CN109774907A - Concatenation type mixing wastewater with air propulsion device - Google Patents
Concatenation type mixing wastewater with air propulsion device Download PDFInfo
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- CN109774907A CN109774907A CN201910090576.4A CN201910090576A CN109774907A CN 109774907 A CN109774907 A CN 109774907A CN 201910090576 A CN201910090576 A CN 201910090576A CN 109774907 A CN109774907 A CN 109774907A
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- propulsion device
- tail portion
- line
- spout
- water inlet
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Abstract
The invention belongs to propulsion device fields, it is related to a kind of concatenation type mixing wastewater with air propulsion device, including multiple admission lines 1, gas spout is circular ring shape pipeline in every group of propulsion device, and lower end seals, the tail portion of admission line is penetrated from the top outer diameter tube wall of the circular ring shape pipeline of gas spout and coupling part is all close connection, the upper end of admission line is perpendicular to deck and is upward through deck, it is mostly section that water inlet line is separated by the circular ring shape pipeline of gas spout, it is closely connect with before and after the inner wall of the pipe on gas spout two-by-two, it is placed on the straight line where the tailing axle of traditional propeller and before and after assembled water inlet line through entire hull, tail portion spout is placed on ship tail portion and closely connect with the tail portion of water inlet line.Concatenation type mixing wastewater with air propulsion device provided by the invention is not influenced using high pressure gas as power source by cavitation, cavitation corrosion, has good runnability under high speed operation environment.
Description
Technical field
The invention belongs to propulsion device fields, and in particular to a kind of concatenation type mixing wastewater with air propulsion device.
Background technique
In recent years, with the rapid development of Optimal Structure Designing and drag reduction technology, the route speed on high-performance naval vessel is obtained
It greatly improves, while also bringing new problem and challenge, i.e., traditional underwater propulsion unit is run under high speed operation environment
Performance is poor.General propeller propulsion is limited in the sail body speed of service within 50 sections, more than after the value, due to liquid-containing air
The influence of change will lead to the thrust of turbomachine and propulsive efficiency declines rapidly, and cavitation corrosion is more tight to the destruction of blade
Weight, therefore the underwater propulsion unit for being suitable for high-speed cruising environment is developed as a kind of urgent need.
Summary of the invention
1, technical problem to be solved:
Traditional underwater propulsion unit on existing naval vessel runnability under high speed operation environment is poor.General propeller promotes handle
The sail body speed of service is limited within 50 sections, after speed is more than 50 sections, since the influence of liquid cavitation will lead to turbine
The thrust and propulsive efficiency of tool decline rapidly, and cavitation corrosion is more serious to the destruction of blade.
2, technical solution:
In order to solve problem above, the present invention provides a kind of concatenation type mixing wastewater with air propulsion device, including multiple admission lines,
Each admission line tail portion is connected with 1 gas spout, further includes water inlet line, tail portion spout, each gas
Body spout is circular ring shape pipeline, and lower end seals, each circular ring shape pipe of the tail portion of the admission line from gas spout
The top outer diameter tube wall in road penetrates and coupling part is all close connection, and each admission line is vertically placed in hull,
The upper end of each admission line perpendicular to deck and is upward through deck, and the water inlet line is by the annulus of gas spout
It is mostly section that shape pipeline, which separates, closely connect with before and after the inner wall of the pipe on gas spout two-by-two, is placed on the tail of traditional propeller
On straight line where axis and assembled water inlet line before and after run through entire hull, the tail portion spout be placed on ship tail portion and
It is closely connect with the tail portion of water inlet line, a turbine is set at the upper orifice of each water inlet line.
The water inlet line upper end is wide pipe, and lower end is narrow pipe, is closely connect at narrow pipe and wide interface tube.
The part that each admission line is higher than deck connects one by right-angle elbow pipe interface at nozzle and is parallel to captain
The round tube in direction, nozzle is towards fore direction, and pipe diameter is identical as wide pipe diameter, the latter air inlet than it is previous into
Port is high, and nozzle is closely connect with nozzle junction.
The latter air inlet is higher by the height of 1/2 wide pipe diameter than previous air inlet.
On the internal diameter tube wall of the circular ring shape pipeline of the gas spout be embedded with multiple small nozzles, multiple small nozzles along
Even tube wall is spirally distributed and the angle of each small nozzle is along tangentially 3 degree of the inclination inwardly of tube wall circumference.
The small nozzle is 6.
The admission line has 3.
Admission line described in 3 is arranged from front to back along ship middle line direction.
The top outer diameter pipe that the rotary shaft of the turbine is parallel to admission line is placed vertically.
The caliber of the water inlet line is rearwardly gradually increased by small by this one end of water inlet, fast when close to tail portion spout
Speed is in the same size with tail portion spout caliber by being reduced to greatly.
3, the utility model has the advantages that
Concatenation type mixing wastewater with air propulsion device technology provided by the invention is anti-compared to propeller propulsion, hydraulic jet propulsion, metal/water
The propulsion modes such as Jet propulsion and jet-propulsion are answered, there are many advantages.The Push Technology is using high pressure gas as power source, no
It is influenced by cavitation, cavitation corrosion, there is good runnability under high speed operation environment.
Detailed description of the invention
Fig. 1 is overall schematic of the invention.
Fig. 2 is top view of the invention.
Fig. 3 is the profile diagram of gas spout of the present invention.
Fig. 4 is the top view of gas spout of the present invention.
Specific embodiment
Below by attached drawing, the present invention is described in detail.
The present invention provides a kind of concatenation type mixing wastewater with air propulsion device, including multiple admission lines 1, each air inlet
1 tail portion of pipeline is all connected with 1 gas spout 3, further includes water inlet line 5, tail portion spout 4, the gas spout 3 is circle
Circulating line, and lower end seals, the top outer diameter of the tail portion of the admission line 1 from the circular ring shape pipeline of gas spout 3
Tube wall penetrates and coupling part is all close connection from the sucking air of admission line 1, the gas-vapor mix in water inlet line 5, then
The propulsive thrust that the injection of spout 4 is formed in tail portion just constitutes the major impetus source of ship advance.
Admission line of the present invention is 3.
The admission line 1 is vertically placed in hull, and the upper end of the admission line 1 is worn perpendicular to deck and upwards
Cross deck.
As shown in Figure 1, the admission line 1 is divided to for two parts wide at the top and narrow at the bottom, top outer diameter Guan Weikuan pipe, lower outer diameter
Pipe is narrow pipe, is closely connect at narrow pipe and wide interface tube, the entirety after the wide pipe of admission line 1 is closely connect with narrow pipe is put vertically
It is placed in hull；Allowing more gases when 2 high speed rotation of turbine, leniently pipe nozzle is inhaled into, and being inhaled into gas, leniently pipe enters
When the lesser narrow pipe of caliber, gas pressure increases, and is finally quickly sprayed with higher pressure from the gas spout 3 of narrow pipe tail portion；
And the power and gas that ship advance is given due to sucking thrust while width pipe sucking gas are after narrow pipe is pressurized
It sprays from gas spout high pressure and is sufficiently merged with water flow, finally just constituted from the propulsive thrust that the injection of ship tail portion spout 4 is formed
The major impetus source that ship advances.
The wide pipe is perpendicular to deck and is upward through deck, and the part higher than deck passes through right-angle elbow pipe at nozzle
Interface connects the round tube for being parallel to captain direction, and nozzle is towards fore direction, and pipe diameter is identical as wide pipe diameter, after
One air inlet is higher by the height of 1/2 wide pipe diameter than previous air inlet, and nozzle is closely connect with nozzle junction, this
Sample design breaks down primarily to preventing rainy day rainwater from causing turbine to be intake from air inlet inflow, reduces previous when air-breathing
Air inlet openings inhibition caused by the latter air inlet, and be due to sucking thrust while sucking gas
Ship provides a part of onward impulse.
The water inlet line 5 is also simultaneously mixing wastewater with air pipeline, it is divided into multistage, two-by-two with the circle on gas spout
Close connection before and after circulating line inner wall, is placed on the straight line where the tailing axle of traditional propeller and assembled water inlet line
Entire hull is run through in front and back；Caliber is rearwardly gradually increased by small by this one end of water inlet, when close to tail portion spout rapidly by
It is reduced to greatly consistent with 4 pipe diameter size of tail portion spout；Water inlet line 5 in this way design can it is more convenient with 3 groups of gas spout
It fills and replaces and alleviate air-water mixture to the pressure of tube wall, to guarantee that air-water mixture at the uniform velocity flows in water inlet line
It is dynamic.
As shown in Figure 3 and Figure 4, the internal diameter of the circular ring shape pipeline of the gas spout 3, which closes, is embedded with multiple small nozzles on tube wall,
Multiple small nozzles be spirally distributed along even tube wall and the angle of each small nozzle along tube wall circumference tangentially inwardly
3 degree of inclination.The design in this way of gas spout 3 can allow gas to spray simultaneously from each height of water inlet line 5 and form helical form height
Pressure gas stream carries out more fully air water with the water flow in water inlet line 5 and merges, while improving mixing wastewater with air in water inlet line 5
The speed that object integrally at the uniform velocity flows.
The small nozzle is 6.
When ship advances, water flow is flowed into from 5 nozzle of water inlet line of place foremost part of ship sprays with from each gas spout 3
High pressure gas out at the uniform velocity flow in water inlet line 5 after adequately merging, most fast through pressure when the spout of ship tail portion afterwards
Speed increases to which high-voltage high-speed sprays.Ship is controlled by 6 left and right adjusting of rudder blade after air-water mixture is sprayed from tail portion spout 4
The direction that oceangoing ship advances.
Although the present invention has been described by way of example and in terms of the preferred embodiments, they be not it is for the purpose of limiting the invention, it is any ripe
This those skilled in the art is practised, without departing from the spirit and scope of the invention, can make various changes or retouch from working as, therefore guarantor of the invention
Shield range should be subject to what claims hereof protection scope was defined.
Claims (10)
1. a kind of concatenation type mixing wastewater with air propulsion device, it is characterised in that: including multiple admission lines (1), each air inlet
Pipeline (1) tail portion is all connected with 1 gas spout (3), further includes water inlet line (5), tail portion spout (4), each gas
Body spout (3) is circular ring shape pipeline, and lower end seals, and the tail portion of each admission line (1) is sprayed from corresponding gas
The top outer diameter tube wall of the circular ring shape pipeline of mouth (3) penetrates and coupling part is all close connection, each admission line (1)
It is vertically placed in hull, the upper end of each admission line (1) perpendicular to deck and is upward through deck, the water inlet
It is mostly section that pipeline (5) is separated by the circular ring shape pipeline of gas spout (3), two-by-two and before and after the inner wall of the pipe on gas spout (3)
Close connection is placed on the straight line where the tailing axle of traditional propeller and before and after assembled water inlet line (5) through entire
Hull, the tail portion spout (4) are placed on ship tail portion and closely connect with the tail portion of water inlet line (5), each water inlet line
(1) turbine (2) are set at upper orifice.
2. concatenation type mixing wastewater with air propulsion device as described in claim 1, it is characterised in that: the water inlet line upper end is
Width pipe, lower end are narrow pipe, are closely connect at narrow pipe and wide interface tube.
3. concatenation type mixing wastewater with air propulsion device as described in claim 1, it is characterised in that: each admission line (1) is higher than
The part on deck connects the round tube for being parallel to captain direction by right-angle elbow pipe interface at nozzle, and nozzle is towards fore side
To, and pipe diameter is identical as wide pipe diameter, the latter air inlet is higher than previous air inlet, and nozzle and nozzle junction are equal
Close connection.
4. concatenation type mixing wastewater with air propulsion device as claimed in claim 3, it is characterised in that: the latter air inlet than
Previous air inlet is higher by the height of 1/2 wide pipe diameter.
5. concatenation type mixing wastewater with air propulsion device as described in claim 1, it is characterised in that: the circle of the gas spout (3)
Multiple small nozzles are embedded on the internal diameter tube wall of circulating line, multiple small nozzles are spirally distributed and often along even tube wall
The angle of a small nozzle tangentially tilts 3 degree along tube wall circumference inwardly.
6. concatenation type mixing wastewater with air propulsion device as claimed in claim 5, it is characterised in that: the small nozzle is 6.
7. the concatenation type mixing wastewater with air propulsion device as described in claim 1-6 any claim, it is characterised in that: described
Admission line (1) has 3.
8. concatenation type mixing wastewater with air propulsion device as claimed in claim 7, it is characterised in that: admission line (1) described in 3
It is arranged from front to back along ship middle line direction.
9. the concatenation type mixing wastewater with air propulsion device as described in claim 1-6 any claim, it is characterised in that: the whirlpool
The top outer diameter pipe that the rotary shaft of wheel (2) is parallel to admission line (1) is placed vertically.
10. the concatenation type mixing wastewater with air propulsion device as described in claim 1-6 any claim, it is characterised in that: described
The caliber of water inlet line (5) is rearwardly gradually increased by small by this one end of water inlet, rapidly by big when close to tail portion spout (4)
It is reduced to consistent with tail portion spout (4) pipe diameter size.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910090576.4A CN109774907A (en) | 2019-01-30 | 2019-01-30 | Concatenation type mixing wastewater with air propulsion device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910090576.4A CN109774907A (en) | 2019-01-30 | 2019-01-30 | Concatenation type mixing wastewater with air propulsion device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109774907A true CN109774907A (en) | 2019-05-21 |
Family
ID=66503618
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910090576.4A Withdrawn CN109774907A (en) | 2019-01-30 | 2019-01-30 | Concatenation type mixing wastewater with air propulsion device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109774907A (en) |
-
2019
- 2019-01-30 CN CN201910090576.4A patent/CN109774907A/en not_active Withdrawn
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| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190521 |
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| WW01 | Invention patent application withdrawn after publication |