CN202273762U - Turbo-charged gas compressing system - Google Patents
Turbo-charged gas compressing system Download PDFInfo
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- CN202273762U CN202273762U CN 201120393104 CN201120393104U CN202273762U CN 202273762 U CN202273762 U CN 202273762U CN 201120393104 CN201120393104 CN 201120393104 CN 201120393104 U CN201120393104 U CN 201120393104U CN 202273762 U CN202273762 U CN 202273762U
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Abstract
The utility model disclose a turbo-charged gas compressing system, which comprises a gas compressor, an impeller gas compressor and an impeller power mechanism, wherein the gas outlet of the impeller gas compressor is communicated with a compressor gas inlet channel of the gas compressor; a compressor gas supply channel of the gas compressor is communicated with the gas inlet of the impeller power mechanism; and the impeller power mechanism is used for outputting power to the impeller gas compressor. Compared with the conventional gas compressing system, the turbo-charged gas compressing system provided by the utility model has the characteristics of small size, light weight and high efficiency, and has a wide application prospect.
Description
Technical field
The utility model relates to the gas compression field, especially a kind of gas compression system.
Background technique
Generally speaking the tradition gas compressor, all have bulky, inefficient characteristics, and progression is many, thereby has been caused the defective that weight is big, manufacture cost is high.Therefore, need a kind of new gas compression system of invention.
Summary of the invention
In order to address the above problem, the technological scheme that the utility model proposes is following:
A kind of turbosupercharging gas compression system; Comprise gas compressor, impeller gas compressor and impeller power machine structure; The gas outlet of said impeller gas compressor is communicated with the compressor gas-entered passageway of said gas compressor; The compressor gas supplied passage of said gas compressor is communicated with the gas access of said impeller power machine structure, and said impeller power machine structure is to said impeller gas compressor outputting power.
The gas outlet of said impeller power machine structure is communicated with the finished product gas storage tank.
On said compressor gas supplied passage, establish Jet injector.
On said compressor gas supplied passage, establish the firing chamber.
On the said compressor gas supplied passage between said gas compressor and the said firing chamber, establish regenerator, the gas outlet of said impeller power machine structure is communicated with the heated fluid of said regenerator inlet.
Optionally, establishing Jet injector between said turbo-compressor and the said firing chamber and/or between said firing chamber and said impeller power machine structure.
A kind of turbosupercharging gas compression system comprises gas compressor, impeller gas compressor and impeller power machine structure, and the gas outlet of said impeller gas compressor is communicated with the compressor gas-entered passageway of said gas compressor; Establish on the compressor gas supplied passage of said gas compressor the air feed by-pass port or with the finished product gas storage tank of the compressor gas supplied channel connection of said gas compressor on establish the air feed by-pass port; Said air feed by-pass port is communicated with through the gas access of bypass tube with said impeller power machine structure, and said impeller power machine structure is to said impeller gas compressor outputting power.
On said bypass tube, establish Jet injector.
On said bypass tube, establish the firing chamber.
On said bypass tube, establish control valve.
On the said bypass tube between said air feed by-pass port and the said firing chamber, establish regenerator, the gas outlet of said impeller power machine structure is communicated with the heated fluid of said regenerator inlet.
Optionally, establishing Jet injector between said air feed by-pass port and the said firing chamber and/or between said firing chamber and said impeller power machine structure.
On said compressor gas-entered passageway, establish cooler, and/or on said compressor gas supplied passage, establish cooler.
The gas outlet of said impeller power machine structure is communicated with the gas access of secondary impeller power machine structure.
Said compressor gas supplied passage is communicated with through striding a grade connecting tube with communication passage between said impeller power machine structure and the secondary impeller power machine structure.
Establish control valve said striding on grade connecting tube.
Said impeller power machine structure is to said gas compressor outputting power.
Said gas compressor is made as piston gas compressor.
Said impeller gas compressor is made as the multistage turbine gas compressor, and/or said impeller power machine structure is made as multistage power turbine.
On said gas compressor, establish the heat extraction device; And/or on said impeller gas compressor, establish the heat extraction device; And/or on said impeller power machine structure, establish the heat extraction device, and/or on said compressor gas-entered passageway, establish the heat extraction device, and/or on said compressor gas supplied passage, establish the heat extraction device.
The gas outlet of said impeller power machine structure is communicated with the cooling gas inlet of said heat extraction device, utilizes through the low-temperature receiver of the gas after the said impeller power machine structure cooling as said heat extraction device and uses.
The gas outlet of said impeller power machine structure is communicated with the gas access of said impeller gas compressor, makes through the gas after the said impeller power machine structure cooling and gets into said impeller gas compressor again.
The principle of the utility model is: all or part of of pressurized gas that utilizes said gas compressor (for example piston gas compressor) output is directly or through the heating of said firing chamber or behind said Jet injector injection low-pressure gas, promote said impeller power machine structure; Said impeller mechanism is to the said impeller gas compressor outputting power on the said compressor air inlet machine passage that is arranged on said gas compressor, said impeller gas compressor need compressed gas boosting after or send into said gas compressor after the supercharging cooling; With the part of the pressurized gas of said gas compressor output directly or through the heating of said firing chamber or behind said Jet injector injection low-pressure gas, promote in the structure of said impeller power machine structure, will export as the finished product pressurized gas by another part gas of the pressurized gas of said gas compressor output; Directly or through the heating of said firing chamber or behind said Jet injector injection low-pressure gas, promote in the structure of said impeller power machine structure, will be by the gas that the gas outlet of said impeller power machine structure is discharged direct or behind said regenerator, export the pressurized gas of said gas compressor output whole as the finished product pressurized gas; In other words, the utility model is to have utilized said impeller gas compressor that the gas of needs compression is carried out supercharging, thereby has reduced the volume and weight of whole system, has improved efficient.
In the utility model, the communication passage that described working medium of striding the impeller power machine structure (being secondary impeller power machine structure) of the working medium inlet that is meant the impeller power machine structure that is communicated with upper level grade connecting tube and next stage enters the mouth.
In the utility model, said firing chamber can be made as continuous combustion chambers, also can be made as the intermittent type firing chamber.
In the utility model, so-called gas compressor is meant the mechanism that all can compress gas, for example piston compressor, rotary screw compressor, impeller type gas compressor, roots blower, fluid gas compressor etc.; So-called fluid gas compressor is meant the mechanism that utilizes fluid that gas is compressed, and the mechanism that for example utilizes Jet injector (sparger) that gas is compressed for example pumps into liquid mechanism that makes the gas boosting in the container in the container etc. again.
Turbosupercharging gas compression system disclosed in the utility model can make said power turbine mechanism and said impeller gas compressor be in work under the quite high rotating speed, gives full play to the advantage of said power turbine mechanism and said impeller gas compressor.Moreover; In this system; If the pressurized gas to getting into said power turbine mechanism carries out certain cooling, just can make the temperature of the gas outlet of said power turbine mechanism be in lower even quite low level, for this reason; The gas that is come out by the gas outlet of said power turbine mechanism can be used as low-temperature receiver and is used for purposes such as refrigeration, also can be used as low-temperature receiver and uses with gas, working medium or parts to the cooling of the needs in the said turbosupercharging gas compression system and cool off.
In the utility model, so-called compressor air-discharging road is meant the pressurized gas passage that is communicated with the pressurized gas outlet of said gas compressor; So-called compressor intake duct is meant the gas channel that is communicated with the gas access of said gas compressor; So-called exhaust is meant by the high pressure compressed gas after the said gas compressor compression; So-called cooler is meant the device that all can cool off gas; It can be radiator; Also can be to be the heat exchanger of purpose with the cooling, can also be the hybrid exhaust cooling device that the fluid that temperature is lower mixes with high pressure compressed gas, and so-called hybrid exhaust cooling device is meant high pressure compressed gas and cryogen are directly mixed the cooler that conducts heat; Its essence is a container; Exhaust and cryogen are mixed in this container, in order to increase the uniformity of mixing, in this container, can establish flow guide structure, stirring mechanism or fluidic architecture; So-called heat extraction device is meant the device that heat is externally discharged, and it can be a radiator, also can be to be the heat exchanger of purpose with the cooling; So-called multistage is meant a plurality of impeller gas compressor series connection or a plurality of power turbine mechanisms in series; Putting in order of so-called first single-stage and second single-stage is that starting point is foundation along the gas connection pipe road to leave the cylinder distance with the cylinder, apart from cylinder near be the first order, taking second place is the second level, the rest may be inferred.
In the utility model, so-called connection is meant direct connection, through the indirect communication of several processes (comprise with other material mixing etc.) or through controlled connections such as pump, control valves.
In the utility model, so-called power turbine mechanism is meant that all utilize gas flow the expand mechanism of external work done, for example power turbine, power turbine etc.
In the utility model, so-called impeller gas compressor is meant the device that all utilize impeller that gas is compressed, and like centrifugal compressor, axial flow compressor etc., it can be single-stage, multistage, also can be a plurality of single-stages or a plurality of multistage combining.
In the utility model, the heated fluid of so-called regenerator inlet is meant and is arranged on the inlet that being used on the said regenerator imports heated fluid, and in regenerator, the fluid that temperature raises is called and is heated fluid, and the fluid that temperature reduces is called heated fluid.
In the utility model; The so-called Jet injector of between A and B, establishing is meant that A is communicated with the Jet injector power gas jetburner of said Jet injector; The Jet injector gas outlet of said Jet injector is communicated with B; The Jet injector low-pressure gas of said Jet injector inlet can with atmosphere, also can be communicated with other sources of the gas; For example so-called " on said compressor gas supplied passage, establishing Jet injector " is meant the Jet injector power gas jetburner that flows into said Jet injector of said compressor gas supplied passage, and the Jet injector gas outlet of said Jet injector is communicated with the stream that goes of said compressor gas supplied passage; When establishing Jet injector on the said compressor gas supplied passage between the gas access of said firing chamber and said impeller power machine structure; Said firing chamber is communicated with the Jet injector power gas jetburner of said Jet injector through a section of said compressor gas supplied passage, and the Jet injector gas outlet of said Jet injector is communicated with the gas access of said impeller power machine structure through another section of said compressor gas supplied passage; When establishing Jet injector on the said compressor gas supplied passage between said gas compressor and said firing chamber; The gas outlet of said gas compressor is communicated with the Jet injector power gas jetburner of said Jet injector through a section of said compressor gas supplied passage, and the Jet injector gas outlet of said Jet injector another section on said compressor gas supplied passage is communicated with the gas access of said firing chamber; Again for example; So-called " on said bypass tube, establishing Jet injector " is meant that said air feed by-pass port is communicated with the Jet injector power gas jetburner of said Jet injector through a section of said bypass tube, and the Jet injector gas outlet of said Jet injector is communicated with the gas access of said impeller power machine structure through another section of said bypass tube; When said bypass tube is provided with the firing chamber; Said Jet injector can be positioned on the said bypass tube of said burner ends; During concrete the connection; The Jet injector power gas jetburner that flows into said Jet injector of said bypass tube, the Jet injector gas outlet of said Jet injector is communicated with the stream that goes of said bypass tube.
In the utility model, so-called compressor gas supplied passage is meant that said gas compressor externally exports the passage of pressurized gas, and in traditional gas compression system, said gas compressor air supply duct is communicated with the finished product gas storage tank usually.
In the utility model, so-called compressor gas-entered passageway is meant the passage that needs compressed gas to get into said gas compressor.
In the utility model, so-called Jet injector is meant through the non-motive fluid of motive fluid injection, the device that two fluid interactions are discharged from an outlet, and so-called Jet injector can be gas jet pump (being jet pump), also can be liquid-jet pump; So-called Jet injector can be traditional Jet injector, also can be non-traditional Jet injector.
In the utility model; So-called traditional Jet injector is meant what the pipe by two suit settings constituted; Inwardly pipe provides high voltage power gas; Interior pipe high voltage power gas sprays in outer tube, the device that other gases (from the gas of outer tube entering) between the inner and outer pipes are moved along the injection direction generation of interior pipe high voltage power gas; The outer tube of so-called Jet injector can have the reducing and expansion district, and outer tube can be made as Venturi tube, and interior pipe nozzle can be made as Laval nozzle, and so-called reducing and expansion district is meant the zone that section area changes in the outer tube; Said Jet injector has three interfaces at least or claims passage, i.e. Jet injector power gas jetburner, Jet injector low-pressure gas inlet and Jet injector gas outlet.
In the utility model; So-called non-traditional Jet injector is meant and is made up of two or more mutual sheathing settings or the pipe that is set up in parallel each other; Wherein at least one pipe is communicated with motive gas source, and flowing of the power gas in the motive gas source can cause that the gas in other pipes produces the device of directional flow; The pipe of so-called Jet injector can have the reducing and expansion district, can be made as Venturi tube, and the nozzle of pipe can be made as Laval nozzle, and so-called reducing and expansion district is the zone that section area changes in the vial; Said Jet injector has three interfaces at least or claims passage, i.e. Jet injector power gas jetburner, Jet injector low-pressure gas inlet and Jet injector gas outlet; Said Jet injector can comprise a plurality of Jet injector power gas jetburners; In the structure that comprises a plurality of Jet injector power gas jetburners; Said Jet injector power gas jetburner can be arranged in the pipeline center district of said Jet injector low-pressure gas inlet; Also can be arranged near the tube wall of said Jet injector low-pressure gas inlet, said Jet injector power gas jetburner also can be the annular spray mouth around said Jet injector low-pressure gas inlet pipe wall.
In the utility model, said Jet injector comprises multistage Jet injector, multiple jets pump and pulsing jet pump etc.
In the utility model; Known technology according to gas compression field and engine art; Establish necessary parts, unit and system in the place of necessity, fuel inlet (or fuel injector), oxidant inlet (or oxygen-containing gas) for example should be set on said firing chamber, should establish spark plug etc. where necessary.
The beneficial effect of the utility model is following:
Turbosupercharging gas compression system disclosed in the utility model has the advantages that volume is little, in light weight, efficient is high for existing gas compression system, have broad application prospects.
Description of drawings
Shown in Figure 1 is the utility model embodiment 1 structural representation;
Shown in Figure 2 is the utility model embodiment 2 structural representation;
Shown in Figure 3 is the utility model embodiment 3 structural representation;
Shown in Figure 4 is the utility model embodiment 4 structural representation;
Shown in Figure 5 is the utility model embodiment 5 structural representation;
Shown in Figure 6 is the utility model embodiment 6 structural representation;
Shown in Figure 7 is the utility model embodiment 7 structural representation;
Shown in Figure 8 is the utility model embodiment 8 structural representation;
Shown in Figure 9 is the utility model embodiment 9 structural representation;
Shown in Figure 10 is the utility model embodiment 10 structural representation;
Shown in Figure 11 is the utility model embodiment 11 structural representation;
Shown in Figure 12 is the utility model embodiment 12 structural representation;
Shown in Figure 13 is the utility model embodiment 13 structural representation;
Shown in Figure 14 is the utility model embodiment 14 structural representation;
Shown in Figure 15 is the utility model embodiment 15 structural representation;
Shown in Figure 16 is the utility model embodiment 16 structural representation;
Shown in Figure 17 is the utility model embodiment 17 structural representation;
Shown in Figure 180 is the utility model embodiment 18 structural representation;
Shown in Figure 19 is the utility model embodiment 19 structural representation;
Shown in Figure 20 is the utility model embodiment 20 structural representation;
Shown in Figure 21 is the utility model embodiment 21 structural representation;
Shown in Figure 22 is the utility model embodiment 22 structural representation;
Shown in Figure 23 is the utility model embodiment 23 structural representation;
Shown in Figure 24 is the utility model embodiment 24 structural representation;
Shown in Figure 25 is the utility model embodiment 25 structural representation;
Shown in Figure 26 is the utility model embodiment 26 structural representation,
Among the figure:
1 gas compressor, 2 impeller gas compressors, 3 impeller power machine structures, 4 compressor gas-entered passageways, 5 compressor gas supplied passages, 6 air feed by-pass ports, 7 finished product gas storage tanks, 8 regenerators, 9 bypass tubes, 12 Jet injectors, 13 firing chambers, 15 control valves, 16 coolers, 17 level impeller power machine structures, 18 are striden a grade connecting tube, 20 multistage turbine gas compressors, 21 multistage power turbines, 22 multistage turbocompressors, 23 multistage power turbines, 24 heat extraction devices, 25 heat exchangers.
Embodiment
Turbosupercharging gas compression system as shown in Figure 1; Comprise gas compressor 1, impeller gas compressor 2 and impeller power machine structure 3; The gas outlet of said impeller gas compressor 2 is communicated with the compressor gas-entered passageway 4 of said gas compressor 1; The compressor gas supplied passage 5 of said gas compressor 1 is communicated with the gas access of said impeller power machine structure 3,3 pairs of said impeller gas compressor 2 outputting powers of said impeller power machine structure, and said gas compressor 1 is made as the gas piston gas compressor.
During practical implementation, said gas compressor can also be rotary screw compressor, impeller type gas compressor, roots blower, fluid gas compressor etc.
Turbosupercharging gas compression system as shown in Figure 2, its difference with embodiment 1 is: the gas outlet of said impeller power machine structure 3 is communicated with finished product gas storage tank 7, and the gas of the gas outlet of said impeller power machine structure 3 is used as pressurized gas.
Turbosupercharging gas compression system as shown in Figure 3; Itself and embodiment's 1 difference is: on the said compressor gas supplied passage 5 between the gas access of said compressor gas supplied passage 5 and said impeller power machine structure 3, establish Jet injector 12; Be that through said compressor gas supplied passage 5 one section of the pressurized gas outlet of said gas compressor 1 is communicated with the Jet injector power gas jetburner of said Jet injector 12; The Jet injector gas outlet of said Jet injector 12 is communicated with the gas access of said impeller power machine structure 3 through another section of said compressor gas supplied passage 5; The Jet injector low-pressure gas inlet and the atmosphere of said Jet injector 12; Optionally, the Jet injector low-pressure gas of said Jet injector 12 inlet also can be communicated with other sources of the gas.
Turbosupercharging gas compression system as shown in Figure 4, itself and embodiment's 1 difference is: on the said compressor gas supplied passage 5 between the gas access of said compressor gas supplied passage 5 and said impeller power machine structure 3, establish firing chamber 13.
Turbosupercharging gas compression system as shown in Figure 5; Itself and embodiment's 4 difference is: on the said compressor gas supplied passage 5 between said gas compressor 1 and the said firing chamber 13, establish regenerator 8; The gas outlet of said impeller power machine structure 3 is communicated with the heated fluid inlet of said regenerator 8; The outlet of the heated fluid of said regenerator 8 is communicated with finished product gas storage tank 7, and the gas that will pass through the gas outlet of the said impeller power machine structure 3 that said regenerator 8 lowers the temperature uses as pressurized gas.
Turbosupercharging gas compression system as shown in Figure 6; Itself and embodiment's 4 difference is: on the said compressor gas supplied passage 5 between said firing chamber 13 and the said impeller power machine structure 3, establish Jet injector 12; Be that said firing chamber 13 is communicated with the Jet injector power gas jetburner of said Jet injector 12 through said compressor gas supplied passage 5; The Jet injector gas outlet of said Jet injector 12 is communicated with said firing chamber 13 through said compressor gas supplied passage 5; The Jet injector low-pressure gas inlet and the atmosphere of said Jet injector 12; 3 pairs of said gas compressor 1 outputting powers of said impeller power machine structure, optionally, the Jet injector low-pressure gas of said Jet injector 12 inlet also can be communicated with other sources of the gas.
Turbosupercharging gas compression system as shown in Figure 7; Itself and embodiment's 4 difference is: on the said compressor gas supplied passage 5 between said gas compressor 1 and the said firing chamber 13, establish Jet injector 12; The gas outlet that is said gas compressor 1 is communicated with the Jet injector power gas jetburner of said Jet injector 12 through said compressor gas supplied passage 5; The Jet injector gas outlet of said Jet injector 12 is communicated with the gas access of said firing chamber 13 through said compressor gas supplied passage 5; The Jet injector low-pressure gas inlet and the atmosphere of said Jet injector 12, optionally, the Jet injector low-pressure gas of said Jet injector 12 inlet also can be communicated with other sources of the gas.
Turbosupercharging gas compression system as shown in Figure 8 comprises gas compressor 1, impeller gas compressor 2 and impeller power machine structure 3, and the gas outlet of said impeller gas compressor 2 is communicated with the compressor gas-entered passageway 4 of said gas compressor 1; On the compressor gas supplied passage 5 of said gas compressor 1, establish air feed by-pass port 6; Said air feed by-pass port 6 is communicated with the gas access of said impeller power machine structure 3; 3 pairs of said impeller gas compressor 2 outputting powers of said impeller power machine structure; Said compressor gas supplied passage 5 is communicated with finished product gas storage tank 7, and said gas compressor 1 is made as the gas piston gas compressor.
During practical implementation, said gas compressor can also be rotary screw compressor, impeller type gas compressor, roots blower, fluid gas compressor etc.
In the disclosed scheme of present embodiment; Gas at first gets into said impeller gas compressor 2; In said impeller gas compressor 2, be pressurized the back and get into said gas compressor 1; Further being compressed supercharging in said gas compressor 1 after, gas discharges said gas compressor 1; The gas of being discharged by said gas compressor 1 removes to promote said impeller power machine structure 3, makes 3 pairs of impeller gas compressor 2 outputting powers of said impeller power machine structure, and another part of the gas of being discharged by gas compressor 1 is stored in the said finished product gas storage tank 7 as the high pressure compressed gas of system's output; So just give full play to impeller gas compressor 2 and gas compressor 1 advantage separately, realized gas compression system efficiently.
Turbosupercharging gas compression system as shown in Figure 9 comprises gas compressor 1, impeller gas compressor 2 and impeller power machine structure 3, and the gas outlet of said impeller gas compressor 2 is communicated with the compressor gas-entered passageway 4 of said gas compressor 1; With finished product gas storage tank 7 that the compressor gas supplied passage 5 of said gas compressor 1 is communicated with on establish air feed by-pass port 6; Said air feed by-pass port 6 is communicated with the gas access of said impeller power machine structure 3,3 pairs of said impeller gas compressor 2 outputting powers of said impeller power machine structure.
Embodiment 10
Turbosupercharging gas compression system shown in figure 10; Itself and embodiment's 8 difference is: on the said bypass tube 9 between the gas access of said air feed by-pass port 6 and said impeller power machine structure 3, establish Jet injector 12; Being said air feed by-pass port 6 is communicated with the Jet injector power gas jetburner of said Jet injector 12 through a section of said bypass tube 9; The Jet injector gas outlet of said Jet injector 12 is communicated with the gas access of said impeller power machine structure 3 through another section of said bypass tube 9; The Jet injector low-pressure gas inlet and the atmosphere of said Jet injector 12, optionally, the Jet injector low-pressure gas of said Jet injector 12 inlet also can be communicated with other sources of the gas.
Embodiment 11
Turbosupercharging gas compression system shown in figure 11; Itself and embodiment's 8 difference is: on the bypass tube 9 between the gas access of said air feed by-pass port 6 and said impeller power machine structure 3, establish firing chamber 13,3 pairs of said gas compressor 1 outputting powers of said impeller power machine structure.
Turbosupercharging gas compression system shown in figure 12; Itself and embodiment's 8 difference is: on the bypass tube 9 between the gas access of said air feed by-pass port 6 and said impeller power machine structure 3, establish control valve 15, the effect of said control valve 15 is to be used for adjusting pressurized gas that said gas compressor 1 the produces ratio as the power gas of said impeller power machine structure 3.
Turbosupercharging gas compression system shown in figure 13; Itself and embodiment's 11 difference is: between said air feed by-pass port 6 and said firing chamber 13, establish regenerator 8, the gas outlet of said impeller power machine structure 3 is communicated with the heated fluid inlet of said regenerator 8.
Embodiment 14
Turbosupercharging gas compression system shown in figure 14; Itself and embodiment's 11 difference is: on the said bypass tube 9 between said air feed by-pass port 6 and the said firing chamber 13, establish Jet injector 12; Being said air feed by-pass port 6 is communicated with the Jet injector power gas jetburner of said Jet injector 12 through a section of said bypass tube 9; The Jet injector gas outlet of said Jet injector 12 is communicated with said firing chamber 13 through another section of said bypass tube 9; The Jet injector low-pressure gas inlet and the atmosphere of said Jet injector 12, optionally, the Jet injector low-pressure gas of said Jet injector 12 inlet also can be communicated with other sources of the gas.
Turbosupercharging gas compression system shown in figure 15; Itself and embodiment's 11 difference is: on the said bypass tube 9 between said firing chamber 13 and the said impeller power machine structure 3, establish Jet injector 12; Being said firing chamber 13 is communicated with the Jet injector power gas jetburner of said Jet injector 12 through a section of said bypass tube 9; The Jet injector gas outlet of said Jet injector 12 is communicated with the gas access of said impeller power machine structure 3 through another section of said bypass tube 9; The Jet injector low-pressure gas inlet and the atmosphere of said Jet injector 12, optionally, the Jet injector low-pressure gas of said Jet injector 12 inlet also can be communicated with other sources of the gas.
Embodiment 16
Turbosupercharging gas compression system shown in figure 16; Itself and embodiment's 1 difference is: on said compressor gas-entered passageway 4, establish cooler 16; The effect of said cooler 16 is to cool off for the air inlet of giving said gas compressor 1, improves intake efficiency.
Turbosupercharging gas compression system shown in figure 17, itself and embodiment's 8 difference is: on said compressor gas-entered passageway 4, establish cooler 16.The purpose that is provided with like this is that the gas that gets into said gas compressor 1 is cooled off, and increases the amount of the gas that gets into said gas compressor 1, improves the efficient of calming the anger of said gas compressor 1.
During practical implementation, can also on said compressor gas supplied passage 5, establish cooler 16.
Turbosupercharging gas compression system shown in figure 18, its difference with embodiment 8 is: the gas outlet of said impeller power machine structure 3 is communicated with the gas access of secondary impeller power machine structure 17.
Embodiment 19
Turbosupercharging gas compression system shown in figure 19; Its difference with embodiment 18 is: said compressor gas supplied passage 5 is communicated with through striding grade connecting tube 18 with communication passage between said impeller power machine structure 3 and the secondary impeller power machine structure 17, is used for increasing the power gas of said secondary impeller power machine structure 17.
Turbosupercharging gas compression system shown in figure 20; Itself and embodiment's 19 difference is: establish control valve 15 on grade connecting tube 18 said striding, the effect of said control valve 15 is to be used for adjusting pressurized gas that said gas compressor 1 the produces ratio as the power gas of said secondary impeller power machine structure 17.
Turbosupercharging gas compression system shown in figure 21, itself and embodiment's 1 difference is: said impeller gas compressor is made as multistage turbine gas compressor 20, and said impeller power machine structure is made as multistage power turbine 21.The purpose that is provided with like this is in order to improve the power of said impeller power machine structure 3, to improve the efficient of calming the anger of said impeller gas compressor 2 simultaneously equally.
During practical implementation, also can only said impeller gas compressor be made as multistage turbine gas compressor 20, or only said impeller power machine structure be made as multistage power turbine 21.
Turbosupercharging gas compression system shown in figure 22; Itself and embodiment's 1 difference is: said impeller gas compressor is made as the multistage turbocompressor of being made up of a plurality of single stage turbine gas compressors 22, and said impeller power machine structure is made as the multistage power turbine of being made up of a plurality of single-stage power turbines 23.The coaxial setting of first single-stage power turbine in first single stage turbine gas compressor in the said multistage turbocompressor 22 and the said multistage power turbine 23; The coaxial setting of second said power turbine of single-stage in second single stage turbine gas compressor in the said multistage turbocompressor 22 and the said multistage power turbine 23, the rest may be inferred.The purpose that is provided with like this is in order to improve the power of said impeller power machine structure 3, to improve the efficient of calming the anger of said impeller gas compressor 2 simultaneously equally.
During practical implementation, also can only said impeller gas compressor be made as the multistage turbocompressor of being made up of a plurality of single stage turbine gas compressors 22, or only said impeller power machine structure be made as the multistage power turbine of being made up of a plurality of single-stage power turbines 23.
Turbosupercharging gas compression system shown in figure 23; Itself and embodiment's 22 difference is: the coaxial setting of first single-stage power turbine in second the coaxial setting of single-stage power turbine in first single stage turbine gas compressor in the said multistage turbocompressor 22 and the said multistage power turbine 23, second single stage turbine gas compressor in the said multistage turbocompressor 22 and said multistage power turbine 23.Putting in order of so-called first single-stage and second single-stage is that starting point is foundation along the gas connection pipe road to leave the cylinder distance with the cylinder, apart from cylinder near be the first order, taking second place is the second level, the rest may be inferred.
Turbosupercharging gas compression system shown in figure 24, itself and embodiment's 1 difference is: on said impeller gas compressor 2, establish heat extraction device 24, said heat extraction device 24 is made as radiator.The purpose that is provided with like this is that the gas in the said impeller gas compressor 2 is cooled off, and realizes the approximately constant temperature compression, improves the efficient of calming the anger of said impeller gas compressor 2.
During practical implementation; Can also on said gas compressor 1, establish heat extraction device 24; And/or on said impeller power machine structure 3, establish heat extraction device 24, and/or on said compressor gas-entered passageway 4, establish heat extraction device 24, and/or on said compressor gas supplied passage 5, establish heat extraction device 24.
Embodiment 25
Turbosupercharging gas compression system shown in figure 25; Itself and embodiment's 24 difference is: on said compressor gas-entered passageway 4, establish the heat extraction device; On said compressor gas supplied passage 5, establish the heat extraction device; It is the heat exchanger 25 of purpose that said heat extraction device is made as with the cooling, and the gas outlet of said impeller power machine structure 3 is communicated with the cooling gas inlet of said heat exchanger 25, utilizes through the gas after said impeller power machine structure 3 coolings and uses as low-temperature receiver; Gas is cooled off, improve the compression efficiency of system.
Embodiment 26
Turbosupercharging gas compression system shown in figure 26; Its difference with embodiment 1 is: the gas outlet of said impeller power machine structure 3 is communicated with the gas access of said impeller gas compressor 2, makes through the gas after said impeller power machine structure 3 coolings and gets into said impeller gas compressor 2 again.The purpose that is provided with like this is that air inlet is cooled off equally, increases the amount of the gas that gets into impeller gas compressor 2, improves the efficient of calming the anger of impeller gas compressor 2, improves the utilization ratio of gas simultaneously.
Obviously; The utility model is not limited to above embodiment, according to the known technology and the technological scheme disclosed in the utility model of related domain, can derive or association goes out many flexible programs; All these flexible programs also should be thought the protection domain of the utility model.
Claims (20)
1. turbosupercharging gas compression system; It is characterized in that: comprise gas compressor (1), impeller gas compressor (2) and impeller power machine structure (3); The gas outlet of said impeller gas compressor (2) is communicated with the compressor gas-entered passageway (4) of said gas compressor (1); The compressor gas supplied passage (5) of said gas compressor (1) is communicated with the gas access of said impeller power machine structure (3), and said impeller power machine structure (3) is to said impeller gas compressor (2) outputting power.
2. turbosupercharging gas compression system according to claim 1, it is characterized in that: the gas outlet of said impeller power machine structure (3) is communicated with finished product gas storage tank (7).
3. turbosupercharging gas compression system according to claim 1 is characterized in that: on said compressor gas supplied passage (5), establish Jet injector (12).
4. turbosupercharging gas compression system according to claim 1 is characterized in that: on said compressor gas supplied passage (5), establish firing chamber (13).
5. like the said turbosupercharging gas compression system of claim 4; It is characterized in that: on the said compressor gas supplied passage (5) between said gas compressor (1) and said firing chamber (13), establish regenerator (8), the gas outlet of said impeller power machine structure (3) is communicated with the heated fluid inlet of said regenerator (8).
6. turbosupercharging gas compression system; It is characterized in that: comprise gas compressor (1), impeller gas compressor (2) and impeller power machine structure (3), the gas outlet of said impeller gas compressor (2) is communicated with the compressor gas-entered passageway (4) of said gas compressor (1); Establish on the compressor gas supplied passage (5) of said gas compressor (1) air feed by-pass port (6) or with finished product gas storage tank (7) that the compressor gas supplied passage (5) of said gas compressor (1) is communicated with on establish air feed by-pass port (6); Said air feed by-pass port (6) is communicated with through the gas access of bypass tube (9) with said impeller power machine structure (3), and said impeller power machine structure (3) is to said impeller gas compressor (2) outputting power.
7. like the said turbosupercharging gas compression system of claim 6, it is characterized in that: on said bypass tube (9), establish Jet injector (12).
8. like the said turbosupercharging gas compression system of claim 6, it is characterized in that: on said bypass tube (9), establish firing chamber (13).
9. like the said turbosupercharging gas compression system of claim 6, it is characterized in that: on said bypass tube (9), establish control valve (15).
10. like the said turbosupercharging gas compression system of claim 8; It is characterized in that: on the said bypass tube (9) between said air feed by-pass port (6) and said firing chamber (13), establish regenerator (8), the gas outlet of said impeller power machine structure (3) is communicated with the heated fluid inlet of said regenerator (8).
11. like claim 1 or 6 said turbosupercharging gas compression systems, it is characterized in that: on said compressor gas-entered passageway (4), establish cooler (16), and/or on said compressor gas supplied passage (5), establish cooler (16).
12. like one of any said turbosupercharging gas compression system of claim 1 to 10, it is characterized in that: the gas outlet of said impeller power machine structure (3) is communicated with the gas access of secondary impeller power machine structure (17).
13. like the said turbosupercharging gas compression system of claim 12, it is characterized in that: said compressor gas supplied passage (5) is communicated with through striding a grade connecting tube (18) with communication passage between said impeller power machine structure (3) and the secondary impeller power machine structure (17).
14., it is characterized in that: establish control valve (15) on grade connecting tube (18) said striding like the said turbosupercharging gas compression system of claim 13.
15. like claim 4,5,8 or 10 said turbosupercharging gas compression systems, it is characterized in that: said impeller power machine structure (3) is to said gas compressor (1) outputting power.
16. like one of any said turbosupercharging gas compression system of claim 1 to 10, it is characterized in that: said gas compressor (1) is made as piston gas compressor.
17. like one of any said turbosupercharging gas compression system of claim 1 to 10, it is characterized in that: said impeller gas compressor (2) is made as multistage turbine gas compressor (20), and/or said impeller power machine structure (3) is made as multistage power turbine (21).
18. like one of any said turbosupercharging gas compression system of claim 1 to 10; It is characterized in that: on said gas compressor (1), establish heat extraction device (24); And/or on said impeller gas compressor (2), establish heat extraction device (24); And/or on said impeller power machine structure (3), establish heat extraction device (24), and/or on said compressor gas-entered passageway (4), establish heat extraction device (24), and/or on said compressor gas supplied passage (5), establish heat extraction device (24).
19. like the said turbosupercharging gas compression system of claim 18, it is characterized in that: the gas outlet of said impeller power machine structure (3) is communicated with the cooling gas inlet of said heat extraction device (24).
20. like one of any said turbosupercharging gas compression system of claim 1 to 10, it is characterized in that: the gas outlet of said impeller power machine structure (3) is communicated with the gas access of said impeller gas compressor (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201120393104 CN202273762U (en) | 2010-10-22 | 2011-10-15 | Turbo-charged gas compressing system |
Applications Claiming Priority (9)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201010516234.3 | 2010-10-22 | ||
| CN2010105162343A CN101988426A (en) | 2010-10-22 | 2010-10-22 | Turbine composite gas compression system |
| CN201110172749.0 | 2011-06-24 | ||
| CN201110172749 | 2011-06-24 | ||
| CN201110196467 | 2011-07-14 | ||
| CN201110196467.4 | 2011-07-14 | ||
| CN201120259093 | 2011-07-21 | ||
| CN201120259093.1 | 2011-07-21 | ||
| CN 201120393104 CN202273762U (en) | 2010-10-22 | 2011-10-15 | Turbo-charged gas compressing system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202273762U true CN202273762U (en) | 2012-06-13 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201120393104 Expired - Fee Related CN202273762U (en) | 2010-10-22 | 2011-10-15 | Turbo-charged gas compressing system |
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| Country | Link |
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| CN (1) | CN202273762U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103075247A (en) * | 2013-01-11 | 2013-05-01 | 中国兵器工业集团第七0研究所 | Multi-stage working engine |
| CN103089433A (en) * | 2013-01-15 | 2013-05-08 | 中国兵器工业集团第七0研究所 | Stable-combustion water-cooled turbine engine |
| CN106499647A (en) * | 2015-09-07 | 2017-03-15 | 熵零股份有限公司 | A kind of gain method and its device, system |
| CN117072463A (en) * | 2023-09-05 | 2023-11-17 | 南京磁谷科技股份有限公司 | Multistage magnetic suspension centrifugal air compressor, design and use method |
-
2011
- 2011-10-15 CN CN 201120393104 patent/CN202273762U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103075247A (en) * | 2013-01-11 | 2013-05-01 | 中国兵器工业集团第七0研究所 | Multi-stage working engine |
| CN103089433A (en) * | 2013-01-15 | 2013-05-08 | 中国兵器工业集团第七0研究所 | Stable-combustion water-cooled turbine engine |
| CN106499647A (en) * | 2015-09-07 | 2017-03-15 | 熵零股份有限公司 | A kind of gain method and its device, system |
| CN117072463A (en) * | 2023-09-05 | 2023-11-17 | 南京磁谷科技股份有限公司 | Multistage magnetic suspension centrifugal air compressor, design and use method |
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