CN201165955Y - V type oil-free reciprocating vacuum pump - Google Patents
V type oil-free reciprocating vacuum pump Download PDFInfo
- Publication number
- CN201165955Y CN201165955Y CNU2008200311725U CN200820031172U CN201165955Y CN 201165955 Y CN201165955 Y CN 201165955Y CN U2008200311725 U CNU2008200311725 U CN U2008200311725U CN 200820031172 U CN200820031172 U CN 200820031172U CN 201165955 Y CN201165955 Y CN 201165955Y
- Authority
- CN
- China
- Prior art keywords
- vacuum pump
- groups
- fuselage
- piston
- slideway
- Prior art date
Links
- 229910001141 Ductile iron Inorganic materials 0.000 claims abstract description 10
- 230000001154 acute Effects 0.000 claims abstract description 5
- 239000003921 oils Substances 0.000 claims description 15
- 239000003570 air Substances 0.000 claims description 10
- 239000011901 water Substances 0.000 claims description 5
- 230000000712 assembly Effects 0.000 claims description 3
- 239000000314 lubricants Substances 0.000 description 4
- 238000005461 lubrication Methods 0.000 description 3
- 230000000875 corresponding Effects 0.000 description 2
- 239000007789 gases Substances 0.000 description 2
- 238000000034 methods Methods 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000000498 cooling water Substances 0.000 description 1
- 238000005755 formation reactions Methods 0.000 description 1
- 238000007710 freezing Methods 0.000 description 1
- 239000000446 fuels Substances 0.000 description 1
- 239000012208 gear oils Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000010705 motor oils Substances 0.000 description 1
- 230000002035 prolonged Effects 0.000 description 1
Abstract
Description
Technical field
The utility model relates to the technical field of structures of vacuum pump.
Background technique
Existing vacuum pump fuselage slideway and fuselage are an integral body, and slideway is splash lubrication, and after the running, slideway may be pulled, and causes the maintenance expenses height; Existing vacuum pump bottom air inlet and exhaust valve is arranged in the Stuffing box inner chamber, is not easy to maintenance; Existing vacuum pump piston rod is connected with crosshead with extension bar, extension bar with piston, piston rod and locks unreliablely, easily becomes flexible after the long-term operation, causes phenomenons such as cylinder cap and piston damage.
The model utility content
The utility model purpose be to design a kind ofly take up an area of that the space is little, long service life, the V-type oilless reciprocating vacuum pump being convenient to safeguard.
The utility model comprises fuselage, a set of bell cranks mechanism, be connected two connecting rods on the crank mechanism, respectively with two two groups of crosshead slippers, two groups of slideways, two groups of piston assemblys, two cylinders, two cylinder caps that connecting rod is supporting, angle between described two connecting rod axis is an acute angle, two groups of detachable respectively being connected on the fuselage of slideway, described slideway is the spheroidal graphite cast iron slideway.
During running, under the driving of motor, the slidercrank mechanism that is made of bent axle, connecting rod, crosshead slipper and fuselage passes to piston with the linear reciprocating motion of crosshead slipper by piston rod, realizes suction gas process.Because the angle between two connecting rod axis of the present utility model is an acute angle, the V-shape structure of formation, mutually perpendicular arrangement can reduce floor space of the present utility model greatly between two more existing connecting rod axis.In addition, because the utility model adopts the spheroidal graphite cast iron slideway, and split type spheroidal graphite cast iron slideway and fuselage ways of connecting, not only intensity improves, and directly increases the service life, and maintains easily, and reduces operating cost.
The utility model is provided with air inlet and exhaust valve on the top of cylinder head, and air inlet and exhaust valve down is set on the circumferential surface of cylinder, has also made things convenient for maintenance and detection.
The slideway sidewall is offered oil inlet hole, and described oil inlet hole is connected with external oil feed pump.Adopt this pressure lubrication mode, lubricant oil has guaranteed the sufficient lubrication of slideway by shaft head gear oil pump and external motor oil pump fuel feeding behind oil separator, has reduced the wearing and tearing of slideway and crosshead, has prolonged working life.
Piston rod adds the end that seam is connected crosshead slipper by screw thread.Guaranteed the Location accuracy of piston rod.
In addition, also be provided with direct selling between piston rod and the crosshead slipper, can further guarantee between piston rod and the crosshead slipper not loosening after the long-term operation.
Connect upper and lower cover plate respectively in the piston rod end that is connected with piston, be connected by bolt between upper and lower cover plate and the piston.Because piston rod and piston adopt upper and lower cover plate to add the Placement of bolt, guarantee between piston rod and the piston be connected after the long-term operation loosening.
On fuselage, divide to add the inlet and outlet air flue is set.Can reduce the height of porting, and when maintenance Stuffing box, cylinder, cylinder head, not need to dismantle airduct, reduce repair density, reduce maintenance load.
Bottom at fuselage is provided with water storage cavity.Can feed cooling water summer, reduces the temperature of lubricant oil; Can feed hot water or water vapour winter, improves the temperature of lubricant oil, avoids the freezing of lubricant oil (this mode of heating is compared with the external electric heater, reliable, safety, economy), thereby guarantee the running reliably and with long-term of equipment.
Description of drawings
Fig. 1 is a kind of structural representation of the present utility model.
Embodiment
As shown in Figure 1, the utility model mainly by fuselage 14, a set of bell cranks mechanism 15, be connected two connecting rods 13 on the crank mechanism 15, form with supporting two groups of crosshead slippers of two connecting rods 13 10, two groups of spheroidal graphite cast iron slideways 11, two groups of piston assemblys 4, two cylinders 3, two cylinder caps 1 respectively.
On the top of cylinder head 1 air inlet and exhaust valve 2 is set, air inlet and exhaust valve 5 down is set on the circumferential surface of cylinder 2.
Crank mechanism 15 is supported on the fuselage 14, is acute angle at the angle of fixing on the output shaft of crank mechanism 15 between 13, two connecting rod 13 axis of two connecting rods.
Two groups of spheroidal graphite cast iron slideways 11 are connected on the fuselage 14 by bolt is detachable respectively, and the sidewall of spheroidal graphite cast iron slideway 11 is offered oil inlet hole, and each oil inlet hole is connected by oil separator 12 with external oil feed pump.Supporting one group of crosshead slipper 10 respectively in two groups of spheroidal graphite cast iron slideways 11, each is organized crosshead slipper 10 and is hinged by bearing pin with corresponding connecting rod 13 respectively.Each upper end of organizing crosshead slipper 10 adds seam by screw thread respectively and is connected with piston rod 7, and between piston rod 7 and the crosshead slipper 10 direct selling is set.
Between cylinder 3 and corresponding spheroidal graphite cast iron slideway 11, separate space 8 is set, the dynamic seal apparatus that comprises stuffing box 6,9 is set respectively between the two ends of separate space 8 and the piston rod 7.
Between two separate spaces 8 suction port 19 is set, sets out gas port on suction port 19 opposites.Periphery at two cylinders 3 is provided with intake and exhaust air flue 17 respectively.
Fuselage 14 is connected on the base 16, in the bottom of fuselage 14 water storage cavity 18 is set.
Claims (8)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008200311725U CN201165955Y (en) | 2008-01-25 | 2008-01-25 | V type oil-free reciprocating vacuum pump |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008200311725U CN201165955Y (en) | 2008-01-25 | 2008-01-25 | V type oil-free reciprocating vacuum pump |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201165955Y true CN201165955Y (en) | 2008-12-17 |
Family
ID=40191341
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2008200311725U CN201165955Y (en) | 2008-01-25 | 2008-01-25 | V type oil-free reciprocating vacuum pump |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201165955Y (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102032141A (en) * | 2010-11-30 | 2011-04-27 | 浙江大学 | Vertical non-oil-contamination energy-saving vacuum pump |
| CN102094785A (en) * | 2011-03-16 | 2011-06-15 | 卢高 | Miniature piston air pump without oil lubrication |
| CN102226450A (en) * | 2011-06-13 | 2011-10-26 | 张庆鹏 | Reciprocating screw vacuum compressor |
| CN102226466A (en) * | 2011-06-13 | 2011-10-26 | 张庆鹏 | Reciprocating screw transmission mechanism |
| CN103216428B (en) * | 2013-04-26 | 2015-08-12 | 中国石油大学(北京) | Well casing gas gas collection pump |
| CN106917789A (en) * | 2017-04-25 | 2017-07-04 | 大连海事大学 | V-shape piston rod hydraulic motor |
-
2008
- 2008-01-25 CN CNU2008200311725U patent/CN201165955Y/en not_active IP Right Cessation
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102032141A (en) * | 2010-11-30 | 2011-04-27 | 浙江大学 | Vertical non-oil-contamination energy-saving vacuum pump |
| CN102094785A (en) * | 2011-03-16 | 2011-06-15 | 卢高 | Miniature piston air pump without oil lubrication |
| CN102226450A (en) * | 2011-06-13 | 2011-10-26 | 张庆鹏 | Reciprocating screw vacuum compressor |
| CN102226466A (en) * | 2011-06-13 | 2011-10-26 | 张庆鹏 | Reciprocating screw transmission mechanism |
| CN102226450B (en) * | 2011-06-13 | 2013-04-10 | 张庆鹏 | Reciprocating screw vacuum compressor |
| CN102226466B (en) * | 2011-06-13 | 2013-10-02 | 张庆鹏 | Reciprocating screw transmission mechanism |
| CN103216428B (en) * | 2013-04-26 | 2015-08-12 | 中国石油大学(北京) | Well casing gas gas collection pump |
| CN106917789A (en) * | 2017-04-25 | 2017-07-04 | 大连海事大学 | V-shape piston rod hydraulic motor |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| C14 | Grant of patent or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170711 Address after: 225402 west of Dai Wang Road, Chengdong Industrial Park, Taixing, Jiangsu Patentee after: Jiangsu Industrial Pump Technology Development Co Ltd Address before: 225400, No. 35, Dong Yan, Yan tou Town, Yan Town, Jiangsu, Taixing Patentee before: Xue Jianguo |
|
| TR01 | Transfer of patent right | ||
| CU01 | Correction of utility model patent |
Correction item: Patentee|Address Correct: Jiangsu Asia Pacific Industrial Pump Technology Development Co Ltd|225402 west of Dai Wang Road, Chengdong Industrial Park, Taixing, Jiangsu False: Jiangsu Industrial Pump Technology Development Co Ltd|225402 west of Dai Wang Road, Chengdong Industrial Park, Taixing, Jiangsu Number: 30-02 Volume: 33 |
|
| CU01 | Correction of utility model patent | ||
| CX01 | Expiry of patent term |
Granted publication date: 20081217 |
|
| CX01 | Expiry of patent term |