CN102636085A - Aerial mine - Google Patents
Aerial mine Download PDFInfo
- Publication number
- CN102636085A CN102636085A CN2011100354002A CN201110035400A CN102636085A CN 102636085 A CN102636085 A CN 102636085A CN 2011100354002 A CN2011100354002 A CN 2011100354002A CN 201110035400 A CN201110035400 A CN 201110035400A CN 102636085 A CN102636085 A CN 102636085A
- Authority
- CN
- China
- Prior art keywords
- aluminum
- aerial
- foil
- mine
- balloon
- 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
Abstract
The invention belongs to an aerial mine. The aerial mine adopts a solar film battery as a balloon, a horizontal propeller is arranged below the balloon, an aluminum-foil device is arranged below the propeller, and a longitudinal propeller is arranged in front of the aluminum-foil device, and a tailfin is arranged at the rear part of the aluminum-foil device; and a motor, explosive, a storage battery, and a remote controller are arranged in the aluminum-foil device. An aluminum-foil shell is coated as red and equipped with a plurality of infrared light-emitting tubes. The aluminum-foil can disturb radar, and the infrared light-emitting tube can disturb an infrared guided missile. The device can be manufactured as aerial mines of different sizes and shapes and can be used as an aircraft for various purposes, such as a scout. The device is low in cost and easy for manufacturing, thousands of aerial mines are densely distributed in the sky, and wander in day and night for a long time. The explosive in the aerial mine can intercept the missile and blow up an airplane when the airplane collides the aerial mine. The aerial mine is the best weapon for the defense of bridges, dams and important positions, and is the best method for dealing with the attack of missiles and airplanes. The missile defense system of the United States is too small in control range and too high in construction cost.
Description
Technical field: the present invention relates to a kind of empty thunder.
Background technology: in the military affairs at present land mine is arranged, submarine mine does not have the sky thunder exactly.
Summary of the invention: study a kind of empty thunder, anti-radar is surveyed, the attack of guided missile, aircraft, and defendance territorial sky and critical facility are inviolable.
Technical scheme: make a balloon with solar film battery, a screw is installed below the balloon, the thin device of an aluminium is installed below the screw.
A small propeller is installed in the front of the thin device of aluminium, and an empennage is installed in the back.Miniature motor, explosive, battery, remote control are installed in aluminium foil device the inside.Miniature motor connects two screws, aluminium foil crust of the device coating Red, and a plurality of infrared light emission pipes are installed on shell.
Description of drawings: figure is empty thunder profile.
Among the figure, 1-solar film battery balloon; The 2-transverse propeller; The 3-miniature motor; The 4-explosive; The 5-battery; The 6-remote control; 7-longitudinal spiral oar; 8-aluminium foil shell; The 9-empennage; 10-infrared light emission pipe.
The practical implementation method: make a balloon 1. with solar film battery, balloon is full of hydrogen or nitrogen in 1..Transverse propeller of balloon following installation 1. 2.; Aluminium foil canning of screw following installation 2. 8.; A small-sized longitudinal spiral oar is installed in aluminium foil device front 8. 7.; Empennage is installed in the back 9., aluminium foil device the inside 8. install miniature motor 3., explosive 4., battery 5., remote control 6., 2., 7. 3. miniature motor connect two screws.Aluminum hull outside coating Red 8., and shell 8. above several infrared light emission pipes of installation 10..
Thin-film solar cells has been invented by foreign country, just handy it make a balloon 1., 1. balloon on the one hand be empty thunder generation lift, solar cell is that 3. miniature motor provides power supply on the other hand.3. miniature motor drives two screws and 2., 7. rotates, for empty thunder provides auxiliary lifting.Battery 5. with electrical power storage that daytime, solar cell produced battery 5. in, the power supply in evening.So empty thunder just can aloft be gone around round the clock for a long time.6. remote control stretches out antenna, and antenna and ground command center's contact are controlled it and aloft located, and fly, rise and fall.Aluminium foil shell metal 8. disturbs radar detection.Shell is coating Red 8., and redness can absorb the infrared ray in the sunshine.In addition, 10. 8. shell install the infrared light emission pipe, and 10. the infrared light emission pipe is tack, the light scattering, and it is used to disturb the infrared guidance guided missile, when explosive effect 4. is interception guided missile and aircraft collision it is demolished.
The thin device volume of aluminium is little, in light weight, and 1. balloon goes up to the air with the enough empty thunder of electric energy that solar cell produces.It is big just big that empty thunder is wanted, and little just little, can make different shape, and various uses can also be made other forms of flight apparatus, like EP-3 electronic reconnaissance plane EP-3.His cost is low, makes easily, is covered with up to ten thousand empty thunders in can be on high, and bridge, dam and significant points are deployed troops on garrison duty.It is to guided missile, aircraft attack defending best bet, and this wolf pack (ten thousand empty thunders) way is more effective than the guided missile defence system of the U.S., and the guided missile defence system cost of the U.S. is too high.
Claims (2)
1. empty thunder is characterized in that: make a balloon with solar film battery, a screw is installed below the balloon, an aluminium foil device is installed below the screw.
2. empty thunder according to claim 1 is characterized in that: a small propeller is installed in the front of aluminium foil device, and an empennage is installed in the back.Miniature motor, explosive, battery, remote control are installed in aluminium foil device the inside.Miniature motor connects two screws, aluminium foil crust of the device coating Red, and a plurality of infrared light emission pipes are installed on shell.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011100354002A CN102636085A (en) | 2011-02-10 | 2011-02-10 | Aerial mine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011100354002A CN102636085A (en) | 2011-02-10 | 2011-02-10 | Aerial mine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102636085A true CN102636085A (en) | 2012-08-15 |
Family
ID=46620576
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011100354002A Pending CN102636085A (en) | 2011-02-10 | 2011-02-10 | Aerial mine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102636085A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104571125A (en) * | 2014-12-18 | 2015-04-29 | 北京控制工程研究所 | Control method for utilizing standard trajectory to deal with multiple return conditions |
| CN105311839A (en) * | 2014-06-25 | 2016-02-10 | 上海本星电子科技有限公司 | Balloon aerial height positioner |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1305920A (en) * | 1999-07-04 | 2001-08-01 | 秦兆山 | Air defence mine |
| US6324982B1 (en) * | 1997-11-17 | 2001-12-04 | Commissariat A L'energie Atomique | Process for artificially triggering an avalanche and device for applying this process |
| CN1521084A (en) * | 2003-02-15 | 2004-08-18 | 刘春桥 | Composite airship |
-
2011
- 2011-02-10 CN CN2011100354002A patent/CN102636085A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6324982B1 (en) * | 1997-11-17 | 2001-12-04 | Commissariat A L'energie Atomique | Process for artificially triggering an avalanche and device for applying this process |
| CN1305920A (en) * | 1999-07-04 | 2001-08-01 | 秦兆山 | Air defence mine |
| CN1521084A (en) * | 2003-02-15 | 2004-08-18 | 刘春桥 | Composite airship |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105311839A (en) * | 2014-06-25 | 2016-02-10 | 上海本星电子科技有限公司 | Balloon aerial height positioner |
| CN104571125A (en) * | 2014-12-18 | 2015-04-29 | 北京控制工程研究所 | Control method for utilizing standard trajectory to deal with multiple return conditions |
| CN104571125B (en) * | 2014-12-18 | 2016-01-27 | 北京控制工程研究所 | A kind ofly utilize the multiple control method returning condition of normal trajectory reply |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US8448894B2 (en) | Method and apparatus for a mobile aerial sustained solar power-plant | |
| WO2014013270A1 (en) | Method of flying an unmanned aerial vehicle | |
| CN108482635B (en) | Inflator wing type aircraft capable of being parked | |
| CN102166931A (en) | New energy multifunctional airplane | |
| CN103043214A (en) | Folding type unmanned plane | |
| CN200967562Y (en) | High subsonic speed unmanned plane | |
| CN103832591A (en) | Multifunctional new energy airplane | |
| CN102520727A (en) | Reconnaissance system with unmanned plane | |
| CN103693197A (en) | Submarine-launched unmanned aerial vehicle | |
| CN103968714A (en) | Defending bomb device hung in air | |
| CN102636085A (en) | Aerial mine | |
| CN202453736U (en) | Unmanned aerial vehicle reconnaissance system | |
| CN205352204U (en) | A intercepting device for aircraft interception | |
| CN204514195U (en) | A kind of high-performance cruise formula target missile | |
| CN105620751A (en) | Saucer type vertical lifting type flight device | |
| WO2017030470A1 (en) | Cruise missile-armed ground effect vehicle | |
| CN102147217A (en) | Solar-cell umbrella type aerial detonator | |
| CN209521849U (en) | A kind of airship formula unmanned plane | |
| CN102589368A (en) | Space mine | |
| CN101975529A (en) | High-altitude rocket launching system | |
| CN112849412A (en) | Hydrogen-electricity nacelle body integrated scouting and batting unmanned aerial vehicle | |
| CN204626320U (en) | The fog-dissipation device that portable field controls | |
| CN107008017B (en) | A kind of dedicated multifunction detecting dummy vehicle of teenager's defence education | |
| RU2769455C1 (en) | Aerial target simulator | |
| Darcy | Russian-English aerospace dictionary |
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: 20120815 |