IP Library Granted Patent US 8,695,321
Granted Patent B2
US 8,695,321 · App. 12/671,308 · Granted Apr 15, 2014

Gas turbine control apparatus and control method for generating an electric motor torque instruction based on the detected exhaust gas temperature

Inventors: Kazuhiro Takeda (Hiroshima, JP); Masahiro Kobayashi (Hiroshima, JP); Hideki Nagao (Hiroshima, JP); Yoshiyuki Okamoto (Hiroshima, JP)
Assignee: Mitsubishi Heavy Industries, Ltd.
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Quick Facts
Patent No.
US 8,695,321
App. No.
12/671,308
Granted
Apr 15, 2014
Kind
B2
Abstract

A control apparatus for controlling a compressor driven by a driving unit generating driving power by a gas turbine and an electric motor includes: a temperature detection section for detecting an exhaust gas temperature of the gas turbine; and a control section for generating a motor torque instruction value for the electric motor based on the detected exhaust gas temperature. Such a control apparatus can realize a control so as not to distribute a load on the electric motor when the exhaust gas temperature of the gas turbine is low and a driving power is low. As a result, the operation efficiency can be enhanced.

Claims (85)

1. A control apparatus for controlling a compressor driven by a driving unit generating driving power by a gas turbine and an electric motor, the control apparatus comprising:

a temperature detection section configured to detect an exhaust gas temperature of the gas turbine; and

a control section configured to generate a motor torque instruction value for the electric motor based on the detected exhaust gas temperature,

wherein the control section is configured to store a function, generate a function value by substituting an argument of the function for the detected exhaust gas temperature as the motor torque instruction value.

2. A control apparatus for controlling a compressor driven by a driving unit generating driving power by a gas turbine and an electric motor, the control apparatus comprising:

a temperature detection section configured to detect an exhaust gas temperature of the gas turbine; and

a control section configured to generate a motor torque instruction value for the electric motor based on the detected exhaust gas temperature,

wherein the control section is configured to generate the motor torque instruction value to reduce a deviation between the detected exhaust gas temperature and an inputted temperature set value.

3. A control apparatus for controlling a compressor driven by a driving unit generating driving power by a gas turbine and an electric motor, the control apparatus comprising:

a temperature detection section configured to detect an exhaust gas temperature of the gas turbine; and

a control section configured to generate a motor torque instruction value for the electric motor based on the detected exhaust gas temperature,

wherein the control section is configured to perform a speed control by generating a gas turbine fuel valve opening instruction value of the gas turbine based on a speed detection value being a detected value of a revolution speed of the compressor and an inputted speed set value.

4. The control apparatus according to claim 3 , wherein the control section is configured to:

generate a temperature dependent instruction value based on the detected exhaust gas temperature and distribute the temperature dependent instruction value into the motor torque instruction value and the gas turbine fuel valve opening instruction value; and

generate a speed dependent instruction value for a deviation between the speed detection value and the speed set value to become smaller and distribute the speed dependent instruction value into the motor torque instruction value and the gas turbine fuel valve opening instruction value.

5. The control apparatus according to claim 3 , wherein the control section changes the speed control to an exhaust gas temperature control in which the gas turbine fuel valve opening instruction value is generated based on the exhaust gas temperature when the detected exhaust gas temperature exceeds a predetermined level, and

the control section starts increasing the motor torque instruction value when the speed control is changed to the exhaust gas temperature control.

6. The control apparatus according to claim 3 , wherein the control section is configured to control a ratio of the motor torque instruction value to the gas turbine fuel valve opening instruction value such that the higher the detected exhaust gas temperature is, the larger the ratio is, when the detected exhaust gas temperature is in a predetermined temperature range.

7. The control apparatus according to claim 6 , wherein the control section is configured to control the ratio to be constant in a period where the detected exhaust gas temperature is in a predetermined temperature width when the detected exhaust gas temperature decreases after the ratio becomes a predetermined maximum value.

8. The control apparatus according to claim 6 , wherein the control section is configured to set an upper limit of the predetermined temperature range to an inputted maximum exhaust gas temperature, and generate the motor torque instruction value such that a power of the electric motor becomes maximum when the detected exhaust gas temperature is the upper limit of the predetermined temperature range.

9. The control apparatus according to claim 6 , further comprising:

an atmospheric air temperature detection section configured to detect an atmospheric air temperature; and

a storage section configured to store a correspondence relation between the atmospheric air temperature and a maximum temperature value set as a maximum exhaust gas temperature,

wherein the control section is configured to:

set an upper limit of the predetermined temperature range to be the maximum temperature value corresponding to the detected atmospheric air temperature in the correspondence relation; and

generate the motor torque instruction value such that a power of the electric motor becomes maximum when the detected exhaust gas temperature is at the upper limit of the predetermined temperature range.

10. A control apparatus for controlling a compressor driven by a driving unit generating driving power by a gas turbine and an electric motor, the control apparatus comprising:

a temperature detection section configured to detect an exhaust gas temperature of the gas turbine; and

a control section configured to generate a motor torque instruction value for the electric motor based on the detected exhaust gas temperature,

wherein the control section is configured to add a predetermined value to the motor torque instruction value for a predetermined period when a load of the driving unit decreases at a change rate larger than a predetermined level.

11. A control apparatus for controlling a compressor driven by a driving unit generating driving power by a gas turbine and an electric motor, the control apparatus comprising:

a temperature detection section configured to detect an exhaust gas temperature of the gas turbine; and

a control section configured to generate a motor torque instruction value for the electric motor based on the detected exhaust gas temperature,

wherein the control section is configured to:

generate a plurality of motor torque instruction value candidates among from a first motor torque instruction value candidate to a ninth motor torque instruction value candidate; and

determine the motor torque instruction value to be a maximum of the plurality of motor torque instruction value candidates,

wherein the first motor torque instruction value candidate is generated by generating a function value by substituting an argument of a function preliminary stored in the control section for the detected exhaust gas temperature,

wherein the second motor torque instruction value candidate is generated to reduce a deviation between the detected exhaust gas temperature and an inputted temperature set value,

wherein the third motor torque instruction value candidate is generated by:

generating a temperature dependent instruction value based on the detected exhaust gas temperature and distributing the temperature dependent instruction value into the third motor torque instruction value candidate and a gas turbine fuel valve opening instruction value; and

generating a speed dependent instruction value for a deviation between a speed detection value and a speed set value to become smaller and distributing the speed dependent instruction value into the third motor torque instruction value candidate and the gas turbine fuel valve opening instruction value,

wherein the fourth motor torque instruction value candidate is generated to be increased when a control of the gas turbine is changed from a speed control to an exhaust gas temperature control,

wherein the speed control is a control for generating the gas turbine fuel valve opening instruction value of the gas turbine based on the speed detection value being a detected value of a revolution speed of the compressor and an inputted speed value,

wherein the exhaust gas temperature control is a control changed from the speed control when the detected exhaust gas temperature exceeds a predetermined level, and the gas turbine fuel valve opening instruction value is generated based on the detected exhaust gas temperature,

wherein the fifth motor torque instruction value candidate is generated to control a ratio of the gas turbine fuel valve opening instruction value to the motor torque instruction value such that the higher the detected exhaust gas temperature is, the larger the ratio is, when the detected exhaust gas temperature is in a predetermined temperature range,

wherein the sixth motor torque instruction value candidate is generated to control the ratio of the gas turbine fuel valve opening instruction value to the motor torque instruction value such that the higher the detected exhaust gas temperature is, the larger the ratio is, when the detected exhaust gas temperature is in the predetermined temperature range, and is generated to control the ratio to be constant in a period where the detected exhaust gas temperature is in a predetermined temperature width when the detected exhaust gas temperature decreases after the ratio becomes a predetermined maximum value,

wherein the seventh motor torque instruction value candidate is generated to control the ratio of the gas turbine fuel valve opening instruction value to the motor torque instruction value such that the higher the detected exhaust gas temperature is, the larger the ratio is, when the detected exhaust gas temperature is in the predetermined temperature range, generated to set an upper limit of the predetermined temperature range to an inputted maximum exhaust gas temperature, and generated such that a power of the electric motor becomes maximum when the detected exhaust gas temperature is the upper limit of the predetermined temperature range,

wherein the eighth motor torque instruction value candidate is generated to control the ratio of the gas turbine fuel valve opening instruction value to the motor torque instruction value such that the higher the detected exhaust gas temperature is, the larger the ratio is, when the detected exhaust gas temperature is in the predetermined temperature range, and is generated such that the power of the electric motor becomes maximum when the detected exhaust gas temperature is the upper limit of the predetermined temperature range,

wherein the upper limit of the predetermined temperature range is set to be a maximum exhaust gas temperature corresponding to a detected atmospheric air temperature referring to a correspondence relation between the atmospheric air temperature and a maximum temperature value set as the maximum exhaust gas temperature, and

wherein the ninth motor torque instruction value candidate is generated by adding a predetermined value to the motor torque instruction value when a load of the driving unit decreases at a change rate larger than a predetermined level.

12. A control method for controlling a compressor driven by a driving unit generating driving power by a gas turbine and an electric motor, the control method comprising:

detecting an exhaust gas temperature of the gas turbine; and

generating, via a control section, a motor torque instruction value for the electric motor based on the detected exhaust gas temperature,

wherein, in the generating, the motor torque instruction value is generated by generating a function value by substituting an argument of a function stored in the control section for the detected exhaust gas temperature.

13. The control method according to claim 12 , wherein in the generating, the motor torque instruction value is generated to reduce a deviation between the detected exhaust gas temperature and an inputted temperature set value.

14. The control method according to claim 12 , wherein a speed control is performed by generating a gas turbine fuel valve opening instruction value of the gas turbine based on a speed detection value being a detected value of a revolution speed of the compressor and an inputted speed set value.

15. The control method according to claim 12 , further comprising:

adding a predetermined value to the motor torque instruction value for a predetermined period when a load of the driving unit decreases at a change rate larger than a predetermined level.

16. The control method according to claim 12 , wherein the generating comprises:

generating a plurality of motor torque instruction value candidates among from a first motor torque instruction value candidate to a ninth motor torque instruction value candidate; and

determining the motor torque instruction value to be a maximum of the plurality of motor torque instruction value candidates,

wherein the first motor torque instruction value candidate is generated by generating a function value by substituting an argument of a function preliminary stored in the control section for the detected exhaust gas temperature,

wherein the second motor torque instruction value candidate is generated to reduce a deviation between the detected exhaust gas temperature and an inputted temperature set value,

wherein the third motor torque instruction value candidate is generated by:

generating a temperature dependent instruction value based on the detected exhaust gas temperature and distributing the temperature dependent instruction value into the third motor torque instruction value candidate and a gas turbine fuel valve opening instruction value; and

generating a speed dependent instruction value for a deviation between a speed detection value and a speed set value to become smaller and distributing the speed dependent instruction value into the third motor torque instruction value candidate and the gas turbine fuel valve opening instruction value,

wherein the fourth motor torque instruction value candidate is generated to be increased when a control of the gas turbine is changed from a speed control to an exhaust gas temperature control,

wherein the speed control is a control for generating the gas turbine fuel valve opening instruction value of the gas turbine based on the speed detection value being a detected value of a revolution speed of the compressor and an inputted speed value,

wherein the exhaust gas temperature control is a control changed from the speed control when the detected exhaust gas temperature exceeds a predetermined level, and the gas turbine fuel valve opening instruction value is generated based on the detected exhaust gas temperature,

wherein the fifth motor torque instruction value candidate is generated to control a ratio of the gas turbine fuel valve opening instruction value to the motor torque instruction value such that the higher the detected exhaust gas temperature is, the larger the ratio is, when the detected exhaust gas temperature is in a predetermined temperature range,

wherein the sixth motor torque instruction value candidate is generated to control the ratio of the gas turbine fuel valve opening instruction value to the motor torque instruction value such that the higher the detected exhaust gas temperature is, the larger the ratio is, when the detected exhaust gas temperature is in the predetermined temperature range, and is generated to control the ratio to be constant in a period where the detected exhaust gas temperature is in a predetermined temperature width when the detected exhaust gas temperature decreases after the ratio becomes a predetermined maximum value,

wherein the seventh motor torque instruction value candidate is generated to control the ratio of the gas turbine fuel valve opening instruction value to the motor torque instruction value such that the higher the detected exhaust gas temperature is, the larger the ratio is, when the detected exhaust gas temperature is in the predetermined temperature range, generated to set an upper limit of the predetermined temperature range to an inputted maximum exhaust gas temperature, and generated such that a power of the electric motor becomes maximum when the detected exhaust gas temperature is the upper limit of the predetermined temperature range,

wherein the eighth motor torque instruction value candidate is generated to control the ratio of the gas turbine fuel valve opening instruction value to the motor torque instruction value such that the higher the detected exhaust gas temperature is, the larger the ratio is, when the detected exhaust gas temperature is in the predetermined temperature range, and is generated such that the power of the electric motor becomes maximum when the detected exhaust gas temperature is the upper limit of the predetermined temperature range,

wherein the upper limit of the predetermined temperature range is set to be a maximum exhaust gas temperature corresponding to a detected atmospheric air temperature referring to a correspondence relation between the atmospheric air temperature and a maximum temperature value set as the maximum exhaust gas temperature, and

wherein the ninth motor torque instruction value candidate is generated by adding a predetermined value to the motor torque instruction value when a load of the driving unit decreases at a change rate larger than a predetermined level.

17. The control method according to claim 14 , wherein in the generating, a temperature dependent instruction value is generated based on the detected exhaust gas temperature, and distributed into the motor torque instruction value and the gas turbine fuel valve opening instruction value, and

a speed dependent instruction value is generated for a deviation between the speed detection value and the speed set value to become smaller, and distribute into the motor torque instruction value and the gas turbine fuel valve opening instruction value.

18. The control method according to claim 14 , wherein in the generating, the motor torque instruction value is controlled to be increased when the speed control is changed to an exhaust gas temperature control in which the gas turbine fuel valve opening instruction value is generated based on the exhaust gas temperature, and

the speed control is changed to the exhaust gas temperature control when the detected exhaust gas temperature exceeds a predetermined level.

19. The control method according to claim 14 , wherein in the generating, the motor torque instruction value is generated to control a ratio of the motor torque instruction value to the gas turbine fuel valve opening instruction value such that the higher the detected exhaust gas temperature is, the larger the ratio is, when the detected exhaust gas temperature is in a predetermined temperature range.

20. The control method according to claim 19 , wherein the ratio is controlled to be constant in a period where the detected exhaust gas temperature is in a predetermined temperature width when the detected exhaust gas temperature decreases after the ratio becomes a predetermined maximum value.

21. The control method according to claim 19 , wherein in the generating, an upper limit of the predetermined temperature range is set to an inputted maximum exhaust gas temperature, and the motor torque instruction value is generated such that a power of the electric motor becomes maximum when the detected exhaust gas temperature is the upper limit of the predetermined temperature range.

22. The control method according to claim 19 ,

wherein in the generating, the motor torque is generated such that a power of the electric motor becomes maximum when the detected exhaust gas temperature is at an upper limit of the predetermined temperature range, and

the upper limit of the predetermined temperature range is set to be a maximum temperature value corresponding to a detected atmospheric air temperature in a correspondence relation.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 15, 2010
From: TAKEDA, KAZUHIRO; KOBAYASHI, MASAHIRO; NAGAO, HIDEKI; OKAMOTO, YOSHIYUKI
To: MITSUBISHI HEAVY INDUSTRIES, LTD.
Reel/Frame 024239/0072 →
Priority Claims (1)
JP 2007-337194 · Dec 27, 2007 · national
Continuity (1)
Related Publication 20100319356A1 · Dec 23, 2010