CN202451118U - Reciprocating linear adjustable pumping unit - Google Patents
Reciprocating linear adjustable pumping unit Download PDFInfo
- Publication number
- CN202451118U CN202451118U CN2011205786563U CN201120578656U CN202451118U CN 202451118 U CN202451118 U CN 202451118U CN 2011205786563 U CN2011205786563 U CN 2011205786563U CN 201120578656 U CN201120578656 U CN 201120578656U CN 202451118 U CN202451118 U CN 202451118U
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- China
- Prior art keywords
- fuselage
- reducer
- guide rail
- motion mechanism
- annular rack
- 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 - Fee Related
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- 238000005086 pumping Methods 0.000 title abstract description 11
- 239000003638 chemical reducing agent Substances 0.000 claims abstract description 16
- 230000005540 biological transmission Effects 0.000 claims abstract description 5
- 238000005096 rolling process Methods 0.000 abstract 2
- 230000000694 effects Effects 0.000 description 5
- 230000002950 deficient Effects 0.000 description 2
- 241000283080 Proboscidea <mammal> Species 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
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Abstract
The utility model discloses a reciprocating linear adjustable pumping unit which comprises a base and a hauling pipe, wherein a unit body is arranged on the base, a rolling cylinder is arranged on the end portion of the upper end of the unit body, the hauling pipe is movably connected with a reciprocating linear motion mechanism through the rolling cylinder, and the reciprocating linear motion mechanism is in transmission connection with a power device. The pumping unit is characterized in that the power device is fixedly installed on the unit body. Moreover, the power device comprises a motor and a reducer, and the reducer is fixed on the external wall of the unit body through a reducer base. The reciprocating linear motion mechanism comprises an operating panel, an annular guiding rail and an annular rack, the annular rack is in transmission connection with a driving wheel, the driving wheel is provided with a gear shaft, and the end portion of the gear shaft is located in the annular guiding rail. The pumping unit is simple in structure, reliable in operation, high in operating efficacy, capable of adjusting the operating stroke distance and suitable for different operational requirements. Besides, the pumping unit can be designed for a vertical type and a horizontal type so as to be suitable for different operational environments.
Description
Technical field
The utility model relates to a kind of oil pumper, specifically, relates to a kind of toward the adjustable oil pumper of complex line.
Background technology
At present, oil field machinery oil equipment has a variety of, and the maximum of usefulness are beam-pumping units, also have some blue elephants, like chain drive pumping unit, belt oil pumping machine, makes the vertical oil-pumping machine of switching-over motion with motor positive and inverse.And the patent No. to be 200610070317.8 Chinese invention patent disclose a kind of annular rack type pumping machine, in its technical scheme, with the pinion of annular rack engagement be through sprocket wheel in the chain-wheel box and chain drive; Its defective is: during switching-over; It is to swing to a suitable angle through drive chain case to realize that gear laterally moves, this structure more complicated, and stress condition is bad; Stroke distances is fixing can not regulate, operate unreliable, the operation effect is low.
The utility model content
The technical problem that the utility model will solve is to overcome above-mentioned defective, provide a kind of simple in structure, stroke distances is adjustable, operate reliably, the adjustable oil pumper of past complex line that the operation effect is high.
For addressing the above problem, the technical scheme that the utility model adopted is:
A kind of toward the adjustable oil pumper of complex line; Comprise base and pull rope; Base is provided with fuselage, and end, said fuselage upper end is provided with cylinder, and said pull rope is connected with linear reciprocating motion mechanism through cylinder; The linear reciprocating motion mechanism driving is connected with power set, it is characterized in that: said power set are fixedly mounted on the fuselage.
Say further:
Said power set comprise motor, with the direct-connected reducer of motor, reducer is fixed on the fuselage outer wall through the reducer seat.
Said linear reciprocating motion mechanism comprises working panel; Said working panel is provided with ring-shaped guide rail, is fixed with annular rack on the said working panel, and said annular rack is connected with driving wheel; Said driving wheel is provided with gear shaft, and the end of gear shaft is positioned at ring-shaped guide rail; Said gear shaft is provided with drive away from the end of ring-shaped guide rail, and drive and power set are in transmission connection.
Further say:
Said ring-shaped guide rail is long ring-shaped guide rail.
Said annular rack is length-adjustable long annular rack.
Further say:
Said fuselage is vertically mounted on the base.
Said standard of fuselage is installed on the base.
Be provided with fixed bar between said power set and the fuselage.
Owing to adopted technique scheme, compared with prior art, the utility model is simple in structure, operate reliably, the operation effect is high, can be through the length of adjustment long annular rack and long ring-shaped guide rail, and adjusting impulse stroke distance is to adapt to the different working demand.In addition, the utility model can be designed to vertical and horizontal two kinds of form of structure, can adapt to different working environments.
Below in conjunction with the accompanying drawing and the specific embodiment the utility model is further specified.
Description of drawings
Fig. 1 is the structural representation of a kind of embodiment of the utility model;
Fig. 2 is the structural representation of the said linear reciprocating motion of the embodiment of the utility model mechanism;
Fig. 3 is the A-A view of Fig. 2;
Fig. 4 is the structural representation of the another kind of embodiment of the utility model.
Among the figure: the 1-pull rope; The 2-cylinder; The 3-reverse wheel; 4-linear reciprocating motion mechanism; The 5-fixed bar; The 6-motor; The 7-reducer; The 8-line shaft; 9-reducer seat; The 10-fuselage; The 11-base; The 12-working panel; The 13-ring-shaped guide rail; The 14-power wheel; The 15-annular rack; The 16-bolt; The 17-drive; The 18-driving wheel; The 19-gear shaft; The 20-directive wheel; The 21-connecting lever.
The specific embodiment
Embodiment:
A kind of toward the adjustable oil pumper of complex line, comprise base 11 and pull rope 1, pull rope 1 passes cylinder 2 and reverse wheel 3, is connected with working panel 12.Be vertically installed with fuselage 10 on the base 11; End, said fuselage 10 upper end is provided with cylinder 2; Said pull rope 1 is connected with linear reciprocating motion mechanism 4 through cylinder 2 and the reverse wheel 3 that is arranged in the fuselage 10; Linear reciprocating motion mechanism 4 is connected with power set, and power set are fixedly mounted on the fuselage.
Power set comprise motor 6, with the direct-connected reducer 7 of motor 6, reducer 7 is fixed on fuselage 10 outer walls through reducer seat 9.In the present embodiment, be provided with fixed bar 5 between fuselage 10 and the motor 6, what fixed bar 5 can be to motor 6 fixedly plays booster action.
Like Fig. 2, shown in Figure 3, be provided with fixed bar 5 between said power set and the fuselage 10.Fixed bar 5 can fixedly helping out to motor 6.Said linear reciprocating motion mechanism comprises working panel 12; Said working panel 12 is provided with ring-shaped guide rail 13; Be fixed with annular rack 15 on the said working panel 12; Said annular rack 15 is connected with driving wheel 18, and said driving wheel 18 is provided with gear shaft 19, and an end end of gear shaft 19 is positioned at ring-shaped guide rail 13; Said gear shaft 19 is provided with drive 17 away from the end of ring-shaped guide rail 13, and drive 17 is in transmission connection with power set.
In the present embodiment, reducer 7 is connected with line shaft 8, and the end of line shaft 8 is installed with power wheel 14, power wheel 14 and drive 17 engagements.In addition, the top of gear shaft 19 is installed with directive wheel 20, and directive wheel 20 is installed in the long ring-shaped guide rail 13.In the present embodiment, according to requirements of one's work, ring-shaped guide rail is long ring-shaped guide rail, and annular rack is length-adjustable long annular rack.
During work, starter motor 6, through the effect of reducer 7, power passes to linear reciprocating motion mechanism 4 through line shaft 8.Line shaft 8 drives power wheel 14, and power wheel 14 drives drive 17, and drive 17 drives driving wheel 18 through gear shaft 19.Driving wheel 18 drives the upwards perhaps downward moving linearly of working panel 12 through annular rack 15.The effect of directive wheel 20 is driving wheel 18 to be remained with annular rack 15 often mesh.Like this, pull rope 1 is reciprocating under the drive of linear reciprocating motion mechanism 4, and then realizes the oil pumping operation.
As other embodiment of the utility model, as shown in Figure 4, said fuselage 10 is a horizontal type structure, its underrun fixture or directly be fixed on the base 11.The front end of fuselage 10 is provided with the connecting lever perpendicular with it 21, and the upper/lower terminal of connecting lever 21 is respectively equipped with reverse wheel 3, and cylinder 2 is located at the front end at connecting lever 21 tops, and pull rope 1 passes cylinder 2 and reverse wheel 3 successively, is connected with linear reciprocating motion mechanism 4.
Claims (8)
1. one kind toward the adjustable oil pumper of complex line; Comprise base (11) and pull rope (1); Base (11) is provided with fuselage (10), and end, said fuselage (10) upper end is provided with cylinder (2), and said pull rope (1) is connected with linear reciprocating motion mechanism (4) through cylinder (2); Linear reciprocating motion mechanism (4) is connected with power set, it is characterized in that: said power set are fixedly mounted on the fuselage (10).
2. according to claim 1 toward the adjustable oil pumper of complex line, it is characterized in that: said power set comprise motor (6), with the direct-connected reducer (7) of motor (6), reducer (7) is fixed on fuselage (10) outer wall through reducer seat (9).
3. according to claim 2 toward the adjustable oil pumper of complex line; It is characterized in that: said linear reciprocating motion mechanism (4) comprises working panel (12); Said working panel (12) is provided with ring-shaped guide rail (13), is fixed with annular rack (15) on the said working panel (12), and said annular rack (15) is connected with driving wheel (18); Said driving wheel (18) is provided with gear shaft (19), and the end of gear shaft (19) is positioned at ring-shaped guide rail (13); Said gear shaft (19) is provided with drive (17) away from the end of ring-shaped guide rail (13), and drive (17) is in transmission connection with power set.
4. according to claim 3 toward the adjustable oil pumper of complex line, it is characterized in that: said ring-shaped guide rail (13) is long ring-shaped guide rail.
5. according to claim 3 or the 4 described past adjustable oil pumpers of complex line, it is characterized in that: said annular rack (15) is length-adjustable long annular rack.
6. according to claim 1 toward the adjustable oil pumper of complex line, it is characterized in that: said fuselage (10) is vertically mounted on the base (11).
7. according to claim 1 toward the adjustable oil pumper of complex line, it is characterized in that: said fuselage (10) level is installed on the base (11).
8. according to claim 6 or the 7 described past adjustable oil pumpers of complex line, it is characterized in that: be provided with fixed bar (5) between said power set and the fuselage (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205786563U CN202451118U (en) | 2011-12-31 | 2011-12-31 | Reciprocating linear adjustable pumping unit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205786563U CN202451118U (en) | 2011-12-31 | 2011-12-31 | Reciprocating linear adjustable pumping unit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202451118U true CN202451118U (en) | 2012-09-26 |
Family
ID=46866988
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011205786563U Expired - Fee Related CN202451118U (en) | 2011-12-31 | 2011-12-31 | Reciprocating linear adjustable pumping unit |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202451118U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111320293A (en) * | 2020-03-31 | 2020-06-23 | 金华宣亚环保技术有限公司 | Municipal administration sewage treatment plant convenient to clearance |
-
2011
- 2011-12-31 CN CN2011205786563U patent/CN202451118U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111320293A (en) * | 2020-03-31 | 2020-06-23 | 金华宣亚环保技术有限公司 | Municipal administration sewage treatment plant convenient to clearance |
| CN111320293B (en) * | 2020-03-31 | 2020-11-10 | 山东国晟环境科技有限公司 | Municipal administration sewage treatment plant convenient to clearance |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: YU HAI Free format text: FORMER OWNER: YU HONGLIANG Effective date: 20130911 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| COR | Change of bibliographic data |
Free format text: CORRECT: ADDRESS; FROM: 261000 WEIFANG, SHANDONG PROVINCE TO: 261041 WEIFANG, SHANDONG PROVINCE |
|
| TR01 | Transfer of patent right |
Effective date of registration: 20130911 Address after: 261041, No. 1, unit 1, building 101, Chen Jia village, Yu Da office, Kuiwei District, Weifang, Shandong Patentee after: Yu Hai Address before: 261000 Shandong Weixian city in Weifang Province Road No. 103, Weifang Hua Ling Diesel Power Co. Ltd. Patentee before: Yu Hongliang |
|
| ASS | Succession or assignment of patent right |
Owner name: HUALING DIESEL ENGINE POWER CO., LTD., WEIFANG Free format text: FORMER OWNER: YU HAI Effective date: 20131012 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| COR | Change of bibliographic data |
Free format text: CORRECT: ADDRESS; FROM: 261041 WEIFANG, SHANDONG PROVINCE TO: 261101 WEIFANG, SHANDONG PROVINCE |
|
| TR01 | Transfer of patent right |
Effective date of registration: 20131012 Address after: 261101 Shandong city of Weifang province Hanting Weixian Road East Patentee after: Hualing Diesel Engine Power Co., Ltd., Weifang Address before: 261041, No. 1, unit 1, building 101, Chen Jia village, Yu Da office, Kuiwei District, Weifang, Shandong Patentee before: Yu Hai |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Reciprocating linear adjustable pumping unit Effective date of registration: 20150827 Granted publication date: 20120926 Pledgee: China Co truction Bank Corp Weifang branch Pledgor: Weifang Hua Ling Diesel Engine Co., Ltd.|Yu Hongwei|Yu Hai Registration number: 2015980000211 |
|
| PLDC | Enforcement, change and cancellation of contracts on pledge of patent right or utility model | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20180613 Granted publication date: 20120926 Pledgee: China Co truction Bank Corp Weifang branch Pledgor: Hualing Diesel Engine Power Co., Ltd., Weifang|Yu Hongwei|Yu Hai Registration number: 2015980000211 |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120926 Termination date: 20191231 |