CN201497435U - Rocket type ice slush blasting missile and launching device and system thereof - Google Patents
Rocket type ice slush blasting missile and launching device and system thereof Download PDFInfo
- Publication number
- CN201497435U CN201497435U CN2009201761659U CN200920176165U CN201497435U CN 201497435 U CN201497435 U CN 201497435U CN 2009201761659 U CN2009201761659 U CN 2009201761659U CN 200920176165 U CN200920176165 U CN 200920176165U CN 201497435 U CN201497435 U CN 201497435U
- Authority
- CN
- China
- Prior art keywords
- ice slush
- bomb
- transmitting tube
- bullet
- demolition
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Images
Landscapes
- Working Measures On Existing Buildindgs (AREA)
Abstract
The utility model relates to an ice slush blasting missile, which comprises a warhead (11), a fin (12) and a missile body connecting mechanism (13), wherein the warhead (11) comprises a blasting fuse (111), explosive (112) and a warhead casing (113). The fin (12) comprises a rocket launcher (121) and a stabilizer (122), a rocket engine (121) comprises a combustion chamber casing (1211), an igniter (1212), propellant (1213), a jet tube (1214) and an explosive baffle plate (1215), the stabilizer (122) comprises a guard ring (1221) and a tail wing (1222), and the missile connecting mechanism (13) comprises a warhead skirt (131), a fin skirt (132) and/or a pin (133). The rocket type ice slush blasting missile has the characteristics of highly-effectively, accurately, safety and conveniently casting the ice slush blasting missile on an ice slush for blasting in low cost.
Description
Technical field
The utility model relate to a kind of can in, remote rocket projectile and emitter and the system that delivers the bomb that is used for the explosion ice slush.In particular, the utility model relate to a kind of can be by a plurality of tube-launched, provide flying power by solid propellant rocket, in, deliver the rocket projectile of bomb of explosion ice slush and the method for designing and the technology of emitter and system thereof to target (district) at a distance.
Background technology
Ice flood is commonly called as ice raft, is the obvious hydrology phenomenon that goes up of river level that ice slush causes current generation resistance.Ice slush is gathered into ice berg or ice dam sometimes, causes water level to raise significantly, and final overbank or breach a dyke is called Ling Hong.Ice flood all might take place in the phase of being frozen in the winter time and the phase of constructing a canal in spring.Ice flood as the Yellow River, Heilungkiang, Song Hua River etc., takes place in the great river in the China north easily.
The natural conditions that produce ice flood depend on residing geographical position, river and river course form.At extremely frigid zones, the river flows to high latitude and the river course form is wide at the top and narrow at the bottom from low latitudes, and it is more that the opportunity of serious ice flood appears in the place of the crooked winding in river course.This is that epimere is early than hypomere when thawing because hypomere is early than epimere during river freezeup.And the thick epimere of ice sheet thickness hypomere is thin.After ice slush appears in the river course hypomere, stopped a part of upland water, increased channel storage, when ice-melt was constructed a canal, this part groove retaining sharply discharged, and Ling Feng occurred and transmitted downwards, and poly-more many more along Cheng Bingshui, icy mountain peak increases successively.When the frozen water propagates down stream of upstream, meet the place card ice of turning in narrower section or river course and form ice dam, upper pond level is increased.Ice flood seriously in not, is depended on the river course ice slush to the water level effect, only in the river course serious ice or ice dam appear usually and after, can cause that just water level rises suddenly, and causes serious Ling Hong.
The yellow river ice flood disaster is one of serious natural calamity in downstream, the Yellow River, in history once with frequent breach, be difficult to the control and famous.The Yellow River downstream channel is wide at the top and narrow at the bottom, and is crooked unbroken, and staggered face-off is led in dangerous section, control, and the section that forms ice berg, ice dam easily is more.
At present, the way commonly used of reply ice slush has: aircraft drop a bomb explosion, cannon bombardment explosion, manually go up ice slush and lay explosive blasting etc.
The aircraft explosion of dropping a bomb.Bomb single-shot explosive charge height, demolition effect is good, but employs aircraft, except that the cost consumption of aircraft itself, also need ground to demarcate ground cooperations such as indication bomb-release point, and the bomb-release zone resident needs to evacuate, and prevents miss bomb, near resident's injury causing, therefore, the drop a bomb cost of explosion of aircraft is high, and situation does not unless it is absolutely necessary generally adopt.
Cannon bombardment explosion.Though the cost of single-shot shell is relatively low, the explosive charge of single-shot shell is few, reaches the ice slush of several meters even tens meters at thickness, and explosive effect is not good, wants to reach the purpose of explosion ice slush, needs the shell of enormous amount.In addition, shell is mainly used in the target of bombardment more than tens even tens kilometers, and therefore, with the way of artillery bombardment explosion ice slush, benefit is not good.
The artificial ice slush of going up is laid explosive blasting.Be exactly that personnel climb up ice slush, and explosive is laid in perforating on ice slush, implemented the method for explosion, cost is relatively low, but some ice slush is to float on the surface, and along with water movement, and on the ice slush, ice slush is grown thickly, and personnel are difficult for stopping over, and personal security can not get ensureing.
Because above-mentioned situation, when arriving, the ice news of China need a kind of efficient, safety, the method for explosion ice slush cheaply.Except that the conventional method of above-mentioned three kinds of explosion ice slushes, at present, domestic patent or the report of not retrieving or see other relevant for the effective fragmentation method of river ice slush as yet.
The utility model content
The utility model proposes a kind of efficient height, security is good, operation and maintenance is convenient and cost is low rocket type ice slush demolition bomb and emitter and system.
According to a scheme of the present utility model, a kind of rocket type ice slush demolition bomb is provided, comprising: bullet, projectile tail, and bindiny mechanism, wherein:
Described bullet comprises: fuse, explosive, bullet housing;
Described projectile tail comprises: rocket engine, stabilizer;
Described rocket engine comprises: burning chamber shell, igniter, propellant, jet pipe, grate;
Described stabilizer comprises: guard ring, empennage;
Described bindiny mechanism comprises: bullet skirt, projectile tail skirt and/or pin;
Described bullet by body bindiny mechanism, is connected with projectile tail, forms rocket type ice slush demolition bomb.
According to a scheme of the present utility model, a kind of emitter is provided, comprising: base, support, transmitting tube, bomb retaining device, transmitting tube fixed mount, deflection adjuster, elevation-angle regulator, wherein:
Described transmitting tube fixed mount is fixed together a plurality of transmitting tubes, becomes as a whole;
Described base links to each other with support by the deflection adjuster, and described support links to each other with transmitting tube and transmitting tube fixed mount thereof by elevation-angle regulator, constitutes emitter.
According to a scheme of the present utility model, a kind of rocket type ice slush demolition bomb system is provided, comprising: rocket type ice slush demolition bomb, emitter and subsidiary body is characterized in that:
Described rocket type ice slush demolition bomb is made up of bullet, projectile tail and body bindiny mechanism thereof, wherein:
Described bullet comprises: fuse, explosive, bullet housing;
Described projectile tail comprises: rocket engine, stabilizer;
Described rocket engine comprises: burning chamber shell, igniter, propellant, jet pipe, grate,
Described stabilizer comprises: guard ring, empennage,
Described body bindiny mechanism comprises: bullet skirt, projectile tail skirt and/or pin,
Described bullet by body bindiny mechanism, is connected with projectile tail, forms rocket type ice slush demolition bomb;
Described emitter is made up of base, support, transmitting tube, bomb retaining device, transmitting tube fixed mount, direction regulator, elevation-angle regulator, wherein,
Described base links to each other with support by the deflection adjuster, and described support links to each other with transmitting tube and transmitting tube fixed mount thereof by elevation-angle regulator, constitutes emitter;
Described subsidiary body is made up of ignition lead, terminal box, long lead, control box etc., wherein:
Described ignition lead connects the igniter of rocket engine respectively, and is fixed on the described terminal box on the emitter, and described long lead then connects described terminal box and remote described control box, constitutes the ignition operation circuit of complete described ice slush demolition bomb.
In sum, rocket type ice slush demolition bomb of the present utility model, emitter and subsidiary body etc. have constituted the complete explosion ice slush system of a cover, the technology and the method for the explosion ice slush that this is a kind of efficient height, security is good, cost is low.Rocket type ice slush demolition bomb of the present utility model and emitter and system have following characteristics:
1. far firing range, power are big.Remote explosive-the bullet of delivering.Operating personnel are implementation and operation closely.In the explosion ice slush process of reality, range does not generally need too far away, only needs operating personnel to get final product outside the range of explosive, so on the one hand, can reduce the propellant requirement of engine, reduces cost; On the other hand, also effectively protect operating personnel and other people member's safety.
2. simple and practical.Adopt the solid propellant rocket boosting, that solid propellant rocket has is simple in structure, storage, use, characteristics such as easy to maintenance.
3. mobility is good.Whole system comprises: rocket type ice slush demolition bomb and emitter thereof, all can be vehicle-mounted, and whole system can be transported to suitable position, implement the work of explosion ice slush.
4. fire accuracy height.Because rocket type ice slush demolition bomb adopts transmitting tube (guide pipe) emission, therefore, rocket type ice slush demolition bomb initially just has a direction and a firing angle accurately on the one hand; On the other hand, because projectile tail has guard ring formula stabilizer, make rocket type ice slush demolition bomb, aloft in Fei Hang the process, can be along predetermined ballistic flight, it is not far to add range, make the fire accuracy of rocket type ice slush demolition bomb further improve, scatter further and reduce.
5. cheap.At rocket type ice slush demolition bomb and the emitter thereof described in the utility model, all adopt ripe designing technique, cheap material, processing technology, therefore, cost can reduce greatly.
Rocket type ice slush demolition bomb described in the utility model can be at a distance, efficiently, exactly, safely, easily, at low cost with explosive, be shipped to and implement explosion on the ice slush.
The utility model can also be used for the explosion to mining, various demolishing buildings, river barrier (as: barrier lake) etc. except being used for the explosion ice slush.
Description of drawings
Fig. 1 is the operation principle schematic diagram of rocket type ice slush demolition bomb and emitter and system;
Fig. 2 is an ice slush demolition bomb structural representation;
Fig. 3 is single jet pipe rocket motor structure schematic diagram;
Fig. 4 is an inclination multi nozzle rocket structural representation;
Fig. 5 is an empennage established angle structural representation;
Fig. 6 is a guard ring formula tail structure schematic diagram;
Fig. 7 is no guard ring tail structure schematic diagram;
Fig. 8 is the warhead structure schematic diagram;
Fig. 9 is the projectile tail structural representation;
Figure 10 is the emitter structural scheme of mechanism;
Figure 11 is ice slush demolition bomb and transmitting tube structural representation;
Figure 12 is the bomb retaining device structural representation;
The specific embodiment
Described design of the present utility model and technology, belong to a kind of in, remote uncontrolled missile.Continuous emission by the short time can form the ice slush target: the saturation attack of finite region, " carpet " formula.This equipment utilizes the emission of the rocket principle of reaction, Recoilless, and structure is light, uses flexibly.
Below with reference to accompanying drawings the utility model is described in detail.
As shown in Figure 1, be the rocket type ice slush demolition bomb that the utility model proposed and the operation principle schematic diagram of emitter and system thereof, ice slush demolition bomb (1), behind the ignition trigger, from transmitting tube (23), fly out, under the guide effect of the boosting of rocket engine (121) and transmitting tube (23),, fly to the ice slush target along destined trajectory.
As shown in the figure 2, be the structural representation of ice slush demolition bomb (1).Ice slush demolition bomb (1) is by bullet (11), projectile tail (12), and the body attaching parts (13) of bullet and projectile tail constitute.
Bullet
The bullet (11) of described ice slush demolition bomb (1) comprising: by fuse (111), explosive (112) and bullet housing (113).
The main effect of described bullet (11) is: when bullet (11), and when flight contacts ice slush latter stage, the explosive (112) in the contact fuze (111), initiation bomb head capsule body (113), explosion ice slush.
The kind of described fuse (111) is a lot, in the utility model, adopts and triggers regularly combination fuzes.The purpose of Cai Yonging is like this, and when bullet touched ice slush, contact fuze can be triggered, and causes explosive charge, the explosion ice slush; When bullet is not directly fallen on the ice slush, but when splashing in the other water of ice slush, if only adopt contact fuze, then the explosive in the bullet can not be initiated, and will become duds and stays in the water, becomes the hidden danger of safety in the future, for this type of situation, should adopt the fuse of delay or timing class, in the utility model, the fuse unification with this function is referred to as time fuze.In the utility model, preferably, adopt and trigger regularly combination fuzes.
In actual applications, there are many different types of bullets available, for example: howitzer, armor-piercing bullet, high explosive anti-tank cartridge, high-explosive plastic projectile, concrete piercing cartridge or the like.The blasting technique of bullet is a routine techniques, is not the emphasis of setting forth in the utility model, can consult relevant reference book and technical data.In actual applications, can directly propose concrete specification requirement, in ice slush demolition bomb described in the utility model (1), provide the choice criteria of principle:
1. energy is big: promptly the explosion energy of the explosive of unit mass is big, makes ice slush demolition bomb energy enough limited payload (entrained explosive charge), reaches the effect of the explosion ice slush of maximum.
2. efficient height: when warhead detonation, the energy of explosive has directionality.The energy of explosion is towards the direction of ice slush, but not towards other useless direction, that is, the design of the blasting energy of bullet explosive should have directionality and cumulative effect, with the effect that reaches fully, high efficiency energy utilizes.
3. cost is low: so-called cost is low to be a common requirement, also means to adopt conventional material and mature technique and technology as far as possible.
Projectile tail
As shown in Figure 2, the projectile tail (12) of described ice slush demolition bomb (1) comprising: by rocket engine (121) and stabilizer (122).
Described rocket engine (121) comprising: burning chamber shell (1211), igniter (1212), propellant (1213), jet pipe (1214) and grate (1215), as shown in Figure 3.
Described burning chamber shell (1211) is the apotheca of propellant (1213), also is the operating room (combustion chamber) of propellant (1213) burning.
Described igniter (1212) is a device of starting working at first of whole system work, it mainly acts on, and after the energising, igniter (1212) is lighted, the high-temperature fuel gas that is produced is further lighted propellant (1213), makes described rocket engine (121) start working.
Described propellant (1213) is the source of described ice slush demolition bomb (1) flying power.In the utility model, adopt solid propellant, therefore, in the utility model, described rocket engine may also be referred to as and is the solid propellant solid propellant rocket, or solid propellant rocket.There is multiple solid propellant available: double base propellant, modified double base propellant, composite propellant etc.In the utility model, preferably adopt double base propellant.
Shown in Fig. 3 and 4, described jet pipe (1214) adopts Laval nozzle, that is, the interior profile of jet pipe is to shrink earlier the profile of afterwards expanding, and gas mobile in jet pipe is: gas is compressed earlier, and then expanse, obtains acceleration.In theory, jet pipe is an energy conversion device, with the heat energy that high-temperature high-pressure fuel gas contained that the propellant (1213) that burns is produced, changes the kinetic energy of described ice slush demolition bomb (1) flight into through jet pipe (1214).
In the utility model, two kinds of jet pipes (1214) scheme is provided, therefore described ice slush demolition bomb (1) has two kinds of flying methods: rotation and non-rotating.Two kinds of schemes are described below:
First kind, single jet pipe scheme.Shown in left figure among Fig. 3, be the profile of single jet pipe rocket engine (121), right figure is the rearview of single jet pipe rocket engine (121) among Fig. 3.The rocket engine of this single nozzle structure (121) produces axial thrust to described ice slush demolition bomb (1).If there is not the effect of other mechanism, the body of described ice slush demolition bomb (1) will fly to predeterminated target along destined trajectory without any rotatably.
Second kind, the multi nozzle scheme.Shown in left figure among Fig. 4, be the profile of multi nozzle rocket (121), right figure is the rearview of multi nozzle rocket (121) among Fig. 4, these jet pipes are the jet pipes that tilt.The rocket engine (121) of the multi nozzle structure of this inclination except that producing axial thrust, also produces turning moment to described ice slush demolition bomb (1), causes the body of described ice slush demolition bomb (1), rotatably, flies to predeterminated target along destined trajectory.The rotation of body makes described ice slush demolition bomb (1), and skyborne flight is more stable, and trajectory and bomb-release point are more accurate.
In the utility model, preferably, adopt the multi nozzle design and the technical scheme that tilt.
Described grate (1215), be positioned between described jet pipe (1214) inlet and the described propellant (1213), it mainly acts on is to stop described propellant (1213), prevents that it is in combustion process, stop up described jet pipe (1214), guarantee described rocket engine (121) operate as normal.
Described rocket engine (121) be the power resources of described ice slush demolition bomb (1).After igniter (1212) igniting of described rocket engine (121), light propellant, the high-temperature high-pressure fuel gas that produces after the propellant combustion, after described jet pipe (1214) ejection, produce thrust, the described ice slush demolition bomb of boosting (1), the transmitting tube that flies out along destined trajectory, flies to target.
Described stabilizer (122) comprising: guard ring (1221) and empennage (1222).
As shown in Figure 7, the main effect of described empennage (1222) is to make ice slush demolition bomb (1) keep the stability of airflight, to guarantee the degree of accuracy of bomb-release point.
In the utility model, preferably recommend to adopt simple and easy and general subsonic speed empennage aerofoil profile, guarantee the stability of ice slush demolition bomb (1) flight and the degree of accuracy of bomb-release point on the one hand; On the other hand, reduce the operation of processing, reduce cost.The selection of the aerofoil profile of empennage is not the emphasis that the utility model is introduced, and does not just launch further elaboration here, and interesting technical staff can consult relevant books.
In the utility model, the established angle (1223) by described empennage (1222) has or not, and provides the stationary mode of two kinds of flights for described ice slush demolition bomb (1): rotary and non-rotating.
As shown in Figure 5, empennage established angle (1223) is the center line of empennage and the angle of ice slush demolition bomb (1) axis.
So-called no established angle, be that empennage established angle (1223) is when being zero, the state of flight of ice slush demolition bomb (1) is a non-rotating, be that ice slush demolition bomb (1) is in flight course, body does not rotate, guarantee the stable of ice slush demolition bomb (1) flight attitude by empennage, and the accuracy of trajectory and bomb-release point.
What is called has established angle, and promptly when empennage established angle (1223) was non-vanishing, the state of flight of ice slush demolition bomb (1) was rotary.Ice slush demolition bomb (1) is in flight course, and under the effect of empennage that established angle is arranged and air, missile rotation makes body in flight course, according to the flight of destined trajectory.Usually established angle is chosen as the several years, and concrete numerical value is determined according to parameters such as the full bullet quality of ice slush demolition bomb (1), aerodynamic characteristic, rocket engine thrusts.
Described guard ring (1221) shown in Fig. 6 and 7, in the utility model, proposes two kinds of designs and technical scheme: guard ring formula and no guard ring formula are arranged.
The guard ring formula is arranged.As shown in Figure 6, the top in empennage (1222) installs an endless belt type guard ring (1221) additional, and its effect is: protect empennage (1222) and play the centering effect, keep the bullet axle parallel with launcher-tube line when making described ice slush demolition bomb (1) emission.In addition, in processes such as ice slush demolition bomb (1) installation, carrying, also have effects such as frock.
No guard ring formula.As shown in Figure 7, the top in empennage (1222) is without any guard ring (1221); do not having under the situation of guard ring,, installing some safeguards additional usually on the top of empennage; equally also can reach two effects that guard ring (1221) is arranged, promptly protect empennage (1222) and play the centering effect.
Body bindiny mechanism
The body bindiny mechanism (13) of described ice slush demolition bomb (1) has dual mode usually: monoblock type and split interconnection system.So-called monoblock type is meant bullet and projectile tail in the processing process, and follow-up assembling, transport, use and process such as flight in be an integral body all the time; So-called split interconnection system is meant bullet and projectile tail in the processing process, and separate in the processes such as follow-up assembling and transportation, just before use, promptly just connect into before the emission as a whole, i.e. use preceding with flight course in be an integral body.In the utility model, adopt design of split interconnection system and technical scheme.Only introduced below with regard to the split interconnection system.
Shown in Fig. 8 and 9, the body bindiny mechanism (13) of described ice slush demolition bomb (1) comprising: bullet skirt (131) and projectile tail skirt (132), and pin (133) (not shown).
Described bullet skirt (131) is a cylindrical tube of bullet (11) tail end, and front end is connected with the bullet afterbody, and the rear end is processed with the mechanism that the projectile tail skirt links to each other, as shown in Figure 8.
Described projectile tail skirt (132) is a cylindrical tube of projectile tail (12) front end, and the rear end is connected with the projectile tail head, and front end is processed with the mechanism that the projectile tail skirt links to each other, as shown in Figure 9.
Described pin (133) is an alternate means, when bullet skirt (131) with after projectile tail skirt (132) is connected, with described pin (133) pinning, make it no longer to get loose.
In body described in the utility model bindiny mechanism, preferably, adopt the technology that is threaded, this technology maturity height, processing cost are low, good reliability, working service are convenient.
The effect of the body attaching parts (13) of described ice slush demolition bomb (1) is: make bullet (11) and projectile tail (12) connect into as a whole, and maintenance concentricity, make described ice slush demolition bomb (1) in flight course, according to destined trajectory flight, and hit exactly.
At last, the effect of described ice slush demolition bomb (1) is: after igniter (1212) igniting of described rocket engine (121), light propellant.The high-temperature high-pressure fuel gas that produces after the propellant combustion after described jet pipe (1214) ejection, produces thrust, the described ice slush demolition bomb of boosting (1), and the transmitting tube that flies out (231) along destined trajectory, flies to the target ice slush.When described ice slush demolition bomb (1) when contacting ice slush at last, contact fuze (111), the explosive (112) in the initiation bomb head capsule body (113), explosion ice slush.
Emitter
The emitter (2) of described ice slush demolition bomb (1) comprising: base (21), bearing (22), transmitting tube (23), bomb retaining device (231), transmitting tube fixed mount (24), deflection adjuster (25), elevation-angle regulator (26), as shown in figure 10.
Described base (21) is the pedestal of whole emitter, plays the effect of maintenance and stable whole system.The more thick and heavy metal material of general normal employing is made, and guarantees the stability to whole system.
Described bearing (22) is for standing on the base, and each parts above supporting as transmitting tube (23), reach transmitting tube fixed mount (24) etc.This support requires to have certain weight, to guarantee the stability of system, also requires to have certain intensity simultaneously, can support above-mentioned each parts.
Described transmitting tube (23) is an inner wall smooth, and has the pipe of certain-length, and its length requirement is slightly larger than the full bullet length of described ice slush demolition bomb (1), as shown in figure 11.The main effect of transmitting tube (23) is that the emission to described ice slush demolition bomb (1) has guide effect, therefore in some reference book and technical data, also is known as guide pipe or oriented tube, title difference but principle is identical, in the utility model,, be called transmitting tube for narrating simple unification.
8 curved arrangement modes of transmitting tube shown in Figure 10 shown in 10, only illustrate in the drawings, are not the number and the arrangement mode of explanation transmitting tube, only limit to this a kind of mode shown in Figure 10.The various arrangement modes of the number of transmitting tube from single to a plurality of all belong to protection domain of the present utility model.Therefore, for setting forth succinct cause, in the utility model, when mentioning transmitting tube (23), both can be single transmitting tube, also can be a plurality of transmitting tubes.In actual use, described ice slush demolition bomb (1) both can be launched by single-shot, also can volley by pilosity.
As shown in figure 11, the tail end design at transmitting tube has bomb retaining device (231).The effect of bomb retaining device (231) is, because transmitting tube is the smooth pipe of internal face, and described ice slush demolition bomb (1) is when emission state, the front end of transmitting tube (23) is higher than the rear end, under the gravity effect, and described ice slush demolition bomb (1), may be downwards, skid off from transmitting tube (23), therefore, design bomb retaining device (231) especially and skid off to prevent described ice slush demolition bomb (1).Simultaneously, as shown in figure 12, also leave through hole at the center of bomb retaining device (231), when making rocket engine (121) work, the high temperature wake flame of generation is discharged from through hole, prevents high temperature wake flame ablation transmitting tube (23) and bomb retaining device (231).
In addition, front end at transmitting tube also is provided with a bomb retaining device, prevent when the described ice slush demolition bomb of filling (1) in described transmitting tube (23), described ice slush demolition bomb (1) skids off from the front end of transmitting tube (231), the bomb retaining device of this transmitting tube front end (231) is before ice slush demolition bomb (1) emission, need open, make ice slush demolition bomb (1) from transmitting tube (23), to fly out.
Described transmitting tube fixed mount (24) is for to be fixed together a plurality of transmitting tubes, and forms a device of an integral body, makes each transmitting tube adjusting, in the process at the angle of departure and the elevation angle, keep consistency, as shown in figure 10,
Described deflection adjuster (25) requires transmitting tube and transmitting tube fixed mount (24) thereof to rotate by 360 degree for adjusting and control a mechanism of described ice slush demolition bomb (1) transmit direction.In the utility model, preferably, the deflection adjuster is arranged on the junction (not shown) of base (21) and bearing (22), this is a mature technology, many jammers and crane all have similar techniques, are not repeated at this.
Described elevation-angle regulator (26) requires the adjusting at the elevation angle for adjusting and control a mechanism of described ice slush demolition bomb (1) launching elevation, can be adjustable from zero degree to 90 degree, as shown in figure 10.
Subsidiary body
In the utility model, be protection operating personnel's safety, remote electric ignition mode is adopted in the igniting of rocket engine (121), both can remote wired electric ignition, also can the long-distance wireless remote control igniting.In the utility model, preferably adopt remote wired electric ignition mode, the security of this mode is good, the reliability height.After transmitting tube is advanced in described ice slush demolition bomb (1) filling, harness is drawn, be connected on the terminal box, in the utility model, preferably described terminal box is fixed on the emitter, adopt long lead that terminal box is linked to each other with remote control box again, ignition signal is provided by remote control box.Design like this, on the one hand, operating personnel can remote-controlled operation, guarantees operating personnel's safety; On the other hand, after described ice slush demolition bomb (1) emission, ignition lead all is torn, and this is inevitably, and the long lead that connects terminal box and control box is then intact, can reduce cost.
In sum, the use operating procedure of ice slush demolition bomb described in the utility model is as follows:
The first step shoots: with transmitting tube adjust to level at an angle, be adjusted to zero degree usually so that shoot, adopt manually to shoot, and can repeat filling.The ice slush demolition bomb is loaded in the transmitting tube, close the bomb retaining device of transmitting tube tail end, from the front end of transmitting tube nosefuze is installed again, the ignition lead of rocket engine is linked to each other with auxiliary body, launches in order to igniting.
Second step calibration: adjust the elevation angle and the azimuth of transmitting tube group,, bomb-release point is adjusted to the target area according to pre-designed trajectory.
The emission of the 3rd step: switching on the ignition circuit, rocket engine is started working, boosting ice slush demolition bomb, the transmitting tube that flies out, the ballistic trajectory along predetermined flies to target.
The technical scheme of the ice slush demolition bomb that is adopted according to explosion ice slush of the present utility model is compared with other technical scheme, has following advantage:
1. power is big.Can throw several kilograms to up to a hundred kilograms explosive, both can launch by single-shot, also can multiple launch,, implement spreadability and bomb the limited zone of a slice.
2. security is good.Middle distance is delivered explosive.Operating personnel are implementation and operation closely.In the explosion ice slush process of reality, range does not generally need too far away, only needs operating personnel to get final product outside the range of explosive, so on the one hand, effectively protects operating personnel and other people member's safety; On the other hand, also can reduce the propellant requirement of engine, reduce cost.
2. simple and practical.Adopt the solid propellant rocket boosting, that solid propellant rocket has is simple in structure, storage, use, characteristics such as easy to maintenance.
3. mobility is good.Whole system comprises: rocket type ice slush demolition bomb and emitter thereof, all can be vehicle-mounted, and whole system can be transported to suitable position, implement the work of explosion ice slush.
4. fire accuracy height.On the one hand, owing to adopt the transmitting tube emission, therefore, rocket type ice slush demolition bomb initially just has a direction and a firing angle accurately; On the other hand, because projectile tail has guard ring formula stabilizer, make rocket type ice slush demolition bomb, aloft in Fei Hang the process, can be along predetermined ballistic flight, it is not far to add range, make the fire accuracy of rocket type ice slush demolition bomb further improve, scatter further and reduce.
5. cheap.At rocket type ice slush demolition bomb and the emitter thereof described in the utility model, all adopt ripe designing technique, cheap material, processing technology, therefore, cost can reduce greatly.
Rocket type ice slush demolition bomb described in the utility model can be at a distance, efficiently, exactly, safely, easily, at low cost with explosive, be shipped to and implement explosion on the ice slush.
The above is a preferred embodiment of the present utility model only, is not limited to the utility model, and for a person skilled in the art, the utility model can have various changes and variation.All within spirit of the present utility model and principle, any modification of being done, be equal to replacement, improvement etc., all should be included within the claim scope of the present utility model.
Claims (10)
1. ice slush demolition bomb comprises: bullet (11), projectile tail (12) and body bindiny mechanism (13), wherein:
Described bullet (11) comprising: fuse (111), explosive (112), bullet housing (113);
Described projectile tail (12) comprising: rocket engine (121), stabilizer (122);
Described rocket engine (121) comprising: burning chamber shell (1211), igniter (1212), propellant (1213), jet pipe (1214), grate (1215);
Described stabilizer (122) comprising: guard ring (1221), empennage (1222);
Described body bindiny mechanism (13) comprising: bullet skirt (131), projectile tail skirt (132) and/or pin (133).
2. ice slush demolition bomb as claimed in claim 1, wherein,
Described fuse (111) is for triggering regularly combination fuzes.
3. ice slush demolition bomb as claimed in claim 1, wherein:
Described propellant (1213) is a solid propellant.
4. ice slush demolition bomb as claimed in claim 1 is characterized in that:
Described stabilizer (122) is for one of following two kinds: the guard ring formula is arranged or do not have the guard ring formula.
5. ice slush demolition bomb as claimed in claim 1, wherein:
Described empennage (1222) is for one of following two kinds: established angle is arranged or do not have established angle.
6. ice slush demolition bomb as claimed in claim 1 is characterized in that:
The jet pipe of described rocket engine (1214) type is one of following two kinds: a plurality of jet pipes of single jet pipe or inclination.
7. ice slush demolition bomb according to claim 1 is characterized in that:
Described body bindiny mechanism (13) adopts split interconnection system structure.
8. the emitter of an ice slush demolition bomb comprises: base (21), bearing (22), transmitting tube (23), bomb retaining device (231), transmitting tube fixed mount (24), deflection adjuster (25), elevation-angle regulator (26), wherein:
Described base (21) links to each other with bearing (22) by deflection adjuster (25), and bearing (22) can rotate by 360 degree with respect to base (21);
Described transmitting tube fixed mount (24), the transmitting tube of multi-joint dress layout is fixed together, and links to each other transmitting tube (23) and transmitting tube fixed mount (24) with bearing (22) top by elevation-angle regulator (26), can do 0 and spend with respect to bearing (22) to the pitching of 90 degree;
Described transmitting tube (23) is to the control of leading of ice slush demolition bomb;
Described bomb retaining device (231) is installed on transmitting tube (23) tail end and/or front end; And,
Described ice slush demolition bomb (1) comprising: bullet (11), projectile tail (12) and body bindiny mechanism (13); Wherein:
Described bullet (11) comprising: fuse (111), explosive (112), bullet housing (113);
Described projectile tail (12) comprising: rocket engine (121), stabilizer (122);
Described rocket engine (121) comprising: burning chamber shell (1211), igniter (1212), propellant (1213), jet pipe (1214), grate (1215);
Described stabilizer (122) comprising: guard ring (1221), empennage (1222);
Described body bindiny mechanism (13) comprising: bullet skirt (131), projectile tail skirt (132) and/or pin (133).
9. ice slush demolition bomb emitter according to claim 8 (2), wherein:
Described transmitting tube (23) layout can be following both one of: single and a plurality of.
10. the system of an ice slush demolition bomb, comprising: ice slush demolition bomb (1), emitter (2) and subsidiary body (3) is characterized in that:
Described ice slush demolition bomb (1) is made of bullet (11), projectile tail (12) and body bindiny mechanism (13), wherein:
Described bullet (11) comprising: fuse (111), explosive (112), bullet housing (113);
Described projectile tail (12) comprising: rocket engine (121), stabilizer (122);
Described rocket engine (121) comprising: burning chamber shell (1211), igniter (1212), propellant (1213), jet pipe (1214), grate (1215);
Described stabilizer (122) comprising: guard ring (1221), empennage (1222);
Described body bindiny mechanism (13) comprising: bullet skirt (131), projectile tail skirt (132) and/or pin (133); And,
Described emitter (2) comprising: base (21), bearing (22), transmitting tube (23), bomb retaining device (231), transmitting tube fixed mount (24), deflection adjuster (25), elevation-angle regulator (26), wherein:
Described base (21) links to each other with bearing (22) by deflection adjuster (25), and bearing (22) can rotate by 360 degree with respect to base (21);
Described transmitting tube fixed mount (24), the transmitting tube (23) of multi-joint dress layout is fixed together, and links to each other transmitting tube (23) and transmitting tube fixed mount (24) with bearing (22) top by elevation-angle regulator (26), can do 0 and spend with respect to bearing (22) to the pitching of 90 degree;
Described transmitting tube (23) is to the control of leading of ice slush demolition bomb;
Described bomb retaining device (231) is installed on transmitting tube (23) front end and tail end; And,
Described ice slush demolition bomb (1) comprising: bullet (11), projectile tail (12) and body bindiny mechanism (13); Wherein:
Described bullet (11) comprising: fuse (111), explosive (112), bullet housing (113);
Described projectile tail (12) comprising: rocket engine (121), stabilizer (122);
Described rocket engine (121) comprising: burning chamber shell (1211), igniter (1212), propellant (1213), jet pipe (1214), grate (1215);
Described stabilizer (122) comprising: guard ring (1221), empennage (1222);
Described body bindiny mechanism (13) comprising: bullet skirt (131), projectile tail skirt (132) and/or pin (133); And,
Described subsidiary body (3) comprising: harness, terminal box, long lead and control box, it is characterized in that: described harness, be used to connect igniter and the terminal box that is installed on the emitter on the rocket engine, described long lead is used to connect remote control box and described terminal box.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009201761659U CN201497435U (en) | 2009-09-08 | 2009-09-08 | Rocket type ice slush blasting missile and launching device and system thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009201761659U CN201497435U (en) | 2009-09-08 | 2009-09-08 | Rocket type ice slush blasting missile and launching device and system thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201497435U true CN201497435U (en) | 2010-06-02 |
Family
ID=42440640
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009201761659U Expired - Fee Related CN201497435U (en) | 2009-09-08 | 2009-09-08 | Rocket type ice slush blasting missile and launching device and system thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201497435U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101915182A (en) * | 2010-06-09 | 2010-12-15 | 北京航空航天大学 | Solid-propellant rocket engine |
| CN107741174A (en) * | 2017-10-24 | 2018-02-27 | 江苏永丰机械有限责任公司 | Bullet sprays integral type recoilless gun |
| CN109403919A (en) * | 2017-08-15 | 2019-03-01 | 中国石油化工股份有限公司 | A kind of the pitching sphere and method of acceleration whereabouts |
| CN110906806A (en) * | 2019-11-17 | 2020-03-24 | 长沙深蓝未来智能技术有限公司 | Outer trajectory end-segment bottom explosion speed-increasing penetration armor-piercing bullet |
| CN113790633A (en) * | 2021-09-24 | 2021-12-14 | 哈尔滨工程大学 | Launching device and method for breaking ice under ice |
-
2009
- 2009-09-08 CN CN2009201761659U patent/CN201497435U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101915182A (en) * | 2010-06-09 | 2010-12-15 | 北京航空航天大学 | Solid-propellant rocket engine |
| CN101915182B (en) * | 2010-06-09 | 2013-05-22 | 北京航空航天大学 | Solid-propellant rocket engine |
| CN109403919A (en) * | 2017-08-15 | 2019-03-01 | 中国石油化工股份有限公司 | A kind of the pitching sphere and method of acceleration whereabouts |
| CN107741174A (en) * | 2017-10-24 | 2018-02-27 | 江苏永丰机械有限责任公司 | Bullet sprays integral type recoilless gun |
| CN110906806A (en) * | 2019-11-17 | 2020-03-24 | 长沙深蓝未来智能技术有限公司 | Outer trajectory end-segment bottom explosion speed-increasing penetration armor-piercing bullet |
| CN113790633A (en) * | 2021-09-24 | 2021-12-14 | 哈尔滨工程大学 | Launching device and method for breaking ice under ice |
| CN113790633B (en) * | 2021-09-24 | 2022-12-13 | 哈尔滨工程大学 | Launching device and method for breaking ice under ice |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| RU2362962C1 (en) | "tverityanka" splinter-in-beam supercaliber grenade | |
| RU2247922C2 (en) | False target | |
| US20040244628A1 (en) | Projectile for radially deploying sub-projectiles | |
| CN201497435U (en) | Rocket type ice slush blasting missile and launching device and system thereof | |
| US9494393B1 (en) | Low foreign object damage (FOD) weighted nose decoy flare | |
| CN201181193Y (en) | Extinguishment rocket ammunition capable of spin stabilization, emitting set and system | |
| CN110906806A (en) | Outer trajectory end-segment bottom explosion speed-increasing penetration armor-piercing bullet | |
| CN102032845B (en) | Portable mobile launch type ice slush blaster and ice slush blasting method | |
| CN110044213A (en) | Mine sweeping device | |
| RU2407982C1 (en) | Smoke ammunition | |
| RU128309U1 (en) | TANK CASSETTE UNLOADED CHARGER "TSNA" WITH AIR AND IMPACT EXPLOSION OF SUBSNARIES | |
| RU2158408C1 (en) | Method and device (ammunition) for destruction of ground and air targets | |
| CN201876201U (en) | Portable flexibly-launched ice blaster | |
| KR101609507B1 (en) | Range Extension Form Ramjet Propelled Shell | |
| CN209027377U (en) | A kind of shock trigger type increasing anti-riot rifle grenade of journey | |
| US5363766A (en) | Remjet powered, armor piercing, high explosive projectile | |
| JP6572007B2 (en) | Missile defense system and method | |
| CN202432932U (en) | Magazine and rocket projectile integration mineral rocket projectile | |
| RU2441193C1 (en) | Separating high-explosive fragmentation warhead of volley fire rocket system | |
| RU2705677C2 (en) | Pyrotechnic cartridge for precipitation stimulation | |
| RU2620694C1 (en) | Multiple-warhead rocket for impact on clouds | |
| RU2095739C1 (en) | Fragmentation shell | |
| RU2296944C1 (en) | Projectile-setter of false radar target | |
| RU2108537C1 (en) | Kinetic-action anti-tank missile | |
| US3358603A (en) | Ultra-sonic self-propelled projectile having high l/d ratio |
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: 20100602 Termination date: 20130908 |