CN203835726U - Two-stage compression oil injection screw main engine - Google Patents
Two-stage compression oil injection screw main engine Download PDFInfo
- Publication number
- CN203835726U CN203835726U CN201420269257.2U CN201420269257U CN203835726U CN 203835726 U CN203835726 U CN 203835726U CN 201420269257 U CN201420269257 U CN 201420269257U CN 203835726 U CN203835726 U CN 203835726U
- Authority
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- China
- Prior art keywords
- oil injection
- gear
- driven gear
- injection screw
- level
- 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.)
- Expired - Lifetime
Links
- 238000002347 injection Methods 0.000 title claims abstract description 57
- 239000007924 injection Substances 0.000 title claims abstract description 57
- 238000007906 compression Methods 0.000 title claims abstract description 27
- 230000006835 compression Effects 0.000 title claims abstract description 25
- 239000000446 fuel Substances 0.000 claims description 37
- 238000001816 cooling Methods 0.000 claims description 14
- 238000005461 lubrication Methods 0.000 claims description 14
- 230000008878 coupling Effects 0.000 claims description 7
- 238000010168 coupling process Methods 0.000 claims description 7
- 238000005859 coupling reaction Methods 0.000 claims description 7
- 230000005540 biological transmission Effects 0.000 abstract description 12
- 238000006073 displacement reaction Methods 0.000 abstract description 5
- 230000008901 benefit Effects 0.000 abstract description 3
- 239000003921 oil Substances 0.000 description 9
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 238000012423 maintenance Methods 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000010725 compressor oil Substances 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 238000004945 emulsification Methods 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Landscapes
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
Abstract
The utility model discloses a two-stage compression oil injection screw main engine. The two-stage compression oil injection screw main engine comprises a first-stage oil injection screw compressor, a second-stage oil injection screw compressor, a motor, a gear case and a central supporting frame; a driving gear a first-stage driven gear and a second-stage driven gear are arranged inside the gear box; the first-stage driven gear and the second-stage driven gear and the driving gear are engaged; the driving gear is fixed on a main engine input shaft; a coupler is connected with the main engine input shaft and a motor output shaft; the central supporting frame is connected between the gear box and the motor; the first-stage driven gear is connected with an input end of the first-level oil injection screw compressor; the second-stage driven gear is connected with an input end of a second-level oil injection screw compressor. The two-stage compression oil injection screw main engine has the advantages of improving the transmission efficiency due to the fact that the first-level oil injection screw compressor and the second-level oil injection screw compressor input power coaxially, reducing the number of parts, being compact, reasonable and reliable in structure, convenient to install and maintain, guaranteeing the coaxiality of the main engine input shaft and the motor output shaft and enabling the main engine to be supported due to the central supporting frame and avoiding relative displacement between the motor and the main engine during operation.
Description
Technical field
The utility model belongs to air compressor field, specifically refers to a kind of two stage compression exhaust end base of oil injection threaded bolt main frame.
Background technique
Low pressure fuel injector screw air compressor (0.6Mpa~1.25Mpa) for one-level compression has on the market replaced Piston Air Compressor completely.He is with good unfailing performance, vibrate little, noise is low, easy to operate, few easy workout part, high having obtained of operational efficiency use and favorable comment widely.Although one-level fuel injection helical lobe compressor is reliable and stable, reach the bottleneck that higher pressure is for he, so in mesohigh field or piston multistage compression realizes.
Existing piston machine multistage compression main frame uses the most extensive at mesohigh.He is that the method by improving temperature evaporation condensed water solves the problem that condensed water is separated out in a large number, so his delivery temperature is very high, the floor space that also has him to also have is large, noise is high, and vibration is large, and easily damaged parts is many, the shortcomings such as standby redundancy is many, and maintenance maintenance workload is large.Unit is with piston ring scuffing, and exhaust pressure and the air displacement obvious energy consumption that declines increases.
The middle pressure air compressor of two-stage screw rod series connection, have a fatal defect, because firsts and seconds is directly connected, what airborne moisture will be a large amount of in compression process separates out, separator is transpiring moisture timely, makes to cause emulsification after compressor oil and water mixing.Affected bearing and the gear lubrication of unit, unit shortens working life greatly.So such unit can not reach very high pressure, can not long-time continual operation.This type is eliminated abroad, only uses on the mobile compressor of mine engineering at home.
The medium voltage network of screw air compressor+cooling driers+screw rod pressure-increasing machine three machine series connection is external more novel middle pressure air compression systems at present.Cost is higher, and utilization amount is little.He has obtained very large improvement the shortcoming of appeal.But he is the units connected in series by three difference in functionalitys, so his floor space is still very large, each unit needs debugging coupling mutually.Each system control is relatively independent, higher to operation and maintenance difficulty.
To sum up, replace press in current piston with the advantage of fuel injection helical lobe compressor.Important core is exactly the problem whether two-stage fuel injection compression screw host can solve the problem of condensed water after one-level screw compression and main frame and rationally use the reliability of power (motor) transmission.
Model utility content
In order to address the above problem, the utility model provides a kind of two stage compression exhaust end base of oil injection threaded bolt main frame, two coaxial input powers of fuel injection helical lobe compressor of this two stage compression exhaust end base of oil injection threaded bolt main frame, improve transmission efficiency, reduce number of parts, make more compact structure, reasonable, reliable, be convenient to I&M.
The utility model for the technological scheme that solves its technical problem and adopt is:
A kind of two stage compression exhaust end base of oil injection threaded bolt main frame, comprise an one-level fuel injection helical lobe compressor and a secondary fuel injection helical lobe compressor, be provided with a motor, gear-box and center rest, in described gear-box, be provided with a driving gear, an one-level driven gear and a secondary driven gear, described one-level driven gear and described secondary driven gear engage with described driving gear respectively, described driving gear is fixed on main frame input shaft, described main frame input shaft is connected by coupling with described motor output shaft, described center rest is connected between described gear-box and described motor, described one-level driven gear connects described one-level fuel injection helical lobe compressor input end, described secondary driven gear connects described secondary fuel injection helical lobe compressor input end.
Say further, described one-level fuel injection helical lobe compressor has one-level lubrication and cooling system, and described secondary fuel injection helical lobe compressor has secondary lubrication and cooling system, and described one-level lubrication and cooling system and described secondary lubrication and cooling system are separate.
One-level fuel injection helical lobe compressor is for the production of low-pressure compressed air.Secondary fuel injection helical lobe compressor is for the compressed-air actuated production of pressure.The lubrication and cooling system of I and II fuel injection helical lobe compressor is each separate, mutual noninterference.Gear-box, for the common transmission of I and II fuel injection helical lobe compressor and the speed change of different tooth ratio, is merged into coaxial input power.Center rest is used for the concentric locating with motor, guarantees the coaxality of the input shaft of main frame and the output shaft of motor, and rigid support main frame, guarantees that relative displacement does not appear in motor and main frame in the running.
The beneficial effects of the utility model are: two stage compression exhaust end base of oil injection threaded bolt main frame of the present utility model is mainly made up of two relatively independent fuel injection helical lobe compressors and a gear-box, gear-box is mainly made up of a driving gear and two driven gears, motor is by driving gear of shaft coupling transmission, driving gear is two driven gears of transmission simultaneously again, two driven gears drive respectively one-level fuel injection helical lobe compressor and one-level fuel injection helical lobe compressor by corresponding rotating ratio, improve like this transmission efficiency, reduce number of parts, make more compact structure, rationally, reliably, be convenient to I&M.And the setting of center rest can be guaranteed the coaxality of main frame input shaft and motor output shaft, and rigid support main frame, guarantee that relative displacement does not appear in motor and main frame in the running.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model.
Embodiment
By specific instantiation, embodiment of the present utility model is described below, those skilled in the art can understand advantage of the present utility model and effect easily by content disclosed in the present specification.The utility model also can other different mode be implemented, and, under the category not disclosing departing from the utility model, can give different modifications and change that is.
Embodiment: a kind of two stage compression exhaust end base of oil injection threaded bolt main frame, comprise an one-level fuel injection helical lobe compressor 1 and a secondary fuel injection helical lobe compressor 2, be provided with a motor 3, gear-box 4 and center rest 5, in described gear-box, be provided with a driving gear 41, an one-level driven gear 42 and a secondary driven gear 43, described one-level driven gear 42 and described secondary driven gear 43 engage with described driving gear 41 respectively, described driving gear 41 is fixed on main frame input shaft 6, described main frame input shaft 6 is connected by coupling 7 with described motor output shaft 31, described center rest 5 is connected between described gear-box 4 and described motor 3, described one-level driven gear 42 connects described one-level fuel injection helical lobe compressor 1 input end, described secondary driven gear 43 connects described secondary fuel injection helical lobe compressor 2 input ends.
Described one-level fuel injection helical lobe compressor has one-level lubrication and cooling system, and described secondary fuel injection helical lobe compressor has secondary lubrication and cooling system, and described one-level lubrication and cooling system and described secondary lubrication and cooling system are separate.
Pass through coupling 7 transmissions to driving gear 41 by motor 3, then by driving gear 41 transmission one-level driven gear 42 and secondary driven gears 43.One-level driven gear 42 has more with the rotating ratio of driving gear 41 correspondences and drives one-level fuel injection helical lobe compressor 1 to air first compression.Pressurized air reaches after 0.4~1.0Mpa discharges one-level fuel injection helical lobe compressor 1 does dry processing by external system to pressurized air.Pressurized air is after drying inhaled into secondary fuel injection helical lobe compressor 2 and does after compression again reaches 1.8~4.2Mpa to discharge.Complete like this twice compression process of air.
Due to the oil-way system of one-level fuel injection helical lobe compressor and the shared driving gear of secondary fuel injection helical lobe compressor and oilgear, motor is by driving gear of shaft coupling transmission, driving gear is two driven gears of transmission simultaneously again, two driven gears drive respectively one-level fuel injection helical lobe compressor and one-level fuel injection helical lobe compressor by corresponding rotating ratio, improve like this transmission efficiency, reduce number of parts, made more compact structure, reasonable, reliable, be convenient to I&M.And the setting of center rest can be guaranteed the coaxality of main frame input shaft and motor output shaft, and rigid support main frame, guarantee that relative displacement does not appear in motor and main frame in the running.
The piston multistage compression main frame Contrast on effect of two stage compression exhaust end base of oil injection threaded bolt main frame of the present utility model and prior art is as following table:
| ? | Piston multistage compression main frame | Two stage compression exhaust end base of oil injection threaded bolt main frame |
| Boundary dimension | Greatly | Little |
| Can supply exhaust pressure | Middle high-pressure | Middle pressure |
| Noise | Greatly | Low |
| Vibration | Greatly | Little |
| Delivery temperature | High | Low |
| Source of the gas pulse | Greatly | Little |
| Discharge capacity attenuation degree | Greatly | Little |
| Easily damaged parts | Many | Few |
| Reliability | Generally | High |
| Working life | Shorter | Long |
Claims (2)
1. a two stage compression exhaust end base of oil injection threaded bolt main frame, comprise an one-level fuel injection helical lobe compressor (1) and a secondary fuel injection helical lobe compressor (2), it is characterized in that: be provided with a motor (3), a gear-box (4) and center rest (5), in described gear-box, be provided with a driving gear (41), an one-level driven gear (42) and a secondary driven gear (43), described one-level driven gear (42) and described secondary driven gear (43) engage with described driving gear (41) respectively, described driving gear (41) is fixed on main frame input shaft (6), described main frame input shaft (6) is connected by coupling (7) with described motor output shaft (31), described center rest (5) is connected between described gear-box (4) and described motor (3), described one-level driven gear (42) connects described one-level fuel injection helical lobe compressor (1) input end, described secondary driven gear (43) connects described secondary fuel injection helical lobe compressor (2) input end.
2. two stage compression exhaust end base of oil injection threaded bolt main frame as claimed in claim 1, it is characterized in that: described one-level fuel injection helical lobe compressor has one-level lubrication and cooling system, described secondary fuel injection helical lobe compressor has secondary lubrication and cooling system, and described one-level lubrication and cooling system and described secondary lubrication and cooling system are separate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420269257.2U CN203835726U (en) | 2014-05-23 | 2014-05-23 | Two-stage compression oil injection screw main engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420269257.2U CN203835726U (en) | 2014-05-23 | 2014-05-23 | Two-stage compression oil injection screw main engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203835726U true CN203835726U (en) | 2014-09-17 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420269257.2U Expired - Lifetime CN203835726U (en) | 2014-05-23 | 2014-05-23 | Two-stage compression oil injection screw main engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203835726U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106014996A (en) * | 2016-08-03 | 2016-10-12 | 德斯兰压缩机(上海)有限公司 | Two-stage compression screw air compressor |
| CN108019349A (en) * | 2016-10-28 | 2018-05-11 | 艾尔米克压缩机有限责任公司 | The spiral two-part air compressor of oil spout |
| CN109322824A (en) * | 2016-08-01 | 2019-02-12 | 珠海格力电器股份有限公司 | Screw compressor and multistage screw transmission structure thereof |
| CN116517832A (en) * | 2023-05-24 | 2023-08-01 | 中国船舶集团有限公司第七一一研究所 | Compressor assembly system and low-temperature gas compression method |
-
2014
- 2014-05-23 CN CN201420269257.2U patent/CN203835726U/en not_active Expired - Lifetime
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109322824A (en) * | 2016-08-01 | 2019-02-12 | 珠海格力电器股份有限公司 | Screw compressor and multistage screw transmission structure thereof |
| CN106014996A (en) * | 2016-08-03 | 2016-10-12 | 德斯兰压缩机(上海)有限公司 | Two-stage compression screw air compressor |
| CN108019349A (en) * | 2016-10-28 | 2018-05-11 | 艾尔米克压缩机有限责任公司 | The spiral two-part air compressor of oil spout |
| CN116517832A (en) * | 2023-05-24 | 2023-08-01 | 中国船舶集团有限公司第七一一研究所 | Compressor assembly system and low-temperature gas compression method |
| WO2024239892A1 (en) * | 2023-05-24 | 2024-11-28 | 上海船用柴油机研究所 | Compressor assembly system and low-temperature gas compression method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20140917 |