CN102996404A - Gas compressor - Google Patents

Gas compressor Download PDF

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Publication number
CN102996404A
CN102996404A CN2012105828546A CN201210582854A CN102996404A CN 102996404 A CN102996404 A CN 102996404A CN 2012105828546 A CN2012105828546 A CN 2012105828546A CN 201210582854 A CN201210582854 A CN 201210582854A CN 102996404 A CN102996404 A CN 102996404A
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CN
China
Prior art keywords
casing
rotor
shock tube
end cap
gas
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN2012105828546A
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Chinese (zh)
Inventor
邢小月
谭善学
杜岳
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SHENZHEN LIKE PNEUMATIC TECHNOLOGY Co Ltd
Original Assignee
SHENZHEN LIKE PNEUMATIC TECHNOLOGY Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by SHENZHEN LIKE PNEUMATIC TECHNOLOGY Co Ltd filed Critical SHENZHEN LIKE PNEUMATIC TECHNOLOGY Co Ltd
Priority to CN2012105828546A priority Critical patent/CN102996404A/en
Publication of CN102996404A publication Critical patent/CN102996404A/en
Pending legal-status Critical Current

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Abstract

A gas compressor comprises a casing with two open ends. One end of the casing is in sealing connection with a first end cover, and the other end of the casing is in sealing connection with a second end cover. A rotary shaft located in the casing penetrates into the first end cover and the second end cover. A rotor is fixedly arranged on the rotary shaft, and at least one shock tube axially arranged along the axial direction of the rotary shaft is arranged on the rotor. A high-pressure gas inlet and a lowest-pressure gas outlet which are capable of being communicated with the shock tube are arranged on the first end cover. A compressed high-pressure gas outlet and a to-be-compressed low-pressure gas inlet which are capable of being communicated with the shock tube are arranged on the second end cover. Blades are fixedly arranged on the outer periphery of the rotor, and a drive gas inlet and a drive gas outlet which face the blades rightly are arranged on the casing. The gas compressor adopts high-pressure gas to compress low-pressure gas to achieve gas compression, and the compression efficiency is improved remarkably.

Description

A kind of gas compressor
Technical field
The invention belongs to the compression device field, relate in particular to a kind of gas compressor.
Background technique
At present, existing gas compressor mainly is piston compressor, and its to-and-fro motion by piston directly gas compresses, and compression efficiency is low.
Summary of the invention
The object of the present invention is to provide a kind of gas compressor, it compresses low-pressure gas by pressurized gas, realizes the purpose of pressurized gas, and compression efficiency is high.
The present invention is achieved in that a kind of gas compressor, comprises the casing of both ends open, and an end and first end cap of described casing are tightly connected, and the other end of described casing is connected with the second end bracket enclosed;
Be equipped with a rotating shaft that is positioned at described casing on described the first end cap and the second end cap, the two ends of described rotating shaft are rotationally connected with described the first end cap and the second end cap respectively;
Be installed with a rotor in the described rotating shaft, offer the shock tube of at least one axial setting along described rotating shaft on the described rotor;
Described first end covers and offers pressurized gas inlet and the minimal pressure gas outlet that can communicate with described shock tube, and described pressurized gas inlet is used for pressurized gas are accelerated to the velocity of sound or ultrasound velocity;
Offer compressed rear pressurized gas outlet and the compressed front low-pressure gas entrance that can communicate with described shock tube on described the second end cap;
The outer periphery of described rotor are installed with blade, offer on the described casing with described blade over against the propellant entrance that arranges and propellant outlet.
Particularly, described shock tube along the circumferential direction is evenly distributed on the described rotor.
Particularly, the quantity of described shock tube is 1 ~ 100.
Particularly, described first end covers and is installed with clutch shaft bearing, is installed with the second bearing on described the second end cap, the two ends of described rotating shaft respectively with described clutch shaft bearing be connected bearing and be connected.
Further, also be provided with two sealing plugs between described casing and the rotor, described propellant entrance and propellant outlet are between two described sealing plugs.
Adopt the to-and-fro motion of piston to come directly gas to be compressed different from prior art, gas compressor of the present invention adopts pressurized gas that low-pressure gas is compressed, and realizes the purpose of pressurized gas, and compression efficiency significantly improves.
Description of drawings
In order to be illustrated more clearly in technological scheme of the present invention, the below will do to introduce simply to the accompanying drawing of required use among the embodiment, apparently, accompanying drawing in the following describes only is some embodiments of the present invention, for those of ordinary skills, under the prerequisite of not paying creative work, can also obtain according to these accompanying drawings other accompanying drawing.
Fig. 1 is the schematic representation of the gas compressor that provides of the embodiment of the invention.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the invention, the technological scheme in the embodiment of the invention is clearly and completely described.
As shown in Figure 1, a kind of gas compressor that the embodiment of the invention provides comprises the casing 1 of both ends open, and an end of casing 1 and the first end cap 2 are tightly connected, and the other end of casing 1 and the second end cap 3 are tightly connected;
Be equipped with a rotating shaft 4 that is positioned at casing on described the first end cap 2 and the second end cap 3, be installed with clutch shaft bearing 41 on the first end cap 2, be installed with the second bearing 42 on the second end cap 3, the two ends of rotating shaft 4 respectively with clutch shaft bearing 41 be connected bearing 42 and be connected, thereby the purpose that the two ends of realizing rotating shaft 4 are rotationally connected with the first end cap 2 and the second end cap 3 respectively;
Be installed with a rotor 5 in the described rotating shaft 4, offer the shock tube 6 of at least one axial setting along rotating shaft 4 on the rotor 5, shock tube 6 along the circumferential direction is evenly distributed on the rotor 5, and particularly, the quantity of shock tube 6 is 1 ~ 100;
Offer pressurized gas inlet 21 and the minimal pressure gas outlet 22 that can communicate with shock tube 6 on described the first end cap 2, pressurized gas inlet 21 is used for pressurized gas are accelerated to the velocity of sound or ultrasound velocity;
Offer compressed rear pressurized gas outlet 31 and the compressed front low-pressure gas entrance 32 that can communicate with shock tube 6 on described the second end cap 3;
The outer periphery of described rotor 5 are installed with blade 7, offer on the casing 1 with blade 7 over against the propellant entrance 11 that arranges and propellant outlet 12.
The specific works principle of gas compressor provided by the invention is as follows:
(1) the incident stage: propellant enters in the casing 1 from the gas access 11 that drives casing 1, propellant promotes blade 7 and rotates, blade 7 rotor drivens 5 rotate together, and after rotor 5 rotated, pressurized gas accelerated by pressurized gas inlet 21, spray into successively in the oscillator tube 6 on the rotor 5 with the velocity of sound or supersonic speed, wherein, propellant can be the sub-fraction of pressurized gas shunting, also can be other source of the gas, in addition, the rotation of rotor 4 also can drive by equipment such as motors;
(2) compression stage: the pressurized gas that are accelerated by pressurized gas inlet 21 are to the compressed front low-pressure gas compressed action in the shock tube 6, because spraying into the gas of shock tube 6 from pressurized gas inlet 21 is velocities of sound or supersonic, so can produce shock wave when pressurized gas spray into when shock tube 6 runs into the compressed front low-pressure gas that has existed in the shock tube 6, compressed front low-pressure gas in the pressurized gas that shock wave sprays into just as an invisible piston cuts off and the shock tube 6, and the compressed front low-pressure gas in the shock tube 6 compressed, the temperature and pressure of the compressed front low-pressure gas in the shock tube 6 is all raise, then discharge by compressed rear pressurized gas outlet 31; The pressurized gas that spray into from pressurized gas inlet 21 simultaneously are because to shock tube 6 interior compressed front low-pressure gases actings, self-energy is consumed, and stays in the oscillator tube 6 so become minimal pressure gas;
(3) compressed front low-pressure gas injects the stage: stay the minimal pressure gas in the shock tube 6, rotation along with rotor 4, can be communicated with minimal pressure gas outlet 22 and compressed front low-pressure gas entrance 32, compressed front low-pressure gas enters in the shock tube 6 by compressed front low-pressure gas entrance 32, minimal pressure gas in the shock tube 6 is ejected, minimal pressure gas is discharged by minimal pressure gas outlet 22, and compressed front low-pressure gas is stayed in the shock tube 6; Rotation along with rotor 5, shock tube 6 is communicated with pressurized gas inlet 21 and compressed rear pressurized gas outlet 31, the compressed front low-pressure gas of staying in the shock tube 6 is compressed by the pressurized gas from pressurized gas inlet 21 incidents again, enters next circulation, and so forth circulation.
In sum, adopt the to-and-fro motion of piston to come directly gas to be compressed different from prior art, gas compressor of the present invention adopts pressurized gas that low-pressure gas is compressed, and realizes the purpose of pressurized gas, and compression efficiency significantly improves.Wherein, the composition of pressurized gas and low-pressure gas can be identical, also can be different.
Further, also be provided with two sealing plugs 8 between described casing 1 and the rotor 5, the outlet 12 of propellant entrance 11 and propellant is between two sealing plugs 8, and sealing plug 8 is used for isolated high-voltage gas, propellant and compressed gas, guarantees the normal operation of system.
In addition, the present invention adopts propellant to enter in the casing 1 from propellant entrance 11, propellant promotes blade 7 and rotates, blade 7 rotor drivens 5 rotate together, therefore, rotating shaft 4 of the present invention need not stretch out that casing 1 is outer to be connected with motor and to be rotated by motor driving, the sealability of casing 1 significantly improves, and has greatly reduced the amount of leakage of the interior pressurized gas of casing 1.Simultaneously, be connected with motor because rotating shaft 4 of the present invention need not be stretched out outside the casing 1, therefore, reduced the volume of whole air wave refrigerating device, convenient transportation, installation and operation.
The above is preferred implementation of the present invention; should be pointed out that for those skilled in the art, under the prerequisite that does not break away from the principle of the invention; can also make some improvements and modifications, these improvements and modifications also are considered as protection scope of the present invention.

Claims (5)

1. a gas compressor is characterized in that, comprises the casing of both ends open, and an end and first end cap of described casing are tightly connected, and the other end of described casing is connected with the second end bracket enclosed;
Be equipped with a rotating shaft that is positioned at described casing on described the first end cap and the second end cap, the two ends of described rotating shaft are rotationally connected with described the first end cap and the second end cap respectively;
Be installed with a rotor in the described rotating shaft, offer the shock tube of at least one axial setting along described rotating shaft on the described rotor;
Described first end covers and offers pressurized gas inlet and the minimal pressure gas outlet that can communicate with described shock tube, and described pressurized gas inlet is used for pressurized gas are accelerated to the velocity of sound or ultrasound velocity;
Offer compressed rear pressurized gas outlet and the compressed front low-pressure gas entrance that can communicate with described shock tube on described the second end cap;
The outer periphery of described rotor are installed with blade, offer on the described casing with described blade over against the propellant entrance that arranges and propellant outlet.
2. a kind of gas compressor according to claim 1 is characterized in that, described shock tube along the circumferential direction is evenly distributed on the described rotor.
3. a kind of gas compressor according to claim 1 and 2 is characterized in that, the quantity of described shock tube is 1 ~ 100.
4. a kind of gas compressor according to claim 1 is characterized in that, described first end covers and is installed with clutch shaft bearing, is installed with the second bearing on described the second end cap, the two ends of described rotating shaft respectively with described clutch shaft bearing be connected bearing and be connected.
5. a kind of gas compressor according to claim 1 is characterized in that, also is provided with two sealing plugs between described casing and the rotor, and described propellant entrance and propellant outlet are between two described sealing plugs.
CN2012105828546A 2012-12-28 2012-12-28 Gas compressor Pending CN102996404A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2012105828546A CN102996404A (en) 2012-12-28 2012-12-28 Gas compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2012105828546A CN102996404A (en) 2012-12-28 2012-12-28 Gas compressor

Publications (1)

Publication Number Publication Date
CN102996404A true CN102996404A (en) 2013-03-27

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CN2012105828546A Pending CN102996404A (en) 2012-12-28 2012-12-28 Gas compressor

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106194658A (en) * 2016-08-31 2016-12-07 吴礼智 A kind of gas-liquid exchanger structure and there is the gas-liquid switch type gas compressor of this mechanism
CN115405858A (en) * 2021-05-27 2022-11-29 中国石油化工股份有限公司 Energy-saving pressurization system of multi-pressure system

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2991929A (en) * 1955-05-12 1961-07-11 Stalker Corp Supersonic compressors
JPH11351191A (en) * 1998-06-04 1999-12-21 Mayekawa Mfg Co Ltd High pressure generating method and compressor using this method
CN101363326A (en) * 2008-09-23 2009-02-11 浙江大学 Improved motor for pneumatic tools
CN101813094A (en) * 2008-12-23 2010-08-25 通用电气公司 Supersonic compressor
CN102645046A (en) * 2012-04-01 2012-08-22 深圳市力科气动科技有限公司 Gas wave refrigerator
CN203114566U (en) * 2012-12-28 2013-08-07 深圳市力科气动科技有限公司 Gas compressor

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2991929A (en) * 1955-05-12 1961-07-11 Stalker Corp Supersonic compressors
JPH11351191A (en) * 1998-06-04 1999-12-21 Mayekawa Mfg Co Ltd High pressure generating method and compressor using this method
CN101363326A (en) * 2008-09-23 2009-02-11 浙江大学 Improved motor for pneumatic tools
CN101813094A (en) * 2008-12-23 2010-08-25 通用电气公司 Supersonic compressor
CN102645046A (en) * 2012-04-01 2012-08-22 深圳市力科气动科技有限公司 Gas wave refrigerator
CN203114566U (en) * 2012-12-28 2013-08-07 深圳市力科气动科技有限公司 Gas compressor

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106194658A (en) * 2016-08-31 2016-12-07 吴礼智 A kind of gas-liquid exchanger structure and there is the gas-liquid switch type gas compressor of this mechanism
CN106194658B (en) * 2016-08-31 2018-09-28 吴礼智 A kind of gas-liquid exchanger structure and the gas-liquid switch type gas compressor with the mechanism
CN115405858A (en) * 2021-05-27 2022-11-29 中国石油化工股份有限公司 Energy-saving pressurization system of multi-pressure system

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Application publication date: 20130327