CN105065268A - Air compressor - Google Patents
Air compressor Download PDFInfo
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- CN105065268A CN105065268A CN201510498614.1A CN201510498614A CN105065268A CN 105065268 A CN105065268 A CN 105065268A CN 201510498614 A CN201510498614 A CN 201510498614A CN 105065268 A CN105065268 A CN 105065268A
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- air compressor
- level
- stage
- compression chamber
- male rotor
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Abstract
The invention provides an air compressor, and belongs to the technical field of air compressors. The air compressor solves the technical problems that a motor is large in output power, high in power consumption and low in efficiency. The air compressor comprises a first drive source, a second drive source and an air compressor body. A first-level compression cavity and a second-level compression cavity which are communicated with each other are formed inside the air compressor body. A first-level male rotor and a first-level female rotor which are matched with each other are arranged in the first-level compression cavity. A second-level male rotor and a second-level female rotor which are matched with each other are arranged in the second-level compression cavity. The first drive source is connected with the first-level male rotor, and the second drive source is connected with the second-level male rotor. The air compressor has the beneficial effects of improving the compression efficiency, saving the energy and the like.
Description
Technical field
The invention belongs to air compressor technical field, relate to a kind of air compressor.
Background technique
Air compressor is the main body in compressed air source unit, and it is the device mechanical energy of prime mover (normally motor) being converted to gas pressure energy, is compressed-air actuated pressure generator.Now conventional air compressor has piston type air compressor, screw air compressor, centrifugal compressor, sliding-vane air compressor and scroll type air compressor.
China patent CN103225612A discloses a kind of screw air compressor, and it comprises motor, screw rod, machine barrel, described motor connecting screw rod, and screw rod is arranged in machine barrel; Minimum range between described screw rod and machine barrel is 5mm, and the space between screw rod and machine barrel is oil groove; Machine tube inner wall has annular protrusion, and annular protrusion is placed between two spiral shell ribs of screw rod just, and the space distance between annular protrusion and two spiral shell ribs is greater than 3mm, is less than 6mm; Machine barrel top is provided with inlet hole and exhaust port.This structure is simple, can provide high-pressure air at short notice.
But, be only only the use of one stage of compression in above-mentioned patent and carry out pressurized air, cause output power of motor large, consume energy higher and efficiency is low.
Summary of the invention
The present invention be directed to the problems referred to above that existing technology exists, provide a kind of screw air compressor adopting two-stage compression, technical problem to be solved by this invention is: how to reduce energy consumption, improves compression efficiency.
Object of the present invention realizes by following technical proposal:
A kind of air compressor, comprise driving source one, driving source two and fuselage, the one stage of compression chamber and two-stage compression chamber that are connected is offered in described fuselage, the one-level male rotor matched and one-level female rotor is provided with in described one stage of compression chamber, the secondary male rotor matched and secondary female rotor is provided with in described two-stage compression chamber, described driving source one is connected with one-level male rotor, and described driving source two is connected with secondary male rotor.
Its working principle is as follows: this air compressor is when compressing, the one-level male rotor being positioned at one stage of compression chamber is driven to rotate by driving source one, one-level male rotor drives the one-level female rotor be mated to rotate, thus the one stage of compression realized air, air after compressed arrives two-stage compression chamber, the secondary male rotor being positioned at two-stage compression chamber is driven to rotate by driving source two, secondary male rotor drives the secondary female rotor be mated to rotate, thus the two-stage compression realized air, the air after final compression is discharged from relief opening.
In above-mentioned a kind of air compressor, between described one stage of compression chamber and two-stage compression chamber, be provided with cooling unit.After being designed with cooling unit, volume of air can be made to diminish, promote compression efficiency, and reduce output power of motor simultaneously.
In above-mentioned a kind of air compressor, described one stage of compression chamber is arranged on the top in two-stage compression chamber along compressor body short transverse.
In above-mentioned a kind of air compressor, described one-level male rotor, one-level female rotor, secondary male rotor and secondary female rotor are spirality.After being designed to spirality, can make one-level male rotor and one-level female rotor, the cooperation between secondary male rotor and secondary female rotor is rotated convenient and efficient.
In above-mentioned a kind of air compressor, described driving source one and driving source two are magneto.After driving source is designed to magneto, can energy consumption be reduced, raise the efficiency.Driving source in the application can be electronic, pneumatic, and this Pneumatic actuator can adopt the form of cylinder as driving source.Driving source belongs to prior art with the installation Placement of fuselage, is no longer repeated.
Compared with prior art, the present invention has the following advantages:
1, have employed the structure of two stage compression in the application, compared with documents, which raises compression efficiency, reduce output power of motor, reach energy-conservation effect;
2, be designed with cooling unit, compared with documents, it makes volume of air diminish, and promotes compression efficiency, and reduces output power of motor simultaneously.
3, have employed two separately-driven structures of driving source in the application, compared with documents, it can control one-level male rotor respectively and secondary male rotor rotates, and one-level male rotor and secondary male rotor rotating speed can independently adjust.
Accompanying drawing explanation
Fig. 1 is the structural representation in this air compressor one stage of compression chamber in embodiment.
Fig. 2 is the structural representation of this air compressor entirety in embodiment.
Fig. 3 is the structural representation in this air compressor two-stage compression chamber in embodiment.
In figure, 1, fuselage; 2, one stage of compression chamber; 3, two-stage compression chamber; 4, one-level male rotor; 5, one-level female rotor; 6, secondary male rotor; 7, secondary female rotor.
Embodiment
Be below specific embodiments of the invention and by reference to the accompanying drawings, technological scheme of the present invention is further described, but the present invention be not limited to these embodiments.
As Fig. 1, Fig. 2, shown in Fig. 3, this air compressor comprises fuselage 1, offer the one stage of compression chamber 2 and two-stage compression chamber 3 that are connected from top to down along compressor body short transverse in fuselage 1, intermeshing helical one-level male rotor 4 and one-level female rotor 5 is placed with in one stage of compression chamber 2, the intermeshing male rotor of secondary twist 6 and secondary female rotor 7 is placed with in two-stage compression chamber 3, when air compressor is started working, first magneto drives the one-level male rotor 4 being positioned at one stage of compression chamber 2 be attached thereto to rotate, one-level male rotor 4 drives the one-level female rotor 5 be engaged with to rotate, thus one stage of compression is realized to air.
The present embodiment preferably has, and between one stage of compression chamber 2 and two-stage compression chamber 3, cooling unit is housed.This cooling unit can adopt means conventional in prior art, such as oil cooler.Air after one stage of compression is through oil cooling system, oil nozzle ejection fogging oil, smaller volume after air and fogging oil cool, enter two-stage compression chamber 3 afterwards, second magneto drives the secondary male rotor 6 being positioned at two-stage compression chamber 3 be attached thereto to rotate, secondary male rotor 6 drives the secondary female rotor 7 be engaged with to rotate, thus realizes two-stage compression to air.
Specific embodiment described herein is only to the explanation for example of the present invention's spirit.Those skilled in the art can make various amendment or supplement or adopt similar mode to substitute to described specific embodiment, but can't depart from spirit of the present invention or surmount the scope that appended claims defines.
Claims (5)
1. an air compressor, it is characterized in that, comprise driving source one, driving source two and fuselage (1), the one stage of compression chamber (2) and two-stage compression chamber (3) that are connected is offered in described fuselage (1), the one-level male rotor (4) and one-level female rotor (5) that match is provided with in described one stage of compression chamber (2), the secondary male rotor (6) and secondary female rotor (7) that match is provided with in described two-stage compression chamber (3), described driving source one is connected with one-level male rotor (4), described driving source two is connected with secondary male rotor (6).
2. a kind of air compressor according to claim 1 and 2, is characterized in that, is provided with cooling unit between described one stage of compression chamber (2) and two-stage compression chamber (3).
3. a kind of air compressor according to claim 1, is characterized in that, described one stage of compression chamber (2) is arranged on the top of two-stage compression chamber (3) along compressor body short transverse.
4. a kind of air compressor according to claim 1 and 2, it is characterized in that, described one-level male rotor (4), one-level female rotor (5), secondary male rotor (6) and secondary female rotor (7) are spirality.
5. a kind of air compressor according to claim 1, is characterized in that, described driving source one and driving source two are magneto.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510498614.1A CN105065268A (en) | 2015-08-14 | 2015-08-14 | Air compressor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510498614.1A CN105065268A (en) | 2015-08-14 | 2015-08-14 | Air compressor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105065268A true CN105065268A (en) | 2015-11-18 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510498614.1A Pending CN105065268A (en) | 2015-08-14 | 2015-08-14 | Air compressor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105065268A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106593867A (en) * | 2016-12-31 | 2017-04-26 | 上海偌托新能源科技有限公司 | Double-permanent-magnet two-level screw compressor |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2002021759A (en) * | 2000-06-30 | 2002-01-23 | Hitachi Ltd | Screw compressor |
| CN101487470A (en) * | 2008-12-19 | 2009-07-22 | 武汉凯龙技术开发有限责任公司 | Double-machine two-stage screw type low-temperature compressor unit |
| CN203051122U (en) * | 2012-12-03 | 2013-07-10 | 上海信然压缩机有限公司 | Two-stage cooling type double-screw two-stage supercharging air compressor |
| CN204877937U (en) * | 2015-08-14 | 2015-12-16 | 温岭市鑫磊空压机有限公司 | Air compressor |
-
2015
- 2015-08-14 CN CN201510498614.1A patent/CN105065268A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2002021759A (en) * | 2000-06-30 | 2002-01-23 | Hitachi Ltd | Screw compressor |
| CN101487470A (en) * | 2008-12-19 | 2009-07-22 | 武汉凯龙技术开发有限责任公司 | Double-machine two-stage screw type low-temperature compressor unit |
| CN203051122U (en) * | 2012-12-03 | 2013-07-10 | 上海信然压缩机有限公司 | Two-stage cooling type double-screw two-stage supercharging air compressor |
| CN204877937U (en) * | 2015-08-14 | 2015-12-16 | 温岭市鑫磊空压机有限公司 | Air compressor |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106593867A (en) * | 2016-12-31 | 2017-04-26 | 上海偌托新能源科技有限公司 | Double-permanent-magnet two-level screw compressor |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| CB02 | Change of applicant information | ||
| CB02 | Change of applicant information |
Address after: 317500 Taizhou city Zhejiang City Chengxi Industrial Park in Taizhou, Zhejiang Applicant after: Compressor Xinlei Limited by Share Ltd Address before: 317500 Taizhou city Zhejiang City Chengxi Industrial Park in Taizhou, Zhejiang Applicant before: Wenling Xinlei Air Compressor Co., Ltd. |
|
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20151118 |