CN101832740B - Airspace defense method and air floating mine thereof - Google Patents
Airspace defense method and air floating mine thereof Download PDFInfo
- Publication number
- CN101832740B CN101832740B CN 201010184121 CN201010184121A CN101832740B CN 101832740 B CN101832740 B CN 101832740B CN 201010184121 CN201010184121 CN 201010184121 CN 201010184121 A CN201010184121 A CN 201010184121A CN 101832740 B CN101832740 B CN 101832740B
- Authority
- CN
- China
- Prior art keywords
- balloon
- bomb
- fitted
- hydrogen
- air
- 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.)
- Expired - Fee Related
Links
- 238000000034 method Methods 0.000 title claims abstract description 20
- 230000007123 defense Effects 0.000 title abstract description 4
- 239000001257 hydrogen Substances 0.000 claims abstract description 57
- 229910052739 hydrogen Inorganic materials 0.000 claims abstract description 57
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims abstract description 56
- 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 15
- 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
- 238000013459 approach Methods 0.000 description 3
- 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
- 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
Images
Landscapes
- Electrolytic Production Of Non-Metals, Compounds, Apparatuses Therefor (AREA)
- Photovoltaic Devices (AREA)
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 aerial hydrogen balloon thereof.
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 the 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 in advance theoretician, Italian general Zhu Liaoduhei 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 the 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 aerial hydrogen balloon of the method.
For achieving the above object, spatial domain of the present invention defence method is transparent hydrogen balloon or the 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 for keeping aerial floating.Enemy's aerial target that the miniature bomb of high energy is used for attacking bump or approaches the thunder that wafts, the simultaneously high energy microminiaturization of bomb 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 certain theater of war overhead.Aerial hydrogen balloon of the present invention is deployed troops on garrison duty behind certain spatial domain, can be with 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 the 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 aerial hydrogen balloon that is used for enforcement 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 for keeping aerial floating.Enemy's aerial target that the miniature bomb of high energy is used for attacking bump or approaches the thunder that wafts, the miniature bomb quality of high energy is light, cost is 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 by the enemy, more be conducive to applicable greatly rule, high density mould and deploy troops on garrison duty.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 certain theater of war overhead.Aerial hydrogen balloon of the present invention is deployed troops on garrison duty behind certain spatial domain, can effective blockade or 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 not enough in solar radiation 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 the 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 by opening electrolytic hydrogen generator hydrogen make-up in the balloon according to the setting height standard, and Ji is opened balloon venting electrically-controlled valve and reduced balloon altitude.
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 automatically starts self-desttruction equipment after the default hang time thunder that wafts was lost efficacy, to prevent from accidentally injuring and recovering 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 are conducive to 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, is conducive to improve 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 is conducive to simplify the configuration of valve and auxiliary equipment thereof.When the electrolytic hydrogen generator produces hydrogen, the larger 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 comprised of the multilayer balloon that is filled with respectively hydrogen or helium of inside and outside suit.So design, oxygen output tube also be fitted with check (non-return) valve be conducive to avoid extraneous air to enter or generator in electrolyte leakage.When balloon was comprised of the multilayer balloon that is filled with respectively hydrogen or helium of inside and outside suit, in case outer balloon layer breaks, the air defence that still can also inner balloon layer continues to stagnate was driven.
It has certain ageing blockade spatial domain, forces to block the advantage of overtime self-destruction.Tackle " thunder drifted by wind " only have two kinds by way of: the one, the bump of flying; The 2nd, use most advanced and sophisticated electronic guidance weapon; But its cost is too high, loses more than gain.So the large scale and high density aerial hydrogen balloon of the present invention 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.Aerial hydrogen balloon of the present invention can be by rocket or guided missile or the laying of aircraft large scale and high density, continue to float in certain spatial domain, the enemy's aerial target that is used for attacking bump or approaches the thunder that wafts plays with low-cost and forces to block or containment enemy air power, defends the purpose of control of the air.
Description of drawings
Fig. 1 is the structural representation of aerial hydrogen balloon the first embodiment of the present invention;
Fig. 2 is the structural representation of aerial hydrogen balloon the second embodiment of the present invention.
The specific embodiment
Spatial domain of the present invention defence method is transparent hydrogen balloon or the 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 the 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, aerial hydrogen balloon of the present invention 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 the 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 wire 4.
Embodiment two, and as shown in Figure 2, aerial hydrogen balloon of the present invention 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 the 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 wire 4 below bomb 2 and is linked to each other.
Claims (6)
1. a spatial domain defence method is characterized in that the method is at set up defences transparent hydrogen balloon or the helium balloon of the equipped miniature bomb of high energy of spatial domain laying; Described bomb is revealed the removal of mines by the self-desttruction equipment of equipped 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 the solar battery power power supply 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 the balloon; The described power supply balloon altitude that is electrically connected is kept controller in the system, and this controller connects air pressure position indicator or flying height instrument, hydrogen generator and balloon venting electrically-controlled valve.
2. described spatial domain defence method according to claim 1, it is characterized in that realizing by following aerial hydrogen balloon: described aerial hydrogen balloon is comprised of transparent hydrogen balloon or the equipped miniature bomb of high energy of helium balloon; Described balloon is furnished with the balloon altitude of being powered by solar battery power and keeps system; 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 the 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.
3. described spatial domain defence method according to claim 2 is characterized in that described bomb is furnished with the self-desttruction equipment of 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.
4. described spatial domain defence method according to claim 3 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 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.
5. described spatial domain defence method according to claim 4, 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.
6. described spatial domain defence method according to claim 5 is characterized in that oxygen output tube also is fitted with check (non-return) valve; Balloon is comprised of the multilayer balloon that is filled with respectively hydrogen or helium 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 CN101832740A (en) | 2010-09-15 |
| CN101832740B true CN101832740B (en) | 2013-04-03 |
Family
ID=42716895
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201010184121 Expired - Fee Related CN101832740B (en) | 2010-05-27 | 2010-05-27 | Airspace defense method and air floating mine thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101832740B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
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 not_active Expired - Fee Related
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 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN101832740A (en) | 2010-09-15 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US9448029B1 (en) | Autonomous unmanned tower military mobile intermodal container and method of using the same | |
| KR20190036513A (en) | System and method for guiding a cannon shell in flight | |
| CN108482635B (en) | Inflator wing type aircraft capable of being parked | |
| CN105539788B (en) | A kind of underwater aircraft carrier | |
| CN109383806B (en) | Triggering method for launching fire monitor of fire-fighting unmanned aerial vehicle | |
| CN102923284A (en) | Invisible aircraft carrier with higher combat power and survivability | |
| CN204415731U (en) | A kind of delivery-approach tactics controls to use unmanned vehicle system | |
| CN101832740B (en) | Airspace defense method and air floating mine thereof | |
| CN103968714A (en) | Defending bomb device hung in air | |
| CN201672864U (en) | Aerial hydrogen balloon | |
| WO2022242248A1 (en) | Intelligent multi-rotor rescue throwing device and control method | |
| CN205669960U (en) | A kind of 38mm primary-secondary type poly-bag bullet | |
| CN108128456A (en) | Unmanned helicopter-mounted fire-fighting fire extinguishing gondola | |
| CN104990465B (en) | Follow the trail of and scout locator and the guided missile with the locator | |
| RU2413156C1 (en) | Controlled independent universal positional underwater anti-aircraft (anti-ship) complex ("spider") and method of its implementation | |
| CN217100426U (en) | Intelligent multi-rotor wing rescue throwing device | |
| CN206269677U (en) | Military vehicle laser communication compacting and enemy and we's identification integrated system | |
| US20190359330A1 (en) | Airborne space anti-missile system | |
| CN213631812U (en) | Novel pulse power source structure | |
| CN109813187B (en) | Air mine for anti-invasion airplane and working method thereof | |
| CN206131896U (en) | Urge compound strike type non -fatal ammunition of tear kinetic energy | |
| CN102636085A (en) | Aerial mine | |
| CN110470182A (en) | Big gun throws formula weapon station | |
| CN205102705U (en) | Track guided missile of reconnoitering locator and having this locator | |
| CN215851909U (en) | Small unmanned aerial vehicle intelligent parachuting tracking device based on air pressure and attitude detection |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| ASS | Succession or assignment of patent right |
Owner name: SHANGHAI ZHONGDING HAILONG NEW ENERGY TECHNOLOGY C Free format text: FORMER OWNER: ZHU ENCAN Effective date: 20111018 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| COR | Change of bibliographic data |
Free format text: CORRECT: ADDRESS; FROM: 100073 FENGTAI, BEIJING TO: 200092 HONGKOU, SHANGHAI |
|
| TA01 | Transfer of patent application right |
Effective date of registration: 20111018 Address after: 200092 Shanghai Kongjiang Road No. 1690 14 floor of the Hotel Phoenix Applicant after: Shanghai Zhongding Hailong New Energy Technology Co.,Ltd. Address before: 100073 Beijing city Fengtai District North Liuliqiao No. 4 Naval Equipment Research Institute of the Ministry of Applicant before: Zhu Encan |
|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190725 Address after: 200090 Shanghai city Yangpu District Gongqing Road No. 400 in Dragon Technology Patentee after: Shanghai Zhonghailong High and New Technology Research Institute Address before: 200092 Shanghai Kongjiang Road No. 1690 14 floor of the Hotel Phoenix Patentee before: Shanghai Zhongding Hailong New Energy Technology Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210210 Address after: 572912 Qiongzhong ecological science and Technology Industrial Park, jiachai farm, Qiongzhong Li and Miao Autonomous County, Hainan Province Patentee after: Qiongzhong zhonghailong High Tech Research Institute Address before: 2000 90 Zhonghailong Science and Technology, No. 400 Gongqing Road, Yangpu District, Shanghai Patentee before: SHANGHAI ZHONGHAILONG HIGH AND NEW TECHNOLOGY Research Institute |
|
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130403 |