CN114100388A - Gas-liquid mixing and pressurizing device for gas turbine - Google Patents
Gas-liquid mixing and pressurizing device for gas turbine Download PDFInfo
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- CN114100388A CN114100388A CN202111150007.8A CN202111150007A CN114100388A CN 114100388 A CN114100388 A CN 114100388A CN 202111150007 A CN202111150007 A CN 202111150007A CN 114100388 A CN114100388 A CN 114100388A
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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
- F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
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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
- F02C7/22—Fuel supply systems
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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
- F02C7/22—Fuel supply systems
- F02C7/224—Heating fuel before feeding to the burner
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Abstract
The invention discloses a gas-liquid mixing and pressurizing device for a gas turbine, which has the beneficial effects that gas-liquid raw materials generate high-speed rotating airflow in a mixing box through a pressurizing and mixing structure, and the phenomena of uneven liquid drainage, incomplete support combustion or insufficient fuel in the extrusion process of liquid atomization in the mixing box are avoided. The utility model provides a gas-liquid mixing pressure device for gas turbine, includes a pair of mixing box, gas turbine, the former case of liquid and production support, and is a pair of the mixing box gas turbine and the former case of liquid install in on the production support, install the transfer structure on the production support, the transfer structural connection is in a pair of the mixing box and on the gas turbine, it is a pair of install the pressurization mixed structure in the mixing box, install heat cycle structure on the gas turbine, heat cycle structure connect in the transfer is structural.
Description
Technical Field
The invention relates to the technical field of heat mixing of gas turbines, in particular to a gas-liquid mixing and pressurizing device for a gas turbine.
Background
The Gas Turbine (Gas Turbine) is an internal combustion type power machine which takes continuously flowing Gas as a working medium to drive an impeller to rotate at a high speed and converts the energy of fuel into useful work, and is a rotary impeller type heat engine; the compressed air enters a combustion chamber, is mixed with the injected fuel and then is combusted to form high-temperature gas, and then flows into a gas turbine to expand and do work to push a turbine impeller to drive a compressor impeller to rotate together; the work-doing capability of the heated high-temperature gas is obviously improved, so that the gas turbine still has residual work as the output mechanical work of the gas turbine while driving the compressor. When gas and liquid are mixed, the gas and liquid are mixed and extruded into a gas turbine after atomization and spraying are needed, the phenomenon of uneven liquid drainage and the phenomenon of incomplete support combustion or insufficient fuel are easy to occur in the extrusion process, and therefore, the scheme is generated by intensive research aiming at the problems.
Disclosure of Invention
The technical scheme of the invention for realizing the aim is as follows: the gas-liquid mixing and pressurizing device for the gas turbine comprises a pair of mixing boxes, the gas turbine, a liquid raw material box and a production support, wherein the mixing boxes, the gas turbine and the liquid raw material box are arranged on the production support;
the pressurized mixing structure comprises: the device comprises a pair of pressure driving machines, a pair of pressure transmission helical gears, a pair of pressure driving helical gears, a pair of pressure threaded pipes, a pair of pressure threaded rods, a pair of pressure extrusion plates, a pair of concave driving circular ring blocks, a plurality of concave driving circular ring blocks, a pair of driving square-wave discs, a plurality of driving circular discs, a plurality of driving magnetic iron blocks, a pair of stirring driving machines, a pair of stirring driving helical gears, a pair of stirring transmission square-wave helical gears and a plurality of stirring blades;
the pair of pressure driving machines are respectively arranged on the top ends of the pair of mixing boxes, the pair of pressure threaded pipes are respectively inserted on the pair of mixing boxes through bearings, the pair of pressure threaded rods are respectively movably inserted on the inner sides of the pair of pressure threaded pipes, the pair of pressure driving bevel gears are respectively arranged on the driving ends of the pair of pressure driving machines, the pair of pressure driving bevel gears are respectively engaged with the pair of pressure transmission bevel gears, the pair of pressure extrusion plates are respectively arranged on the pair of pressure threaded rods, the pair of concave driving circular ring blocks are respectively arranged on the top ends of the pair of pressure extrusion plates, the pair of driving circular discs are respectively movably inserted on the inner sides of the pair of concave driving circular ring blocks, and the plurality of concave driving circular ring blocks are respectively arranged on the pair of pressure extrusion plates in a circular shape, the stirring driving bevel gear is installed on the driving end of the stirring driving machine, and the stirring driving bevel gear is respectively engaged with the stirring driving bevel gear and is a plurality of in a pair of the driving bevel gear, a plurality of the driving magnet blocks are respectively installed on the driving bevel gear, and a plurality of the driving magnet blocks are respectively installed on the driving bevel gear and are a plurality of in the driving disk, and a plurality of the stirring pieces are respectively installed on the driving disk.
Preferably, the relay structure includes: the device comprises a pair of liquid transfer boxes, a pair of air transfer boxes, a hydraulic box, a liquid pump, a hydraulic flow dividing pipe, two pairs of extrusion hydraulic cylinders, two pairs of transfer extrusion plates, two pairs of transfer valves and a pair of feeding sealing valves;
a pair of the liquid transfer boxes and a pair of the air transfer boxes are arranged on the production bracket, two pairs of the transfer valves are respectively arranged on the pair of the liquid transfer boxes and the pair of the air transfer boxes, and the other ends of the two pairs of transfer valves are respectively connected to a pair of mixing boxes, a pair of feeding sealing valves are respectively arranged on the pair of mixing boxes, and a pair of the feeding sealing valves are respectively connected to the gas turbine, two pairs of the extrusion hydraulic cylinders are respectively arranged at the inner sides of a pair of the liquid transfer boxes and a pair of the air transfer boxes, two pairs of the transfer extrusion plates are respectively arranged at the pushing ends of two pairs of the extrusion hydraulic cylinders, the hydraulic tank is arranged on the production bracket, the liquid pump is arranged on the hydraulic tank, the hydraulic shunt tubes are arranged on the liquid pump and are respectively connected to the pushing ends of the two pairs of extrusion hydraulic cylinders.
Preferably, the heat circulation structure comprises: the air exhaust pipe comprises an air exhaust pipe, an air suction pump, an air exhaust valve, four pairs of air exhaust flow dividing pipes, a plurality of heat dissipation pipes, two pairs of square-shaped limiting blocks and a plurality of heat dissipation circular ring pieces;
the blast pipe install in gas turbine is last, the aspiration pump install in on the blast pipe, exhaust valve install in on the aspiration pump, four are right exhaust shunt tubes cartridge respectively in a pair of liquid transfer box and a pair of on the both sides of air transfer box, and four are right exhaust shunt tubes connect respectively in on the exhaust valve, a plurality of the cooling tube is connected respectively in four right exhaust on the shunt tubes, a plurality of the heat dissipation ring piece is installed respectively in a plurality of on the cooling tube, two pairs the shape stopper of returning is installed respectively in a pair of liquid transfer box and a pair of on the air transfer box.
Preferably, a pair of the mixing tanks, a pair of the liquid transfer tanks, and a pair of the air transfer tanks are respectively provided with a pressure sensor inside.
Preferably, the exhaust pipe and the four pairs of exhaust branch pipes are provided with heat insulation layers on the outer sides.
Preferably, a pair of coil pipes is respectively arranged on the inner sides of the pair of mixing boxes, and the two pairs of coil pipes are respectively connected to the two pairs of transfer valves.
Preferably, the outer sides of the concave transmission circular ring blocks are provided with plastic layers.
Preferably, a plurality of concave type transmission ring piece and a pair of the inboard of concave type drive ring piece have seted up the auxiliary ball groove respectively, a plurality of be provided with the plastics ball groove pad in the auxiliary ball groove respectively, a plurality of the inboard of plastics ball groove pad is provided with the plastics ball respectively.
Preferably, a temperature sensor is provided inside each of the pair of mixing tanks, the pair of liquid transfer tanks, and the pair of air transfer tanks.
Preferably, a liquid level meter is respectively arranged on each pair of the liquid transfer boxes.
According to the gas-liquid mixing and pressurizing device for the gas turbine, which is manufactured by the technical scheme of the invention, gas-liquid raw materials generate high-speed rotating airflow in the mixing box through the pressurizing and mixing structure, so that the phenomenon that the gas-liquid is not uniformly mixed due to the fact that liquid is directly atomized and extruded in the mixing box, water vapor is liquefied into small water drops when meeting cold and is attached to the inner side of the mixing box, the phenomenon that the gas turbine is not uniformly combusted or insufficient fuel is generated in the using process is avoided, meanwhile, the air and the fuel liquid need to be preheated firstly during combustion, the phenomenon that the air and the fuel liquid are excessively liquefied and combusted to absorb heat is avoided, and the heat in smoke after combustion is converted into the preheating heat source of the air and the fuel liquid.
Drawings
Fig. 1 is a schematic front view of a gas-liquid mixing and pressurizing device for a gas turbine according to the present invention.
Fig. 2 is a schematic side view of a gas-liquid mixing and pressurizing device for a gas turbine according to the present invention.
Fig. 3 is a schematic top view of the gas-liquid mixing and pressurizing device for a gas turbine according to the present invention.
Fig. 4 is an enlarged view of a portion "a" in fig. 1.
Fig. 5 is an enlarged view of a portion "B" in fig. 3.
In the figure: 1. a mixing box; 2. a gas turbine; 3. a liquid feedstock tank; 4. producing a bracket; 5. a feeding sealing valve; 6. a pressure driver; 7. pressurizing the transmission helical gear; 8. pressurizing and driving the bevel gear; 9. a pressurized threaded pipe; 10. a pressurized threaded rod; 11. pressing the extrusion plate; 12. a concave driving circular ring block; 13. a concave transmission circular ring block; 14. driving the clip disk; 15. a transmission disc; 16. a driving magnet block; 17. a transmission magnet block; 18. a stirring driver; 19. stirring the driving bevel gear; 20. stirring and driving the square bevel gear; 21. a stirring sheet; 22. a liquid transfer tank; 23. an air transfer box; 24. a hydraulic tank; 25. a liquid pump; 26. a hydraulic shunt tube; 27. an extrusion hydraulic cylinder; 28. transferring the extrusion plate; 29. a transfer valve.
Detailed Description
The present invention will be described in detail with reference to the accompanying drawings, and as shown in fig. 1 to 5, a gas-liquid mixing and pressurizing device for a gas turbine 2 includes a pair of mixing tanks 1, a gas turbine 2, a liquid raw material tank 3, and a production support 4, wherein the pair of mixing tanks 1, the gas turbine 2, and the liquid raw material tank 3 are mounted on the production support 4, a transfer structure is mounted on the production support 4, the transfer structure is connected to the pair of mixing tanks 1 and the gas turbine 2, a pressurizing and mixing structure is mounted in the pair of mixing tanks 1, a heat circulation structure is mounted on the gas turbine 2, and the heat circulation structure is connected to the transfer structure; the pressurized mixing structure comprises: a pair of pressure driving machines 6, a pair of pressure transmission bevel gears 7, a pair of pressure driving bevel gears 8, a pair of pressure threaded pipes 9, a pair of pressure threaded rods 10, a pair of pressure extrusion plates 11, a pair of concave driving circular ring blocks 12, a plurality of concave driving circular ring blocks 13, a pair of driving circular disc 14, a plurality of driving circular disc 15, a plurality of driving magnet blocks 16, a plurality of driving magnet blocks 17, a pair of stirring driving machines 18, a pair of stirring driving bevel gears 19, a pair of stirring transmission circular bevel gears 20 and a plurality of stirring blades 21; a pair of said pressure driving machines 6 are respectively mounted on the top ends of a pair of said mixing tanks 1, a pair of said pressure threaded pipes 9 are respectively inserted on a pair of said mixing tanks 1 through bearings, a pair of said pressure threaded rods 10 are respectively movably inserted on the inner sides of a pair of said pressure threaded pipes 9, a pair of said pressure driving helical gears 8 are respectively mounted on the driving ends of a pair of said pressure driving machines 6, and a pair of said pressure driving helical gears 8 are respectively gear-engaged with a pair of said pressure transmission helical gears 7, a pair of said pressure extrusion plates 11 are respectively mounted on a pair of said pressure threaded rods 10, a pair of said concave driving circular blocks 12 are respectively mounted on the top ends of a pair of said pressure extrusion plates 11, a pair of said driving circular discs 14 are respectively movably inserted on the inner sides of a pair of said concave driving circular blocks 12, a plurality of said concave driving circular blocks 13 are respectively circularly mounted on a pair of said pressure extrusion plates 11, the plurality of transmission discs 15 are respectively movably inserted into the inner sides of the plurality of concave transmission circular ring blocks 13, a pair of stirring transmission circular bevel gears 20 are respectively installed on the pair of driving circular ring blocks 14, a pair of stirring drivers 18 are respectively installed on the pair of concave transmission circular ring blocks 12, a pair of stirring driving bevel gears 19 are respectively installed on the driving ends of the pair of stirring drivers 18, the pair of stirring driving bevel gears 19 are respectively engaged with the pair of stirring transmission circular bevel gears 20, the plurality of driving magnet blocks 16 are respectively installed on the pair of driving circular ring blocks 14, the plurality of transmission magnet blocks 17 are respectively installed on the plurality of transmission discs 15, and the plurality of stirring blades 21 are respectively installed on the plurality of transmission discs 15; the transfer structure includes: a pair of liquid transfer boxes 22, a pair of air transfer boxes 23, a hydraulic box 24, a liquid pump 25, a hydraulic shunt tube 26, two pairs of extrusion hydraulic cylinders 27, two pairs of transfer extrusion plates 28, two pairs of transfer valves 29 and a pair of feeding sealing valves 5; a pair of the liquid transfer boxes 22 and a pair of the air transfer boxes 23 are mounted on the production support 4, two pairs of the transfer valves 29 are respectively mounted on the pair of the liquid transfer boxes 22 and the pair of the air transfer boxes 23, the other ends of the two pairs of the transfer valves 29 are respectively connected to the pair of the mixing boxes 1, a pair of the feeding sealing valves 5 are respectively mounted on the pair of the mixing boxes 1, the pair of the feeding sealing valves 5 are respectively connected to the gas turbine 2, two pairs of the extrusion hydraulic cylinders 27 are respectively mounted on the inner sides of the pair of the liquid transfer boxes 22 and the pair of the air transfer boxes 23, two pairs of the transfer extrusion plates 28 are respectively mounted on the pushing ends of the two pairs of the extrusion hydraulic cylinders 27, the hydraulic boxes 24 are mounted on the production support 4, and the liquid pump 25 is mounted on the hydraulic boxes 24, the hydraulic shunt tubes 26 are installed on the liquid pump 25, and the hydraulic shunt tubes 26 are respectively connected to the pushing ends of the two pairs of extrusion hydraulic cylinders 27; the heat circulation structure comprises: the air exhaust pipe comprises an air exhaust pipe, an air suction pump, an air exhaust valve, four pairs of air exhaust flow dividing pipes, a plurality of heat dissipation pipes, two pairs of square-shaped limiting blocks and a plurality of heat dissipation circular ring pieces; the exhaust pipe is mounted on the gas turbine 2, the air pump is mounted on the exhaust pipe, the exhaust valve is mounted on the air pump, four pairs of exhaust flow dividing pipes are respectively inserted on two sides of a pair of the liquid transfer box 22 and a pair of the air transfer box 23, the four pairs of exhaust flow dividing pipes are respectively connected to the exhaust valve, a plurality of the radiating pipes are respectively connected to the four pairs of exhaust flow dividing pipes, a plurality of the radiating circular ring pieces are respectively mounted on a plurality of the radiating pipes, and two pairs of the clip-shaped limiting blocks are respectively mounted on a pair of the liquid transfer box 22 and a pair of the air transfer box 23; pressure sensors are respectively arranged on the inner sides of the pair of mixing boxes 1, the pair of liquid transfer boxes 22 and the pair of air transfer boxes 23; heat insulation layers are arranged on the outer sides of the exhaust pipe and the four pairs of exhaust flow dividing pipes; a pair of coil pipes are respectively arranged on the inner sides of the mixing boxes 1, and the two pairs of coil pipes are respectively connected to the two pairs of transfer valves 29; a plastic layer is arranged on the outer sides of the concave transmission circular ring blocks 13; auxiliary ball grooves are respectively formed in the inner sides of the plurality of concave transmission circular ring blocks 13 and the pair of concave driving circular ring blocks 12, plastic ball groove pads are respectively arranged in the plurality of auxiliary ball grooves, and plastic balls are respectively arranged on the inner sides of the plurality of plastic ball groove pads; temperature sensors are respectively arranged on the inner sides of the pair of mixing tanks 1, the pair of liquid transfer tanks 22 and the pair of air transfer tanks 23; a liquid level meter is provided on each of the pair of liquid transfer tanks 22.
The embodiment is characterized by comprising a pair of mixing boxes, a gas turbine, a liquid raw material box and a production support, wherein the mixing boxes, the gas turbine and the liquid raw material box are arranged on the production support; the pressurized mixing structure comprises: the device comprises a pair of pressure driving machines, a pair of pressure transmission helical gears, a pair of pressure driving helical gears, a pair of pressure threaded pipes, a pair of pressure threaded rods, a pair of pressure extrusion plates, a pair of concave driving circular ring blocks, a plurality of concave driving circular ring blocks, a pair of driving square-wave discs, a plurality of driving circular discs, a plurality of driving magnetic iron blocks, a pair of stirring driving machines, a pair of stirring driving helical gears, a pair of stirring transmission square-wave helical gears and a plurality of stirring blades; a pair of pressure driving machines are respectively arranged on the top ends of a pair of mixing boxes, a pair of pressure threaded pipes are respectively inserted on the pair of mixing boxes through bearings, a pair of pressure threaded rods are respectively movably inserted on the inner sides of the pair of pressure threaded pipes, a pair of pressure driving helical gears are respectively arranged on the driving ends of the pair of pressure driving machines, the pair of pressure driving helical gears are respectively engaged with the pair of pressure driving helical gears, a pair of pressure extrusion plates are respectively arranged on the pair of pressure threaded rods, a pair of concave driving circular blocks are respectively arranged on the top ends of the pair of pressure extrusion plates, a pair of driving circular discs are respectively movably inserted on the inner sides of the pair of concave driving circular blocks, a plurality of concave driving circular blocks are respectively arranged on the pair of pressure extrusion plates in a circular shape, a plurality of driving circular discs are respectively movably inserted on the inner sides of the plurality of concave driving circular blocks, a pair of stirring driving circular helical gears are respectively arranged on the pair of driving circular discs, the stirring driving device comprises a pair of concave driving circular blocks, a pair of stirring driving bevel gears, a plurality of driving magnet blocks, a plurality of stirring sheets and a plurality of stirring driving circular discs, wherein the stirring driving circular blocks are respectively arranged on the concave driving circular blocks; produce the high-speed rotatory air current of gas-liquid raw materials in the mixing box through pressurization mixed structure, it is inhomogeneous to have avoided direct liquid atomization extrusion production gas-liquid mixture in the mixing box, vapor meets the inboard that cold can liquefy into the water droplet and adhere to the mixing box, produce gas turbine and appear burning inhomogeneous or the not enough phenomenon of fuel appearing in the use, air and liquid fuel need preheat earlier when burning simultaneously, both can avoid liquefying and the too much phenomenon of burning heat absorption to appear, through the heat conversion in the smog after will burning for the preheating heat source of air and liquid fuel.
All the electrical components in the present application are connected with the power supply adapted to the electrical components through the wires, and an appropriate controller should be selected according to actual conditions to meet control requirements, and specific connection and control sequences.
Example (b): the smoke in the gas turbine 2 is guided to the exhaust pipe by the air pump, the smoke is guided to four pairs of exhaust branch pipes by the air exhaust valve, the smoke is guided to a plurality of radiating pipes by the four pairs of exhaust branch pipes, the heat is respectively radiated to the inner sides of a pair of liquid transfer boxes 22 and a pair of air transfer boxes 23 by the radiating circular ring sheets on the radiating pipes, meanwhile, the transfer extrusion plates 28 on the pushing ends of two pairs of extrusion hydraulic cylinders 27 are respectively driven by the expansion of two pairs of extrusion hydraulic cylinders 27, the lifting in the pair of liquid transfer boxes 22 and the pair of air transfer boxes 23 are respectively installed by the two pairs of transfer extrusion plates 28, the air and the liquid in the liquid raw material box 3 are respectively pumped to the inner sides of the air transfer boxes 23 and the liquid transfer boxes 22, then the air and the gas liquid are extruded to the inner side of the mixing box 1, and the operation is carried out by the pressurizing driver 6 on the mixing box 1, the pressurizing driving bevel gear 8 on the driving end of the pressurizing driver 6 is driven to rotate, the pressurizing driving bevel gear 8 drives the pressurizing driving bevel gear 7 engaged with the gear to rotate, the pressurizing threaded pipe 9 on the pressurizing driving bevel gear 7 is driven to rotate by the pressurizing driving bevel gear 8, the pressurizing threaded rod 10 in the pressurizing threaded pipe 9 in the pressurizing threaded pipe is driven to rotate by the rotation of the pressurizing threaded pipe 9, so that the pressurizing threaded rod 10 is lifted along the inner side of the pressurizing threaded pipe 9, the pressurizing extrusion plate 11 on the pressurizing threaded rod 10 is driven by the pressurizing threaded rod 10, the liquid and the air in the air transit box 23 and the liquid transit box 22 are pumped to the inner side of the mixing box 1 by the lifting of the pressurizing extrusion plate 11, the stirring driving bevel gear 19 on the driving end of the stirring driver 18 is driven to rotate by the operation of the stirring driver 18 on the concave driving circular ring block 12 on the pressurizing extrusion plate 11, and the stirring driving bevel gear 19 drives the stirring driving circular bevel gear 20 engaged with the gear to rotate, the helical gear 20 is driven to drive the square-shaped circular disk 14 to rotate by stirring and transmission, the square-shaped circular disk 14 is driven to drive the plurality of driving magnet blocks 16 thereon to rotate by driving, the square-shaped circular disk 14 is driven to drive the plurality of driving magnet blocks 16 thereon to respectively magnetically drive the plurality of driving magnet blocks 17 on the plurality of driving disks 15 to rotate, the driving disks 15 thereon are respectively driven to rotate by the driving magnet blocks 17, the stirring plates 21 thereon are respectively driven by the plurality of rotating driving disks 15, and the stirring plates 21 rotating at high speed are used for generating mixed and rotating air flows in the pair of mixing boxes 1, so that gas liquid and air are mixed to generate mixed air flows, the mixed air flows are extruded into the gas turbine by the lifting of the pressurizing and extruding plate 11, the mixed gas liquid generates centrifugal rotating air flows by the pressurizing and mixing structure, and the effect of uniform mixing is achieved, avoided direct transfer to pump, produced inhomogeneous phenomenon, absorbed the heat on a plurality of heat dissipation ring piece through earlier with liquid and gas simultaneously to reach and retrieve the heat in the smog, required heat before reaching combustion temperature to air and fuel when having avoided the burning simultaneously.
Preferably, the transfer structure further includes: a pair of liquid transfer boxes 22, a pair of air transfer boxes 23, a hydraulic box 24, a liquid pump 25, a hydraulic shunt tube 26, two pairs of extrusion hydraulic cylinders 27, two pairs of transfer extrusion plates 28, two pairs of transfer valves 29 and a pair of feeding sealing valves 5;
a pair of the liquid transfer boxes 22 and a pair of the air transfer boxes 23 are mounted on the production support 4, two pairs of the transfer valves 29 are respectively mounted on the pair of the liquid transfer boxes 22 and the pair of the air transfer boxes 23, the other ends of the two pairs of the transfer valves 29 are respectively connected to the pair of the mixing boxes 1, a pair of the feeding sealing valves 5 are respectively mounted on the pair of the mixing boxes 1, the pair of the feeding sealing valves 5 are respectively connected to the gas turbine 2, two pairs of the extrusion hydraulic cylinders 27 are respectively mounted on the inner sides of the pair of the liquid transfer boxes 22 and the pair of the air transfer boxes 23, two pairs of the transfer extrusion plates 28 are respectively mounted on the pushing ends of the two pairs of the extrusion hydraulic cylinders 27, the hydraulic boxes 24 are mounted on the production support 4, and the liquid pump 25 is mounted on the hydraulic boxes 24, the hydraulic pressure shunt pipe 26 is installed on the liquid pump 25, and the hydraulic pressure shunt pipe 26 is connected to the pushing ends of the two pairs of squeezing hydraulic cylinders 27, respectively.
Preferably, the heat circulation structure further includes: the air exhaust pipe comprises an air exhaust pipe, an air suction pump, an air exhaust valve, four pairs of air exhaust flow dividing pipes, a plurality of heat dissipation pipes, two pairs of square-shaped limiting blocks and a plurality of heat dissipation circular ring pieces;
the blast pipe install in gas turbine 2 is last, the aspiration pump install in on the blast pipe, the exhaust valve install in on the aspiration pump, four are right the exhaust shunt tubes cartridge respectively in a pair of liquid transfer box 22 and a pair of on the both sides of air transfer box 23, and four are right the exhaust shunt tubes connect respectively in on the exhaust valve, a plurality of the cooling tube is connected respectively in four right on the exhaust shunt tubes, a plurality of the heat dissipation ring piece is installed respectively in a plurality of on the cooling tube, two pairs the shape stopper of returning is installed respectively in a pair of liquid transfer box 22 and a pair of on the air transfer box 23.
Preferably, a pair of the mixing tanks 1, a pair of the liquid transfer tanks 22, and a pair of the air transfer tanks 23 are provided with pressure sensors inside, respectively.
Preferably, the exhaust pipe and the four pairs of exhaust branch pipes are provided with heat insulation layers on the outer sides.
Preferably, a pair of coil pipes is disposed inside the mixing box 1, and the two pairs of coil pipes are connected to the two pairs of transfer valves 29.
Preferably, a plastic layer is disposed on the outer side of the plurality of concave transmission circular ring blocks 13.
As a preferable scheme, further, a plurality of the concave transmission ring blocks 13 and the pair of concave driving ring blocks 12 are respectively provided with an auxiliary ball groove on the inner side, a plurality of the auxiliary ball grooves are respectively provided with a plastic ball groove pad, and a plurality of the plastic ball groove pads are respectively provided with a plastic ball on the inner side.
Preferably, temperature sensors are provided inside the pair of mixing tanks 1, the pair of liquid transfer tanks 22, and the pair of air transfer tanks 23, respectively.
Preferably, a liquid level meter is provided on each of the pair of liquid transfer tanks 22.
The technical solutions described above only represent the preferred technical solutions of the present invention, and some possible modifications to some parts of the technical solutions by those skilled in the art all represent the principles of the present invention, and fall within the protection scope of the present invention.
Claims (10)
1. A gas-liquid mixing and pressurizing device for a gas turbine comprises a pair of mixing boxes, the gas turbine, a liquid raw material box and a production support; the method is characterized in that: the pair of mixing boxes, the gas turbine and the liquid raw material box are arranged on the production support, a transfer structure is arranged on the production support and connected to the pair of mixing boxes and the gas turbine, a pressurizing mixing structure is arranged in the pair of mixing boxes, a heat circulation structure is arranged on the gas turbine and connected to the transfer structure;
the pressurized mixing structure comprises: the device comprises a pair of pressure driving machines, a pair of pressure transmission helical gears, a pair of pressure driving helical gears, a pair of pressure threaded pipes, a pair of pressure threaded rods, a pair of pressure extrusion plates, a pair of concave driving circular ring blocks, a plurality of concave driving circular ring blocks, a pair of driving square-wave discs, a plurality of driving circular discs, a plurality of driving magnetic iron blocks, a pair of stirring driving machines, a pair of stirring driving helical gears, a pair of stirring transmission square-wave helical gears and a plurality of stirring blades;
the pair of pressure driving machines are respectively arranged on the top ends of the pair of mixing boxes, the pair of pressure threaded pipes are respectively inserted on the pair of mixing boxes through bearings, the pair of pressure threaded rods are respectively movably inserted on the inner sides of the pair of pressure threaded pipes, the pair of pressure driving bevel gears are respectively arranged on the driving ends of the pair of pressure driving machines, the pair of pressure driving bevel gears are respectively engaged with the pair of pressure transmission bevel gears, the pair of pressure extrusion plates are respectively arranged on the pair of pressure threaded rods, the pair of concave driving circular ring blocks are respectively arranged on the top ends of the pair of pressure extrusion plates, the pair of driving circular discs are respectively movably inserted on the inner sides of the pair of concave driving circular ring blocks, and the plurality of concave driving circular ring blocks are respectively arranged on the pair of pressure extrusion plates in a circular shape, the stirring driving bevel gear is installed on the driving end of the stirring driving machine, and the stirring driving bevel gear is respectively engaged with the stirring driving bevel gear and is a plurality of in a pair of the driving bevel gear, a plurality of the driving magnet blocks are respectively installed on the driving bevel gear, and a plurality of the driving magnet blocks are respectively installed on the driving bevel gear and are a plurality of in the driving disk, and a plurality of the stirring pieces are respectively installed on the driving disk.
2. The gas-liquid mixing and pressurizing device for a gas turbine as claimed in claim 1, wherein: the transfer structure includes: the device comprises a pair of liquid transfer boxes, a pair of air transfer boxes, a hydraulic box, a liquid pump, a hydraulic flow dividing pipe, two pairs of extrusion hydraulic cylinders, two pairs of transfer extrusion plates, two pairs of transfer valves and a pair of feeding sealing valves;
a pair of the liquid transfer boxes and a pair of the air transfer boxes are arranged on the production bracket, two pairs of the transfer valves are respectively arranged on the pair of the liquid transfer boxes and the pair of the air transfer boxes, and the other ends of the two pairs of transfer valves are respectively connected to a pair of mixing boxes, a pair of feeding sealing valves are respectively arranged on the pair of mixing boxes, and a pair of the feeding sealing valves are respectively connected to the gas turbine, two pairs of the extrusion hydraulic cylinders are respectively arranged at the inner sides of a pair of the liquid transfer boxes and a pair of the air transfer boxes, two pairs of the transfer extrusion plates are respectively arranged at the pushing ends of two pairs of the extrusion hydraulic cylinders, the hydraulic tank is arranged on the production bracket, the liquid pump is arranged on the hydraulic tank, the hydraulic shunt tubes are arranged on the liquid pump and are respectively connected to the pushing ends of the two pairs of extrusion hydraulic cylinders.
3. The gas-liquid mixing and pressurizing device for a gas turbine as claimed in claim 2, wherein: the heat circulation structure comprises an exhaust pipe, an air pump, an exhaust valve, four pairs of exhaust flow dividing pipes, a plurality of radiating pipes, two pairs of square-shaped limiting blocks and a plurality of radiating circular ring pieces;
the blast pipe install in gas turbine is last, the aspiration pump install in on the blast pipe, exhaust valve install in on the aspiration pump, four are right exhaust shunt tubes cartridge respectively in a pair of liquid transfer box and a pair of on the both sides of air transfer box, and four are right exhaust shunt tubes connect respectively in on the exhaust valve, a plurality of the cooling tube is connected respectively in four right exhaust on the shunt tubes, a plurality of the heat dissipation ring piece is installed respectively in a plurality of on the cooling tube, two pairs the shape stopper of returning is installed respectively in a pair of liquid transfer box and a pair of on the air transfer box.
4. The gas-liquid mixing and pressurizing device for a gas turbine as claimed in claim 3, wherein: pressure sensors are respectively arranged on the inner sides of the pair of mixing boxes, the pair of liquid transfer boxes and the pair of air transfer boxes.
5. The gas-liquid mixing and pressurizing device for the gas turbine as claimed in claim 4, wherein: and heat insulation layers are arranged on the outer sides of the exhaust pipes and the four pairs of exhaust flow dividing pipes.
6. The gas-liquid mixing and pressurizing device for the gas turbine as claimed in claim 5, wherein: and the inner sides of the mixing boxes are respectively provided with a pair of coil pipes, and the two pairs of coil pipes are respectively connected to the two pairs of transfer valves.
7. The gas-liquid mixing and pressurizing device for the gas turbine as claimed in claim 6, wherein: and plastic layers are arranged on the outer sides of the concave transmission circular ring blocks.
8. The gas-liquid mixing and pressurizing device for a gas turbine as claimed in claim 7, wherein: the inner sides of the plurality of concave type transmission circular ring blocks and the pair of concave type driving circular ring blocks are respectively provided with an auxiliary ball groove, the inner sides of the plurality of auxiliary ball grooves are respectively provided with a plastic ball groove pad, and the inner sides of the plurality of plastic ball groove pads are respectively provided with a plastic ball.
9. The gas-liquid mixing and pressurizing device for a gas turbine as claimed in claim 8, wherein: temperature sensors are respectively arranged on the inner sides of the pair of mixing boxes, the pair of liquid transfer boxes and the pair of air transfer boxes.
10. The gas-liquid mixing and pressurizing device for a gas turbine as claimed in claim 9, wherein: and the liquid level meters are respectively arranged on the liquid transfer boxes.
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