CN107701311B - A kind of high-efficiency gas turbine intake air temperature regulating system - Google Patents
A kind of high-efficiency gas turbine intake air temperature regulating system Download PDFInfo
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- CN107701311B CN107701311B CN201710991060.8A CN201710991060A CN107701311B CN 107701311 B CN107701311 B CN 107701311B CN 201710991060 A CN201710991060 A CN 201710991060A CN 107701311 B CN107701311 B CN 107701311B
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- flow deflector
- air
- flow
- gas turbine
- guide port
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Classifications
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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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/057—Control or regulation
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
- F02C7/141—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
- F02C7/143—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid before or between the compressor stages
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/95—Preventing corrosion
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Drying Of Gases (AREA)
Abstract
The invention discloses a kind of high-efficiency gas turbine intake air temperature regulating systems, it is related to gas turbine, including hollow cool-down dehumidification main body, cool-down dehumidification body interior is successively arranged pretreatment chamber, define multistage filtering room, pre-dehumidified room and the cool-down dehumidification room of connection from air inlet to gas outlet direction；Air corrosion removal device is equipped in pretreatment chamber；Dehumidifier, humidity sensor and temperature sensor one are equipped in pre-dehumidified room；Pre-dehumidified room is equipped with air guide port one and air guide port two, and the flow of air guide port one is greater than the flow of air guide port two；Surface air cooler and mixing arrangement are equipped in cool-down dehumidification room；Surface air cooler includes refrigeration coil, and refrigeration coil includes coil pipe one and coil pipe two, and the entrance of coil pipe one is connected to air guide port one and is internally provided with refrigerant, and the entrance of coil pipe two is connected to air guide port two；Mixing arrangement is equipped with branch pipe one, branch pipe two and general pipeline.When the present invention carries out cool-down dehumidification to air, the loss of cooling capacity and heat is substantially reduced, energy-saving.
Description
Technical field
The present invention relates to gas turbines, more particularly to a kind of high-efficiency gas turbine intake air temperature regulating system.
Background technique
Gas turbine is a kind of mechanical using gas as working media, internal combustion, continuous rotary, vane type thermal power.It
Mainly it is made of compressor, combustion chamber and the big component of combustion gas turbine three, compressor is from extraneous continuous sucking air and is allowed to be pressurized,
Air themperature also correspondinglys increase simultaneously；The air and fuel for being sent to combustion chamber are mixed and burned the combustion gas for becoming high temperature, high pressure；Combustion
Gas expansion work in turbine pushes turbine that compressor and generator is driven to rotate together at high speed；The exhaust gas being discharged from turbine
Drain into atmosphere nature heat release.In this way, the chemical energy of fuel is just transformed into thermal energy by gas turbine, and partial heat energy is transformed into machine
Tool energy.
There are two types of methods for the power output and the thermal efficiency for improving gas turbine: one is raising burning initial temperature, another method is
Reduce gas turbine inlet air temperature.Initial temperature of burning is an important parameter, it refers to maximum temperature achieved in circulation, at present
Defining combustion gas turbine initial temperature, there are three types of methods: one, the outlet temperature of combustion chamber；Two, the combustion after combustion gas turbine first order nozzle ring
Temperature degree；Three, to enter the mean temperature that all air mass flows of combustion gas turbine calculate.But improve combustion turbine initial temperature by
It to the limitation of turbine material and cooling technology, and reduces gas turbine inlet air temperature and is not limited by metal material etc. then, be suitable for
The gas turbine of any model.
Summer, underground chamber region moisture be mainly derived from outdoor fresh air, personnel dissipate wet and wall and dissipate wetting phase for fresh air
Bring into indoor moisture come it is more much smaller than then.So big humidity load far can not reach according to conventional air-conditioning system
Dehumidification requirements.The constant temperature unit for generalling use direct sweat cooling, due to refrigerant and the direct heat exchange of air, can achieve compared with
Low apparatus dew point, absolute humidity reduces, to achieve the purpose that dehumidifying.But it is relatively low by the air themperature of dehumidifying, it needs
Within the scope of can be only achieved reasonable supply air temperature difference by reheating.When dehumidifying, then whole air cooling-down dehumidifying add by electricity
Hot device heater riser temperature.In this process, low caused by dehumidifying since the refrigerating capacity that air needs is much larger than the load in room
Warm air promotes temperature by heater again, also needs to consume a large amount of heating amount, the loss of cold and hot neutralization is quite big.
Summary of the invention
The present invention in view of the above technical problems, the shortcomings that overcoming the prior art, provides a kind of high-efficiency gas turbine air inlet temperature
Spend regulating system, when the air of gas handling system carries out cool-down dehumidification, cooling capacity and heat due to dehumidifying caused by lose and be substantially reduced,
It realizes energy-saving.
In order to solve the above technical problems, the present invention provides a kind of high-efficiency gas turbine intake air temperature regulating system, including
Hollow cool-down dehumidification main body, cool-down dehumidification main body include air inlet and air outlet, cool-down dehumidification body interior from air inlet to
Gas outlet direction is successively arranged pretreatment chamber, define multistage filtering room, pre-dehumidified room and the cool-down dehumidification room of connection；
Air corrosion removal device is equipped in pretreatment chamber；
It is equipped with multistage filter in multistage filtering room, multistage filter includes primary filter, intermediate filter and advanced
Filter；
Dehumidifier, humidity sensor and temperature sensor one are equipped in pre-dehumidified room；Pre-dehumidified room is equipped with one He of air guide port
Air guide port two, the flow of air guide port one are greater than the flow of air guide port two；
Surface air cooler and mixing arrangement are equipped in cool-down dehumidification room；Surface air cooler includes refrigeration coil, and refrigeration coil includes coil pipe
One and coil pipe two, the entrance connection air guide port one of coil pipe one and it is internally provided with refrigerant, the entrance of coil pipe two is connected to air guide port
Two；Mixing arrangement is equipped with branch pipe one, branch pipe two and general pipeline, and branch pipe one is connected to the outlet of coil pipe one, and branch pipe two is connected to coil pipe two
Outlet, the outlet of branch pipe one and branch pipe two is respectively communicated with general pipeline, the gas outlet of the outlet cool-down dehumidification main body of general pipeline.
Technical effect: the inlet air of gas handling system is divided into two parts, the coil pipe that a part passes through surface air cooler by the present invention
One progress deep cooling dehumidifying and cooling, another part then by the coil pipe two of not refrigerant, then again mix two parts air
The state that can extremely blow is blown, and is neutralized using the temperature difference and psychrometric difference of two parts air, to reach energy conservation
The purpose of consumption reduction.
The technical solution that the present invention further limits is:
Further, pre-dehumidified room further includes controller one, and controller one is controlled by receiving the signal of humidity sensor
Dehumidifier；Controller one controls surface air cooler by receiving the signal of humidity sensor and temperature sensor one.
A kind of preceding high-efficiency gas turbine intake air temperature regulating system is respectively equipped at air guide port one and air guide port two
Flow control valve one and flow control valve two, controller one receive the signal of humidity sensor and temperature sensor one and control stream
Control valve one and flow control valve two.
A kind of preceding high-efficiency gas turbine intake air temperature regulating system is additionally provided with temperature sensor two in general pipeline, mixes
Attach together that set further include controller two, branch pipe one is equipped with flow control valve three, temperature sensor two, flow control valve three with control
Device two processed connects, and controller two receives the signal of temperature sensor two and controls the flow of flow control valve three.
A kind of preceding high-efficiency gas turbine intake air temperature regulating system, the interior flow-guiding channel with screw type of general pipeline,
Branch pipe one connects the same nozzle of general pipeline with the outlet of branch pipe two.
A kind of preceding high-efficiency gas turbine intake air temperature regulating system, general pipeline is interior to be equipped with guiding subassembly, guiding subassembly
Including axis piece and several guide vanes, guide vane is uniformly distributed in the length direction of axis piece, and each guide vane includes water conservancy diversion
Piece one, flow deflector two, flow deflector three and flow deflector four, flow deflector one, flow deflector two, flow deflector three are identical with flow deflector four
And its shape is sector, curved edge is bonded with total inside pipe wall, flow deflector one and flow deflector two and flow deflector three and water conservancy diversion
Piece four is respectively arranged on the upper and lower position of two sides, and flow deflector one is connected with flow deflector three in top, flow deflector one and flow deflector two with
And flow deflector three is connected with flow deflector four respectively at side, axis piece level is interspersed between flow deflector one and flow deflector two, side
Flow deflector one and the flow deflector three and flow deflector four of flow deflector two and the other side be located at the front and back two in axis leaf length direction
On a position.
A kind of preceding high-efficiency gas turbine intake air temperature regulating system, the adjacent regions of flow deflector one and flow deflector two
Arranged in a crossed manner, flow deflector three and the adjacent regions of flow deflector four are arranged in a crossed manner.
A kind of preceding high-efficiency gas turbine intake air temperature regulating system, air corrosion removal device includes setting gradually
Alkaline cleaner and anti-salt damage filter device, anti-salt damage filter device include the coarse strainer and close strainer of overlapping, coarse strainer and close filter
Net is made of hydrophobic ultrafine glass fibre.
The beneficial effects of the present invention are:
(1) effect of pre-dehumidified room is tentatively dehumidified when inlet air humidity is very big in the present invention, after mitigating
Burden when continuous processing；
(2) each processing step can be realized automatic detection in the present invention, and real time monitoring is adjusted, so as to more precisely
Ground controls the processing parameter of each step；
(3) mixing diversion pipe mixes two parts air shunted more uniformly in the present invention, so that air be made to reach
Good ventilation state；
(4) air corrosion removal device can pre-process air in the present invention, remove sulfur dioxide, salt etc. in air
Corrosive substance prevents the blade of air corrosion gas turbine, ensures the runnability of gas turbine.
Detailed description of the invention
Fig. 1 is the system diagram of the present embodiment；
Fig. 2 is the inner manifold structural schematic diagram of the present embodiment；
Wherein: 1, general pipeline；2, axis piece；3, guide vane；301, flow deflector one；302, flow deflector two；303, flow deflector three；
304, flow deflector four.
Specific embodiment
A kind of high-efficiency gas turbine intake air temperature regulating system provided in this embodiment, structure are as shown in Figs. 1-2.
The system includes hollow cool-down dehumidification main body, and cool-down dehumidification main body includes air inlet and air outlet.Cool-down dehumidification
Body interior is successively arranged pretreatment chamber, define multistage filtering room, pre-dehumidified room and the cooling of connection from air inlet to gas outlet direction
Moist chamber.
Air corrosion removal device is equipped in pretreatment chamber.Air corrosion removal device includes the alkaline cleaner set gradually and prevents
Salt damage filter device, anti-salt damage filter device include the coarse strainer and close strainer of overlapping, and coarse strainer and close strainer are by hydrophobicity
Ultra-fine fibre glass is made.
It is equipped with multistage filter in multistage filtering room, multistage filter includes primary filter, intermediate filter and advanced
Filter.
Dehumidifier, humidity sensor and temperature sensor one are equipped in pre-dehumidified room, pre-dehumidified room is equipped with one He of air guide port
Air guide port two, the flow of air guide port one are greater than the flow of air guide port two.
Surface air cooler and mixing arrangement are equipped in cool-down dehumidification room.Surface air cooler includes refrigeration coil, and refrigeration coil includes coil pipe
One and coil pipe two, the entrance connection air guide port one of coil pipe one and it is internally provided with refrigerant, the entrance of coil pipe two is connected to air guide port
Two.
Pre-dehumidified room further includes controller one.Controller one controls dehumidifier by receiving the signal of humidity sensor；Control
Device one processed controls surface air cooler by receiving the signal of humidity sensor and temperature sensor one.Air guide port one and air guide port two are punished
Not She You flow control valve one and flow control valve two, controller one receives the signal of humidity sensor and temperature sensor one simultaneously
Control the flow of flow control valve one and flow control valve two.
Mixing arrangement is equipped with branch pipe one, branch pipe two and general pipeline 1, and branch pipe one is connected to the outlet of coil pipe one, and branch pipe two is connected to disk
The outlet of pipe two, the outlet of branch pipe one and branch pipe two are respectively communicated with general pipeline 1, and the outlet cool-down dehumidification main body of general pipeline 1 goes out
Port.Temperature sensor two is additionally provided in general pipeline 1, mixing arrangement further includes controller two, and branch pipe one is equipped with flow control valve
Three, temperature sensor two, flow control valve three are connect with controller two, and controller two receives the signal of temperature sensor two simultaneously
Control the flow of flow control valve three.
There is the flow-guiding channel of screw type, branch pipe one connects the same nozzle of general pipeline 1 with the outlet of branch pipe two in general pipeline 1.
Guiding subassembly is equipped in general pipeline 1, guiding subassembly includes axis piece 2 and several guide vanes 3, and guide vane 3 is uniformly distributed in axis piece 2
Length direction, each guide vane 3 include flow deflector 1, flow deflector 2 302, flow deflector 3 303 and flow deflector 4 304,
Flow deflector 1, flow deflector 2 302, flow deflector 3 303 are identical with flow deflector 4 304 and its shape is sector, arc
Edge is bonded with 1 inner wall of general pipeline, and flow deflector 1 and flow deflector 2 302 and flow deflector 3 303 and flow deflector 4 304 are distinguished
Set on the upper and lower position of two sides, flow deflector 1 is connected with flow deflector 3 303 in top, flow deflector 1 and flow deflector two
302 and flow deflector 3 303 connected with flow deflector 4 304 respectively at side, 2 level of axis piece is interspersed in flow deflector 1 and leads
Between flow 2 302, the flow deflector 1 and flow deflector 2 302 of side and the flow deflector 3 303 and flow deflector four of the other side
304 are located on former and later two positions of 2 length direction of axis piece, and the adjacent regions of flow deflector 1 and flow deflector 2 302 are handed over
Fork setting, flow deflector 3 303 and the adjacent regions of flow deflector 4 304 are arranged in a crossed manner.
Air enters intake air temperature regulating system, enters pre-dehumidified room from the air inlet of cool-down dehumidification main body；Pre-dehumidified room
The moisture signal of interior humidity sensor detection air is simultaneously transferred to controller one, and controller one judges whether according to the signal value
Control dehumidifier is tentatively dehumidified；Meanwhile controller one controls flow control valve one and flow control valve according to the signal value
Two uninterrupted, air respectively enter the coil pipe one and coil pipe two of surface air cooler from the air guide port one and air guide port two of pre-dehumidified room
It is interior；At this point, detecting the initial temperature of air by temperature sensor one and being transferred to controller one, controller one is according to the temperature
Value controls the one refrigerating state parameter of coil pipe of surface air cooler, and the air in coil pipe one is mixed by entering after refrigerant progress depth dehumidifying
The branch pipe one set is attached together, and the air in coil pipe two then enters branch pipe two in the case where parameter state is constant；Temperature sensor
Two detect the temperature of the air in branch pipe one and are transferred to controller two, and controller two controls flow control according to the temperature value
The uninterrupted of valve three, so that the air that branch pipe one and branch pipe two come out obtains optimum proportioning；Two parts air is from general pipeline 1
Into by constantly merging during guiding subassembly, the acquisition uniform air of state is finally reached good air-supply shape
State.
In addition to the implementation, the present invention can also have other embodiments.It is all to use equivalent substitution or equivalent transformation shape
At technical solution, fall within the scope of protection required by the present invention.
Claims (8)
1. a kind of high-efficiency gas turbine intake air temperature regulating system, it is characterised in that: described including hollow cool-down dehumidification main body
Cool-down dehumidification main body includes air inlet and air outlet, the cool-down dehumidification body interior from the air inlet to gas outlet direction according to
Secondary pretreatment chamber, define multistage filtering room, pre-dehumidified room and the cool-down dehumidification room for being equipped with connection；
Air corrosion removal device is equipped in the pretreatment chamber；
Be equipped with multistage filter in the multistage filtering room, the multistage filter include primary filter, intermediate filter and
Advanced filter；
Dehumidifier, humidity sensor and temperature sensor one are equipped in the pre-dehumidified room；The pre-dehumidified room is equipped with air guide port
One and air guide port two, the flow of the air guide port one is greater than the flow of the air guide port two；
Surface air cooler and mixing arrangement are equipped in the cool-down dehumidification room；The surface air cooler includes refrigeration coil, the refrigeration coil
Including coil pipe one and coil pipe two, the entrance of the coil pipe one is connected to the air guide port one and is internally provided with refrigerant, the disk
The entrance of pipe two is connected to the air guide port two；The mixing arrangement is equipped with branch pipe one, branch pipe two and general pipeline (1), the branch pipe one
It is connected to the outlet of the coil pipe one, the branch pipe two is connected to the outlet of the coil pipe two, the outlet of the branch pipe one and branch pipe two
It is respectively communicated with general pipeline (1), the gas outlet of cool-down dehumidification main body described in the outlet of the general pipeline (1).
2. a kind of high-efficiency gas turbine intake air temperature regulating system according to claim 1, it is characterised in that: described pre- to remove
Moist chamber further includes controller one, and the controller one controls the dehumidifier by receiving the signal of humidity sensor；The control
Device one processed controls the surface air cooler by receiving the signal of humidity sensor and temperature sensor one.
3. a kind of high-efficiency gas turbine intake air temperature regulating system according to claim 2, it is characterised in that: the air guide
Flow control valve one and flow control valve two are respectively equipped at mouth one and air guide port two, the controller one receives the humidity and passes
The signal of sensor and temperature sensor one simultaneously controls the flow control valve one and flow control valve two.
4. a kind of high-efficiency gas turbine intake air temperature regulating system according to claim 3, it is characterised in that: the general pipeline
(1) it is additionally provided with temperature sensor two in, the mixing arrangement further includes controller two, and the branch pipe one is equipped with flow control valve
Three, the temperature sensor two, flow control valve three are connect with the controller two, and the controller two receives temperature sensing
The signal of device two and the flow for controlling the flow control valve three.
5. a kind of high-efficiency gas turbine intake air temperature regulating system according to claim 1, it is characterised in that: the general pipeline
(1) there is the flow-guiding channel of screw type, the branch pipe one connects the same nozzle of the general pipeline (1) with the outlet of branch pipe two in.
6. a kind of high-efficiency gas turbine intake air temperature regulating system according to claim 5, it is characterised in that: the general pipeline
(1) guiding subassembly is equipped in, the guiding subassembly includes axis piece (2) and several guide vanes (3), and the guide vane (3) is equal
The even length direction for being distributed in the axis piece (2), each guide vane (3) includes flow deflector one (301), flow deflector two
(302), flow deflector three (303) and flow deflector four (304), the flow deflector one (301), flow deflector two (302), flow deflector three
(303) identical with flow deflector four (304) and its shape is sector, and curved edge is bonded with the general pipeline (1) inner wall, institute
It states flow deflector one (301) and flow deflector two (302) and the flow deflector three (303) and flow deflector four (304) is respectively arranged on two
The upper and lower position of side, the flow deflector one (301) connect with flow deflector three (303) in top, the flow deflector one (301) and lead
Flow two (302) and the flow deflector three (303) are connected with flow deflector four (304) respectively at side, and the axis piece (2) is horizontal
It is interspersed between the flow deflector one (301) and flow deflector two (302), the flow deflector one (301) and flow deflector two of side
(302) axis piece (2) length direction is located at the flow deflector three (303) of the other side and flow deflector four (304)
On former and later two positions.
7. a kind of high-efficiency gas turbine intake air temperature regulating system according to claim 6, it is characterised in that: the water conservancy diversion
Piece one (301) and the adjacent regions of flow deflector two (302) are arranged in a crossed manner, the flow deflector three (303) and flow deflector four (304)
Adjacent regions are arranged in a crossed manner.
8. a kind of high-efficiency gas turbine intake air temperature regulating system according to claim 1, it is characterised in that: the air
Corrosion removal device includes the alkaline cleaner set gradually and anti-salt damage filter device, and the anti-salt damage filter device includes overlapping
Coarse strainer and close strainer, the coarse strainer and close strainer are made of hydrophobic ultrafine glass fibre.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710991060.8A CN107701311B (en) | 2017-10-23 | 2017-10-23 | A kind of high-efficiency gas turbine intake air temperature regulating system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710991060.8A CN107701311B (en) | 2017-10-23 | 2017-10-23 | A kind of high-efficiency gas turbine intake air temperature regulating system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107701311A CN107701311A (en) | 2018-02-16 |
| CN107701311B true CN107701311B (en) | 2019-09-13 |
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ID=61182675
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710991060.8A Active CN107701311B (en) | 2017-10-23 | 2017-10-23 | A kind of high-efficiency gas turbine intake air temperature regulating system |
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| Country | Link |
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| CN (1) | CN107701311B (en) |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1198197A (en) * | 1995-08-24 | 1998-11-04 | 查里斯·R·科伦伯格 | Method and apparatus for cooling inlet air of gas turbine and internal combustion engine prime movers |
| CN104511214A (en) * | 2014-11-28 | 2015-04-15 | 成都博世德能源科技股份有限公司 | Efficient air inlet device used for gas turbine |
| CN205400907U (en) * | 2016-03-03 | 2016-07-27 | 北京石油化工学院 | Miniature for gas turbine gas mixer of external -burning marsh gas |
-
2017
- 2017-10-23 CN CN201710991060.8A patent/CN107701311B/en active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1198197A (en) * | 1995-08-24 | 1998-11-04 | 查里斯·R·科伦伯格 | Method and apparatus for cooling inlet air of gas turbine and internal combustion engine prime movers |
| CN104511214A (en) * | 2014-11-28 | 2015-04-15 | 成都博世德能源科技股份有限公司 | Efficient air inlet device used for gas turbine |
| CN205400907U (en) * | 2016-03-03 | 2016-07-27 | 北京石油化工学院 | Miniature for gas turbine gas mixer of external -burning marsh gas |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107701311A (en) | 2018-02-16 |
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