CN203163617U - Novel bomb - Google Patents
Novel bomb Download PDFInfo
- Publication number
- CN203163617U CN203163617U CN 201320201062 CN201320201062U CN203163617U CN 203163617 U CN203163617 U CN 203163617U CN 201320201062 CN201320201062 CN 201320201062 CN 201320201062 U CN201320201062 U CN 201320201062U CN 203163617 U CN203163617 U CN 203163617U
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- China
- Prior art keywords
- bomb
- microprocessor
- range sensor
- novel
- armament
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Abstract
The utility model relates to a novel bomb. The novel bomb comprises a bomb body 1, wherein the bomb body 1 is internally provided with a cavity 2; the cavity 2 is filled with explosive 3; a plurality of run-through holes 4 are formed in the outer wall and the inner wall of the bomb body 1; a steel needle 5 is placed in each hole 4; each steel needle 5 is hollowed; a pair of elastic metal strips 6 is placed at the tail part of each steel needle 5; the elastic metal strips 6 are splayed; an initiating system 8 is arranged in the cavity 2; the initiating system 8 comprises a microprocessor 9, a radio receiving device 10, a distance sensor 11, an initiating device 12 and a power supply 13; and the power supply 13 supplies electric energy to the whole initiating system 8. The novel bomb has the following advantages that firstly, a plurality of bomb splinters can be scattered after the bomb is exploded, and the bomb can be initiated at a certain height from the ground surface, so that the lethal area and killing effect can be effectively improved; secondly, the novel bomb is simple in structure and convenient to use; and thirdly, the novel bomb is low in cost and convenient for large-scale production.
Description
Technical field
The utility model relates to a kind of military bomb.
Background technology
Present military bomb is made by filling explosive in the metallic object basically, ignition charge, and metallic object is fried to fragmentate, and spreads out, and hits people and thing, damages.But because metallic object various piece unbalance stress, the shell fragment that causes metallic object to be blown is not of uniform size, and the shell fragment that has is too big, cause flying speed lower, attacking ability is less, and the number of shell fragment is fewer, moreover GP bomb is just to be detonated after landing, and the lethal area of bomb is limited.If bomb just is detonated apart from the ground certain altitude, it is bigger that the lethal area of bomb can become.So can divide a lot of shell fragments that shed after pressing for a kind of blowing, and just be detonated apart from the ground certain altitude, can effectively improve the novel bomb of lethal area and fragmentation effect.
Summary of the invention
The purpose of this utility model is: can divide a lot of shell fragments that shed after a kind of blowing is provided, and just be detonated apart from the ground certain altitude, can effectively improve the novel bomb of lethal area and fragmentation effect.
A kind of novel bomb of the present utility model, comprise body 1, a cavity 2 is arranged in the described body 1, fill explosive 3 in the described cavity 2, the outer wall of described body 1 and inwall have the hole of much running through 4, place draw point 5 in the described hole 4, described draw point 5 is hollow, described draw point 5 afterbodys are settled a pair of resilient metal strip 6,6 one-tenth splayeds of described resilient metal strip, settle a fuzing system, armament 8 in described 2, described fuzing system, armament 8 comprises microprocessor 9, radio system 10, range sensor 11, igniter 12, power supply 13, described power supply 13 provides electric energy for whole fuzing system, armament 8, after described radio system 10 receives the control signal that the ground staff sends, send control signal to microprocessor 9, described range sensor 11 sends the signal that receives to microprocessor 9, when being provided with bomb in the described microprocessor 9 and igniting apart from the height on ground, when microprocessor 9 receives the control signal that radio system 10 transmits earlier, receive the signal that range sensor 11 transmits again, and bomb arrived ignite height after, microprocessor 9 is controlled igniter 12 immediately, bomb is detonated immediately, described range sensor 11 is installed in the front end of body 1 shell, and described range sensor 11 is connected with fuzing system, armament by lead 14.
The utility model is to transform on the basis of existing bomb, at bomb fuzing system, armament is installed, bomb can just can be detonated apart from the ground certain altitude, and a large amount of draw points of arrangement in the bomb body, after bomb is detonated, draw point will be launched fast, just may cause huge injury to the enemy.
The utlity model has following some advantage:
1. can divide a lot of shell fragments that shed after bomb is blown, and just be detonated apart from the ground certain altitude, can effectively improve lethal area and fragmentation effect;
2. simple in structure, real easy to use;
3. with low cost, be convenient to a large amount of productions.
Description of drawings
Fig. 1 is structural representation of the present utility model;
Among the figure: 4 draw points, 5 resilient metal strips, 6 fuzing system, armaments 8 of body 1 cavity 2 explosives 3 holes
Fig. 2 is the schematic block circuit diagram of fuzing system, armament of the present utility model;
Among the figure: microprocessor 9 radio systems 10 range sensors 11 igniters 12 power supplys 13
Fig. 3 is the structural representation of draw point of the present utility model;
Among the figure: draw point 5 resilient metal strips 6.
The specific embodiment
The utility model will be further described below in conjunction with accompanying drawing.
A kind of novel bomb of the present utility model, comprise body 1, a cavity 2 is arranged in the described body 1, fill explosive 3 in the described cavity 2, the outer wall of described body 1 and inwall have the hole of much running through 4, place draw point 5 in the described hole 4, described draw point 5 is hollow, described draw point 5 afterbodys are settled a pair of resilient metal strip 6,6 one-tenth splayeds of described resilient metal strip, settle a fuzing system, armament 8 in described 2, described fuzing system, armament 8 comprises microprocessor 9, radio system 10, range sensor 11, igniter 12, power supply 13, described power supply 13 provides electric energy for whole fuzing system, armament 8, after described radio system 10 receives the control signal that the ground staff sends, send control signal to microprocessor 9, described range sensor 11 sends the signal that receives to microprocessor 9, when being provided with bomb in the described microprocessor 9 and igniting apart from the height on ground, when microprocessor 9 receives the control signal that radio system 10 transmits earlier, receive the signal that range sensor 11 transmits again, and bomb arrived ignite height after, microprocessor 9 is controlled igniter 12 immediately, bomb is detonated immediately, described range sensor 11 is installed in the front end of body 1 shell, and described range sensor 11 is connected with fuzing system, armament by lead 14.
During use, at first be placed in bomb in the artillery or on the military aircraft, then emission, bomb sends radio control signal in-flight again, wait bomb to enter the enemy position after, the detected bomb of range sensor apart from the distance on ground reached ignite height after, bomb is detonated immediately.The ignition of bomb arranges in the microprocessor of fuzing system, armament highly in advance.After bomb is detonated, the air pressure moment rising in the body, gas can promote draw point, and the resilient metal strip of draw point afterbody will stressedly shrink, and draw point transmitted at high speed is immediately gone out, and just may cause huge injury to the enemy.
Claims (1)
1. novel bomb, comprise body (1), it is characterized in that, a cavity (2) is arranged in the described body (1), fill explosive (3) in the described cavity (2), the outer wall of described body (1) and inwall have the hole of much running through (4), place draw point (5) in the described hole (4), described draw point (5) is hollow, described draw point (5) afterbody is settled a pair of resilient metal strip (6), described resilient metal strip (6) becomes splayed, settle a fuzing system, armament (8) in described (2), described fuzing system, armament (8) comprises microprocessor (9), radio system (10), range sensor (11), igniter (12), power supply (13), described power supply (13) provides electric energy for whole fuzing system, armament (8), after described radio system (10) receives the control signal that the ground staff sends, send control signal to microprocessor (9), described range sensor (11) sends the signal that receives to microprocessor (9), when being provided with bomb in the described microprocessor (9) and igniting apart from the height on ground, when microprocessor (9) receives the control signal that radio system (10) transmits earlier, receive the signal that range sensor (11) transmits again, and bomb arrived ignite height after, microprocessor (9) is controlled igniter (12) immediately, bomb is detonated immediately, described range sensor (11) is installed in the front end of body (1) shell, and described range sensor (11) is connected with fuzing system, armament by lead (14).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201320201062 CN203163617U (en) | 2013-04-22 | 2013-04-22 | Novel bomb |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201320201062 CN203163617U (en) | 2013-04-22 | 2013-04-22 | Novel bomb |
Publications (1)
Publication Number | Publication Date |
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CN203163617U true CN203163617U (en) | 2013-08-28 |
Family
ID=49024795
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN 201320201062 Expired - Fee Related CN203163617U (en) | 2013-04-22 | 2013-04-22 | Novel bomb |
Country Status (1)
Country | Link |
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CN (1) | CN203163617U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106482588A (en) * | 2016-11-28 | 2017-03-08 | 湖北航天飞行器研究所 | A kind of device for circumference adjustment fragment emission direction |
-
2013
- 2013-04-22 CN CN 201320201062 patent/CN203163617U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106482588A (en) * | 2016-11-28 | 2017-03-08 | 湖北航天飞行器研究所 | A kind of device for circumference adjustment fragment emission direction |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C17 | Cessation of patent right | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130828 Termination date: 20140422 |