuel used in the engine system.

15. A system comprising:

an engine system;

a turbocharger system in fluid communication with the engine system, the turbocharger system including:

a turbine component configured to receive an exhaust gas from the engine system, the exhaust gas being output from the engine system in an exhaust line which is received at an input of the turbine component;

a rotatable shaft coupled to the turbine component;

a compressor component coupled to the rotatable shaft, wherein the compressor component is configured to deliver a compressed air stream to the engine system;

a controller configured to adjust an engine system speed based on the temperature of the exhaust gas being outside of a temperature safety window; and

a sensor disposed in the exhaust line being in communication with the controller, the sensor being configured to measure a first temperature and a second temperature of the exhaust gas disposed in the exhaust line;

the system operating according to the following method:

measuring the first temperature of the exhaust gas by the sensor,

determining via the controller if the measured first temperature of the exhaust gas is less than a minimum temperature value or greater than a maximum temperature value, the minimum temperature value and maximum temperature values defining a temperature safety window of the system;

calculating an engine speed of the engine system via the controller;

if the measured first temperature of the exhaust gas is determined to be less than the minimum temperature value of the temperature safety window or greater than the maximum temperature value of the temperature safety window, adjusting a first speed setpoint of the engine system by the calculated engine speed via the controller to produce a second speed setpoint of the engine system;

changing the operational speed of the engine system by the controller based on the second speed setpoint of the engine system that results in the operational temperature of the exhaust gas in the exhaust line being altered so that when a second temperature of the exhaust gas is measured by the sensor at a later time period of operation of the system after the step of changing the operational speed, the measured second temperature of the exhaust gas is determined by the controller to be less than the maximum temperature value of the temperature safety window and greater than the minimum temperature value of the temperature safety window such that the operational temperature of the exhaust gas is controlled.

16. The system of claim 15 , wherein the engine system comprises an internal combustion engine configured to react a fuel supply with the compressed air stream to yield the exhaust gas.

17. The system of claim 15 , wherein the step of adjusting the first speed setpoint includes an adjustment to produce the second speed setpoint that is decreased from the first speed setpoint when the measured first temperature of the exhaust gas is determined to be greater than the maximum temperature value, and the step of adjusting the first speed setpoint includes an adjustment to produce the second speed setpoint that is increased from the first speed setpoint when the measured first temperature of the exhaust gas is determined to be less than the minimum temperature value.

18. The system of claim 15 , wherein the calculated engine speed of the engine system is calculated in a product, integral, derivative (PID) loop within the controller, is at least partially based on an input from a user of the engine system, and is defined in revolutions per minute (RPM).

19. The system of claim 15 , wherein the maximum temperature value of the temperature safety window is a maximum safe temperature within a temperature safety operating range of the turbocharger system.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE RECEIVING PARTY ENTITY PREVIOUSLY RECORDED AT REEL: 48489 FRAME: 001. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Apr 11, 2019
From: GENERAL ELECTRIC COMPANY
To: AI ALPINE US BIDCO INC
Reel/Frame 049858/0407 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 3, 2019
From: GENERAL ELECTRIC COMPANY
To: AI ALPINE US BIDCO LLC
Reel/Frame 048489/0001 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 11, 2013
From: KNUDSEN, JULIAN R.; GOSSELIN, TROY CHRISTOPHER; XIONG, YUPENG; VON DER EHE, JAMES KRISTOPHER
To: GENERAL ELECTRIC COMPANY
Reel/Frame 031756/0898 →
Continuity (1)
Related Publication 20150159572A1 · Jun 11, 2015