CN105413900A - Turbine gas-liquid injection device - Google Patents
Turbine gas-liquid injection device Download PDFInfo
- Publication number
- CN105413900A CN105413900A CN201510978134.5A CN201510978134A CN105413900A CN 105413900 A CN105413900 A CN 105413900A CN 201510978134 A CN201510978134 A CN 201510978134A CN 105413900 A CN105413900 A CN 105413900A
- Authority
- CN
- China
- Prior art keywords
- accelerator
- guide pipe
- fluid
- turbine gas
- circular cone
- 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.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
- B05B1/00—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means
- B05B1/34—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl
- B05B1/3405—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl to produce swirl
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
- B05B13/00—Machines or plants for applying liquids or other fluent materials to surfaces of objects or other work by spraying, not covered by groups B05B1/00 - B05B11/00
- B05B13/02—Means for supporting work; Arrangement or mounting of spray heads; Adaptation or arrangement of means for feeding work
Landscapes
- Hydraulic Turbines (AREA)
Abstract
The invention provides a turbine gas-liquid injection device which comprises a housing, wherein a fluid inlet and a fluid outlet are formed in the housing; a fixing device is arranged at the fluid inlet; a non-magnetic hard alloy tube and a composite high polymer magnet are arranged on the inner part of the housing; a vortex generator and a polymerization accelerator are arranged on the inner part of the non-magnetic hard alloy tube; the vortex generator is in seamless connection with the polymerization accelerator; the polymerization accelerator comprises a cylindrical accelerator and a conical guide tube; the vortex generator is in seamless connection with the cylindrical accelerator; the cylindrical accelerator is in seamless connection with the conical guide tube; the composite high polymer magnet is arranged at the outer side of the conical guide tube; and a fluid atomizing striker pin is arranged on the bottom of the housing. The turbine gas-liquid injection device can be used for splitting a liquid molecule surface layer, and improving mixing adhesion between liquid molecules and gas molecules, is simple in structure and capable of being used for a long time.
Description
Technical field
The present invention relates to a kind of liquid injection apparatus industrially, be specifically related to a kind of turbine gas liquid jetting device.
Background technology
At present, injection apparatus on market, be referred to as shower nozzle or nozzle, mainly contain burner class nozzle and non-combustible burner class shower nozzle, relevant apparatus is a critical component in the application apparatus such as jet, oil spout, spraying, sandblasting, owing to using the industry with application, the difference in market, the design of injection apparatus and function are that the special project in particular area uses substantially, at other field or need to use on the equipment of injecting-unit can not effectively compatible use, compatible bad, the scope of application is narrower.
Summary of the invention
The present invention is directed to the technical problem of above-mentioned existence, propose a kind of turbine gas liquid jetting device, can use in the device outside needing the outside kinetic energy of fluid to flow out, and fluid velocity and lifting fluid diffusingsurface can be improved, without the need to increasing other special installations, effect of premix atomization can be reached.
Technical scheme of the present invention is: a kind of turbine gas liquid jetting device, comprise: shell, described shell is arranged fluid inlet port and fluid outlet, described fluid inlet port place arranges fixture, described enclosure arranges non-magnesium hard alloy pipe and composite high-molecular magnetic, described non-magnesium hard alloy pipe inside arranges eddy generator and convergent accelerator, described eddy generator and convergent accelerator connection, described convergent accelerator comprises and arranges cylinder accelerator and circular cone guide pipe, described eddy generator and cylinder accelerator connection, described cylinder accelerator and circular cone guide pipe connection, the arranged outside composite high-molecular magnetic of described circular cone guide pipe, the bottom of described shell arranges fluid atomizing striker.
Further, described fixture is the screw thread being arranged on fluid inlet port.
Further, further, described eddy generator comprises: blade, impeller, bearing and base plate, and described blade is arranged on impeller, and described impeller is fixed on bearing, and described bearing is fixed on described base plate, and the surrounding of described base plate arranges through hole.
Further, the quantity of described blade is 10-120, and each blade is with the distortion of 10-60 degree.
Further, described bearing adopts titanium alloy material to make.
Further, described cylinder accelerator and circular cone guide pipe are poroid hollow cylindrical structure, wherein the poroid hollow structure of cylinder accelerator aligns with the through hole of base plate, and the poroid hollow cylindrical structure of described circular cone guide pipe aligns with the poroid hollow cylindrical structure of cylinder accelerator.
Further, the poroid hollow cylindrical structure of described cylinder accelerator and circular cone guide pipe is 10-100, and the through hole of described base plate is 10-100.
Beneficial effect of the present invention:
1, the invention provides a kind of turbine gas liquid jetting device, fluid molecule superficial layer can be divided, by diminishing of fluid molecule volume, decomposed liq molecule also reaches the state of atomization, utilize vibrations and the translation characteristic of gas molecule, raising fluid molecule mixes degree of adhesion with gas molecule, and device structure is simple, can Long-Time Service.
2, blade adopts composite to make, blade quantity adopts 10-120, each blade with the distortion of 10-60 degree, when fluid enters into eddy generator, rotated centered by titanium alloy bearing under the effect of impeller by potential energy fluid forces blade, form swirling fluid.
3, titanium alloy has antimagnetic corrosion resistance, and adopt titanium alloy as bearing, blade, under the promotion of potential energy fluid, rotates centered by bearing.
4, when swirling fluid enters into poroid hollow cylindrical structure inside from poroid hollow circuit cylinder inlet port, first after being arranged on high power magnet wherein and the sequence of electric charge systematicness is carried out to it, taper guide pipe is entered into from poroid hollow circuit cylinder delivery outlet, swirling fluid is spouting from taper guide pipe convergence mouth by taper guide pipe, forms the orderly electric charge arrangement of whirlpool rapidly fluid; Swirling fluid forms the atomization shape of 10-100 micron under the effect of fluid atomizing striker rapidly.
Accompanying drawing explanation
Fig. 1 is a kind of turbine gas liquid jetting device structure chart that the present invention proposes;
Fig. 2 is the described eddy generator structure chart that the present invention proposes;
Fig. 3 is the described impeller blade design top view that the present invention proposes;
Fig. 4 is the described cylinder accelerator structure figure that the present invention proposes;
Fig. 5 is the described circular cone guide pipe structure chart that the present invention proposes.
Shown in figure: 1, shell; 11, fluid inlet port; 12, fluid outlet; 13, fixture; 2, eddy generator; ; 21, blade; 22, impeller; 23, bearing; 24, base plate; 3, cylinder accelerator; 4, circular cone guide pipe; 5, composite high-molecular magnetic; 6, fluid atomizing striker.
Detailed description of the invention
See Fig. 1, it is a kind of turbine gas liquid jetting device structure chart that the present invention proposes.
As shown in Figure 1, a kind of turbine gas liquid jetting device, comprise: shell 1, described shell 1 is arranged fluid inlet port 11 and fluid outlet 12, described fluid inlet port 11 place arranges fixture 13, described shell 1 inside arranges non-magnesium hard alloy pipe and composite high-molecular magnetic 5, described non-magnesium hard alloy pipe inside arranges eddy generator 2 and convergent accelerator, described eddy generator 2 and convergent accelerator connection, described convergent accelerator comprises and arranges cylinder accelerator 3 and circular cone guide pipe 4, described eddy generator 2 and cylinder accelerator 3 connection, described cylinder accelerator 3 and circular cone guide pipe 4 connection, the arranged outside composite high-molecular magnetic 5 of described circular cone guide pipe 4, the bottom of described shell 1 arranges fluid atomizing striker 6.
In the embodiment of the present invention, the fluid inlet port of fluid above shell enters, make fluid produce whirlpool by eddy generator and enter into convergent accelerator, by cylinder accelerator, the fluid entered is accelerated, then by circular cone guide pipe, fluid is carried out the outlet mixed from circular cone guide pipe to spray, the fluid sprayed from the outlet of circular cone guide pipe, through the effect of fluid atomizing striker, forms 10-100 micron atomization shape and exports.
In the embodiment of the present invention, by arranging fixture on shell, this injection apparatus can be connected with application apparatus, wherein fixture can be arranged according to the interface of application apparatus, can be threaded, also can be that bolt connects, or book card hoop connected mode, specifically based on practical application structure, preferably, fixture 13 adopts helicitic texture, easy installation and removal.
See Fig. 2 and Fig. 3, wherein Fig. 2 is the described eddy generator structure chart that the present invention proposes; Fig. 3 is the described impeller blade design top view that the present invention proposes.
As shown in Figures 2 and 3, eddy generator 2 comprises: blade 21, impeller 22, bearing 23 and base plate 24, and blade 21 is arranged on impeller 22, and impeller 22 is fixed on bearing 23, and bearing 23 is fixed on described base plate 24, and the surrounding of base plate 24 arranges through hole.
Further, the quantity of blade 21 is 10-120, and each blade 21 is with the distortion of 10-60 degree.
In the embodiment of the present invention, blade adopts composite to make, and blade quantity adopts 10-120, each blade is with the distortion of 10-60 degree, when fluid enters into eddy generator, rotated centered by titanium alloy bearing under the effect of impeller by potential energy fluid forces blade, form swirling fluid.
Further, described bearing 23 adopts titanium alloy material to make.
In the embodiment of the present invention, titanium alloy has antimagnetic corrosion resistance, and adopt titanium alloy as bearing, blade, under the promotion of potential energy fluid, rotates centered by bearing.
See Fig. 4 and Fig. 5, wherein Fig. 4 is the described cylinder accelerator structure figure that the present invention proposes; Fig. 5 is the described circular cone guide pipe structure chart that the present invention proposes.
As shown in Figure 4 and Figure 5, cylinder accelerator 3 and circular cone guide pipe 4 are poroid hollow cylindrical structure, wherein the poroid hollow structure of cylinder accelerator 3 aligns with the through hole of base plate 24, and the poroid hollow cylindrical structure of circular cone guide pipe 4 aligns with the poroid hollow cylindrical structure of cylinder accelerator 3.
In the embodiment of the present invention, when swirling fluid enters into poroid hollow cylindrical structure inside from poroid hollow circuit cylinder inlet port, first after being arranged on high power magnet wherein and the sequence of electric charge systematicness is carried out to it, taper guide pipe is entered into from poroid hollow circuit cylinder delivery outlet, swirling fluid is spouting from taper guide pipe convergence mouth by taper guide pipe, forms the orderly electric charge arrangement of whirlpool rapidly fluid.
In the embodiment of the present invention, cylinder accelerator is identical with the number of openings of base plate with the quantity of the poroid hollow cylindrical structure of circular cone guide pipe, and corresponding setting, be convenient to the outflow of gas-liquid, the quantity of poroid hollow cylindrical structure and through hole is more, the speed of swirling fluid is faster, and the effect that gas-liquid is decomposed is better.Preferably, the poroid hollow cylindrical structure of cylinder accelerator 4 and circular cone guide pipe 5 is 10-100, and the through hole of described base plate is 10-100.
In the embodiment of the present invention, whirlpool orderly electric charge arrangement fluid is under the effect of composite high-molecular magnetic rapidly, forms the swirling fluid rapidly of reversal charge arrangement.
The invention provides a kind of turbine gas liquid jetting device, fluid molecule superficial layer can be divided, by diminishing of fluid molecule volume, decomposed liq molecule also reaches the state of atomization, utilize vibrations and the translation characteristic of gas molecule, raising fluid molecule mixes degree of adhesion with gas molecule, and device structure is simple, can Long-Time Service.
Above to invention has been detailed introduction, but the invention is not restricted to above-mentioned embodiment, in the ken that those of ordinary skill in the art possess, can also make a variety of changes under the prerequisite not departing from present inventive concept.Do not depart from the spirit and scope of the present invention and can make other changes many and remodeling.Should be appreciated that and the invention is not restricted to specific embodiment, scope of the present invention is defined by the following claims.
Claims (7)
1. a turbine gas liquid jetting device, it is characterized in that, comprise: shell (1), described shell (1) is arranged fluid inlet port (11) and fluid outlet (12), described fluid inlet port (11) place arranges fixture (13), described shell (1) inside arranges non-magnesium hard alloy pipe and composite high-molecular magnetic (5), described non-magnesium hard alloy pipe inside arranges eddy generator (2) and convergent accelerator, described eddy generator (2) and convergent accelerator connection, described convergent accelerator comprises and arranges cylinder accelerator (3) and circular cone guide pipe (4), described eddy generator (2) and cylinder accelerator (3) connection, described cylinder accelerator (3) and circular cone guide pipe (4) connection, the arranged outside composite high-molecular magnetic (5) of described circular cone guide pipe (4), the bottom of described shell (1) arranges fluid atomizing striker (6).
2. a kind of turbine gas liquid jetting device according to claim 1, is characterized in that, described fixture (13) is for being arranged on the screw thread of fluid inlet port.
3. a kind of turbine gas liquid jetting device according to claim 1, it is characterized in that, described eddy generator (2) comprising: blade (21), impeller (22) bearing (23) and base plate (24), described blade (21) is arranged on impeller (22), described impeller 22) be fixed on bearing (23), described bearing (23) is fixed on described base plate (24), and the surrounding of described base plate (24) arranges through hole.
4. a kind of turbine gas liquid jetting device according to claim 1, is characterized in that, the quantity of described blade (21) is 10-120, and each blade (21) is with the distortion of 10-60 degree.
5. a kind of turbine gas liquid jetting device according to claim 1, is characterized in that, described bearing (23) adopts titanium alloy material to make.
6. a kind of turbine gas liquid jetting device according to claim 1, it is characterized in that, described cylinder accelerator (3) and circular cone guide pipe (4) are poroid hollow cylindrical structure, wherein the poroid hollow structure of cylinder accelerator (3) aligns with the through hole of base plate (24), and the poroid hollow cylindrical structure of described circular cone guide pipe (4) aligns with the poroid hollow cylindrical structure of cylinder accelerator (3).
7. a kind of turbine gas liquid jetting device according to claim 1, is characterized in that, the poroid hollow cylindrical structure of described cylinder accelerator (4) and circular cone guide pipe (5) is 10-100, and the through hole of described base plate (24) is 10-100.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510978134.5A CN105413900A (en) | 2015-12-23 | 2015-12-23 | Turbine gas-liquid injection device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510978134.5A CN105413900A (en) | 2015-12-23 | 2015-12-23 | Turbine gas-liquid injection device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105413900A true CN105413900A (en) | 2016-03-23 |
Family
ID=55492698
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510978134.5A Pending CN105413900A (en) | 2015-12-23 | 2015-12-23 | Turbine gas-liquid injection device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105413900A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2084393U (en) * | 1990-11-06 | 1991-09-11 | 潞安矿务局科研所 | Dust-proof nozzle |
| CN2744418Y (en) * | 2004-10-12 | 2005-12-07 | 游仓杰 | Spraying cup for static powder spraying gun |
| WO2010026826A1 (en) * | 2008-09-05 | 2010-03-11 | 株式会社 日立製作所 | Fuel injection valve, and method for fitting two parts |
| CN201896161U (en) * | 2010-11-08 | 2011-07-13 | 中国石油化工股份有限公司 | Catalytic cracking and atomizing feeding spray nozzle |
| CN205269949U (en) * | 2015-12-23 | 2016-06-01 | 关峻宇 | Turbine gas -liquid injection apparatus |
-
2015
- 2015-12-23 CN CN201510978134.5A patent/CN105413900A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2084393U (en) * | 1990-11-06 | 1991-09-11 | 潞安矿务局科研所 | Dust-proof nozzle |
| CN2744418Y (en) * | 2004-10-12 | 2005-12-07 | 游仓杰 | Spraying cup for static powder spraying gun |
| WO2010026826A1 (en) * | 2008-09-05 | 2010-03-11 | 株式会社 日立製作所 | Fuel injection valve, and method for fitting two parts |
| CN201896161U (en) * | 2010-11-08 | 2011-07-13 | 中国石油化工股份有限公司 | Catalytic cracking and atomizing feeding spray nozzle |
| CN205269949U (en) * | 2015-12-23 | 2016-06-01 | 关峻宇 | Turbine gas -liquid injection apparatus |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
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| AD01 | Patent right deemed abandoned |
Effective date of abandoning: 20180831 |
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| AD01 | Patent right deemed abandoned |