CN113550831A - Active steam turbine combustion parameter control system and method for unmanned vehicle - Google Patents
Active steam turbine combustion parameter control system and method for unmanned vehicle Download PDFInfo
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- CN113550831A CN113550831A CN202110852679.7A CN202110852679A CN113550831A CN 113550831 A CN113550831 A CN 113550831A CN 202110852679 A CN202110852679 A CN 202110852679A CN 113550831 A CN113550831 A CN 113550831A
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/48—Control of fuel supply conjointly with another control of the plant
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/48—Control of fuel supply conjointly with another control of the plant
- F02C9/50—Control of fuel supply conjointly with another control of the plant with control of working fluid flow
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Abstract
The invention is suitable for the technical field of unmanned driving, and provides an active steam turbine combustion parameter control system and a method for an unmanned vehicle, wherein a fixed air-fuel ratio is preset, an air intake amount and a fuel intake amount are fixed, an ignition angle is changed, so as to obtain an optimal ignition angle under the air intake amount and the fuel intake amount, then when the ignition angle is used, the air intake amount and the fuel intake amount are preferentially adopted, then the air intake amount and the fuel intake amount are gradually changed, the optimal air intake amount and the fuel intake amount of each ignition angle are obtained by traversing according to the method and are recorded, then when the active steam turbine is in use, the corresponding ignition angle, the air intake amount and the fuel intake amount are selected according to the requirement of combustion parameters, so that the optimal combustion rate is ensured to be adopted each time, the combustion parameters of a combustion system cannot be automatically adjusted according to the actual combustion condition, and the insufficient combustion of fuel is easily caused, thereby causing the problems of energy waste and environmental pollution.
Description
Technical Field
The invention belongs to the technical field of unmanned driving, and particularly relates to an active steam turbine combustion parameter control system and method for an unmanned vehicle.
Background
The active steam turbine can also be called a self-rotating steam turbine, and the working characteristics of the active steam turbine can also be called as: a recoil, self-rotating steam turbine. The steam turbine has more than one hundred years of application history, and is still an irreplaceable power device till now and even in the future. Although the steam consumption is large and the heat efficiency is low, the steam consumption is subject to continuous optimization, but some problems are congenital physiological problems, and a plurality of defects which cannot be overcome exist until now.
The combustion system cannot automatically adjust combustion parameters according to actual combustion conditions, so that insufficient fuel combustion is easily caused, energy waste and environmental pollution are caused, and the whole fuel energy consumption of the steam turbine is high.
The steam turbine has high energy consumption, and only has a normal demand problem in the past era of unlimited energy, but the steam turbine continues to the current era of increasingly short energy sources, and focuses on a principle problem which is difficult to bear.
Disclosure of Invention
The invention provides an active steam turbine combustion parameter control system and method for an unmanned vehicle, and aims to solve the problems that a combustion system cannot automatically adjust combustion parameters according to actual combustion conditions, so that insufficient fuel combustion is easily caused, and energy waste and environmental pollution are caused.
The invention is realized in this way, an active steam turbine combustion parameter control system for an unmanned vehicle comprises a flow detection module, a combustion control module and a control module, wherein the flow detection module is used for detecting flow values of fuel inlet quantity and air inlet quantity in real time and sending the collected flow values to the combustion control module through a vehicle machine network;
the flue gas analysis module is used for measuring the content of carbon monoxide and oxygen in the flue gas in real time and transmitting the data to the combustion control module in real time through a vehicle-mounted machine network;
the fuel analysis module is used for measuring the current fuel heat value and components and sending the acquired data to the combustion control module through the vehicle-mounted machine network;
and the combustion control module is used for controlling and adjusting combustion parameters according to the data uploaded by the flow detection module, the flue gas analysis module and the fuel analysis module and selecting corresponding ignition angles.
Preferably, the flow detection module comprises a first microprocessor, a first serial communication circuit, a flow meter, a first power supply and crystal oscillator circuit, a first communication circuit and a 5V power supply output circuit,
the flow meter is bidirectionally connected with the first microprocessor through the serial communication circuit,
the power supply and crystal oscillator circuit is connected with the power supply input end and the clock signal input end of the microprocessor and is used for providing a working power supply and a clock signal for the microprocessor;
the communication circuit is bidirectionally connected with the microprocessor and is used for being connected with a vehicle machine network;
and the 5V power output circuit is connected with the power input end of the microprocessor and is used for providing a working power supply for the flowmeter.
Preferably, the flue gas analysis module comprises a second microprocessor, a temperature acquisition circuit, a carbon monoxide sensor signal processing circuit, a carbon monoxide sensor, an oxygen sensor signal processing circuit, a second power supply, a crystal oscillator circuit and a second communication circuit,
the carbon monoxide sensor is connected with the signal input end of the microprocessor through the carbon monoxide sensor signal processing circuit and is used for collecting the content of carbon monoxide in the flue gas;
the oxygen sensor is connected with the signal input end of the microprocessor through an oxygen sensor signal processing circuit and is used for collecting the content of oxygen in the flue gas;
the temperature acquisition circuit is connected with the signal input end of the microprocessor and is used for acquiring the temperature information of the flue gas;
the power supply and crystal oscillator circuit is connected with the power supply input end and the clock signal input end of the microprocessor and is used for providing a working power supply and a clock signal for the microprocessor;
the communication circuit is connected with the microprocessor in a bidirectional mode and is used for being connected with a vehicle machine network.
Preferably, the fuel analysis module comprises a third microprocessor, a fuel on-line analyzer, a second serial communication circuit, a third power supply and crystal oscillator circuit, a third communication circuit and a 24V power supply output end circuit,
the fuel on-line analyzer is bidirectionally connected with the microprocessor through the serial communication circuit and is used for detecting the components of the fuel;
the power supply and crystal oscillator circuit is connected with the power supply input end and the clock signal input end of the microprocessor and is used for providing a working power supply and a clock signal for the microprocessor;
the communication circuit is bidirectionally connected with the microprocessor and is used for being connected with a vehicle machine network;
and the 24V power output circuit is connected with the power input end of the microprocessor and is used for providing a working power supply for the fuel on-line analyzer.
Preferably, the combustion control module comprises a fourth microprocessor, a display circuit, a key circuit, a fourth power supply, a crystal oscillator circuit, a communication circuit, a third serial communication circuit, a 4-20mA output circuit and a power-down memory,
the third serial communication circuit is connected with the microprocessor in a bidirectional mode and is used for achieving communication with the frequency converter to achieve the purpose of controlling the air intake;
the 4-20mA output circuit is connected with the output end of the microprocessor and is used for controlling the electric valve to realize the control of the fuel inlet amount;
the power-down memory is bidirectionally connected with the microprocessor and is used for storing the searched combustion parameter data;
the display circuit is connected with the signal output end of the microprocessor and is used for displaying various data;
the key circuit is connected with the signal input end of the microprocessor and is used for setting various parameters and commands;
the power supply and crystal oscillator circuit is connected with the power supply input end and the clock signal input end of the microprocessor and is used for providing a working power supply and a clock signal for the microprocessor;
the communication circuit is connected with the microprocessor in a bidirectional mode and is used for being connected with a vehicle machine network.
A method for applying an active turbine combustion parameter control system for an unmanned vehicle comprises the following steps:
step one, starting a steam turbine;
adjusting the air-fuel ratio of the steam turbine to a first preset air-fuel ratio;
adjusting the ignition angle of the steam turbine to a first preset ignition angle; different intake air quantities and fuel intake quantities are introduced;
detecting the central temperature inside the steam turbine;
step five, circulating the step three and the step four to obtain a plurality of first temperature values which correspond to the first preset ignition angles with different sizes one by one;
and step six, comparing the first temperature values, and taking a first preset ignition angle corresponding to the maximum value in the first temperature values as a target ignition angle.
Compared with the prior art, the invention has the beneficial effects that: the invention discloses an active steam turbine combustion parameter control system and method for an unmanned vehicle, which comprises the steps of presetting a fixed air-fuel ratio, fixing air intake and fuel intake, changing an ignition angle to obtain the optimal ignition angle under the air intake and the fuel intake, then when the ignition angle is used, the air intake amount and the fuel intake amount are preferentially adopted, then the air intake amount and the fuel intake amount are gradually changed, the optimal air intake amount and the fuel intake amount of each ignition angle are obtained by traversing according to the method and recorded, and when the ignition angle is used, according to the requirement of combustion parameters, the selection of corresponding ignition angle, intake air amount and fuel intake amount is carried out, the optimal combustion rate is guaranteed to be adopted each time, the problem that the combustion system cannot automatically adjust the combustion parameters according to the actual combustion condition, the fuel is easily combusted insufficiently, and the energy waste and the environmental pollution are caused is solved.
Drawings
FIG. 1 is a flow chart of an active turbine combustion parameter control system for an unmanned vehicle according to the present invention;
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
Referring to fig. 1, the present invention provides a technical solution:
the flow detection module comprises a first microprocessor, a first serial communication circuit, a flow meter, a first power supply and crystal oscillator circuit, a first communication circuit and a 5V power supply output circuit, wherein the flow meter is preferably an eddy current flow meter, and can be any one of other flow meters in the prior art which are suitable for the flow meter. The flow meter is bidirectionally connected with the first microprocessor through the serial communication circuit, and the power supply and the crystal oscillator circuit are connected with the power supply input end and the clock signal input end of the microprocessor and used for providing a working power supply and a clock signal for the microprocessor; the communication circuit is bidirectionally connected with the microprocessor and is used for being connected with a vehicle machine network; the 5V power output circuit is connected with the power input end of the microprocessor and used for providing working power for the flowmeter.
The stm32f103 is used as a central processing unit in module hardware design, the RS485 communication circuit is mainly responsible for data communication of the vortex flowmeter so as to obtain current real-time flow data, the 5V power output circuit is mainly used for providing a working power supply for the vortex flowmeter, and the communication circuit is mainly used for real-time communication with the combustion communication module.
The flue gas analysis module comprises a second microprocessor, a temperature acquisition circuit, a carbon monoxide sensor signal processing circuit, a carbon monoxide sensor, an oxygen sensor signal processing circuit, a second power supply, a crystal oscillator circuit and a second communication circuit, preferably, the temperature acquisition circuit is a PT100 temperature acquisition circuit, and certainly, any one of other prior art can be used as the temperature acquisition circuit applicable to the application.
The carbon monoxide sensor is connected with the signal input end of the microprocessor through a carbon monoxide sensor signal processing circuit and is used for collecting the content of carbon monoxide in the flue gas; the oxygen sensor is connected with the signal input end of the microprocessor through an oxygen sensor signal processing circuit and is used for collecting the content of oxygen in the flue gas; the temperature acquisition circuit is connected with the signal input end of the microprocessor and is used for acquiring the temperature information of the flue gas; the power supply and crystal oscillator circuit is connected with the power supply input end and the clock signal input end of the microprocessor and used for providing a working power supply and a clock signal for the microprocessor; the communication circuit is connected with the microprocessor in a bidirectional mode and is used for being connected with a vehicle machine network.
The module hardware design uses stm32f103 as a central processing unit, the carbon monoxide sensor processing circuit and the oxygen sensor processing circuit are mainly used for processing data brought by collecting continuous sensors and sending the data to a CPU, the PT100 processing circuit is mainly used for processing the data collected by the PT100 temperature sensor, and the communication circuit is mainly used for communicating with the combustion communication module in real time.
The fuel analysis module comprises a third microprocessor, a fuel online analyzer, a second serial communication circuit, a third power supply and crystal oscillator circuit, a third communication circuit and a 24V power supply output end circuit, wherein the fuel online analyzer is bidirectionally connected with the microprocessor through the serial communication circuit and is used for detecting the components of the fuel; the power supply and crystal oscillator circuit is connected with the power supply input end and the clock signal input end of the microprocessor and used for providing a working power supply and a clock signal for the microprocessor; the communication circuit is bidirectionally connected with the microprocessor and is used for being connected with a vehicle machine network; and the 24V power output circuit is connected with the power input end of the microprocessor and is used for providing working power for the fuel on-line analyzer.
The module hardware design takes stm32f103 as a central processing unit, the RS485 communication circuit is mainly responsible for communicating with the fuel on-line analyzer so as to obtain the main components and the calorific value of the current fuel, the 24V power output circuit is mainly used for providing a working power supply for the fuel on-line analyzer, and the communication circuit is mainly used for communicating with the combustion communication module in real time.
The combustion control module comprises a fourth microprocessor, a display circuit, a key circuit, a fourth power supply, a crystal oscillator circuit, a communication circuit, a third serial communication circuit, a 4-20mA output circuit and a power failure memory, wherein the third serial communication circuit is connected with the microprocessor in a bidirectional mode and used for achieving communication with the frequency converter so as to achieve the purpose of controlling the air intake; the 4-20mA output circuit is connected with the output end of the microprocessor and is used for controlling the electric valve to realize the control of the fuel inlet amount; the power-down memory is bidirectionally connected with the microprocessor and is used for storing the searched combustion parameter data; the display circuit is connected with the signal output end of the microprocessor and is used for displaying various data; the key circuit is connected with the signal input end of the microprocessor and is used for setting various parameters and commands; the power supply and crystal oscillator circuit is connected with the power supply input end and the clock signal input end of the microprocessor and used for providing a working power supply and a clock signal for the microprocessor; the communication circuit is connected with the microprocessor in a bidirectional mode and is used for being connected with a vehicle machine network.
In the design of module hardware, stm32f103 is used as a central processing unit, an RS485 communication circuit mainly realizes communication with a frequency converter so as to achieve the purpose of controlling the air intake, a 4-20mA output circuit mainly controls an electric valve to realize the control of fuel intake, a power failure memory mainly stores searched combustion parameter data, a communication circuit mainly obtains data fed back by different modules in real time, and an LCD display circuit and a key circuit are mainly used for better performing man-machine interaction.
The system mainly obtains data collected by different modules in real time through a vehicle machine network, and calculates, analyzes and processes all the collected data in the combustion control module so as to control the air-fuel ratio in the combustion process to achieve high combustion efficiency. The combustion parameters at different continuous output points under different fuel components and different heat output powers can be automatically searched through the combined action system of each module. The automatic proportional combustion of the combustor can be realized, the fuel can be fully combusted, and the energy-saving and environment-friendly effects are achieved.
The main functions of the combustion control module are: the normal combustion of the combustor is controlled, the continuity of heat energy output is realized mainly by controlling the fuel feeding quantity and the air intake quantity, the system automatically searches and adjusts the combustion parameters of different heat power output points to realize more intellectualization, and the searched combustion parameters can be stored for subsequent normal combustion. The system mainly obtains the air intake of the steam turbine, the fuel intake quantity, the fuel components and the contents of carbon monoxide and oxygen in the flue gas in real time through a vehicle machine network. The control of the air intake is mainly controlled by controlling the frequency of the frequency converter through RS485 communication, and the fuel intake amount is mainly controlled by controlling the electric valve through 4-20mA current to realize different fuel intake amounts. Meanwhile, the module has a key setting function and an LCD display function.
The combustion control module mainly comprises the following working procedures:
before the turbine is not normally operated: starting a steam turbine; adjusting the air-fuel ratio of the steam turbine to a first preset air-fuel ratio; adjusting the ignition angle of the steam turbine to a first preset ignition angle; introducing a first intake air quantity and a first fuel intake quantity; detecting the central temperature inside the steam turbine; so as to obtain first temperature values corresponding to first preset ignition angles corresponding to the first intake air amount and the first fuel intake amount; adjusting the ignition angle to a second preset ignition angle, introducing the same first intake air amount and the same first fuel intake amount again to obtain a corresponding second temperature value, testing the rest ignition angles in such a way, and comparing all the temperature values to obtain the first intake air amount and the optimal ignition angle under the first fuel intake amount;
then changing the air intake or fuel intake, sequentially changing the preset ignition angle according to the method to obtain corresponding temperature values, and comparing the temperature values to obtain the optimal ignition angle under the air intake or fuel intake;
and sequentially and repeatedly trying to obtain the air intake amount, the fuel intake amount and the corresponding ignition angle within the optimal combustion filter range.
When the system is used, the system automatically searches the combustion parameter function through the fuel, determines the fuel components through the analysis of the fuel, automatically calculates the data of the optimal fuel intake quantity and the optimal air intake quantity under different heat output powers according to the fuel components, and then selects the optimal ignition angle according to the fuel intake quantity and the air intake quantity data to obtain the optimal air-fuel ratio.
The system starts ignition, after ignition is successful, the system mainly controls the micro-regulation (including the selection of the air intake quantity, the fuel intake quantity and the ignition angle) of the calculated air-fuel ratio from the lowest heat output power according to the data transmitted back in real time by the flue gas analysis module so as to achieve the highest combustion efficiency, the system continuously carries out the micro-regulation on the combustion parameters on all different heat output power points from the lowest heat output power to the highest heat output power, all the regulated data are stored, and after parameter search is completed, the turbine can automatically realize the operation of the best combustion efficiency under different heat output powers.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents and improvements made within the spirit and principle of the present invention are intended to be included within the scope of the present invention.
Claims (7)
1. The utility model provides an active steam turbine burning parameter control system for unmanned vehicle which characterized in that: the system comprises a flow detection module, a combustion control module and a flow control module, wherein the flow detection module is used for detecting flow values of fuel inlet quantity and air inlet quantity in real time and sending the acquired flow values to the combustion control module through a vehicle machine network;
the flue gas analysis module is used for measuring the content of carbon monoxide and oxygen in the flue gas in real time and transmitting the data to the combustion control module in real time through a vehicle-mounted machine network;
the fuel analysis module is used for measuring the current fuel heat value and components and sending the acquired data to the combustion control module through the vehicle-mounted machine network;
and the combustion control module is used for controlling and adjusting combustion parameters according to the data uploaded by the flow detection module, the flue gas analysis module and the fuel analysis module and selecting corresponding ignition angles.
2. The active turbine combustion parameter control system for the unmanned vehicle as claimed in claim 1, wherein: the flow detection module comprises a first microprocessor, a first serial communication circuit, a flow meter, a first power supply and crystal oscillator circuit, a first communication circuit and a 5V power supply output circuit,
the flow meter is bidirectionally connected with the first microprocessor through the serial communication circuit,
the power supply and crystal oscillator circuit is connected with the power supply input end and the clock signal input end of the microprocessor and is used for providing a working power supply and a clock signal for the microprocessor;
the communication circuit is bidirectionally connected with the microprocessor and is used for being connected with a vehicle machine network;
and the 5V power output circuit is connected with the power input end of the microprocessor and is used for providing a working power supply for the flowmeter.
3. The active turbine combustion parameter control system for the unmanned vehicle as claimed in claim 1, wherein: the flue gas analysis module comprises a second microprocessor, a temperature acquisition circuit, a carbon monoxide sensor signal processing circuit, a carbon monoxide sensor, an oxygen sensor signal processing circuit, a second power supply, a crystal oscillator circuit and a second communication circuit,
the carbon monoxide sensor is connected with the signal input end of the microprocessor through the carbon monoxide sensor signal processing circuit and is used for collecting the content of carbon monoxide in the flue gas;
the oxygen sensor is connected with the signal input end of the microprocessor through an oxygen sensor signal processing circuit and is used for collecting the content of oxygen in the flue gas;
the temperature acquisition circuit is connected with the signal input end of the microprocessor and is used for acquiring the temperature information of the flue gas;
the power supply and crystal oscillator circuit is connected with the power supply input end and the clock signal input end of the microprocessor and is used for providing a working power supply and a clock signal for the microprocessor;
the communication circuit is connected with the microprocessor in a bidirectional mode and is used for being connected with a vehicle machine network.
4. The active turbine combustion parameter control system for the unmanned vehicle as claimed in claim 1, wherein: the fuel analysis module comprises a third microprocessor, a fuel on-line analyzer, a second serial communication circuit, a third power supply and crystal oscillation circuit, a third communication circuit and a 24V power supply output end circuit,
the fuel on-line analyzer is bidirectionally connected with the microprocessor through the serial communication circuit and is used for detecting the components of the fuel;
the power supply and crystal oscillator circuit is connected with the power supply input end and the clock signal input end of the microprocessor and is used for providing a working power supply and a clock signal for the microprocessor;
the communication circuit is bidirectionally connected with the microprocessor and is used for being connected with a vehicle machine network;
and the 24V power output circuit is connected with the power input end of the microprocessor and is used for providing a working power supply for the fuel on-line analyzer.
5. The active turbine combustion parameter control system for the unmanned vehicle as claimed in claim 1, wherein: the combustion control module comprises a fourth microprocessor, a display circuit, a key circuit, a fourth power supply and crystal oscillator circuit, a communication circuit, a third serial communication circuit, a 4-20mA output circuit and a power-down memory,
the third serial communication circuit is connected with the microprocessor in a bidirectional mode and is used for achieving communication with the frequency converter to achieve the purpose of controlling the air intake;
the 4-20mA output circuit is connected with the output end of the microprocessor and is used for controlling the electric valve to realize the control of the fuel inlet amount;
the power-down memory is bidirectionally connected with the microprocessor and is used for storing the searched combustion parameter data;
the display circuit is connected with the signal output end of the microprocessor and is used for displaying various data;
the key circuit is connected with the signal input end of the microprocessor and is used for setting various parameters and commands;
the power supply and crystal oscillator circuit is connected with the power supply input end and the clock signal input end of the microprocessor and is used for providing a working power supply and a clock signal for the microprocessor;
the communication circuit is connected with the microprocessor in a bidirectional mode and is used for being connected with a vehicle machine network.
6. The active turbine combustion parameter control system for the unmanned vehicle as claimed in claim 5, wherein: the microprocessor uses ARM7stm32f series microprocessor;
the serial communication circuit is an RS485 serial communication circuit;
the power down memory is an AT24C08 type memory.
7. A method for applying an active turbine combustion parameter control system for an unmanned vehicle is characterized by comprising the following steps: the method comprises the following steps:
step one, starting a steam turbine;
adjusting the air-fuel ratio of the steam turbine to a first preset air-fuel ratio;
adjusting the ignition angle of the steam turbine to a first preset ignition angle; different intake air quantities and fuel intake quantities are introduced;
detecting the central temperature inside the steam turbine;
step five, circulating the step three and the step four to obtain a plurality of first temperature values which correspond to the first preset ignition angles with different sizes one by one;
and step six, comparing the first temperature values, and taking a first preset ignition angle corresponding to the maximum value in the first temperature values as a target ignition angle.
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| US5533329A (en) * | 1993-05-17 | 1996-07-09 | Hitachi, Ltd. | Control apparatus for and control method of gas turbine |
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| US20110004390A1 (en) * | 2008-09-29 | 2011-01-06 | Mitsubishi Heavy Industries, Ltd. | Gas turbine control method and device |
| US20120275899A1 (en) * | 2009-05-08 | 2012-11-01 | Gas Turbine Efficiency Sweden Ab | Automated tuning of gas turbine combustion systems |
| CN104533646A (en) * | 2014-12-31 | 2015-04-22 | 安徽江淮汽车股份有限公司 | Combustion parameter adjusting method and combustion parameter adjusting device of supercharged engine |
| CN205655323U (en) * | 2016-04-08 | 2016-10-19 | 高台县聚庆新能源设备有限公司 | Control system based on but CANopen network automatic adjustment combustion parameter |
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2021
- 2021-07-27 CN CN202110852679.7A patent/CN113550831A/en active Pending
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5533329A (en) * | 1993-05-17 | 1996-07-09 | Hitachi, Ltd. | Control apparatus for and control method of gas turbine |
| CN1816684A (en) * | 2003-07-02 | 2006-08-09 | 麦斯国际有限公司 | Electrical power generation system and method |
| US20110004390A1 (en) * | 2008-09-29 | 2011-01-06 | Mitsubishi Heavy Industries, Ltd. | Gas turbine control method and device |
| US20120275899A1 (en) * | 2009-05-08 | 2012-11-01 | Gas Turbine Efficiency Sweden Ab | Automated tuning of gas turbine combustion systems |
| CN104533646A (en) * | 2014-12-31 | 2015-04-22 | 安徽江淮汽车股份有限公司 | Combustion parameter adjusting method and combustion parameter adjusting device of supercharged engine |
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Application publication date: 20211026 |