CN101819011A - Torpedo - Google Patents
Torpedo Download PDFInfo
- Publication number
- CN101819011A CN101819011A CN200910133000A CN200910133000A CN101819011A CN 101819011 A CN101819011 A CN 101819011A CN 200910133000 A CN200910133000 A CN 200910133000A CN 200910133000 A CN200910133000 A CN 200910133000A CN 101819011 A CN101819011 A CN 101819011A
- Authority
- CN
- China
- Prior art keywords
- torpedo
- rotor
- axial line
- hollow sleeve
- shell
- 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 relates to a torpedo. 8 to 12 round holes 3 are formed in a shell of the torpedo around a torpedo axis OO' on the same circumference at the conical end of the torpedo; the axes of the round holes are crossed with the torpedo axis OO' at the same point, and the included angles between the axes of the round holes and the torpedo axis OO' are equal; all the round holes are crossed at the torpedo axis OO' and form a conical hole; a rotor 15 of a hollow-sleeve type rotor asynchronous motor is arranged on the tail part of the torpedo; a waterpower propulsion worm wheel 10 is coaxial with the hollow sleeve of the rotor 15 and is fixedly arranged at the tail end of the hollow sleeve of the rotor 15; a mouse cage is embedded into the other end of the rotor 15; the conical hole formed by the intersection of all the round holes 3 is communicated with the hollow sleeve of the rotor 15; the rotor 15 is arranged in a motor base 14 of the asynchronous motor and is positioned by a motor rotor positioning ring 9; a stator coil 12 is embedded in the motor base of the asynchronous motor; and the motor base 14 and the torpedo shell form a whole.
Description
Technical field
The present invention relates to torpedo technique.
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 torpedo.
The present invention is a kind of torpedo, comprise a battery area 4, appliance controller 5, afterbody has four balance wing 6, two vertical direction wings 7, two horizontal direction wings 8, its 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 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 15 of the asynchronous motor of one hollow shell type rotor is installed at the torpedo afterbody, the axis of the hollow sleeve of rotor 15 is coaxial with torpedo axial line OO ', waterpower ahead turbine 10 is coaxial and be fixedly mounted on the tail end of the hollow sleeve of rotor 15 with the hollow sleeve of rotor 15, the other end of rotor 15 embeds mouse cage 13, all circular holes 3 taper hole that forms that crosses communicates with the hollow sleeve of rotor 15, in the support 14 of rotor 15 installations and asynchronous motor, by rotor locating ring 9 location, embedding in the support 14 has stator coil 12, and support 14 is an integral body with torpedo shell.
Usefulness of the present invention is: torpedo is owing to self exist propulsion capability, translational speed, the direction of motion can be regulated automatically, after the formula torpedo emission of can making a return voyage, lose target, under the control of the computer of the appliance controller of the formula torpedo that can make a return voyage and transmitting station, can make the formula torpedo that to make a return voyage change direction, cancel strike order, the recovery of making a return voyage.
Description of drawings
Fig. 1 is the appearance assumption diagram of torpedo of the present invention, and Fig. 2 is that K is to view among Fig. 1, and Fig. 3 is that P-P among Fig. 1 is to partial sectional view.
The specific embodiment
As shown in Figure 1, the present invention is a kind of torpedo, and the torpedo axial line is OO '.As shown in Figure 2,4 is battery area, 5 is appliance controller, the torpedo afterbody has four balance wing 6, two vertical direction wings 7, two horizontal direction wings 8, 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 3,2 is bullet, target detector and fuse 1 are installed in the tapered end of torpedo, 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 3 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 15 of the asynchronous motor of one hollow shell type rotor is installed at the torpedo afterbody, the axis of the hollow sleeve of rotor 15 is coaxial with torpedo axial line OO ', waterpower ahead turbine 10 is coaxial and be fixedly mounted on the tail end of the hollow sleeve of rotor 15 with the hollow sleeve of rotor 15, the other end of rotor 15 embeds mouse cage 13, all circular holes 3 taper hole that forms that crosses communicates with the hollow sleeve of rotor 15, in the support 14 of rotor 15 installations and asynchronous motor, by rotor locating ring 9 location, there is sealing ring 11 sealing at the position that contacts, embedding in the support 14 has stator coil 12, and support 14 is an integral body with torpedo shell.
Torpedo of the present invention is controlled the rotating speed of asynchronous motor by the feedback signal of target detector under the control of appliance controller 5, regulates thrust power, and the translational speed of torpedo is regulated; Realize target following by the deflection angle of adjusting two horizontal direction wings 8, two vertical direction wings 7.The battery that the electric energy of electrical system and motor is adorned by battery area 4 provides.
As shown in Figure 3, torpedo of the present invention is under the control of appliance controller 5, feedback signal by target detector 1 is controlled the rotating speed of asynchronous motor, regulate the rotating speed of waterpower ahead turbine 10, by waterpower ahead turbine 10 water in the circular hole 3 is discharged by the afterbody of torpedo, produce thrust power forward, appliance controller 5 is discerned by target direction simultaneously, the pivot angle of two horizontal direction wings 7 of control, direction of rotation to the formula torpedo that can make a return voyage is regulated, the pivot angle of two vertical direction wings 8 of control is to fly-height adjustments in the water of the formula torpedo that can make a return voyage.When flying in water, torpedo flies by four balance wing 6 held stationaries that differ 90 °.
Claims (1)
1. torpedo, comprise a battery area (4), appliance controller (5), afterbody has four balance wing (6), two vertical direction wings (7), two horizontal direction wings (8), 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 (3) are intersected in torpedo axial line (OO ') and form a taper hole, the rotor (15) of the asynchronous motor of one hollow shell type rotor is installed at the torpedo afterbody, the axis of the hollow sleeve of rotor (15) is coaxial with torpedo axial line (OO '), waterpower ahead turbine (10) is coaxial and be fixedly mounted on the tail end of the hollow sleeve of rotor (15) with the hollow sleeve of rotor (15), the other end of rotor (15) embeds mouse cage (13), all circular holes taper hole that forms that crosses communicates with the hollow sleeve of rotor (15), in the support (14) of rotor (15) installation and asynchronous motor, locate by rotor locating ring (9), embedding in the support (14) has stator coil (12), and support (14) is an integral body with torpedo shell.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN200910133000A CN101819011A (en) | 2009-03-30 | 2009-03-30 | Torpedo |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN200910133000A CN101819011A (en) | 2009-03-30 | 2009-03-30 | Torpedo |
Publications (1)
Publication Number | Publication Date |
---|---|
CN101819011A true CN101819011A (en) | 2010-09-01 |
Family
ID=42654198
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN200910133000A Pending CN101819011A (en) | 2009-03-30 | 2009-03-30 | Torpedo |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN101819011A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106595407A (en) * | 2016-11-25 | 2017-04-26 | 中国船舶重工集团公司第七0研究所 | Trajectory control system for movably laying anchored mines of remote self-propelled mine |
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 |
-
2009
- 2009-03-30 CN CN200910133000A patent/CN101819011A/en active Pending
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106595407A (en) * | 2016-11-25 | 2017-04-26 | 中国船舶重工集团公司第七0研究所 | Trajectory control system for movably laying anchored mines of remote self-propelled mine |
CN106595407B (en) * | 2016-11-25 | 2019-04-26 | 中国船舶重工集团公司第七一0研究所 | A kind of long-range self-propelled mine movement lays the trajectory control system of mooring mine |
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 | |
US9994314B2 (en) | Methods and systems for transitioning an aerial vehicle between hover flight and crosswind flight | |
US20150180186A1 (en) | Systems and Apparatus for Cable Management | |
KR101737751B1 (en) | Path based power generation control for an aerial vehicle | |
US9531246B2 (en) | Bi-rotational generator | |
EP3004632B1 (en) | Submersible power plant having multiple turbines | |
EP3046835B1 (en) | Methods and systems for transitioning an aerial vehicle between hover flight and crosswind flight | |
IL198968A (en) | Spin stabilized projectile trajectory control device | |
WO2016003713A1 (en) | Drive mechanisms for use in controlling rotation and twist of a tether | |
WO2013056275A4 (en) | Aircraft | |
US20150330367A1 (en) | Drive Mechanism Utilizing a Tubular Shaft and Fixed Central Shaft | |
JP6550503B2 (en) | Wind power motor for vehicles | |
US9878775B2 (en) | Dual-pitch support for a propeller | |
CN205940308U (en) | A prefabricated angle of attack device for high -speed penetration test of body | |
CN101819011A (en) | Torpedo | |
US20190154003A1 (en) | Multi-Tether Clock-Face De-Twist | |
CN101819010A (en) | Water spray type torpedo | |
EP3622172B1 (en) | A wind installation comprising a wind turbine and an airborne wind energy system | |
CN204623811U (en) | A kind of novel submerge device maneuvering system | |
CN112696989A (en) | Ballistic trajectory correcting device based on relay control | |
CN201049212Y (en) | Ornithopter electromagnetic steering device | |
CN210862401U (en) | Ballistic trajectory correction device based on relay control | |
CN110174653A (en) | A kind of millimeter wave test table that portable revolving speed is remote-controlled | |
CN110104148A (en) | A kind of propulsion regulating device of unmanned bathyscaphe | |
RU2725331C1 (en) | Correcting fuse for rotating projectile and method of application thereof |
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 |