CN103363849A - Dispenser type lightning triggering rocket bomb bullet - Google Patents
Dispenser type lightning triggering rocket bomb bullet Download PDFInfo
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- CN103363849A CN103363849A CN2013103370805A CN201310337080A CN103363849A CN 103363849 A CN103363849 A CN 103363849A CN 2013103370805 A CN2013103370805 A CN 2013103370805A CN 201310337080 A CN201310337080 A CN 201310337080A CN 103363849 A CN103363849 A CN 103363849A
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Abstract
The invention relates to a dispenser type lightning triggering rocket bomb bullet, and belongs to the technical field of rockets. The dispenser type lightning triggering rocket bomb bullet adopts the structure of a dispenser bomb, and a plurality of lightning triggering bullets can be delivered and released remotely at one time. According to the dispenser type lightning triggering rocket bomb bullet, the one-way paying off mode in a traditional lightning triggering bomb is changed into a two-way paying off mode, the speed of removing the spiral structure of a metal wire and releasing the metal wire is increased, and the axial tensile stress which is generated in the paying off process of lightning triggering bomb metal wire is relieved effectively. Due to the fact that a bearing is arranged between the front end of the metal wire and a lead pendent screw, the metal wire is prevented from driving the whole lead pendent screw to rotate at high speed, the rotary tension which is generated in the paying off process of the lightning triggering bullet metal wire is relieved effectively, and the probability that the metal wire is broken is reduced. A delay fuse is used in the lightning triggering bullet, and the design thought that an traditional fuse is started and ignited according to preset time is abandoned, the moment that the lightning triggering bullet reaches the preset altitude is regarded as the moment that an ignition signal is output, and the technical problem that the error of the trajectory height which is calculated through flying time increases along with increase of the firing range is solved fundamentally.
Description
Technical field
The present invention relates to a kind of primary-secondary type and draw thunder rocket projectile bullet, belong to bullet arrow technical field.
Background technology
Adopting metal wire to draw thunder is a kind of artificially triggered lightning method commonly used, and the method is to draw the thunder bullet from ground to air-launched to carry out artificially triggered lightning.The structure that tradition is drawn the thunder bullet comprises coiling liner, metal wire, vertical head spiral shell, separates buster and time delays fuse as shown in Figure 1; Metal wire one end is spirally wound in the coiling and is lining with, and the other end directly is fixed on vertical head spiral shell rear end.Behind the pellet injection, start to separate buster through the time delays retardation time of fuse, make vertical head spiral shell and bullet body portion from; When vertical head spiral shell traction metal wire descended, metal wire discharged along coiling liner one-way spiral, finishes and draws the thunder operation.
There is following shortcoming in the thunder bullet that draws of traditional structure:
1 draws the launching technique that the thunder bullet adopts ground propellant powder emission, and the flying distance of bullet more closely and once can only be launched one and be drawn the thunder bullet, lacks once long-range emission and throws in a plurality of abilities of drawing the thunder bullet.
2 metal wires are shed medicine and are detonated separation of lead when hanging one's head spiral shell and housing, and separating rate is larger, and the metal wire single direction rotation discharges, and the rotation rate of release is slower, makes metal wire must bear larger tensile stress, easily fracture.
When the traction of 3 vertical head spiral shells is wrapped in the metal wire decline that is lining with in the coiling, the spiral winding limit that the coiling liner is removed on the metal wire limit descends, the revolving force that metal wire produces drives vertical head spiral shell and aloft rotates, because vertical head spiral shell quality is larger, so that metal bears larger rotation tension force, easily fracture.
Time of ignition when 4 bullets will be launched is as timing zero point, by releasing a parachute, discharge metal wire after the regular hour time-delay, this structure can only be by bullet flying speed and flight time estimation bullet overhead distance when casting aside parachute and discharging metal wire, have the larger conversion error with delay time and flying speed reduced height during the operation of single-shot bullet, it is relatively poor to release a parachute, discharge the height of line uniformity during multiple bullet operation.
Summary of the invention
The objective of the invention is to solve tradition and draw the flying distance of the bullet that the thunder bullet exists and more closely and once can only launch one and draw thunder bullet, metal wire dispose procedure and bear larger rotation tension force and tensile stress and make its easily fracture and can not accurately highly discharge the problem such as metal wire, and provide a kind of primary-secondary type to draw thunder rocket projectile bullet.
The objective of the invention is to be achieved through the following technical solutions:
A kind of primary-secondary type of the present invention draws the thunder rocket projectile, comprises blast cap, bullet cabin housing, control cabinet housing, engine, stabilising arrangement, draws thunder bullet, bullet push pedal, bullet buster, the fuse that opens the cabin, igniter;
Draw the thunder bullet and comprise that vertical head spiral shell, bearing, lower coiling liner, bullet housing, upper coiling liner, metal wire, separation buster, bullet separate fuse, parachute arm-tie, fuze power supply switch, baffle ring, parachute;
The front end of vertical head spiral shell is real core cone structure, the outer, rear end of the vertical head spiral shell connected unit that extended back, and the end, rear end of vertical head spiral shell is processed with bearing mounting hole;
Lower coiling liner is the cylindrical member that an end has the end, and the end face that the end one end is arranged of lower coiling liner extends forward the bearing connected unit;
Upper coiling liner is the cylindrical member that an end has the end, and the outer that the end one end is arranged of upper coiling liner extends outward connected unit, and this bottom center has the buster installing hole;
The rear end that bullet separates fuse is designed with the fuze power supply switch that pulls open startup, and bullet separates the front end of fuse and draws the igniting signal output interface;
The bearing connected unit of lower coiling liner front end is installed in the bearing mounting hole of vertical head spiral shell rear end, and the bearing connected unit of lower coiling liner is connected by bearing with the bearing mounting hole of vertical head spiral shell; The connected unit that upper coiling liner is located by outer, its rear end is fixed on the leading portion of bullet enclosure interior, fixedly separated buster in the buster installing hole of substrate surface in the upper coiling; The rear end of the coiling liner bullet of packing into successively separates fuse, parachute arm-tie on the bullet enclosure interior; The ignition signal output interface that bullet separation fuse front end is drawn is connected with the firing circuit that separates buster, the fuze power supply switch that bullet separates the fuse rear end links to each other by the front end of stay cord with the parachute arm-tie, the bullet housing rear end inner wall of end baffle ring that is threaded, parachute is connected to the rear end of parachute arm-tie by the umbrella rope, and is folded in the bullet housing between parachute arm-tie and the baffle ring; The front end of bullet housing is connected by shear pin with the connected unit of vertical head spiral shell rear end, and the upper coiling liner of bullet enclosure interior is docked with the lower coiling liner of vertical head spiral shell inside; Metal wire one end is spirally wound on the sidewall of coiling liner and is fixed on the connected unit of coiling liner rear end, and the other end of metal wire is spirally wound on the sidewall of lower coiling liner and is fixed on the rear end of lower coiling liner;
The end, rear end of bullet cabin housing inwardly is processed with the screens ring, and all draw the end to end bullet cabin housing of putting into successively rocket projectile of thunder bullet, and places the bullet push pedal between the screens ring of the rear end of drawing the thunder bullet of rearmost end and bullet cabin housing;
The bullet buster is installed in the control cabinet housing from front to back successively, fuse opens the cabin; The firing circuit of bullet buster links to each other with the fuse ignition signal output interface that opens the cabin;
The front end of bullet cabin housing is connected by shear pin with blast cap, and the rear end of bullet cabin housing is threaded with the control cabinet housing, and the bullet buster of control cabinet enclosure interior front end and the bullet push pedal of enclosure interior rear end, bullet cabin are aligned; The open the cabin delayed startup circuit of fuse of control cabinet housing rear end connecting engine and stabilising arrangement, control cabinet enclosure interior rear end is connected with the igniter wire of engine interior front end.
The sidewall of bullet push pedal has the sealing ring mounting groove, and sealing ring is installed in bullet push pedal and housing junction, bullet cabin.
Bullet separates fuse and comprises height judge module, bookbinding module, gps satellite locating module, starts module;
The gps satellite locating module is measured in real time and is drawn the residing height above sea level of thunder bullet, and this height above sea level data transmission module is passed to the height judge module;
The bookbinding module receives the elevation information bookbinding, and this altitude information is transferred to the height judge module;
The height judge module stores bookbinding module height comparison information, and receive in real time the height above sea level information of gps satellite locating module, when judging the height comparison information of the satisfied bookbinding of the height above sea level information module that the gps satellite locating module imports in real time, send enabling signal to starting module;
Instant control point ignition circuit igniting after the enabling signal of startup module reception height judge module;
The bookbinding module links to each other with the height judge module by data wire respectively with the gps satellite locating module, and bookbinding module and gps satellite location are respectively to height judge module transmission elevation information; The height judge module links to each other with the startup module by data wire, and the height judge module sends enabling signal to starting module; Starting module is connected with the firing circuit wire that separates buster.
The course of work:
Before drawing the thunder rocket bomb transmitting, separate bookbinding module in the fuse to its bookbinding height comparison information by each bullet that draws the thunder bullet respectively, height value when namely subscribing vertical head spiral shell and separating with the bullet housing, the bookbinding module sends to the height judge module with the height comparison information, and the height judge module should the height comparison information be stored; Rocket projectile makes engine operation by igniter, makes the fuse that opens the cabin begin timing in the time of the igniter igniting; After the retardation time of fuse that opens the cabin finishes, to bullet buster output ignition signal, bullet is shed the snack made with traditional Chinese medicines fire and is detonated, the thunder bullet that draws that the powder gases that produces makes the bullet push pedal promote front end moves to rocket warhead section, blast cap is cut off with the shear pin that bullet cabin housing is connected, blast cap and bullet cabin housing are come off, draw the thunder bullet and from the housing of bullet cabin, dish out successively; Under the effect of air drag, the parachute of bullet housing rear end is opened after drawing the thunder bullet and being dished out, made and draw the thunder bullet and slow down to descend; Pulling moved up by the relative bullet housing of parachute arm-tie that the umbrella rope connects with its rear end when parachute was opened, and the baffle ring that is threaded by bullet housing rear end inner wall of end is to upper limit, the parachute arm-tie separates the fuze power supply switch of fuse rear end by stay cord pulling bullet in moving past journey, make bullet separate the electric power starting of fuse and start working;
Bullet separates the in real time measurement of gps satellite locating module of fuse and draws the residing height above sea level of thunder bullet, and with this height above sea level data transmission module pass to the height judge module, when the height judge module is judged the height comparison information of the satisfied bookbinding of the height above sea level information module that the gps satellite locating module imports in real time, send enabling signal to starting module; Immediately export ignition signal to the firing circuit that separates buster after the enabling signal of startup module reception height judge module, make separation buster ignition and detonation; Separate powder gases that buster produces through upper coiling liner and the effect of the lower coiling liner inner core rear end to vertical head spiral shell, cut off the shear pin that is connected between vertical head spiral shell and the bullet housing, realization vertical head spiral shell separates with the bullet housing; The two ends of metal wire respectively along upper coiling liner and the simultaneously spiral release of lower coiling liner, thereby implement to draw the thunder operation along with the rapid decline of vertical head spiral shell.
Beneficial effect
The present invention adopts the shrapnel structure to solve once to deliver at a distance and discharges a plurality of problems of drawing the thunder bullet, can in female bullet of long-distance flight a plurality of thunder bullets that draw be installed.
The present invention changes two-way unwrapping wire into by the unidirectional unwrapping wire that tradition is drawn in the thunder bullet, accelerates metal wire and removes the speed that spiral discharges, and has effectively alleviated the axial tension tension force that produces when drawing thunder bullet metal wire unwrapping wire; By between metal wire front end and vertical head spiral shell, introducing bearing, avoid metal wire to drive whole vertical head spiral shell High Rotation Speed, effectively alleviated the rotation tension force that produces when drawing thunder bullet unwrapping wire metal wire; Thereby reduced the possibility of metal wire fracture.
The time-delay fuze that the present invention uses in drawing the thunder bullet, abandoned the mentality of designing of passing through the Preset Time starting ignition in traditional fuse, to reach and subscribe height above sea level as the moment of output ignition signal, and solve by the flight time at all and calculated the technological difficulties that the error of ballistic ordinate can increase along with the increase of range.
Description of drawings
Fig. 1 draws the structural representation of thunder bullet for tradition;
Fig. 2 is the structural representation that primary-secondary type of the present invention draws the thunder rocket projectile;
Fig. 3 is that primary-secondary type of the present invention draws the structural representation that draws the thunder bullet in the thunder rocket projectile;
Fig. 4 is that primary-secondary type of the present invention draws and draws thunder bullet separation process schematic diagram in the thunder rocket projectile;
Fig. 5 is that primary-secondary type of the present invention draws the module diagram that thunder rocket projectile neutron bomb separates fuse;
Wherein, 1-blast cap; 2-bullet cabin housing; 3-control cabinet housing; The 4-engine; The 5-stabilising arrangement; 6 draw the thunder bullet; The push pedal of 7-bullet; 8-bullet buster; The 9-fuse that opens the cabin; The 10-igniter; 11-vertical head spiral shell; The 12-bearing; Liner winds the line under the 13-; 14-bullet housing; The upper coiling of 15-liner; The 16-metal wire; 17-separates buster; The 18-bullet separates fuse; 19-parachute arm-tie; The 20-bullet separates fuze switch; The 21-baffle ring; The 22-parachute.
The specific embodiment
Below in conjunction with drawings and Examples content of the present invention is further described.
Embodiment
A kind of primary-secondary type of the present invention draws the thunder rocket projectile, as shown in Figure 2, comprises blast cap 1, bullet cabin housing 2, control cabinet housing 3, engine 4, stabilising arrangement 5, draws thunder bullet 6, bullet push pedal 7, bullet buster 8, the fuse 9 that opens the cabin, igniter 10;
As shown in Figure 3, drawing thunder bullet 6 comprises vertical head spiral shell 11, bearing 12, lower coiling liner 13, bullet housing 14, upper coiling liner 15, metal wire 16, separates buster 17, bullet separation fuse 18, parachute arm-tie 19, fuze power supply switch 20, baffle ring 21, parachute 22;
The front end of vertical head spiral shell 11 is real core cone structure, the outer, rear end of the vertical head spiral shell connected unit that extended back, and the end, rear end of vertical head spiral shell is processed with bearing mounting hole;
The rear end that bullet separates fuse 18 is designed with the fuze power supply switch 20 that pulls open startup, and bullet separates the front end of fuse 18 and draws the igniting signal output interface;
The bearing connected unit of lower coiling liner 13 front ends is installed in the bearing mounting hole of vertical head spiral shell rear end, and the bearing connected unit of lower coiling liner is connected by bearing 12 with the bearing mounting hole of vertical head spiral shell; The connected unit that upper coiling liner 15 is located by outer, its rear end is fixed on the leading portion of bullet housing 14 inside, fixedly separated buster 17 in the buster installing hole of upper coiling liner 15 bottom surfaces; The rear ends of the inner upper coiling liners 15 of bullet housing 14 bullet of packing into successively separates fuse 18, parachute arm-tie 19; The ignition signal output interface that bullet separation fuse 18 front ends are drawn is connected with the firing circuit that separates buster 17, the fuze power supply switch 20 that bullet separates fuse 18 rear ends links to each other by the front end of stay cord with parachute arm-tie 19, the bullet housing 14 rear end inner wall of ends baffle ring 21 that is threaded, parachute 22 is connected to the rear end of parachute arm-tie 19 by the umbrella rope, and is folded in the bullet housing 14 between parachute arm-tie 19 and the baffle ring 21; The front end of bullet housing 14 is connected by shear pin with the connected unit of vertical head spiral shell 11 rear ends, and the upper coiling liner 15 of bullet housing 14 inside is docked with the lower coiling liner 13 of vertical head spiral shell 11 inside; Metal wire 16 1 ends are spirally wound on the sidewall of coiling liner 15 and are fixed on the coiling liner 15 rear end connected units, and the other end of metal wire is spirally wound on the sidewall of lower coiling liner 13 and is fixed on the rear end of lower coiling liner 13;
The end, rear end of bullet cabin housing 2 inwardly is processed with the screens ring, and all draw the end to end bullet cabin housing 2 of putting into successively rocket projectile of thunder bullet, and places bullet push pedal 7 between the screens ring of the rear end of drawing the thunder bullet of rearmost end and bullet cabin housing 2;
The front end of bullet cabin housing 2 is connected by shear pin with blast cap, and the rear end of bullet cabin housing 2 is threaded with control cabinet housing 3, and the bullet buster 8 of control cabinet housing 3 interior forward end and the bullet push pedal 7 of housing 2 inner rear ends, bullet cabin are aligned; The open the cabin delayed startup circuit of fuse 9 of control cabinet housing 3 rear end connecting engines 4 and stabilising arrangement 5, control cabinet housing 3 inner rear ends is connected with the igniter wire of engine 4 interior forward end.
The sidewall of bullet push pedal 7 has the sealing ring mounting groove, and bullet push pedal 7 is installed sealing ring with housing 2 junctions, bullet cabin.
Bullet separates fuse 18, as shown in Figure 5, comprises height judge module, bookbinding module, gps satellite locating module, starts module;
The gps satellite locating module is measured in real time and is drawn the residing height above sea level of thunder bullet, and this height above sea level data transmission module is passed to the height judge module;
The bookbinding module receives the elevation information bookbinding, and this altitude information is transferred to the height judge module;
The height judge module stores bookbinding module height comparison information, and receive in real time the height above sea level information of gps satellite locating module, when judging the height comparison information of the satisfied bookbinding of the height above sea level information module that the gps satellite locating module imports in real time, send enabling signal to starting module;
Instant control point ignition circuit igniting after the enabling signal of startup module reception height judge module;
The bookbinding module links to each other with the height judge module by data wire respectively with the gps satellite locating module, and bookbinding module and gps satellite location are respectively to height judge module transmission elevation information; The height judge module links to each other with the startup module by data wire, and the height judge module sends enabling signal to starting module; Starting module is connected with the firing circuit wire that separates buster 17.
The course of work:
Before drawing the thunder rocket bomb transmitting, separate bookbinding module in the fuse 18 to its bookbinding height comparison information by each bullet that draws thunder bullet 6 respectively, height value when namely subscribing vertical head spiral shell 11 and separating with bullet housing 14, the bookbinding module sends to the height judge module with the height comparison information, and the height judge module should the height comparison information be stored; Rocket projectile makes engine 4 work by igniter 10, makes the fuse 9 beginning timing of opening the cabin in the time of igniter 10 igniting; After fuse 9 time-delays of opening the cabin finish, to bullet buster 8 output ignition signals, bullet is shed the snack made with traditional Chinese medicines fire and is detonated, the thunder bullet 6 that draws that the powder gases that produces makes bullet push pedal 7 promote front end moves to rocket warhead section, blast cap 1 is cut off with the shear pin that bullet cabin housing 2 is connected, blast cap 1 and bullet cabin housing 2 are come off, draw the thunder bullet and from bullet cabin housing 2, dish out successively; Under the effect of air drag, the parachute 22 of bullet housing 14 rear ends is opened after drawing thunder bullet 6 and being dished out, made and draw thunder bullet 6 and slow down and descend; Pulling moved up by the parachute arm-tie 19 relative bullet housings 14 that the umbrella rope connects with its rear end when parachute 22 was opened, and the baffle ring 21 that is threaded by bullet housing 14 rear end inner wall of ends is to upper limit, parachute arm-tie 19 separates the fuze power supply switch 20 of fuse 18 rear ends by stay cord pulling bullet in moving past journey, make bullet separate the electric power starting of fuse 18 and start working;
Bullet separates the in real time measurement of gps satellite locating module of fuse 18 and draws the residing height above sea level of thunder bullet, and with this height above sea level data transmission module pass to the height judge module, when the height judge module is judged the height comparison information of the satisfied bookbinding of the height above sea level information module that the gps satellite locating module imports in real time, send enabling signal to starting module; Immediately export ignition signal to the firing circuit that separates buster 17 after the enabling signal of startup module reception height judge module, make separation buster 17 ignition and detonations; The powder gases upper coiling liner 15 of process that separation buster 17 produces and the 13 inner core effects of lower coiling liner are to the rear end of vertical head spiral shell 11, cut off the shear pin that is connected between vertical head spiral shell 11 and the bullet housing 14, realization vertical head spiral shell 11 separates with bullet housing 14, as shown in Figure 4; The two ends of metal wire 16 respectively along upper coiling liner 15 and simultaneously spiral release of lower coiling liner 13, thereby implement to draw the thunder operation along with the rapid decline of vertical head spiral shell.
Claims (2)
1. a primary-secondary type draws thunder rocket projectile bullet, it is characterized in that: comprise that vertical head spiral shell, bearing, lower coiling liner, bullet housing, upper coiling liner, metal wire, separation buster, bullet separate fuse, parachute arm-tie, fuze power supply switch, baffle ring, parachute;
The front end of vertical head spiral shell is real core cone structure, the outer, rear end of the vertical head spiral shell connected unit that extended back, and the end, rear end of vertical head spiral shell is processed with bearing mounting hole;
Lower coiling liner is the cylindrical member that an end has the end, and the end face that the end one end is arranged of lower coiling liner extends forward the bearing connected unit;
Upper coiling liner is the cylindrical member that an end has the end, and the outer that the end one end is arranged of upper coiling liner extends outward connected unit, and this bottom center has the buster installing hole;
The rear end that bullet separates fuse is designed with the fuze power supply switch that pulls open startup, and bullet separates the front end of fuse and draws the igniting signal output interface;
The bearing connected unit of lower coiling liner front end is installed in the bearing mounting hole of vertical head spiral shell rear end, and the bearing connected unit of lower coiling liner is connected by bearing with the bearing mounting hole of vertical head spiral shell; The connected unit that upper coiling liner is located by outer, its rear end is fixed on the leading portion of bullet enclosure interior, fixedly separated buster in the buster installing hole of substrate surface in the upper coiling; The rear end of the coiling liner bullet of packing into successively separates fuse, parachute arm-tie on the bullet enclosure interior; The ignition signal output interface that bullet separation fuse front end is drawn is connected with the firing circuit that separates buster, the fuze power supply switch that bullet separates the fuse rear end links to each other by the front end of stay cord with the parachute arm-tie, the bullet housing rear end inner wall of end baffle ring that is threaded, parachute is connected to the rear end of parachute arm-tie by the umbrella rope, and is folded in the bullet housing between parachute arm-tie and the baffle ring; The front end of bullet housing is connected by shear pin with the connected unit of vertical head spiral shell rear end, and the upper coiling liner of bullet enclosure interior is docked with the lower coiling liner of vertical head spiral shell inside; Metal wire one end is spirally wound on the sidewall of coiling liner and is fixed on the connected unit of coiling liner rear end, and the other end of metal wire is spirally wound on the sidewall of lower coiling liner and is fixed on the rear end of lower coiling liner.
2. a kind of primary-secondary type as claimed in claim 1 draws thunder rocket projectile bullet, it is characterized in that: bullet separates fuse and comprises height judge module, bookbinding module, gps satellite locating module, starts module;
The gps satellite locating module is measured in real time and is drawn the residing height above sea level of thunder bullet, and this height above sea level data transmission module is passed to the height judge module;
The bookbinding module receives the elevation information bookbinding, and this altitude information is transferred to the height judge module;
The height judge module stores bookbinding module height comparison information, and receive in real time the height above sea level information of gps satellite locating module, when judging the height comparison information of the satisfied bookbinding of the height above sea level information module that the gps satellite locating module imports in real time, send enabling signal to starting module;
Instant control point ignition circuit igniting after the enabling signal of startup module reception height judge module;
The bookbinding module links to each other with the height judge module by data wire respectively with the gps satellite locating module, and bookbinding module and gps satellite location are respectively to height judge module transmission elevation information; The height judge module links to each other with the startup module by data wire, and the height judge module sends enabling signal to starting module; Starting module is connected with the firing circuit wire that separates buster.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310337080.5A CN103363849B (en) | 2013-08-06 | 2013-08-06 | Dispenser type lightning triggering rocket bomb bullet |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201310337080.5A CN103363849B (en) | 2013-08-06 | 2013-08-06 | Dispenser type lightning triggering rocket bomb bullet |
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| CN103363849A true CN103363849A (en) | 2013-10-23 |
| CN103363849B CN103363849B (en) | 2015-05-20 |
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| CN201310337080.5A Active CN103363849B (en) | 2013-08-06 | 2013-08-06 | Dispenser type lightning triggering rocket bomb bullet |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111981916A (en) * | 2020-07-27 | 2020-11-24 | 晋西工业集团有限责任公司 | Lightning-triggering shrapnel capable of preventing bullet collision |
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| US3910189A (en) * | 1974-03-25 | 1975-10-07 | Us Air Force | Deployment of conductors into the atmosphere |
| US4653379A (en) * | 1983-07-06 | 1987-03-31 | Commissariat A L'energie Atomique | Filament deployment means |
| JP2003329400A (en) * | 2002-05-13 | 2003-11-19 | Nof Corp | Thunder inducing rocket |
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| CN101390484A (en) * | 2007-09-17 | 2009-03-25 | 王道洪 | Lightning attractor and method thereof |
| CN102878870A (en) * | 2012-10-24 | 2013-01-16 | 晋西工业集团有限责任公司 | Extinguishment shrapnel type rocket bomb |
| CN203385330U (en) * | 2013-08-06 | 2014-01-08 | 晋西工业集团有限责任公司 | Bullet of cluster type lightning attracting rocket bomb |
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Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3910189A (en) * | 1974-03-25 | 1975-10-07 | Us Air Force | Deployment of conductors into the atmosphere |
| US4653379A (en) * | 1983-07-06 | 1987-03-31 | Commissariat A L'energie Atomique | Filament deployment means |
| JP2003329400A (en) * | 2002-05-13 | 2003-11-19 | Nof Corp | Thunder inducing rocket |
| CN1982836A (en) * | 2005-12-13 | 2007-06-20 | 中国科学院寒区旱区环境与工程研究所 | Safety artificial detonating special rocket with parachuting unit |
| CN101390484A (en) * | 2007-09-17 | 2009-03-25 | 王道洪 | Lightning attractor and method thereof |
| CN102878870A (en) * | 2012-10-24 | 2013-01-16 | 晋西工业集团有限责任公司 | Extinguishment shrapnel type rocket bomb |
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| CN111981916A (en) * | 2020-07-27 | 2020-11-24 | 晋西工业集团有限责任公司 | Lightning-triggering shrapnel capable of preventing bullet collision |
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| Publication number | Publication date |
|---|---|
| CN103363849B (en) | 2015-05-20 |
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