CN203385330U - Bullet of cluster type lightning attracting rocket bomb - Google Patents
Bullet of cluster type lightning attracting rocket bomb Download PDFInfo
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- CN203385330U CN203385330U CN201320474333.9U CN201320474333U CN203385330U CN 203385330 U CN203385330 U CN 203385330U CN 201320474333 U CN201320474333 U CN 201320474333U CN 203385330 U CN203385330 U CN 203385330U
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Abstract
The utility model relates to a bullet of a cluster type lightning attracting rocket bomb, and belongs to the technical field of bombs and rockets. According to the bullet of the cluster type lightning attracting rocket bomb, a cluster bomb structure is adopted, so that the problems of remotely casting and releasing a plurality of lightning attracting bullets at one time are solved. Single-directional line release of a traditional lightning attracting bomb is changed into bi-directional line release, so that the speed of relieving metal line spiral release is increased, and axial tension tensile stress generated when a metal line of the lightning attracting bomb is released is effectively relieved. A bearing is additionally arranged between the front end of the metal line and a lead nutation screw, so that the situation that the metal line drives the whole lead nutation screw to rotate at high speed is avoided, rotation tensile stress generated when the metal line of the lightning attracting bullet is released is effectively relieved, and then the possibility that the metal line is cracked is reduced. According to the bullet of the cluster type lightning attracting rocket bomb, the moment when a preset altitude is reached is used as the moment when a delay fuze outputs an ignition signal, the delay fuze is applied to the lightning attracting rocket bomb, and therefore the technical problem that errors of the height of a trajectory increase along with the increase of the firing range is fundamentally solved, wherein the height is calculated according to flight time.
Description
Technical field
The utility model relates to a kind of primary-secondary type and draws thunder rocket projectile bullet, belongs to and plays the 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 as shown in Figure 1, comprises coiling liner, metal wire, vertical head spiral shell, separates buster and time delays fuse; Metal wire one end is spirally wound in coiling and is lining with, and the other end directly is fixed on vertical head spiral shell rear end.After pellet injection, through the time delays retardation time of fuse, start to separate buster, make vertical head spiral shell and bullet body portion from; When vertical head spiral shell traction metal wire descends, metal wire discharges along coiling liner one-way spiral, completes 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 while 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 3 vertical head spiral shell tractions are wrapped in the metal wire decline be lining with in 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, make metal bear 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 distance overhead when casting aside parachute and discharging metal wire, there is the larger conversion error by delay time and flying speed reduced height during the operation of single-shot bullet, release a parachute, discharge the height of line uniformity during multiple bullet operation poor.
The utility model content
The purpose of this utility model is will solve tradition to 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 provides a kind of primary-secondary type to draw thunder rocket projectile bullet.
The purpose of this utility model is achieved through the following technical solutions:
A kind of primary-secondary type of the present utility model 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 arranged 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; Upper coiling liner is fixed on the leading portion of bullet enclosure interior by the connected unit at place, outer, its rear end, fixedly separated buster in the buster installing hole of substrate surface in upper coiling; On the bullet enclosure interior, the rear end of the coiling liner bullet of packing into successively separates fuse, parachute arm-tie; 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 is connected with the front end of parachute arm-tie by stay cord, 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 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, allly draws 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 is connected 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; Control cabinet housing rear end connecting engine and stabilising arrangement, the open the cabin delayed startup circuit of fuse of 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 and is drawn the residing height above sea level of thunder bullet in real time, 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 the height above sea level information that judgement gps satellite locating module imports in real time meets the height comparison information of bookbinding module, to starting module, send enabling signal;
Instant control point ignition circuit igniting after the enabling signal of startup module reception height judge module;
The bookbinding module is connected 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 is connected 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, the bullet that draws the thunder bullet by each respectively separates bookbinding module in fuse to its bookbinding height comparison information, height value when subscribing vertical head spiral shell and separating with the bullet housing, the bookbinding module sends to the height judge module by the height comparison information, and the height judge module is stored this height comparison information; Rocket projectile makes engine operation by igniter, and the fuse that makes to open the cabin in the time of the igniter igniting starts timing; 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 produced 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 dish out from the housing of bullet cabin successively; Draw the thunder bullet by after dishing out under the effect of air drag, the parachute of bullet housing rear end is opened, make to draw the thunder bullet and slow down to descend; When opening, parachute pull the relative bullet housing of parachute arm-tie connected by the umbrella rope with its rear end to move up, and the baffle ring be threaded by bullet housing rear end inner wall of end is to upper limit, the parachute arm-tie pulls bullet to separate the fuze power supply switch of fuse rear end by stay cord upper in moving past journey, makes bullet separate the electric power starting of fuse and start working;
Bullet separates the gps satellite locating module of fuse and measures and draw the residing height above sea level of thunder bullet in real time, and this height above sea level data transmission module is passed to the height judge module, when the height judge module judges 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, to starting module, send enabling signal; Immediately export ignition signal to the firing circuit that separates buster after the enabling signal of startup module reception height judge module, make to separate the buster ignition and detonation; Separate powder gases that buster produces through upper coiling liner and the effect of lower coiling liner inner core the rear end to vertical head spiral shell, cut off the shear pin be connected between vertical head spiral shell and bullet housing, realize separating of vertical head spiral shell and bullet housing; The thunder operation, along with the rapid decline of vertical head spiral shell, respectively along upper coiling liner and the spiral release simultaneously of lower coiling liner, thereby is implemented to draw in the two ends of metal wire.
Beneficial effect
The utility model adopts the shrapnel structure to solve and once delivers at a distance and discharge 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 utility model changes two-way unwrapping wire into by unidirectional unwrapping wire tradition drawn in the thunder bullet, accelerates metal wire and removes the speed that spiral discharges, and has effectively alleviated the axial tension tension force produced while 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 produced while drawing thunder bullet unwrapping wire metal wire; Thereby reduced the possibility of metal wire fracture.
The time-delay fuze that the utility model is applied in drawing the thunder bullet, abandoned in traditional fuse by the mentality of designing of Preset Time starting ignition, to reach and subscribe the moment of height above sea level as the output ignition signal, and solve at all and calculated the technological difficulties that the error of ballistic ordinate can increase along with the increase of range by the flight time.
The accompanying drawing explanation
Fig. 1 is traditional structural representation that draws the thunder bullet;
Fig. 2 is the structural representation that the utility model primary-secondary type draws the thunder rocket projectile;
Fig. 3 is that the utility model primary-secondary type draws the structural representation that draws the thunder bullet in the thunder rocket projectile;
Fig. 4 is that the utility model primary-secondary type draws in the thunder rocket projectile and draws thunder bullet separation process schematic diagram;
Fig. 5 is that the utility model primary-secondary type 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 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 utility model is further described.
Embodiment
A kind of primary-secondary type of the present utility model 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 arranged 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; Upper coiling liner 15 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 by the connected unit at place, outer, its rear end; 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 is connected with the front end of parachute arm-tie 19 by stay cord, 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 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 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, allly draws 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;
Bullet buster 8 is installed in control cabinet housing 3 from front to back successively, fuse 9 opens the cabin; The firing circuit of bullet buster 8 is connected with the fuse 9 ignition signal output interfaces that open the cabin;
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; Control cabinet housing 3 rear end connecting engines 4 and stabilising arrangement 5, the open the cabin delayed startup circuit of fuse 9 of the inner rear end of control cabinet housing 3 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 bullet cabin housing 2 junctions.
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 and is drawn the residing height above sea level of thunder bullet in real time, 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 the height above sea level information that judgement gps satellite locating module imports in real time meets the height comparison information of bookbinding module, to starting module, send enabling signal;
Instant control point ignition circuit igniting after the enabling signal of startup module reception height judge module;
The bookbinding module is connected 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 is connected 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, the bullet that draws thunder bullet 6 by each respectively separates bookbinding module in fuse 18 to its bookbinding height comparison information, height value when subscribing vertical head spiral shell 11 and separating with bullet housing 14, the bookbinding module sends to the height judge module by the height comparison information, and the height judge module is stored this height comparison information; Rocket projectile makes engine 4 work by igniter 10, and the fuse 9 that makes to open the cabin in the time of igniter 10 igniting starts timing; 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 produced 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 dish out from bullet cabin housing 2 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 to draw thunder bullet 6 and slow down and descend; Parachute 22 pulls the relative bullet housing 14 of parachute arm-tie 19 connected by the umbrella rope with its rear end to move up when opening, and the baffle ring 21 be threaded by bullet housing 14 rear end inner wall of ends is to upper limit, parachute arm-tie 19 pulls bullet to separate the fuze power supply switch 20 of fuse 18 rear ends by stay cord upper in moving past journey, makes bullet separate the electric power starting of fuse 18 and start working;
Bullet separates the gps satellite locating module of fuse 18 and measures and draw the residing height above sea level of thunder bullet in real time, and this height above sea level data transmission module is passed to the height judge module, when the height judge module judges 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, to starting module, send enabling signal; Immediately export ignition signal to the firing circuit that separates buster 17 after the enabling signal of startup module reception height judge module, make to separate 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 be connected between vertical head spiral shell 11 and bullet housing 14, realize separating of vertical head spiral shell 11 and bullet housing 14, as shown in Figure 4; The thunder operation, along with the rapid decline of vertical head spiral shell, respectively along upper coiling liner 15 and lower coiling liner 13 spiral release simultaneously, thereby is implemented to draw in the two ends of metal wire 16.
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 arranged 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; Upper coiling liner is fixed on the leading portion of bullet enclosure interior by the connected unit at place, outer, its rear end, fixedly separated buster in the buster installing hole of substrate surface in upper coiling; On the bullet enclosure interior, the rear end of the coiling liner bullet of packing into successively separates fuse, parachute arm-tie; 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 is connected with the front end of parachute arm-tie by stay cord, 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 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 and is drawn the residing height above sea level of thunder bullet in real time, 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 the height above sea level information that judgement gps satellite locating module imports in real time meets the height comparison information of bookbinding module, to starting module, send enabling signal;
Instant control point ignition circuit igniting after the enabling signal of startup module reception height judge module;
The bookbinding module is connected 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 is connected 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 |
|---|---|---|---|
| CN201320474333.9U CN203385330U (en) | 2013-08-06 | 2013-08-06 | Bullet of cluster type lightning attracting rocket bomb |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320474333.9U CN203385330U (en) | 2013-08-06 | 2013-08-06 | Bullet of cluster type lightning attracting rocket bomb |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203385330U true CN203385330U (en) | 2014-01-08 |
Family
ID=49873808
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320474333.9U Withdrawn - After Issue CN203385330U (en) | 2013-08-06 | 2013-08-06 | Bullet of cluster type lightning attracting rocket bomb |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203385330U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103363849A (en) * | 2013-08-06 | 2013-10-23 | 晋西工业集团有限责任公司 | Dispenser type lightning triggering rocket bomb bullet |
| CN108110434A (en) * | 2017-12-16 | 2018-06-01 | 贵州航天电子科技有限公司 | A kind of answer signal decay cover |
-
2013
- 2013-08-06 CN CN201320474333.9U patent/CN203385330U/en not_active Withdrawn - After Issue
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103363849A (en) * | 2013-08-06 | 2013-10-23 | 晋西工业集团有限责任公司 | Dispenser type lightning triggering rocket bomb bullet |
| CN103363849B (en) * | 2013-08-06 | 2015-05-20 | 晋西工业集团有限责任公司 | Dispenser type lightning triggering rocket bomb bullet |
| CN108110434A (en) * | 2017-12-16 | 2018-06-01 | 贵州航天电子科技有限公司 | A kind of answer signal decay cover |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20140108 Effective date of abandoning: 20150520 |
|
| RGAV | Abandon patent right to avoid regrant |