CN107738725B - A kind of supercavity submarine navigation device - Google Patents
A kind of supercavity submarine navigation device Download PDFInfo
- Publication number
- CN107738725B CN107738725B CN201710895504.8A CN201710895504A CN107738725B CN 107738725 B CN107738725 B CN 107738725B CN 201710895504 A CN201710895504 A CN 201710895504A CN 107738725 B CN107738725 B CN 107738725B
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- China
- Prior art keywords
- air bag
- sail body
- supercavity
- ring
- column part
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B1/00—Hydrodynamic or hydrostatic features of hulls or of hydrofoils
- B63B1/32—Other means for varying the inherent hydrodynamic characteristics of hulls
- B63B1/34—Other means for varying the inherent hydrodynamic characteristics of hulls by reducing surface friction
- B63B1/38—Other means for varying the inherent hydrodynamic characteristics of hulls by reducing surface friction using air bubbles or air layers gas filled volumes
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
- B63G8/00—Underwater vessels, e.g. submarines; Equipment specially adapted therefor
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B1/00—Hydrodynamic or hydrostatic features of hulls or of hydrofoils
- B63B1/32—Other means for varying the inherent hydrodynamic characteristics of hulls
- B63B1/34—Other means for varying the inherent hydrodynamic characteristics of hulls by reducing surface friction
- B63B1/38—Other means for varying the inherent hydrodynamic characteristics of hulls by reducing surface friction using air bubbles or air layers gas filled volumes
- B63B2001/382—Other means for varying the inherent hydrodynamic characteristics of hulls by reducing surface friction using air bubbles or air layers gas filled volumes by making use of supercavitation, e.g. for underwater vehicles
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T70/00—Maritime or waterways transport
- Y02T70/10—Measures concerning design or construction of watercraft hulls
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Ocean & Marine Engineering (AREA)
- Measurement Of Velocity Or Position Using Acoustic Or Ultrasonic Waves (AREA)
Abstract
The present invention provides a kind of supercavity submarine navigation devices, including sail body and ring-shaped skirt;The sail body includes leading portion tapered segment and column part;Leading portion tapered segment surface is equipped with several annular grooves, the trailing exterior surface of the sail body column part installs ring-shaped skirt, the air bag of several mutually disconnected annulars is equipped with inside the ring-shaped skirt, the tail portion of the sail body column part of the inside air bag is externally provided with air vent, for being connected to the air bag and the sail body internal cavities;When the air bag unaerated, the ring-shaped skirt does not protrude sail body column part outer surface.The present invention can be designed by improving the structure of sail body, effectively realized the supercavity that steady steaming body leading portion is formed, reduced running resistance, the noise reduction of sail body, improve the underwater sailing body speed of a ship or plane.
Description
Technical field
The present invention relates to submarine navigation device field, in particular to a kind of supercavity submarine navigation device.
Background technique
Submarine navigation device is a kind of navigation in underwater sail body, and it is even military can to complete underwater exploration, detecting
On attack defence etc. tasks.Ocean development becomes more and more important current, and submarine navigation device is further by the attention of every country, nothing
By being occupied an important position civilian or on military.The speed of a ship or plane of underwater sailing body is lower always for a long time, and reason is boat
Row resistance is big;If improving the speed of a ship or plane, sail body surface local pressure is down to the saturated vapour pressure of water, cavitation phenomenon occurs, brings vibration
It dynamic, noise and the adverse consequences such as degrades, causes unpredicted economic loss.Cavitation phenomenon is on human lives and engineer application
A kind of recurrent physical phenomenon, can be divided into according to object and cavitation condition when liquid relative motion: non-cavitation condition is faced
Boundary's cavitation condition, local cavitation state and supercavitation state.But cavitation phenomenon has its available aspect, such as Russia again
Researcher studies for a long period of time, and discovery can reduce the resistance of underwater sailing body using supercavity, and underwater sailing body is included in substantially
In huge vacuole, so that nearby liquid medium becomes gas on sail body surface, since air drag is much smaller than liquid resistance, thus
Sail body stroke resistance is reduced, and avoids cavitation bring adverse effect.On sail body head, installation has expansion now
The cavitation device of acute angle shape is opened, the cavity of package sail body is formed, is more common artificial ventilation's supercavity generation method, is held
It is easily generated to stablize smooth vacuole surface.
Patent publication No. is that the patent of invention of 104590481 A of CN discloses " combined type cavitation device ", in the patent of invention
In, inventor provides a kind of combined type cavitation device comprising and conical sections and frustum-conical portion, leading portion are conical sections,
Back segment is that the structure of frustum-conical portion designs.Patent publication No. is that the patent of invention of 105352704 A of CN discloses that " one kind can
Become the circular cone cavitation device of cone angle ", in the patent of invention, inventor provides the head that cavitation device is mounted on sail body, including one
The construction design method of fixed disc and multiple sliding discs.But they only provide the design method of cavitation device, there is no just
The stabilization of vacuole optimizes.
Summary of the invention
In response to the deficiencies in the existing technology, the present invention provides a kind of supercavity submarine navigation devices, are navigated by water by improving
The structure of body designs, and effectively realizes the supercavity that steady steaming body leading portion is formed, reduces running resistance, the noise reduction of sail body, mention
The high underwater sailing body speed of a ship or plane.
The present invention achieves the above technical objects by the following technical means.
A kind of supercavity submarine navigation device, including sail body and ring-shaped skirt;The sail body includes leading portion tapered segment
And column part;Leading portion tapered segment surface is equipped with several annular grooves, the tail portion appearance of the sail body column part
Ring-shaped skirt is installed in face, and the air bag of several mutually disconnected annulars, the boat of the inside air bag are equipped with inside the ring-shaped skirt
The tail portion of row body column part is externally provided with air vent, for being connected to the air bag and the sail body internal cavities;When the gas
When capsule unaerated, the ring-shaped skirt does not protrude sail body column part outer surface.
Further, the annular groove is equally spaced on leading portion tapered segment, and the annular groove quantity is 3-4.
Further, the ring-shaped skirt outer diameter is identical as sail body column part outer diameter.
Further, the air bag is the elastic material of fold, and when the air bag unaerated, several air bags are weighed mutually
It is folded.
Further, the air bag is no less than 3.
Further, the air vent is uniformly distributed along sail body column part axis,
Further, the quantity of the air vent is no less than 8 in any air bag.
The beneficial effects of the present invention are:
1. supercavity submarine navigation device of the present invention is equipped with annular groove, annular by leading portion tapered segment surface
The effect of groove be store gas under normal pressure, into it is underwater when, stored by air facilitate sky caused by cavitation device
Bubble is further grown up, so that covering entire sail body.
2. supercavity submarine navigation device of the present invention, ring-shaped skirt is equipped with by tail portion, in ring-shaped skirt inner cavity
Be provided with air vent, air vent is through sail body surface connection navigation intracoelomic cavity, when supercavity occurs after entering under water, gas supply
Gas in inner cavity is filled in the air bag of ring-shaped skirt by hole because pressure acts on, so that air bag expands, effectively prevent supercavity tail
Portion is involved in plume, improves the stability of supercavity.
Detailed description of the invention
Fig. 1 is supercavity submarine navigation device structural schematic diagram of the present invention.
Fig. 2 is the ring-shaped skirt Local map of supercavity submarine navigation device of the present invention.
Fig. 3 is sectional view when ring-shaped skirt of the present invention expands.
In figure:
1- sail body;2- circular cone cavitation device;3- ring-shaped skirt;4- annular groove;5- air vent.
Specific embodiment
Present invention will be further explained with reference to the attached drawings and specific examples, but protection scope of the present invention is simultaneously
It is without being limited thereto.
As depicted in figs. 1 and 2, supercavity submarine navigation device of the present invention, including sail body 1 and ring-shaped skirt 3;?
Cross section is the top of circular elongated sail body 1, is bolted and is equipped with conical cavitation device, the sail body 1 includes
Leading portion tapered segment and column part;Leading portion tapered segment surface is equipped with several annular grooves 4,1 cylinder of sail body
Partial trailing exterior surface installs ring-shaped skirt 3, and the air bag of several mutually disconnected annulars is equipped with inside the ring-shaped skirt 3,
The tail portion of 1 column part of sail body of the inside air bag is externally provided with air vent 5, for being connected to the air bag and the sail body
1 internal cavities;When the air bag unaerated, the ring-shaped skirt 3 does not protrude 1 column part outer surface of sail body.By preceding
Section tapered segment surface is equipped with annular groove 4, and the effect of annular groove 4 is to store gas under normal pressure, into it is underwater when, institute
The air of storage facilitates vacuole caused by cavitation device and further grows up, so that covering entire sail body.The annular is recessed
Slot 4 is equally spaced on leading portion tapered segment, and 4 quantity of annular groove is 3-4.
Ring-shaped skirt is installed by tail portion, be provided with air vent in ring-shaped skirt inner cavity, air vent is through navigation body surface
Face connection navigation intracoelomic cavity, when supercavity occurs after entering under water, gas in inner cavity is filled with by air vent because pressure acts on
In the air bag of ring-shaped skirt, so that air bag expands, it effectively prevent supercavity tail portion to be involved in plume, improves the stabilization of supercavity
Property.3 outer diameter of ring-shaped skirt is identical as 1 column part outer diameter of sail body, for reducing resistance.The air bag is the bullet of fold
Property material, when the air bag unaerated, several air bags overlap each other.The air bag is no less than 3.5 edge of air vent
1 column part axis of sail body is uniformly distributed, and the quantity of the air vent 5 is no less than 8 in any air bag, easily and fast will be described
The gas of 1 internal cavities of sail body enters air bag by pressure difference.
The present invention increases expandable ring-shaped skirt 3, supercavity submarine navigation device fortune by the structure of improvement aircraft
It is higher-pressure region before ring-shaped skirt 3 when row, rear portion is low-pressure area, and gas is avoided to be inhaled into plume, stablizes vacuole and is wrapped up
Sail body range navigated by water in supercavity so that underwater navigation physical efficiency is stable, effectively realize reduce sail body operation resistance
Power reaches noise reduction effect, improves the underwater sailing body speed of a ship or plane.
The embodiment is a preferred embodiment of the present invention, but present invention is not limited to the embodiments described above, not
In the case where substantive content of the invention, any conspicuous improvement that those skilled in the art can make, replacement
Or modification all belongs to the scope of protection of the present invention.
Claims (6)
1. a kind of supercavity submarine navigation device, which is characterized in that including sail body (1) and ring-shaped skirt (3);The sail body
It (1) include leading portion tapered segment and column part;Leading portion tapered segment surface is equipped with several annular grooves (4), the boat
The trailing exterior surface of row body (1) column part installs ring-shaped skirt (3), does not connect mutually inside the ring-shaped skirt (3) equipped with several
The air bag of logical annular, the tail portion of sail body (1) column part of the inside air bag is externally provided with air vent (5), for being connected to
The air bag and the sail body (1) internal cavities;When the air bag unaerated, the not prominent navigation of the ring-shaped skirt (3)
Body (1) column part outer surface;The air bag is the elastic material of fold, and when the air bag unaerated, several air bags are mutual
It overlaps.
2. supercavity submarine navigation device according to claim 1, which is characterized in that the annular groove (4) is in leading portion circle
It is equally spaced on wimble fraction, annular groove (4) quantity is 3-4.
3. supercavity submarine navigation device according to claim 1, which is characterized in that ring-shaped skirt (3) outer diameter and boat
Row body (1) column part outer diameter is identical.
4. supercavity submarine navigation device according to claim 1, which is characterized in that the air bag is no less than 3.
5. supercavity submarine navigation device according to claim 1, which is characterized in that the air vent (5) is along sail body (1)
Column part axis is uniformly distributed.
6. supercavity submarine navigation device according to claim 5, which is characterized in that the air vent (5) in any air bag
Quantity be no less than 8.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201710895504.8A CN107738725B (en) | 2017-09-28 | 2017-09-28 | A kind of supercavity submarine navigation device |
Applications Claiming Priority (1)
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CN201710895504.8A CN107738725B (en) | 2017-09-28 | 2017-09-28 | A kind of supercavity submarine navigation device |
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CN107738725A CN107738725A (en) | 2018-02-27 |
CN107738725B true CN107738725B (en) | 2019-05-31 |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111332438A (en) * | 2020-04-04 | 2020-06-26 | 西北工业大学 | Active load reduction structure of aircraft |
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CN110274750B (en) * | 2019-07-25 | 2020-10-30 | 哈尔滨工业大学 | Supercavitation navigation body test model with elastic tail edge |
CN111301604B (en) * | 2020-04-07 | 2022-03-15 | 西北工业大学 | Underwater cavitation load reduction rod structure for underwater vehicle throwing |
CN111806174B (en) * | 2020-06-10 | 2022-05-17 | 中山大学 | Aircraft structure capable of repeatedly entering and exiting water |
CN111959674B (en) * | 2020-07-03 | 2022-03-11 | 西北工业大学 | Strong mobility supercavitation navigation device based on straight rudder preposed hydrodynamic layout |
CN112918614B (en) * | 2021-01-22 | 2022-03-29 | 中国人民解放军国防科技大学 | Supercavitation navigation body and cavitation bubble flow control method adopting wake flow injection |
CN113879448A (en) * | 2021-09-29 | 2022-01-04 | 哈尔滨工业大学 | Tail ring stable high-speed water-entering navigation body |
CN114813035B (en) * | 2022-04-12 | 2023-03-21 | 厦门大学 | Thermal surface cavitation synergistic resistance reduction test device and method |
CN116534182A (en) * | 2023-03-31 | 2023-08-04 | 中国船舶集团有限公司第七一九研究所 | Miniature underwater thermodynamic navigation body micro-bubble drag-reducing noise-reducing device |
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CN105314063A (en) * | 2014-08-01 | 2016-02-10 | 郭宏斌 | A resistance-reducing technology mainly based on gas cushion resistance reduction |
CN105352704A (en) * | 2015-11-19 | 2016-02-24 | 中国运载火箭技术研究院 | Conical cavitator with changeable cone angle |
CN105620652A (en) * | 2016-03-01 | 2016-06-01 | 哈尔滨工程大学 | Maneuvering control and gas leakage inhibition type retractable cavitator and multi-stage retractable cavitator |
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CN203732238U (en) * | 2014-03-25 | 2014-07-23 | 哈尔滨工业大学 | Ventilation device for underwater supercavitation navigation body scaled model test |
CN103926051A (en) * | 2014-05-06 | 2014-07-16 | 中国船舶重工集团公司第七○二研究所 | Supercavitating navigation body model with internal steering gear |
CN105314063A (en) * | 2014-08-01 | 2016-02-10 | 郭宏斌 | A resistance-reducing technology mainly based on gas cushion resistance reduction |
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CN111332438A (en) * | 2020-04-04 | 2020-06-26 | 西北工业大学 | Active load reduction structure of aircraft |
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