CN102147216A - Defence bomb - Google Patents
Defence bomb Download PDFInfo
- Publication number
- CN102147216A CN102147216A CN2011100622059A CN201110062205A CN102147216A CN 102147216 A CN102147216 A CN 102147216A CN 2011100622059 A CN2011100622059 A CN 2011100622059A CN 201110062205 A CN201110062205 A CN 201110062205A CN 102147216 A CN102147216 A CN 102147216A
- Authority
- CN
- China
- Prior art keywords
- shell
- compressed gas
- defence
- bomb
- sealing plate
- 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.)
- Granted
Links
- 239000000919 ceramic Substances 0.000 claims abstract description 22
- 238000001514 detection method Methods 0.000 claims abstract description 7
- 238000007789 sealing Methods 0.000 claims description 19
- 238000005273 aeration Methods 0.000 abstract 2
- 238000004519 manufacturing process Methods 0.000 abstract 2
- 238000005516 engineering process Methods 0.000 description 3
- 230000001133 acceleration Effects 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- 238000010923 batch production Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
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- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Adornments (AREA)
Abstract
The invention discloses a defence bomb belonging to the technical field of armament. The defence bomb comprises a shell, a compressed gas cabin, an aeration and detection port, an execution unit, a control unit, bomb hanging devices, a ceramic ball, rivets, a rear cover plate, a seal plate and a release port. The defence bomb is characterized in that the shell is provided with the bomb hanging devices; the front section in the shell is provided with the compressed gas cabin; the compressed gas cabin is provided with the aeration and detection port; the rear part of the compressed gas cabin is provided with the release port; the release port is sealed with the seal plate which is locked by the execution unit; the execution unit is connected with the control unit; the ceramic ball is arranged in the shell behind the seal plate; and the rear cover plate covers the back of the shell and is fixed on the shell by the rivets. The defence bomb has the advantages of low cost and high practicality, is simple to design and manufacture and is easy for mass production and large-scale assembly.
Description
Technical field
The present invention relates to a kind of defence bullet, relate in particular to the defence bullet, belong to the ordnance technical field.
Background technology
At present, the airborne defence bullet of known technology, when our aircraft rear is subjected to the attack of enemy's aircraft in the aircraft air battle, our aircraft has only in time dodges enemy missile or tackles enemy missile or enemy's aircraft with our defence bullet, the defence bullet exists bullet few at present, the scope of attack is little, emission back enemy plane can in time be found, dodge easily, shortcomings such as cost height, before the present invention does not make, do not have to have and adopt compressed air propelling and Ceramic Balls to use as the defence bullet that hits thing, it is open that the patent searching document does not have the new technical scheme of this technology.
Summary of the invention
For overcome in the prior art do not have have adopt compressed air to advance and Ceramic Balls as the deficiency of the defence bullet of strike thing, the purpose of this reality invention is propelling of employing compressed air and Ceramic Balls to be arranged as the defence bullet that hits thing in order to provide a kind of, this defence bullet can be under the prerequisite that reduces cost, reach the things that hit hits the enemy more, the scope of attack is big, reaction fast, do not found after the Ceramic Balls emission by enemy radar, compressed air is not found by enemy's infrared sensor after launching as power source, a plurality of strike things hit enemy plane and enemy missile simultaneously, reach defence and attack the purpose of taking into account.
The present invention solves the technical scheme that its technical problem takes: by shell, the Compressed Gas storehouse, inflation and detection mouth, performance element, control module, hang ereisma, Ceramic Balls, rivet, back shroud, sealing plate, liberation port is formed, it is characterized in that leaving on the shell extension ereisma, the leading portion of enclosure is the Compressed Gas storehouse, leave inflation on the Compressed Gas storehouse and detect mouth, liberation port is left at rear portion, Compressed Gas storehouse, sealing plate is sealed on the liberation port, by performance element that sealing plate is locked, performance element is connected with control module, dress Ceramic Balls in the sealing plate back case, post-planking cover is fixed on the shell with rivet in the shell back.During use before fighter plane takes off, inflate and detect for the Compressed Gas storehouse to inflation and detection mouth, by hang ereisma with this defence bullet be placed in the fighter plane rear portion under, pursue and attack in the enemy plane dead astern or enemy missile is in the dead astern when being subjected to, in the time of closely, the pilot sends instruction, control module is controlled the trip release that performance element breaks away from sealing plate, Compressed Gas is discharged from liberation port in the compressed gas storehouse, Compressed Gas promotion sealing plate slides backward the promotion Ceramic Balls fast and promotes back shroud backward, when the suffered power of fixing rivet during greater than self riveted power, fixing rivet breaks away from the moment of shell, back shroud and Ceramic Balls and sealing plate launch out shell simultaneously, because with atmosphere pressure reduction is arranged in the shell, Ceramic Balls is umbrella shape when coming out in shell rearward sprays, fighter plane is in the reaction acceleration of following moment of jet power, Ceramic Balls is hit enemy plane or enemy missile, reaches anti-enemy's made by the emperor order purpose.
The invention has the beneficial effects as follows simplicity of design, make simply, with low cost, realization batch process and equipment easily on a large scale, reach the things that hit hits the enemy more, the scope of attack is big, and reaction is not found by enemy radar after the Ceramic Balls emission fast, compressed air is not found by enemy's infrared sensor after launching as power source, a plurality of strike things hit enemy plane and enemy missile simultaneously, the purpose that defence and attack take into account, and practicality is bigger.
Description of drawings
The invention will be further described below in conjunction with drawings and Examples.
Fig. 1 is a cross-sectional schematic of the present invention.
Fig. 2 is the A-A cutaway view of Fig. 1 of the present invention.
1. shells among Fig. 2,2. Compressed Gas storehouse, 3. inflation and detect mouthful, 4. performance element, 5. control module is 6. hung ereisma, 7. Ceramic Balls, 8. rivet, 9. back shroud, 10. sealing plate, 11. liberation ports.
The specific embodiment
The present invention is by shell 1, Compressed Gas storehouse 2, inflation and detection mouth 3, performance element 4, control module 5, hang ereisma 6, Ceramic Balls 7, rivet 8, back shroud 9, sealing plate 10, liberation port 11 is formed, it is characterized in that leaving on the shell 1 extension ereisma 6, the leading portion of shell 1 inside is Compressed Gas storehouse 2, leave inflation on the Compressed Gas storehouse 2 and detect mouth 3, liberation port 11 is left at 2 rear portions, Compressed Gas storehouse, sealing plate 10 is sealed on the liberation port 11, by performance element 4 that sealing plate 10 is locked, performance element 4 is connected with control module 5, dress Ceramic Balls 7 in sealing plate 10 back case 1, back shroud 9 covers in the shell back and is fixed on the shell 1 with rivet 8, during use before fighter plane takes off, inflate and detect for Compressed Gas storehouse 2 to inflation and detection mouth 3, by hang ereisma 6 with this defence bullet be placed in the fighter plane rear portion under, pursue and attack in the enemy plane dead astern or enemy missile is in the dead astern when being subjected to, in the time of closely, the pilot sends instruction, control module 5 is controlled the trip release that performance element 4 breaks away from sealing plate 10, Compressed Gas is discharged from liberation port 11 in the compressed gas storehouse 2, Compressed Gas promotion sealing plate 10 slides backward promotion Ceramic Balls 7 fast and promotes back shroud 9 backward, when the suffered power of fixing rivet 8 during greater than self riveted power, fixing rivet 8 breaks away from the moment of shell 1, back shroud 9 and Ceramic Balls 7 and sealing plate 10 launch out shell 1 simultaneously, owing to atmosphere pressure reduction is arranged in the shell 1, Ceramic Balls 7 is umbrella shape when coming out and rearward sprays in shell 1, fighter plane is in the reaction acceleration of following moment of jet power, 7 pairs of enemy planes of Ceramic Balls or enemy missile hit, and reach anti-enemy's made by the emperor order purpose.
Claims (2)
1. defend bullet for one kind, by shell (1), Compressed Gas storehouse (2), inflation and detection mouthful (3), performance element (4), control module (5), hang ereisma (6), Ceramic Balls (7), rivet (8), back shroud (9), sealing plate (10), liberation port (11) is formed, it is characterized in that leaving on the shell (1) extension ereisma (6), the inner leading portion of shell (1) is Compressed Gas storehouse (2), leave inflation on the Compressed Gas storehouse (2) and detect mouthful (3), liberation port (11) is left at rear portion, Compressed Gas storehouse (2), sealing plate (10) is sealed on the liberation port (11), by performance element (4) that sealing plate (10) is locked, performance element (4) is connected with control module (5), dress Ceramic Balls (7) in sealing plate (10) back case (1), back shroud (9) covers in the shell back and is fixed on the shell (1) with rivet (8).
2. a kind of defence bullet according to claim 1 is characterized in that the inner using charged air pressure in Compressed Gas storehouse (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201110062205 CN102147216B (en) | 2011-03-14 | 2011-03-14 | Defence bomb |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201110062205 CN102147216B (en) | 2011-03-14 | 2011-03-14 | Defence bomb |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102147216A true CN102147216A (en) | 2011-08-10 |
| CN102147216B CN102147216B (en) | 2013-05-01 |
Family
ID=44421598
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201110062205 Expired - Fee Related CN102147216B (en) | 2011-03-14 | 2011-03-14 | Defence bomb |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102147216B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103968714A (en) * | 2014-05-15 | 2014-08-06 | 刘少伟 | Defending bomb device hung in air |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2444202Y (en) * | 2000-06-06 | 2001-08-22 | 黄盛贤 | Interference bullet for radar |
| US6279482B1 (en) * | 1996-07-25 | 2001-08-28 | Trw Inc. | Countermeasure apparatus for deploying interceptor elements from a spin stabilized rocket |
| EP1462756A1 (en) * | 2003-02-28 | 2004-09-29 | Giat Industries | Method of defence of a vehicle or a structure against a threat such as a projectile and device to carry out said method |
| CN101021401A (en) * | 2007-03-27 | 2007-08-22 | 刘永刚 | Air defense balloon kite with international standard characters |
| CN101038143A (en) * | 2007-04-11 | 2007-09-19 | 杨海洋 | Flexible hold-up interception method of missile and equipment |
| CN202018245U (en) * | 2011-03-14 | 2011-10-26 | 吴超 | Defense missile |
-
2011
- 2011-03-14 CN CN 201110062205 patent/CN102147216B/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6279482B1 (en) * | 1996-07-25 | 2001-08-28 | Trw Inc. | Countermeasure apparatus for deploying interceptor elements from a spin stabilized rocket |
| CN2444202Y (en) * | 2000-06-06 | 2001-08-22 | 黄盛贤 | Interference bullet for radar |
| EP1462756A1 (en) * | 2003-02-28 | 2004-09-29 | Giat Industries | Method of defence of a vehicle or a structure against a threat such as a projectile and device to carry out said method |
| CN101021401A (en) * | 2007-03-27 | 2007-08-22 | 刘永刚 | Air defense balloon kite with international standard characters |
| CN101038143A (en) * | 2007-04-11 | 2007-09-19 | 杨海洋 | Flexible hold-up interception method of missile and equipment |
| CN202018245U (en) * | 2011-03-14 | 2011-10-26 | 吴超 | Defense missile |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103968714A (en) * | 2014-05-15 | 2014-08-06 | 刘少伟 | Defending bomb device hung in air |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102147216B (en) | 2013-05-01 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee | ||
| CP02 | Change in the address of a patent holder |
Address after: Chongqing city Wansheng District No. 18 West Road 400800 Patentee after: Wu Chao Address before: Yiwu City, Zhejiang province 322022 temple town Patentee before: Wu Chao |
|
| CP02 | Change in the address of a patent holder |
Address after: 317 200 No. 5, Shantou Zhu Group, Xiazhu Village, Chicheng Street, Tiantai County, Taizhou City, Zhejiang Province Patentee after: Wu Chao Address before: Chongqing city Wansheng District No. 18 West Road 400800 Patentee before: Wu Chao |
|
| CP02 | Change in the address of a patent holder | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230103 Address after: 276000 Torch Building, Keji Avenue, high tech Industrial Development Zone, Linyi City, Shandong Province Patentee after: Linyi future technology city development and Construction Group Co.,Ltd. Address before: 317200 No. 5, Shan Zhu Zhu, Xia Zhu Village, Chicheng street, Tiantai County, Taizhou, Zhejiang Patentee before: Wu Chao |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130501 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |