CN101819010A - Water spray type torpedo - Google Patents
Water spray type torpedo Download PDFInfo
- Publication number
- CN101819010A CN101819010A CN200910132999A CN200910132999A CN101819010A CN 101819010 A CN101819010 A CN 101819010A CN 200910132999 A CN200910132999 A CN 200910132999A CN 200910132999 A CN200910132999 A CN 200910132999A CN 101819010 A CN101819010 A CN 101819010A
- Authority
- CN
- China
- Prior art keywords
- torpedo
- rotor
- hollow sleeve
- axial line
- afterbody
- 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
Links
Images
Landscapes
- Hydraulic Turbines (AREA)
Abstract
The invention discloses a water spray type torpedo. 8 to 12 circular holes 3 are formed in a torpedo shell around a torpedo shaft axis OO' on the same circumference of the tapered end part of the torpedo, the shaft axes of the circular holes 3 are crossed on the same point on the torpedo shaft axis OO', all the circular holes 3 are crossed on the torpedo shaft axis OO' and form a tapered hole, the tail part of the torpedo is provided with a rotor 16 of an asynchronous motor of a hollow sleeve type rotor, the axis of a hollow sleeve of the rotor 16 is coaxial with the torpedo shaft axis OO', a hydraulic propulsion turbine 11 is coaxial with the hollow sleeve of the rotor 16 and is fixedly arranged on the tail part of the hollow sleeve of the rotor 16, the tapered hole formed by the crossing of all the circular holes is communicated with the hollow sleeve of the rotor 16, a stator coil 13 is embedded into a frame 15, a tail water spray pipe 8 is arranged at the tail end of the hollow sleeve of the rotor 16, and the tail water spray pipe 8 is coaxial with the torpedo shaft axis OO'; and four direction control water spray pipes 9 are distributed at interval of 90 degrees on the same circumference vertical to the torpedo shaft axis OO', and each direction control water spray pipe is connected with the hollow sleeve of the rotor 16 through a square controlled electromagnetic water valve 10.
Description
Technical field
The present invention relates to the torpedo Push Technology.
Background technology
Torpedo is sent by transmitter in the prior art, advances by inertia, and the ability of not making a return voyage loses when striking target, and can't recall.
Summary of the invention
The purpose of this invention is to provide a kind of water jet torpedo.
The present invention is a kind of water jet torpedo, comprise a battery area 4, appliance controller 5, afterbody has four balance wing 6, target detector and fuse 1 are installed in the tapered end of torpedo, on the same circumference of the tapered end of torpedo, in torpedo shell, have 8~12 circular holes 3 around torpedo axial line OO ', the axial line of each circular hole 3 intersects at torpedo axial line OO ' and goes up on the same point, and the axial line of each circular hole equates with the angle of torpedo axial line OO ', all circular holes are intersected in torpedo axial line OO ' and form a taper hole, the rotor 16 of the asynchronous motor of one hollow shell type rotor is installed at the torpedo afterbody, the axis of the hollow sleeve of rotor 16 is coaxial with torpedo axial line OO ', waterpower ahead turbine 11 is coaxial and be fixedly mounted on the afterbody of the hollow sleeve of rotor 16 with the hollow sleeve of rotor 16, the other end of rotor 16 embeds mouse cage 14, all circular holes 3 taper hole that forms that crosses communicates with the hollow sleeve of rotor 16, in the support 15 of rotor 16 installations and asynchronous motor, embed in the support 15 stator coil 13 is arranged, support 15 is an integral body with torpedo shell, afterbody sparge pipe 8 is installed in the tail end of the hollow sleeve of rotor 16, and afterbody sparge pipe 8 is coaxial with torpedo axial line OO ', the direction control sparge pipe 9 of four 90 ° of distributions of being separated by on vertical with torpedo axial line OO ' same circumference is arranged, and the electromagnetism water valve 10 by a square of control is connected with the hollow sleeve of rotor 16 separately.
Water jet torpedo of the present invention is owing to self exist propulsion capability, translational speed, the direction of motion can be regulated automatically, lose target after torpedo emission, can make torpedo change direction under the control of the computer of appliance controller and transmitting station, cancel strike order, the recovery of making a return voyage.
Description of drawings
Fig. 1 is the appearance assumption diagram of water jet torpedo of the present invention, Fig. 2 be K among Fig. 1 to view, Fig. 3 be among Fig. 1 P-P to cutaway view.
The specific embodiment
As shown in Figure 1, be appearance assumption diagram of the present invention, as shown in Figure 1 and Figure 2, on the same circumference of the tapered end of torpedo, in torpedo shell, have 8~12 circular holes 3 around torpedo axial line OO '.As shown in Figure 3, the axial line of each circular hole 3 intersects at torpedo axial line OO ' and goes up on the same point, and the axial line of each circular hole equates with the angle of torpedo axial line OO ', all circular holes 3 are intersected in torpedo axial line OO ' and form a taper hole, and all circular holes taper hole that forms that crosses communicates with the hollow sleeve of rotor 16.
As shown in Figure 3, water jet torpedo of the present invention, comprise a battery area 4, appliance controller 5, afterbody has four balance wing 6, target detector and fuse 1 are installed in the tapered end of torpedo, the rotor 16 of the asynchronous motor of one hollow shell type rotor is installed at the torpedo afterbody, the axis of the hollow sleeve of rotor 16 is coaxial with torpedo axial line OO ', waterpower ahead turbine 11 is coaxial and be fixedly mounted on the afterbody of the hollow sleeve of rotor 16 with the hollow sleeve of rotor 16, the other end of rotor 16 embeds mouse cage 14, in the support 15 of rotor 16 installations and asynchronous motor, embed in the support 15 stator coil 13 is arranged, support 15 is an integral body with torpedo shell, and afterbody sparge pipe 8 is installed in the tail end of the hollow sleeve of rotor 16, and afterbody sparge pipe 8 is coaxial with torpedo axial line OO ', the direction control sparge pipe 9 of four 90 ° of distributions of being separated by on vertical with torpedo axial line OO ' same circumference is arranged, and the electromagnetism water valve 10 by a square of control is connected with the hollow sleeve of rotor 16 separately.
As shown in Figure 3, the course of work of water jet torpedo is: under the control of appliance controller 5, feedback signal by the target detector in target detector and the fuse 1 is controlled the rotating speed of asynchronous motor, regulate the rotating speed of waterpower ahead turbine 11, by waterpower ahead turbine 11 water in the circular hole 3 is discharged by the afterbody sparge pipe 8 of torpedo, produce thrust power forward, appliance controller 5 is discerned by target direction simultaneously, control the orderly switch of four electromagnetism water valves (9), make the direction control sparge pipe 9 that differs 90 ° on four circumference carry out the side direction water spray, produce the side direction active force, the change of flight direction.Provide the energy by the water spray navigation formula battery 4 that the torpedo fuselage adorned that can make a return voyage.The water spray navigation formula torpedo that can make a return voyage is flown by four balance wing 6 held stationaries when fly in water.
Claims (1)
1. water jet torpedo, comprise a battery area (4), appliance controller (5), afterbody has four balance wing (6), target detector and fuse (1) are installed in the tapered end of torpedo, it is characterized in that on the same circumference of the tapered end of torpedo, in torpedo shell, having 8~12 circular holes (3) around torpedo axial line (OO '), the axial line of each circular hole (3) intersects at torpedo axial line (OO ') and goes up on the same point, and the axial line of each circular hole equates with the angle of torpedo axial line (OO '), all circular holes are intersected in torpedo axial line (OO ') and form a taper hole, the rotor (16) of the asynchronous motor of one hollow shell type rotor is installed at the torpedo afterbody, the axis of the hollow sleeve of rotor (16) is coaxial with torpedo axial line (OO '), waterpower ahead turbine (11) is coaxial and be fixedly mounted on the afterbody of the hollow sleeve of rotor (16) with the hollow sleeve of rotor (16), the other end of rotor (16) embeds mouse cage (14), all circular holes (3) taper hole that forms that crosses communicates with the hollow sleeve of rotor (16), in the support (15) of rotor (16) installation and asynchronous motor, embed in the support (15) stator coil (13) is arranged, support (15) is an integral body with torpedo shell, afterbody sparge pipe (8) is installed in the tail end of the hollow sleeve of rotor (16), and afterbody sparge pipe (8) is coaxial with torpedo axial line (OO '), the direction control sparge pipe (9) of four 90 ° of distributions of being separated by on vertical with torpedo axial line (OO ') same circumference is arranged, and the electromagnetism water valve (10) by a square of control is connected with the hollow sleeve of rotor (16) separately.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN200910132999A CN101819010A (en) | 2009-03-30 | 2009-03-30 | Water spray type torpedo |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN200910132999A CN101819010A (en) | 2009-03-30 | 2009-03-30 | Water spray type torpedo |
Publications (1)
Publication Number | Publication Date |
---|---|
CN101819010A true CN101819010A (en) | 2010-09-01 |
Family
ID=42654197
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN200910132999A Pending CN101819010A (en) | 2009-03-30 | 2009-03-30 | Water spray type torpedo |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN101819010A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106952552A (en) * | 2017-03-15 | 2017-07-14 | 佛山市三水区希望火炬教育科技有限公司 | A kind of special wooden torpedo model of loading and unloading type of teenager's research in defense-related science and technology |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4056073A (en) * | 1974-07-25 | 1977-11-01 | Omnithruster Inc. | Boat thruster |
US4372239A (en) * | 1980-03-03 | 1983-02-08 | General Dynamics, Pomona Division | Undersea weapon with hydropulse system and periodical seawater admission |
CN1033535A (en) * | 1987-12-13 | 1989-06-28 | 李福琼 | Pump integrating electric motor with vane wheel |
CN1029255C (en) * | 1992-03-11 | 1995-07-05 | 付英杰 | Multipurpose asynchronous motor axial-flow pump |
JP2000009399A (en) * | 1998-06-22 | 2000-01-14 | Ishikawajima Harima Heavy Ind Co Ltd | Underwater cruiser |
US7148416B1 (en) * | 1995-08-31 | 2006-12-12 | The United States Of America As Represented By The Secretary Of The Navy | Undersea vehicle |
-
2009
- 2009-03-30 CN CN200910132999A patent/CN101819010A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4056073A (en) * | 1974-07-25 | 1977-11-01 | Omnithruster Inc. | Boat thruster |
US4372239A (en) * | 1980-03-03 | 1983-02-08 | General Dynamics, Pomona Division | Undersea weapon with hydropulse system and periodical seawater admission |
CN1033535A (en) * | 1987-12-13 | 1989-06-28 | 李福琼 | Pump integrating electric motor with vane wheel |
CN1029255C (en) * | 1992-03-11 | 1995-07-05 | 付英杰 | Multipurpose asynchronous motor axial-flow pump |
US7148416B1 (en) * | 1995-08-31 | 2006-12-12 | The United States Of America As Represented By The Secretary Of The Navy | Undersea vehicle |
JP2000009399A (en) * | 1998-06-22 | 2000-01-14 | Ishikawajima Harima Heavy Ind Co Ltd | Underwater cruiser |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106952552A (en) * | 2017-03-15 | 2017-07-14 | 佛山市三水区希望火炬教育科技有限公司 | A kind of special wooden torpedo model of loading and unloading type of teenager's research in defense-related science and technology |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
KR101907310B1 (en) | Fire fighter drone | |
EP3004632B1 (en) | Submersible power plant having multiple turbines | |
EP3046836B1 (en) | Methods and systems for transitioning an aerial vehicle between crosswind flight and hover flight | |
EP3327282B1 (en) | A pressure controlled wind turbine enhancement system | |
KR101737751B1 (en) | Path based power generation control for an aerial vehicle | |
EP2748064B1 (en) | A kite for a system for extracting energy from the wind | |
WO2008118159A3 (en) | Spin stabilizer projectile trajectory control | |
CN101602404A (en) | A kind of aircraft of new structure | |
JP2018114980A (en) | Glider for airborne wind energy production | |
AU2014318437B2 (en) | Methods and systems for transitioning an aerial vehicle between hover flight and crosswind flight | |
CN104747320A (en) | Rotary control solid attitude and orbit control engine | |
CN101819010A (en) | Water spray type torpedo | |
WO2001089650A3 (en) | Lightweight remotely controlled aircraft | |
CN101819011A (en) | Torpedo | |
CN102826220B (en) | Thrust device capable of balancing reactive torque | |
CN103818534A (en) | Direction adjusting device of underwater gliding device and control method thereof | |
CN116604985A (en) | Water-air cross-medium aircraft with foldable wings | |
CN204623811U (en) | A kind of novel submerge device maneuvering system | |
CN115783337A (en) | Active taper sleeve for aerial recovery of unmanned aerial vehicle | |
CN202295216U (en) | Drill type pressure relief accelerating device for torpedo | |
CN103587729A (en) | Double-drive juxtaposed winding device for closing up spatial fly net | |
CN112696989A (en) | Ballistic trajectory correcting device based on relay control | |
CN106516079A (en) | Assembly type aircraft based on micro electromechanical system | |
CN201917278U (en) | Missile booster | |
CN210862401U (en) | Ballistic trajectory correction device based on relay control |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20100901 |