CN101596424A - Rotating nozzle type stirrer - Google Patents
Rotating nozzle type stirrer Download PDFInfo
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- CN101596424A CN101596424A CNA2009100999217A CN200910099921A CN101596424A CN 101596424 A CN101596424 A CN 101596424A CN A2009100999217 A CNA2009100999217 A CN A2009100999217A CN 200910099921 A CN200910099921 A CN 200910099921A CN 101596424 A CN101596424 A CN 101596424A
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- support housing
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- planet
- turbine
- nozzles
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Abstract
The invention discloses rotating nozzle type stirrer, fixed support housing lower end is supported the ball rolling through rotation and is combined with the rotation support housing; The fixed support housing is equipped with the cycloidal-pin wheel decelerator that is sleeved on drive shaft axle sleeve lower end with the inner chamber that the rotation support housing forms, and the drive shaft bore sleeve disposes turbine spindle, and turbine is equipped with in the turbine spindle termination; The lower end of cycloidal-pin wheel decelerator is that output connects sun gear shaft, sun gear shaft respectively with the engagement of the planet gear wheel of both sides, planet gear wheel and planet pinion are installed on the planet axis, planet axis fixes by cycloidal-pin wheel bearing and kuppe, the upper end of cycloidal-pin wheel decelerator is that input connects turbine spindle, sun gear shaft connects fixed gear, and fixed gear and planet pinion engagement are fitted with two nozzles that shift to install on the lateral wall of rotation support housing lower end.The injection direction of two nozzles departs from the center, and the recoil strength of injection can make the rotation of main frame automatic horizontal, can realize a jar interior comprehensive stirring and a mixing.
Description
Technical field
The present invention relates to agitator and make the field, relate in particular to rotating nozzle type stirrer.Be applied to oil product storage tank deposit and the sedimental stirring of radioactive waste tank bottom.
Background technology
The agitating device that relates to the fermentation vat of producing biogas in the prior art.A criss-cross hollow stirring pipe is installed in fermentation vat, with water pump liquid in the pond is extracted out and injected stirring pipe, stir transverse tube and under the reaction force of ejection liquid, make circular motion, make that fermentation raw material reaches abundant stirring in the pond.The advantage of agitator provided by the invention is: flow velocity is low, stirring is abundant, is fit to the technological requirement of fermentation methane.It makes in the fermentation vat mud suspend equably in the pond, increases contacting of bacterial classification and fermentation raw material, mixes no dead angle, thereby improves the biogas output twice, and install simply small investment.But applicability is relatively poor, only limits to the application of fermentation pond.Can't be applied in oil product storage tank deposit and the sedimental stirring of radioactive waste tank bottom.
Also relate to a kind of jet type injecting agitator in the prior art, be provided with drives impeller in the kuppe, drives impeller is passed the sealing and fixing seat by power shaft and is connected transmission mechanism, and the output shaft of transmission mechanism connects rotating mask, and rotating mask is provided with two injector heads at least.It is reasonable in design, the transmission performance that possesses stereoscopic and omnibearing, the fluid of injector head ejection can carry out the stirring of stereoscopic and omnibearing to storage solution, make it keep mobile performance, but it in use needs jar outer driving mechanism that adds, the 360 ° rotations of agitator in jar can not be realized, the stirring of the deposit in all kinds of storage tanks being carried out fully, do not stay the dead angle can't be finished.
Summary of the invention
Technical problem to be solved by this invention is the present situation at prior art, provide a kind of simple in structure, verticity good, stir sufficient rotating nozzle type stirrer.
The present invention solves the problems of the technologies described above the technical scheme that is adopted: rotating nozzle type stirrer, comprise the fixed support housing, and wherein: fixed support housing lower end is supported the ball rolling through rotation and is combined with the rotation support housing; The fixed support housing is equipped with the cycloidal-pin wheel decelerator that is sleeved on drive shaft axle sleeve lower end with the inner chamber that the rotation support housing forms, and the drive shaft bore sleeve disposes turbine spindle, and turbine is equipped with in the turbine spindle termination; The lower end of cycloidal-pin wheel decelerator is that output connects sun gear shaft, sun gear shaft respectively with the engagement of the planet gear wheel of both sides, planet gear wheel and planet pinion are installed on the planet axis, planet axis fixes by cycloidal-pin wheel bearing and kuppe, the upper end of cycloidal-pin wheel decelerator is that input connects turbine spindle, sun gear shaft connects fixed gear, and fixed gear and planet pinion engagement are fitted with two nozzles that shift to install on the lateral wall of rotation support housing lower end.
The measure of taking also comprises:
The above-mentioned turbine of stating is the axial flow unshrouded impeller with at least two blades.
Distance range between two above-mentioned nozzle axial lines is 10 millimeters to 100 millimeters.
Two above-mentioned nozzle axle center linear distance tank bottom distance ranges are 120 millimeters to 180 millimeters.
Two above-mentioned nozzle axle center linear distance tank bottom distance ranges are 155 millimeters.
Distance range between two above-mentioned nozzle 5 axial lines is 50 millimeters.
Compared with prior art, fixed support housing of the present invention lower end is supported ball through rotation and is rolled and be combined with the rotation support housing; The fixed support housing is equipped with the cycloidal-pin wheel decelerator that is sleeved on drive shaft axle sleeve lower end with the inner chamber that the rotation support housing forms, and the drive shaft bore sleeve disposes turbine spindle, and turbine is equipped with in the turbine spindle termination; The lower end of cycloidal-pin wheel decelerator is that output connects sun gear shaft, sun gear shaft respectively with the engagement of the planet gear wheel of both sides, planet gear wheel and planet pinion are installed on the planet axis, planet axis fixes by cycloidal-pin wheel bearing and kuppe, the upper end of cycloidal-pin wheel decelerator is that input connects turbine spindle, sun gear shaft connects fixed gear, and fixed gear and planet pinion engagement are fitted with two nozzles that shift to install on the lateral wall of rotation support housing lower end.Because the injection direction of two nozzles departs from the center, the recoil strength of injection can make the rotation of main frame automatic horizontal; The jet that ejects is smashed a jar interior accumulation stasis of blood slag, makes oil generation convection current in the petroleum tank, thereby realizes comprehensive stirring and mixing in the jar.
Description of drawings
Fig. 1 is a structural representation of the present invention;
Fig. 2 is Fig. 1 plan structure schematic diagram.
The specific embodiment
Below in conjunction with embodiment the present invention is described in further detail:
Fig. 1 is to shown in Figure 2, and 1, sun gear shaft, 2, fixed gear, 3, planet gear wheel, 4, planet pinion, 5, nozzle, 6, cycloidal-pin wheel bearing, 7, kuppe, 8, the rotation support housing, 9, cycloidal-pin wheel decelerator, 10, drive shaft axle sleeve, 11, rotation supports ball, 12, the fixed support housing, 13 turbine spindles, 14 turbines.
Rotating nozzle type stirrer comprises fixed support housing 12, and wherein: fixed support housing 12 lower ends are supported ball 11 rollings through rotation and are combined with rotation support housing 8; Fixed support housing 12 is equipped with the cycloidal-pin wheel decelerator 9 that is sleeved on drive shaft axle sleeve 10 lower ends with the inner chamber that rotation support housing 8 forms, and drive shaft axle sleeve 10 inner chambers dispose turbine spindle 13, and turbine 14 is equipped with in turbine spindle 13 terminations; The lower end of cycloidal-pin wheel decelerator 9 is that output connects sun gear shaft 1, sun gear shaft 1 respectively with planet gear wheel 3 engagement of both sides, planet gear wheel 3 is installed on the planet axis 15 with planet pinion 4, planet axis 15 fixes by cycloidal-pin wheel bearing 6 and kuppe 7, the upper end of cycloidal-pin wheel decelerator 9 is that input connects turbine spindle 13, sun gear shaft 1 connects fixed gear 2, fixed gear 2 and planet pinion 4 engagements are fitted with two nozzles 5 that shift to install on the rotation support housing 8 lower end lateral walls.The turbine of stating 14 is for having the axial flow unshrouded impeller of at least two blades.Distance range between two common nozzle 5 axial lines is 10 millimeters to 100 millimeters; Two nozzle 5 axial lines are 120 millimeters to 180 millimeters apart from the tank bottom distance range.Preferred embodiment is that two distance ranges between nozzle 5 axial lines are 50 millimeters; Two nozzle 5 axial lines are 155 millimeters apart from the tank bottom distance range.
Turbine 14 is drive sources of this system, and former oil spurts and being driven on the turbine 14 in being extracted jar by circulating pump makes turbine 14 rotations, and turbine 14 revolving forces can be sent to crude oil nozzle 5, by nozzle 5 ejections.After wherein turbine 14 passes through the interior high speed reducing ratio of a series of transmissions of transmission mechanism, slow, the smooth rotation of drive main frame; Because the injection direction of two nozzles 5 departs from the center, the recoil strength of injection can make the rotation of main frame automatic horizontal.The jet that ejects is smashed a jar interior accumulation stasis of blood slag, makes oil generation convection current in the petroleum tank, thereby realizes comprehensive stirring and mixing in the jar.
The applicant's former design adds upper bed-plate apart from about 1300 millimeters of tank bottom distance, and the dead angle can be caused in the part.And these structure nozzle 5 centers and distance from bottom only are 155 millimeters, can clear up the bottom cleaner, more thorough, also can regulate height as required, and range of application is wider; And, need to prove that nozzle 5 must be below the crude oil liquid level, otherwise static can take place, cause fire easily.
Though the present invention is described by the reference preferred embodiment,, those skilled in the art should understand, and in the scope of claims, can do the various variation on form and the details.
Claims (6)
1, rotating nozzle type stirrer comprises fixed support housing (12), it is characterized in that: described fixed support housing (12) lower end is supported ball (11) rolling through rotation and is combined with rotation support housing (8); Described fixed support housing (12) is equipped with the cycloidal-pin wheel decelerator (9) that is sleeved on drive shaft axle sleeve (10) lower end with the inner chamber that described rotation support housing (8) forms, drive shaft axle sleeve (10) inner chamber disposes turbine spindle (13), and turbine (14) is equipped with in turbine spindle (13) termination; The lower end of cycloidal-pin wheel decelerator (9) is that output connects sun gear shaft (1), sun gear shaft (1) respectively with the engagement of the planet gear wheel (3) of both sides, planet gear wheel (3) is installed on the planet axis (15) with planet pinion (4), planet axis (15) fixes by cycloidal-pin wheel bearing (6) and kuppe (7), the upper end of cycloidal-pin wheel decelerator (9) is that input connects turbine spindle (13), sun gear shaft (1) connects fixed gear (2), fixed gear (2) and planet pinion (4) engagement are fitted with two nozzles (5) that shift to install on the lateral wall of described rotation support housing (8) lower end.
2, rotating nozzle type stirrer according to claim 1 is characterized in that: described turbine (14) is for having the axial flow unshrouded impeller of at least two blades.
3, rotating nozzle type stirrer according to claim 1 and 2 is characterized in that: the distance range between described two nozzles (5) axial line is 10 millimeters to 100 millimeters.
4, rotating nozzle type stirrer according to claim 1 and 2 is characterized in that: described two nozzles (5) axial line is 120 millimeters to 180 millimeters apart from the tank bottom distance range.
5, rotating nozzle type stirrer according to claim 1 and 2 is characterized in that: described two nozzles (5) axial line is 155 millimeters apart from the tank bottom distance range.
6, rotating nozzle type stirrer according to claim 1 and 2 is characterized in that: the distance range between described two nozzles (5) axial line is 50 millimeters.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2009100999217A CN101596424A (en) | 2009-06-18 | 2009-06-18 | Rotating nozzle type stirrer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2009100999217A CN101596424A (en) | 2009-06-18 | 2009-06-18 | Rotating nozzle type stirrer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101596424A true CN101596424A (en) | 2009-12-09 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNA2009100999217A Pending CN101596424A (en) | 2009-06-18 | 2009-06-18 | Rotating nozzle type stirrer |
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| Country | Link |
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| CN (1) | CN101596424A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102430361A (en) * | 2011-09-09 | 2012-05-02 | 山东大学 | Rotary jet mixer |
| CN104190304A (en) * | 2014-09-15 | 2014-12-10 | 沈阳飞机工业（集团）有限公司 | Jet flow and axial flow combined stirrer |
| CN105268363A (en) * | 2015-10-10 | 2016-01-27 | 芜湖市禾森食品有限公司 | Planetary-gear stirring device for stirring machine |
| CN106422903A (en) * | 2015-08-04 | 2017-02-22 | 峨眉山市驰骋机械制造有限公司 | Novel crude oil stirrer |
-
2009
- 2009-06-18 CN CNA2009100999217A patent/CN101596424A/en active Pending
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102430361A (en) * | 2011-09-09 | 2012-05-02 | 山东大学 | Rotary jet mixer |
| CN104190304A (en) * | 2014-09-15 | 2014-12-10 | 沈阳飞机工业（集团）有限公司 | Jet flow and axial flow combined stirrer |
| CN104190304B (en) * | 2014-09-15 | 2016-08-24 | 沈阳飞机工业（集团）有限公司 | A kind of jet axial flow combined impeller |
| CN106422903A (en) * | 2015-08-04 | 2017-02-22 | 峨眉山市驰骋机械制造有限公司 | Novel crude oil stirrer |
| CN105268363A (en) * | 2015-10-10 | 2016-01-27 | 芜湖市禾森食品有限公司 | Planetary-gear stirring device for stirring machine |
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| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| ASS | Succession or assignment of patent right |
Owner name: NINGBO LIANTONG EQUIPMENT MANUFACTURING CO., LTD. Free format text: FORMER OWNER: LIAN SHIXIONG Effective date: 20101217 |
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| C41 | Transfer of patent application or patent right or utility model | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20101217 Address after: 315207 Ningbo connection equipment manufacturing Co., Ltd., 1368, Luo Dong Road, Zhenhai Town, Zhejiang, Ningbo Applicant after: Ningbo Liantong Equipment Manufacturing Co., Ltd. Address before: 315207 Ningbo connection equipment manufacturing Co., Ltd., 1368, Luo Dong Road, Zhenhai Town, Zhejiang, Ningbo Applicant before: Lian Shixiong |
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| C12 | Rejection of a patent application after its publication | ||
| RJ01 | Rejection of invention patent application after publication |
Open date: 20091209 |