CN101832740A - Airspace defense method and air floating mine thereof - Google Patents
Airspace defense method and air floating mine thereof Download PDFInfo
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- CN101832740A CN101832740A CN201010184121A CN201010184121A CN101832740A CN 101832740 A CN101832740 A CN 101832740A CN 201010184121 A CN201010184121 A CN 201010184121A CN 201010184121 A CN201010184121 A CN 201010184121A CN 101832740 A CN101832740 A CN 101832740A
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- balloon
- air
- bomb
- fitted
- solar cell
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- 238000000034 method Methods 0.000 title claims abstract description 17
- 230000007123 defense Effects 0.000 title abstract description 4
- 239000001257 hydrogen Substances 0.000 claims abstract description 43
- 229910052739 hydrogen Inorganic materials 0.000 claims abstract description 43
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims abstract description 42
- 229910052734 helium Inorganic materials 0.000 claims abstract description 14
- 239000001307 helium Substances 0.000 claims abstract description 14
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims abstract description 14
- 238000013022 venting Methods 0.000 claims description 19
- 238000003860 storage Methods 0.000 claims description 17
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 10
- 239000001301 oxygen Substances 0.000 claims description 10
- 229910052760 oxygen Inorganic materials 0.000 claims description 10
- 230000009545 invasion Effects 0.000 abstract description 5
- 230000000903 blocking effect Effects 0.000 abstract description 2
- 235000015842 Hesperis Nutrition 0.000 abstract 1
- 235000012633 Iberis amara Nutrition 0.000 abstract 1
- 238000004880 explosion Methods 0.000 abstract 1
- 230000002401 inhibitory effect Effects 0.000 abstract 1
- 230000008520 organization Effects 0.000 abstract 1
- 230000002269 spontaneous effect Effects 0.000 abstract 1
- 238000005457 optimization Methods 0.000 description 8
- 238000013461 design Methods 0.000 description 7
- 238000005516 engineering process Methods 0.000 description 2
- 230000035515 penetration Effects 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- 230000032683 aging Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 239000003792 electrolyte Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- 238000005286 illumination Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
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Abstract
The invention relates to an airspace defense method and an air floating mine thereof. In the method, a transparent hydrogen balloon or helium balloon matched with a high-energy miniature bomb is arranged in a fortified airspace. The bomb is matched with a self-destroying device of clock control or controller control for spontaneous explosion mine removal, and is matched with an identification friend or foe system to prevent bombing error. The air floating mine comprises the transparent hydrogen balloon or helium balloon matched with the high-energy miniature bomb, and the balloon is matched with a height maintaining system. The method has the advantages of low cost and easy defense organization, can effectively block or inhibit the air power of the enemy, and is particularly suitable for a side with weak air power for defending against the invasion of an enemy with strong air power. The floating mines can be set at high density in a large scale by rockets or missiles or planes, and continuously float in a certain airspace for attacking an air target of the enemy colliding or approaching the floating mines, thus achieving the purposes of forcibly blocking or inhibiting the air power of the enemy by low cost and safeguarding the mastery of the air.
Description
Technical field
The present invention relates to a kind of defense in the air technology, particularly relate to a kind of spatial domain defence method and the thunder that wafts in the air.
Background technology
Modern war is taken as the leading factor with control of the air, and relative weak tendency one side of air power is difficult to beat back or eliminates the other side air power, then can only be by blocking or generation that containment the other side air power averts a war or the triumph of winning the war.But in the face of surging air penetration, except powerful air power, existing all other weaponrys that can be used in blockade or containment air penetration all are difficult to prove effective.
World air force theoretician, Italian general Zhu Liaoduhei in advance just systematically discussed control of the air before 80 years, he points out: " grasp control of the air and represent a kind of situation, can stop the enemy to fly, can keep oneself flight simultaneously.Grasping control of the air wins exactly.Do not have control of the air, just be domed to failure, and accept the war victor and be ready any condition of forcing." so research and development can effective blockade or the spatial domain defend equipment of containment enemy air power, helps air power weak nation guard control of the air.
Summary of the invention
The object of the invention is to overcome the problems referred to above of prior art, provide a kind of can be with spatial domain defence method than low-cost effective blockade or containment enemy air power, the object of the invention also is to be provided for implementing the thunder that wafts of this method in the air.
For achieving the above object, spatial domain of the present invention defence method is transparent hydrogen balloon or a helium balloon of laying the equipped miniature bomb of high energy in the spatial domain of setting up defences.Transparent balloon is used for strengthening disguised.Hydrogen balloon or helium balloon are used to keep aerial floating.The miniature bomb of high energy is used to attack enemy's aerial target of bump or the approaching thunder that wafts, and the high energy microminiaturization of bomb simultaneously can significantly reduce the heavy burden of balloon.It can be deployed to top, enemy plane field, aircraft carrier road through the top by rocket or guided missile or aircraft emission.Can be used for the territorial air defence or be deployed to the sky, certain theater of war.The present invention's thunder that wafts is in the air deployed troops on garrison duty behind certain spatial domain, can be with the performance or the invasion of low-cost effective blockade or containment enemy air power.
As optimization, described bomb is revealed the removal of mines by the self-desttruction equipment of equipped clock control or controller control, and described bomb is looked other system by equipped enemy and we and prevented miss bomb; Described balloon is kept system by equipped balloon altitude by solar battery power power supply or the power supply of solar cell storage power and is realized the Defensive Target spatial domain.
As optimization, described balloon altitude is kept system and is comprised air pressure position indicator or flying height instrument, controller, the electrolytic hydrogen generator of hydrogen make-up and balloon venting electrically-controlled valve in balloon; The described power supply controller that is electrically connected, controller connect air pressure position indicator or flying height instrument, hydrogen generator and balloon venting electrically-controlled valve.
The thunder that wafts in the air that is used to implement spatial domain of the present invention defence method is the equipped miniature bomb of high energy of transparent hydrogen balloon or helium balloon.So design, transparent balloon are used for strengthening disguised.Hydrogen balloon or helium balloon are used to keep aerial floating.The miniature bomb of high energy is used to attack bump or near enemy's aerial target of the thunder that wafts, and the miniature bomb light weight of high energy, cost are low, and volume is little, can be suitable for small-sized unsettled balloon, the thunder aerial target of wafing is little, and is disguised strong, be difficult for being found, more help suitable rule, high density mould greatly and deploy troops on garrison duty by the enemy.It can be deployed to top, enemy plane field, aircraft carrier road through the top by rocket or guided missile or aircraft emission.Can be used for the territorial air defence or be deployed to the sky, certain theater of war.The present invention's thunder that wafts is in the air deployed troops on garrison duty behind certain spatial domain, can effective blockade or the performance or the invasion of containment enemy air power.
As optimization, described balloon is furnished with the balloon altitude of being powered by solar battery power power supply or solar cell storage power and keeps system.So design increases and can guarantee to continue to float in setting height after distribution ball height is kept system, in height guarantees accurately to block.Solar cell for supplying power can guarantee the continued power under the sufficient sunlight conditions is being arranged and keeping.Electric power storage is in order to guarantee in the solar radiation deficiency or not have under the sunlight conditions, can normally keeping the height that floats.
As optimization, described balloon altitude is kept system and is comprised air pressure position indicator or flying height instrument, controller, the electrolytic hydrogen generator of hydrogen make-up and balloon venting electrically-controlled valve in balloon; The described solar cell storage power controller that is electrically connected, controller connect air pressure position indicator or flying height instrument, hydrogen generator and balloon venting electrically-controlled valve.So design, air pressure position indicator or flying height instrument in time provide showy altitude information to controller, controller in time promotes balloon altitude and Ji and opens balloon venting electrically-controlled valve and reduce balloon altitude by opening electrolytic hydrogen generator hydrogen make-up in balloon according to the setting height standard.
As optimization, described bomb is furnished with the self-desttruction equipment of clock control or controller control, and described bomb is furnished with enemy and we and looks other system; Described bomb is fitted in the balloon inner bottom part, and described solar cell is fitted in the balloon inner top or is fitted in above the bomb.So design, during the self-desttruction equipment clock control, predeterminable self-destruction time reaches and starts self-desttruction equipment automatically after the default hang time thunder that wafts was lost efficacy, to prevent to accidentally injure and recover normal spatial domain.In addition, the self-desttruction equipment of controller control also can initiatively be removed mines at any time according to concrete needs and be recovered normal spatial domain.Described bomb and solar cell are fitted in the balloon inner bottom part and are convenient to discharge the thunder and disguised strong that wafts.Solar cell is fitted in the balloon inner top or is fitted in above the bomb and all conveniently absorbs solar energy.
As optimization, when solar cell was fitted in the balloon inner top, storage power and balloon altitude were kept system and are fitted in below the solar cell; In the time of above solar cell is fitted in bomb, storage power and balloon altitude are kept system and are fitted between bomb and the balloon bottom.So design, when solar cell was fitted in the balloon inner top, storage power and balloon altitude were kept system and are fitted in and help simplified control system and guarantee sunlight illumination below the solar cell; In the time of above solar cell is fitted in bomb, storage power and balloon altitude are kept system and are fitted between bomb and the balloon bottom, and then center of gravity is lower, helps improving balloon stability.
As optimization, the balloon top is furnished with charging connector during the solar cell overhead, and the amount of putting balloon bottom is furnished with charging connector at the bottom of the solar cell, and balloon venting electrically-controlled valve is fitted in the charging connector place, and the oxygen output tube of electrolytic hydrogen generator is outwards drawn from the charging connector place.So design helps simplifying the configuration of valve and auxiliary equipment thereof.When the electrolytic hydrogen generator produces hydrogen, the bigger oxygen of proportion that produces discharged to alleviate the balloon deadweight, help to prolong the hang time, keep the longer time fighting capacity.
As optimization, oxygen output tube also is fitted with check (non-return) valve; Balloon is made up of the multilayer balloon that is filled with hydrogen or helium respectively of inside and outside suit.So design, oxygen output tube also be fitted with check (non-return) valve help avoiding extraneous air to enter or generator in electrolyte leakage.When balloon is made up of the multilayer balloon that is filled with hydrogen or helium respectively of inside and outside suit,, still can also the stagnant air defence of inner balloon layer continuation drive in case outer balloon layer breaks.
It has certain ageing blockade spatial domain, forces to block the advantage of overtime self-destruction.Tackle " thunder drifted by wind " have only two kinds by way of: the one, the bump of flying; Two are to use most advanced and sophisticated electronic guidance weapon; But its cost is too high, loses more than gain.So large scale and high density the present invention's thunder that wafts in the air of deploying troops on garrison duty can restrict the invasion of surging air power, avoids the empty power of weak tendency state to lose control of the air.
After adopting technique scheme, spatial domain of the present invention defence method has workable, and cost is low, is easy to deploy troops on garrison duty, can effective blockade or containment enemy air power, be particularly suitable for the weak side of sky power resist sky power formidable opponent invasion advantage.Thunder is waftd in the present invention in the air can be by rocket or guided missile or the laying of aircraft large scale and high density, continue to float in certain spatial domain, be used to attack enemy's aerial target of bump or the approaching thunder that wafts, play with low-cost and force to block or containment enemy air power, defend the purpose of control of the air.
Description of drawings
Fig. 1 is waft the in the air structural representation of first kind of embodiment of thunder of the present invention;
Fig. 2 is waft the in the air structural representation of second kind of embodiment of thunder of the present invention.
The specific embodiment
Spatial domain of the present invention defence method is transparent hydrogen balloon or a helium balloon of laying the equipped miniature bomb of high energy in the spatial domain of setting up defences.Described bomb is revealed the removal of mines by the self-desttruction equipment of equipped clock control or controller control, and described bomb is looked other system by equipped enemy and we and prevented miss bomb; Described balloon is kept system by equipped balloon altitude by solar battery power power supply or the power supply of solar cell storage power and is realized the Defensive Target spatial domain.Described balloon altitude is kept system and is comprised air pressure position indicator or flying height instrument, controller, the electrolytic hydrogen generator of hydrogen make-up and balloon venting electrically-controlled valve in balloon; The described power supply controller that is electrically connected, controller connect air pressure position indicator or flying height instrument, hydrogen generator and balloon venting electrically-controlled valve.
Embodiment one, and as shown in Figure 1, the present invention's thunder that wafts in the air is that transparent hydrogen balloon or helium balloon 1 inner bottom part are furnished with the miniature bomb 2 of high energy that enemy and we look other system.Be furnished with in the described balloon 1 by the balloon altitude of solar cell storage power power supply and keep system 3.Described balloon altitude is kept system 3 and is comprised air pressure position indicator or flying height instrument, controller, the electrolytic hydrogen generator of hydrogen make-up and balloon venting electrically-controlled valve in balloon; The described power supply controller that is electrically connected, controller connect air pressure position indicator or flying height instrument, hydrogen generator and balloon venting electrically-controlled valve.Described bomb 2 is furnished with the self-desttruction equipment of clock control or controller control.
Described solar cell 31 is fitted in the balloon inner top, and balloon altitude is kept system 3 and is fitted in below the solar cell 31.Balloon altitude is kept between system 3 and the miniature bomb 2 of high energy and is linked to each other by lead 4.
Balloon 1 top is furnished with charging connector 11, and balloon venting electrically-controlled valve is fitted in the charging connector place, and the oxygen output tube of electrolytic hydrogen generator is outwards drawn from the charging connector place.Oxygen output tube also is fitted with check (non-return) valve.
Embodiment two, and as shown in Figure 2, the present invention's thunder that wafts in the air is that transparent hydrogen balloon or helium balloon 1 inner bottom part are furnished with the miniature bomb 2 of high energy that enemy and we look other system.Be furnished with in the described balloon 1 by the balloon altitude of solar cell storage power power supply and keep system 3.Described balloon altitude is kept system 3 and is comprised air pressure position indicator or flying height instrument, controller, the electrolytic hydrogen generator of hydrogen make-up and balloon venting electrically-controlled valve in balloon; The described power supply controller that is electrically connected, controller connect air pressure position indicator or flying height instrument, hydrogen generator and balloon venting electrically-controlled valve.Described bomb 2 is furnished with the self-desttruction equipment of clock control or controller control.
Described solar cell 31 is fitted in above the bomb, and balloon altitude is kept system 3 and is fitted between solar cell 31 and balloon 1 bottom.The base 5 of equipped built-in storage power below the solar cell 31.Storage power in the base 5 is kept system 3 by the balloon altitude of lead 4 below bomb 2 and is linked to each other.
Balloon 1 bottom is furnished with charging connector 11, and balloon venting electrically-controlled valve is fitted in the charging connector place, and the oxygen output tube of electrolytic hydrogen generator is outwards drawn from the charging connector place.Oxygen output tube also is fitted with check (non-return) valve.
Claims (10)
1. a spatial domain defence method is characterized in that it being transparent hydrogen balloon or the helium balloon of laying the equipped miniature bomb of high energy in the spatial domain of setting up defences.
2. according to right 1 described spatial domain defence method, it is characterized in that described bomb reveals the removal of mines by the self-desttruction equipment of equipped clock control or controller control, described bomb is looked other system by equipped enemy and we and is prevented miss bomb; Described balloon is kept system by equipped balloon altitude by solar battery power power supply or the power supply of solar cell storage power and is realized the Defensive Target spatial domain.
3. according to right 2 described spatial domain defence methods, it is characterized in that described balloon altitude keeps system and comprise air pressure position indicator or flying height instrument, controller, the electrolytic hydrogen generator of hydrogen make-up and balloon venting electrically-controlled valve in balloon; The described power supply controller that is electrically connected, controller connect air pressure position indicator or flying height instrument, hydrogen generator and balloon venting electrically-controlled valve.
4. be used to implement the thunder that wafts of the described spatial domain of claim 1 defence method in the air, it is characterized in that it being the equipped miniature bomb of high energy of transparent hydrogen balloon or helium balloon.
5. according to the described thunder that wafts in the air of claim 4, it is characterized in that described balloon is furnished with by the balloon altitude of solar battery power power supply or the power supply of solar cell storage power to keep system.
6. according to the described thunder that wafts of claim 5, it is characterized in that described balloon altitude keeps system and comprise air pressure position indicator or flying height instrument, controller, the electrolytic hydrogen generator of hydrogen make-up and balloon venting electrically-controlled valve in balloon in the air; The described power supply controller that is electrically connected, controller connect air pressure position indicator or flying height instrument, hydrogen generator and balloon venting electrically-controlled valve.
7. according to claim 4 or the 5 or 6 described thunders that waft in the air, it is characterized in that described bomb is furnished with the self-desttruction equipment of clock control or controller control, described bomb is furnished with enemy and we and looks other system; Described bomb is fitted in the balloon inner bottom part, and described solar cell is fitted in the balloon inner top or is fitted in above the bomb.
8. according to the described thunder that wafts of claim 7, it is characterized in that when solar cell was fitted in the balloon inner top, storage power and balloon altitude were kept system and be fitted in below the solar cell in the air; In the time of above solar cell is fitted in bomb, storage power and balloon altitude are kept system and are fitted between bomb and the balloon bottom.
9. the described according to Claim 8 thunder that wafts in the air, the balloon top is furnished with charging connector when it is characterized in that the solar cell overhead, the balloon bottom is furnished with charging connector when putting at the bottom of the solar cell, balloon venting electrically-controlled valve is fitted in the charging connector place, and the oxygen output tube of electrolytic hydrogen generator is outwards drawn from the charging connector place.
10. according to the described thunder that wafts of claim 9, it is characterized in that oxygen output tube also is fitted with check (non-return) valve in the air; Balloon is made up of the multilayer balloon that is filled with hydrogen or helium respectively of inside and outside suit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201010184121 CN101832740B (en) | 2010-05-27 | 2010-05-27 | Airspace defense method and air floating mine thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201010184121 CN101832740B (en) | 2010-05-27 | 2010-05-27 | Airspace defense method and air floating mine thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN101832740A true CN101832740A (en) | 2010-09-15 |
| CN101832740B CN101832740B (en) | 2013-04-03 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201010184121 Active CN101832740B (en) | 2010-05-27 | 2010-05-27 | Airspace defense method and air floating mine thereof |
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| Country | Link |
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| CN (1) | CN101832740B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109813187A (en) * | 2018-12-19 | 2019-05-28 | 山东师范大学 | A kind of aerial thunder and its working method of countering intrusions aircraft |
| CN114326483A (en) * | 2021-12-03 | 2022-04-12 | 中国特种飞行器研究所 | Real-time tracking and self-destruction device for airborne balloon |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB531101A (en) * | 1939-07-11 | 1940-12-30 | Henry James Muir | Means for launching or releasing aerial mines or the like |
| DE3328179A1 (en) * | 1983-08-04 | 1985-02-21 | Franz 2121 Deutsch Evern Anker | Ground-air parachute mine |
| CN85202764U (en) * | 1985-06-29 | 1986-12-24 | 中国人民解放军总参谋部工程兵技术装备研究所 | Hydrogen self-filling false target for radar |
| CN1305920A (en) * | 1999-07-04 | 2001-08-01 | 秦兆山 | Air defence mine |
| CN2586129Y (en) * | 2002-12-03 | 2003-11-12 | 宣士平 | Air mine |
| CN2708231Y (en) * | 2003-03-31 | 2005-07-06 | 吕国雄 | Controllable and recoverable air floatage |
| CN201133936Y (en) * | 2007-03-21 | 2008-10-15 | 甘勃 | Balloon radar system |
| CN201672864U (en) * | 2010-05-27 | 2010-12-15 | 朱恩灿 | Aerial hydrogen balloon |
-
2010
- 2010-05-27 CN CN 201010184121 patent/CN101832740B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB531101A (en) * | 1939-07-11 | 1940-12-30 | Henry James Muir | Means for launching or releasing aerial mines or the like |
| DE3328179A1 (en) * | 1983-08-04 | 1985-02-21 | Franz 2121 Deutsch Evern Anker | Ground-air parachute mine |
| CN85202764U (en) * | 1985-06-29 | 1986-12-24 | 中国人民解放军总参谋部工程兵技术装备研究所 | Hydrogen self-filling false target for radar |
| CN1305920A (en) * | 1999-07-04 | 2001-08-01 | 秦兆山 | Air defence mine |
| CN2586129Y (en) * | 2002-12-03 | 2003-11-12 | 宣士平 | Air mine |
| CN2708231Y (en) * | 2003-03-31 | 2005-07-06 | 吕国雄 | Controllable and recoverable air floatage |
| CN201133936Y (en) * | 2007-03-21 | 2008-10-15 | 甘勃 | Balloon radar system |
| CN201672864U (en) * | 2010-05-27 | 2010-12-15 | 朱恩灿 | Aerial hydrogen balloon |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109813187A (en) * | 2018-12-19 | 2019-05-28 | 山东师范大学 | A kind of aerial thunder and its working method of countering intrusions aircraft |
| CN109813187B (en) * | 2018-12-19 | 2021-05-04 | 山东师范大学 | Air mine for anti-invasion airplane and working method thereof |
| CN114326483A (en) * | 2021-12-03 | 2022-04-12 | 中国特种飞行器研究所 | Real-time tracking and self-destruction device for airborne balloon |
Also Published As
| Publication number | Publication date |
|---|---|
| CN101832740B (en) | 2013-04-03 |
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