CN109386386A - A kind of gas turbine engine systems of dyestuff burning - Google Patents
A kind of gas turbine engine systems of dyestuff burning Download PDFInfo
- Publication number
- CN109386386A CN109386386A CN201811206435.6A CN201811206435A CN109386386A CN 109386386 A CN109386386 A CN 109386386A CN 201811206435 A CN201811206435 A CN 201811206435A CN 109386386 A CN109386386 A CN 109386386A
- Authority
- CN
- China
- Prior art keywords
- output end
- gas turbine
- turbine engine
- engine systems
- equipment
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 239000000975 dye Substances 0.000 title claims abstract description 21
- 239000007789 gas Substances 0.000 claims abstract description 40
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims abstract description 19
- 239000001301 oxygen Substances 0.000 claims abstract description 19
- 229910052760 oxygen Inorganic materials 0.000 claims abstract description 19
- 238000003745 diagnosis Methods 0.000 claims abstract description 15
- 239000000446 fuel Substances 0.000 claims abstract description 13
- 230000036413 temperature sense Effects 0.000 claims description 3
- 230000006835 compression Effects 0.000 claims description 2
- 238000007906 compression Methods 0.000 claims description 2
- 238000002485 combustion reaction Methods 0.000 description 4
- 230000001105 regulatory effect Effects 0.000 description 3
- 239000000567 combustion gas Substances 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 239000002699 waste material Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000001934 delay Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 238000009738 saturating Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000003245 working effect Effects 0.000 description 1
Classifications
-
- 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
-
- 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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/18—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
The invention discloses a kind of gas turbine engine systems of dyestuff burning, including compressor and processor, the compressor input terminal is connected with air inlet pipe, the processor input terminal is connected with input equipment, the processor output end is connected with controller, the controller output end is connected with fuel mixer, the fuel mixer output end is connected with burner, the burner output end is connected with oxygen sensor, temperature sensor and turbine, the turbine output end is connected with state analysis equipment and exhaust pipe, the state analysis equipment output end is connected with sensor fault diagnosis equipment, the sensor fault diagnosis equipment output end is connect with processor input terminal, the exhaust pipe output end is connected with heat-exchanger rig.The present invention improves the operating efficiency of the gas turbine engine systems of dyestuff burning, reduces the number of the carry out on-site test of existing gas turbine engine systems often, time saving and energy saving, also ensures the normal work of gas turbine.
Description
Technical field
The present invention relates to gas-turbine plant technical field, specially a kind of gas turbine engine systems of dyestuff burning.
Background technique
Gas turbine is gas continuously to flow as working medium impeller high speed rotation, is to have by the energy conversion of fuel
Diligent internal combustion type dynamic power machine is a kind of rotary vane type Thermal Motor.Air is inhaled from the outside atmospheric environment in compressor,
And it is allowed to be pressurized by axial-flow compressor step by step compression, while air themperature also correspondinglys increase；Compressed air is pressed to combustion
The fuel for burning room and penetrating is mixed and burned the gas for generating high temperature and pressure；Then expansion work in turbine is entered back into, is pushed saturating
Flat rubber belting dynamic pressure mechanism of qi and external load rotor are rotate together at high speed, and the chemical energy for realizing gas or liquid fuel is partially converted into machine
Tool function, and export electric work.Existing gas turbine engine systems need carry out on-site test often, time-consuming and laborious, delay combustion gas wheel
The normal work of machine, and cannot accomplish the intelligent control to burner, and the gas after burner combustion contains largely
Energy is immediately discharged in atmosphere, waste of energy.
Summary of the invention
The purpose of the present invention is to provide a kind of gas turbine engine systems of dyestuff burning, to solve to mention in above-mentioned background technique
Existing gas turbine engine systems out need carry out on-site test often, time-consuming and laborious, delay the normal work of gas turbine,
And the problem of cannot accomplishing the intelligent control to burner.
In order to solve the above technical problems, the invention provides the following technical scheme: a kind of dyestuff burning gas turbine engine systems,
Including compressor and processor, the compressor input terminal is connected with air inlet pipe, and the processor input terminal is connected with input and sets
Standby, the processor output end is connected with controller, and the controller output end is connected with fuel mixer, and the controller
Output end is connect with compressor input terminal, and the fuel mixer output end is connected with burner, and the burner input terminal
It is connect with the output end of compressor, the burner output end is connected with oxygen sensor, temperature sensor and turbine, the whirlpool
Wheel output end is connected with state analysis equipment and exhaust pipe, and the state analysis equipment output end is connected with sensor fault diagnosis
Equipment, the sensor fault diagnosis equipment input terminal are connect with temperature sensor output end, and the sensor fault diagnosis is set
Standby output end is connect with processor input terminal, and the exhaust pipe output end is connected with heat-exchanger rig, the heat-exchanger rig output end
It is connected with air blower, the air blower output end is connect with air inlet pipe side.
Preferably, the input equipment includes keyboard, mouse and touch pad.
Preferably, the controller output end is connected with alarm.
Preferably, the oxygen sensor and temperature sensor data output end are connect with processor input terminal.
Preferably, the port of the air inlet pipe and air blower pass to the port of air inlet pipe side at a distance of one to three meter.
Preferably, the heat-exchanger rig includes thermally conductive equipment and exhaust equipment.
Preferably, the oxygen sensor setting oxygen-sensitive content is the minimum point of normal range of operation.
Preferably, the temperature sensor setting temperature sense range is the midpoint of normal range of operation.
Compared with prior art, the beneficial effects of the present invention are:
1. the present invention, the oxygen content and temperature in burner can be understood by oxygen sensor and temperature sensor in real time
Degree height, may then pass through controller and regulates and controls to it, can by state analysis equipment and sensor fault diagnosis equipment
Preferably to be detected to turbine and sensor, then regulated and controled by controller, solves existing gas turbine system
System needs carry out on-site test often, time-consuming and laborious, delays the normal work of gas turbine, and cannot accomplish to burner
Intelligent control the technical issues of, improve the dyestuff burning gas turbine engine systems operating efficiency, reduce existing combustion gas
The number of the carry out on-site test of expander system often, it is time saving and energy saving, the normal work of gas turbine is also ensured, convenient for combustion
Burner carries out intelligent control.
2. can be passed through by setting heat-exchanger rig and air blower when the gas turbine engine systems to be burnt using the dyestuff
Heat-exchanger rig exports the heat in discharge, heats through air blower to air inlet pipe, saves the energy, avoid burner
Gas after burning contains big energy and is immediately discharged in atmosphere, waste of energy.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the embodiment of the present invention；
Fig. 2 is the working principle diagram of the embodiment of the present invention.
In figure: 1, compressor；2, processor；3, air inlet pipe；4, input equipment；5, controller；6, alarm；7, fuel is mixed
Clutch；8, burner；9, oxygen sensor；10, temperature sensor；11, turbine；12, state analysis equipment；13, exhaust pipe；
14, sensor fault diagnosis equipment；15, heat-exchanger rig；16, air blower.
Specific embodiment
In order to improve the operating efficiency for the gas turbine engine systems that the dyestuff burns, existing gas turbine engine systems are reduced often
Carry out on-site test number, it is time saving and energy saving, also ensure the normal work of gas turbine, the embodiment of the invention provides one
The gas turbine engine systems of kind dyestuff burning.Following will be combined with the drawings in the embodiments of the present invention, to the skill in the embodiment of the present invention
Art scheme is clearly and completely described, it is clear that and described embodiments are only a part of the embodiments of the present invention, rather than
Whole embodiments.Based on the embodiments of the present invention, those of ordinary skill in the art are not making creative work premise
Under every other embodiment obtained, shall fall within the protection scope of the present invention.
Embodiment 1
A kind of gas turbine engine systems of dyestuff burning, including compressor 1 and place are present embodiments provided referring to FIG. 1-2,
Device 2 is managed, 1 input terminal of compressor is connected with air inlet pipe 3, and 2 input terminal of processor is connected with input equipment 4, and 2 output end of processor connects
It is connected to controller 5,5 output end of controller is connected with fuel mixer 7, and 5 output end of controller and 1 input terminal of compressor connect
It connects, 7 output end of fuel mixer is connected with burner 8, and 8 input terminal of burner is connect with the output end of compressor 1, burner
8 output ends are connected with oxygen sensor 9, temperature sensor 10 and turbine 11, and 11 output end of turbine is connected with state analysis equipment
12 and exhaust pipe 13,12 output end of state analysis equipment be connected with sensor fault diagnosis equipment 14, sensor fault diagnosis is set
Standby 14 input terminals are connect with 10 output end of temperature sensor, 14 output end of sensor fault diagnosis equipment and 2 input terminal of processor
Connection, 13 output end of exhaust pipe are connected with heat-exchanger rig 15, and 15 output end of heat-exchanger rig is connected with air blower 16, and air blower 16 is defeated
Outlet is connect with 3 side of air inlet pipe.
In the present embodiment, by input equipment 4 by input service flow data, then handled by processor 2, then
Using controller 5 carry out control fuel mixer 7 and compressor 1 dosage how much, then compressor 1 is carried out by air inlet pipe 3
Then compressed air passes through oxygen sensor 9 and temperature sensor 10 then by compressed air delivery into burner 8
The oxygen content and temperature height in burner 8 can be understood in real time, may then pass through controller 5 and it is regulated and controled, just
It, can be preferably right by state analysis equipment 12 and sensor fault diagnosis equipment 14 in carrying out intelligent control to burner 8
Turbine 11 and sensor are detected, and the number of the carry out on-site test of existing gas turbine engine systems often, time saving province are reduced
Then power is regulated and controled by controller 5, the gas discharged by exhaust pipe 13 handles export heat through heat-exchanger rig 15, so
The outside for delivering heat to air inlet pipe 3 by air blower 16 afterwards improves the operation of the gas turbine engine systems of dyestuff burning
Efficiency ensure that the normal work of gas turbine.
Embodiment 2
Be further improved on the basis of embodiment 1 referring to FIG. 1-2: input equipment 4 includes keyboard, mouse
And touch pad, it is convenient for input instruction, 5 output end of controller is connected with alarm 6, passes through if sensor goes wrong
Sensor fault diagnosis equipment 14 transmits a signal to processor 2, and then processor 2 starts alarm 6 by controller 5, from
And it carries out notifying that staff repairs, oxygen sensor 9 and 10 data output end of temperature sensor and 2 input terminal of processor
Connection, can understand 8 inner case of burner in real time, and the port of air inlet pipe 3 and air blower 16 pass to the port of 3 side of air inlet pipe
It is structurally reasonable at a distance of one to three meter, guarantee inlet air, do not influenced by discharge exhaust gas, heat-exchanger rig 15 includes thermally conductive equipment
And exhaust equipment, it is structurally reasonable, it is convenient for energy and utilizes again, it is normal work that oxygen-sensitive content, which is arranged, in oxygen sensor 9
Make the minimum point of range, it is possible to reduce the supply number of oxygen, it is to work normally that temperature sense range, which is arranged, in temperature sensor 10
The midpoint of range guarantees the optimum temperature in work, working effect is made to reach highest.
In this practical description, it should be noted that the orientation of the instructions such as term "vertical", "upper", "lower", "horizontal" or
Person's positional relationship is orientation based on the figure or positional relationship, is merely for convenience of this practical and simplified description of description,
Rather than the device or element of instruction or hint meaning must have a particular orientation, and are constructed and grasped with specific orientation
Make, therefore should not be understood as the limitation practical to this.
In this practical description, it is also necessary to explanation, unless otherwise specific regulation and limitation, term " setting ", " peace
Dress ", " connected ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or integrally
Connection, can be mechanical connection, is also possible to be electrically connected, can be and be directly connected to, and be also possible to be connected by intermediary, can
To be the connection inside two elements.For the ordinary skill in the art, can understand as the case may be above-mentioned
Concrete meaning of the term in this is practical.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (8)
1. a kind of gas turbine engine systems of dyestuff burning, including compressor (1) and processor (2), it is characterised in that: the compression
Machine (1) input terminal is connected with air inlet pipe (3), and processor (2) input terminal is connected with input equipment (4), the processor (2)
Output end is connected with controller (5), and controller (5) output end is connected with fuel mixer (7), and the controller (5)
Output end is connect with compressor (1) input terminal, and fuel mixer (7) output end is connected with burner (8), and the burning
Device (8) input terminal is connect with the output end of compressor (1), and burner (8) output end is connected with oxygen sensor (9), temperature
Degree sensor (10) and turbine (11), turbine (11) output end are connected with state analysis equipment (12) and exhaust pipe (13),
State analysis equipment (12) output end is connected with sensor fault diagnosis equipment (14), the sensor fault diagnosis equipment
(14) input terminal is connect with temperature sensor (10) output end, sensor fault diagnosis equipment (14) output end and processor
(2) input terminal connects, and exhaust pipe (13) output end is connected with heat-exchanger rig (15), and heat-exchanger rig (15) output end connects
It is connected to air blower (16), air blower (16) output end is connect with air inlet pipe (3) side.
2. a kind of gas turbine engine systems of dyestuff burning according to claim 1, it is characterised in that: the input equipment
It (4) include keyboard, mouse and touch pad.
3. a kind of gas turbine engine systems of dyestuff burning according to claim 1, it is characterised in that: the controller (5)
Output end is connected with alarm (6).
4. a kind of gas turbine engine systems of dyestuff burning according to claim 1, it is characterised in that: the oxygen sensor
(9) it is connect with temperature sensor (10) data output end with processor (2) input terminal.
5. a kind of gas turbine engine systems of dyestuff burning according to claim 1, it is characterised in that: the air inlet pipe (3)
Port and air blower (16) pass to the port of air inlet pipe (3) side at a distance of one to three meter.
6. a kind of gas turbine engine systems of dyestuff burning according to claim 1, it is characterised in that: the heat-exchanger rig
It (15) include thermally conductive equipment and exhaust equipment.
7. a kind of gas turbine engine systems of dyestuff burning according to claim 1, it is characterised in that: the oxygen sensor
(9) setting oxygen-sensitive content is the minimum point of normal range of operation.
8. a kind of gas turbine engine systems of dyestuff burning according to claim 1, it is characterised in that: the temperature sensor
(10) setting temperature sense range is the midpoint of normal range of operation.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811206435.6A CN109386386A (en) | 2018-10-17 | 2018-10-17 | A kind of gas turbine engine systems of dyestuff burning |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811206435.6A CN109386386A (en) | 2018-10-17 | 2018-10-17 | A kind of gas turbine engine systems of dyestuff burning |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109386386A true CN109386386A (en) | 2019-02-26 |
Family
ID=65427392
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811206435.6A Pending CN109386386A (en) | 2018-10-17 | 2018-10-17 | A kind of gas turbine engine systems of dyestuff burning |
Country Status (1)
| Country | Link |
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| CN (1) | CN109386386A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH07301128A (en) * | 1994-05-02 | 1995-11-14 | Toshiba Corp | Gas turbine exhaust gas temperature control device |
| US20070125064A1 (en) * | 2004-10-20 | 2007-06-07 | Mitsubishi Heavy Industries, Ltd. | Control apparatus of extracted air booster system of integrated gasification combined cycle power plant |
| CN201943820U (en) * | 2010-09-03 | 2011-08-24 | 莫少剑 | Gas turbine system capable of realizing clean combustion of pure oxygen |
| CN102235239A (en) * | 2010-04-09 | 2011-11-09 | 通用电气公司 | System for heating an airstream by recirculating waste heat of a turbomachine |
| CN103069130A (en) * | 2010-08-06 | 2013-04-24 | 埃克森美孚上游研究公司 | Systems and methods for optimizing stoichiometric combustion |
| CN103147860A (en) * | 2005-03-02 | 2013-06-12 | 通用电气公司 | Method and apparatus for gas turbine dry low NOx combustor corrected parameter control |
| CN104141546A (en) * | 2013-05-10 | 2014-11-12 | 通用电气公司 | Gas dosage control for gas engine |
-
2018
- 2018-10-17 CN CN201811206435.6A patent/CN109386386A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH07301128A (en) * | 1994-05-02 | 1995-11-14 | Toshiba Corp | Gas turbine exhaust gas temperature control device |
| US20070125064A1 (en) * | 2004-10-20 | 2007-06-07 | Mitsubishi Heavy Industries, Ltd. | Control apparatus of extracted air booster system of integrated gasification combined cycle power plant |
| CN103147860A (en) * | 2005-03-02 | 2013-06-12 | 通用电气公司 | Method and apparatus for gas turbine dry low NOx combustor corrected parameter control |
| CN102235239A (en) * | 2010-04-09 | 2011-11-09 | 通用电气公司 | System for heating an airstream by recirculating waste heat of a turbomachine |
| CN103069130A (en) * | 2010-08-06 | 2013-04-24 | 埃克森美孚上游研究公司 | Systems and methods for optimizing stoichiometric combustion |
| CN201943820U (en) * | 2010-09-03 | 2011-08-24 | 莫少剑 | Gas turbine system capable of realizing clean combustion of pure oxygen |
| CN104141546A (en) * | 2013-05-10 | 2014-11-12 | 通用电气公司 | Gas dosage control for gas engine |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190226 |
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| RJ01 | Rejection of invention patent application after publication |