CN113587748A - High-reliability artillery artificial hail-suppression rain-enhancement bomb time fuse - Google Patents
High-reliability artillery artificial hail-suppression rain-enhancement bomb time fuse Download PDFInfo
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- CN113587748A CN113587748A CN202110801787.1A CN202110801787A CN113587748A CN 113587748 A CN113587748 A CN 113587748A CN 202110801787 A CN202110801787 A CN 202110801787A CN 113587748 A CN113587748 A CN 113587748A
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C9/00—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition
- F42C9/14—Double fuzes; Multiple fuzes
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- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01G—HORTICULTURE; CULTIVATION OF VEGETABLES, FLOWERS, RICE, FRUIT, VINES, HOPS OR SEAWEED; FORESTRY; WATERING
- A01G15/00—Devices or methods for influencing weather conditions
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/46—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C15/00—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
- F42C15/24—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected by inertia means
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Abstract
The invention discloses a high-reliability artillery artificial hail-suppression rain-increasing bomb time fuse which comprises a fuse body, a delay powder timing ignition mechanism, an electronic timing ignition mechanism, a ball rotor safety and relief mechanism and a detonator, wherein the delay powder timing ignition mechanism is positioned at the front end of the fuse body, the electronic timing ignition mechanism, the ball rotor safety and relief mechanism and the detonator are arranged in a fuse body cavity, the electronic timing ignition mechanism is positioned between the delay powder timing ignition mechanism and the ball rotor safety and relief mechanism, the front end of the detonator is adjacent to the ball rotor safety and relief mechanism, and the rear end of the detonator is used as a fuse output end and is used for detonating explosive charges of artificial hail-suppression rain-increasing bombs containing silver iodide. The delay powder timing ignition mechanism and the electronic timing ignition mechanism are mutually independent, redundant ignition is realized, and the reliability of the fuse action is improved. The time fuse of the high-reliability antiaircraft gun artificial hail suppression and rain enhancement bomb has high safety and good production reproducibility.
Description
Technical Field
The invention belongs to the technical field of civil fuzes, and particularly relates to a high-reliability artillery artificial hail-suppression rain-enhancement bomb time fuze.
Background
The small-caliber antiaircraft gun hail-suppression rain-enhancement bomb is used for artificial hail-suppression rain-enhancement operation in an air shooting mode. The rain enhancement and hail suppression mechanism is as follows: the hail-removing and rain-increasing bomb is launched into a cloud layer to explode, so that the cloud layer which is likely to produce hail is influenced, hail embryos cannot be developed into the hail, or small ice particles fall to the ground before becoming large hail, and the aim of removing the hail is fulfilled; through filling the explosive explosion in the projectile body, can produce the shock wave, influence or change the interior dynamics process of cloud, reach the effect that the big gun was sounded rain and is fallen, make the silver iodide catalyst of dress in the projectile body simultaneously and spread in the long-pending rain cloud layer by the detonation wave, produce a large amount of crystal nucleuses, make "rain cloud" or "hail cloud" conversion, reach the purpose of increasing the rain.
At present, Russia, America, Israel, Thailand and Western Europe are used for carrying out artificial rain enhancement operation abroad, and Russia is the large scale for carrying out artificial hail suppression operation. At present, no report of hail suppression and rain enhancement by using an artillery shooting artificial hail suppression and rain enhancement mode exists abroad.
At present, the safety problem of the domestic hail-suppression rain-increasing bomb is prominent and mainly appears as follows: the pellet is too large after being subjected to air explosion, and the pellet possibly injures people when falling; as civil products, the launching environment and the using environment of the hail-suppression rain-increasing bomb and the fuse thereof launched by the retired small-caliber antiaircraft gun are basically the same as those of military products, even more severe, but the design of the fuse thereof does not meet the relevant requirements of GJB373B-2019 fuse safety design criteria which must be met by the military fuse, and the explosion of the shot bore leads to gun destruction and even the frequent occurrence of accidents of human death; because of the large usage amount, the reliability performance level of the fuse action is limited, and the unexploded explosive casualty accidents caused by the misfire of the fuse almost exist year by year. Hail suppression and rain enhancement operation is disaster prevention and reduction behavior, and the economy is very important. Therefore, the technical key of the small-caliber antiaircraft hail-suppression rain-increase bomb fuze is as follows: improving safety and reducing cost. The safety improvement comprises the reduction of bomb fragments, the reduction of the misfire rate of the fuze, the prevention of the reignition after the ground is blown down in the air, the guarantee of the safety of the disposal of the fuze after the misfire, and the satisfaction of the related requirements (explosion-proof safety, redundancy insurance, delay relief, selection of safe conductive explosives, non-relief state guarantee, and the like) of GJB373B-2019 fuze safety design criteria.
In order to solve these technical key problems, domestic researchers have made many relevant studies. According to the artificial rainfall bomb fuze design disclosed in Chinese invention patent 200620001167.0, the air explosion time is prolonged by connecting 2-4 delay explosive disks in series, but the delay explosive disks and a fire transfer sequence mainly composed of the delay explosive disks do not have an isolation design and therefore cannot meet the requirement of explosion-proof safety. The black powder is filled in an explosion initiating pipe designed by the artificial rainfall bomb fuze disclosed by the Chinese invention patent 00201925.6, and the explosion initiating pipe is too safe, so that the sensitivity requirements of GJB373B-2019 on detonating powder guiding are not met, the designs all have the possibility of early firing accidents such as chamber explosion and the like due to the fact that the ignition mechanism does not ignite in the service processing and launching processes, and have great potential safety hazards. Although the chinese patent 200610095035.3 discloses a powder delay relief and a centrifugal fuse, the centrifugal fuse has only one centrifugal fuse mechanism, rather than two or more centrifugal fuses which are generally arranged in an axisymmetric manner. The centrifugal safety mechanism is difficult to independently fulfill the safety function, so that the requirement of redundant safety is not met, and the safety and reliability are difficult to meet. In addition, the fuse explosion-proof mechanism adopts a vertical disc rotor structure instead of a recognized triangular rotor structure, and the fuse explosion-proof mechanism can be accidentally relieved in a chamber under the condition that the safety explosive column is accidentally cracked after the gunpowder is delayed and relieved, so that the chamber explosion is caused. The artificial hail-suppression rain-increasing bomb described in the chinese invention patents 200820100586.9 and 201220363259.9 has performed relevant improvement around the safety of the fuse, but the slider isolation mechanism designed in 200820100586.9 is not provided with a redundant insurance and a delay relief mechanism, so that the insurance can be relieved in the chamber, and the explosion-suppression safety cannot completely meet the corresponding national military standard requirements, and the potential safety hazard is still not completely solved. 201220363259.9 adopts double ignition detonation channels to provide reliable action, but each ignition detonation channel is provided with no explosion-proof mechanism, so that great potential safety hazard exists. The structure of the Chinese patent 201610952063.6 is slightly complicated, and the production reproducibility of the applied powder and explosive tray timing structure is poor.
In summary, the general problems with the prior art are: the safety of the detonator of the antiaircraft hail-suppression rain-enhancement bomb is low, the reliability is poor, and the producibility is difficult to meet.
Disclosure of Invention
The invention aims to provide a high-reliability time fuse for an antiaircraft gun artificial hail suppression and rain enhancement bomb, which has higher reliability, better safety and strong production reproducibility.
The technical solution for realizing the purpose of the invention is as follows: a high-reliability artillery artificial hail-suppression rain-increasing bomb time detonator comprises a detonator body, a delay powder timing ignition mechanism, an electronic timing ignition mechanism, a ball rotor safety and safety-relief mechanism and a detonator, wherein the delay powder timing ignition mechanism is arranged at the front end of the detonator body, the electronic timing ignition mechanism, the ball rotor safety and safety-relief mechanism and the detonator are arranged in a body cavity of the detonator body, a sixth-order stepped hole is formed downwards from the top surface of the front end of the detonator body, and is respectively a first-order hole, a second-order hole, a third-order hole, a fourth-order hole, a fifth-order hole and a sixth-order hole from front to back, a cover plate is arranged in the first-order hole, the delay powder timing ignition mechanism is arranged in the second-order hole, the third-order hole is used as a fire transmission channel, a magnetic recoil generator is arranged in the fourth-order hole, the electronic timing ignition mechanism is arranged in the fifth-order hole, the ball rotor safety and safety-relief mechanism are adjacent to the electronic timing ignition mechanism and are arranged in the sixth-order hole, the detonator is also arranged in the sixth-relief mechanism, and the detonator is arranged in the detonator, and the detonator body front end of the ball rotor safety-relief mechanism is adjacent to the ball rotor safety-relief mechanism, the rear end is used as a fuse output end and is used for detonating the explosive charge of the artificial hail-suppression rain-enhancement bomb containing silver iodide. The delay powder timing ignition mechanism and the electronic timing ignition mechanism are mutually independent, redundant ignition is realized, and the reliability of the fuse action is improved.
Compared with the prior art, the invention has the following remarkable advantages:
(1) the reliability is higher: compared with the existing product, the delay powder timing ignition mechanism and the electronic timing ignition mechanism have two timing ignition mechanisms, and the two timing ignition mechanisms are independent from each other and can ignite the flame detonator, so that the redundant design of the fuze timing ignition function is realized, and the misfire rate is effectively reduced.
(2) The safety is better: compared with the existing product, the ball rotor is locked by the split ring, the safety pin and the centrifuge in a triple mode under the assembly condition, cannot rotate and is in a dislocation state, and therefore the explosion-proof safety of the fuse is guaranteed. After the safety and safety relief mechanism of the ball rotor is installed in the fuse body, the ball rotor can be prevented from being assembled into a safety relief state by adopting a mode of visual observation and poking inspection from a central hole at the tail part, and the phenomena of missing assembly, wrong assembly and 'dead pressing' of the ball rotor due to impurities, hard edges, burrs and other redundancies are prevented. The ball rotor can rotate in two directions, the axis of the detonating tube on the ball rotor can coincide with the axis of the fuze and the projectile after a certain time delay, and the time for the ball rotor to rotate can ensure that the ball rotor is relieved beyond the safety distance of the projectile, namely, the delayed relief (for example, the ball rotor is 15 m away from a muzzle when used for an antiaircraft with the diameter of 37 mm).
(3) The production reproducibility is strong: compared with the timing principle and structure of a gunpowder and explosive tray in the existing product, the timing of the gunpowder delay tube and the electronic timing are easier to ensure the stable quality and the production efficiency.
(4) The cost is lower: the structure is simple, and most parts are in a revolving body configuration, so that the processing and the inspection are convenient, and the cost is reduced.
The invention is described in further detail below with reference to the figures and the detailed description.
Drawings
Fig. 1 is a structural schematic diagram of a high-reliability artillery artificial hail-suppression rain-enhancement bomb time fuse structure along an axial line section.
Fig. 2 is a schematic view of the electronic timepiece ignition mechanism of fig. 1 taken along the section a-a.
In the figure, 1 is a fuse body, 2 is a delay powder timing ignition mechanism, 3 is an electronic timing ignition mechanism, 4 is a ball rotor safety and safety relief mechanism, and 5 is a detonator; 21 is a cover plate, 22 is a firing pin, 23 is a delay body, and 24 is an adjusting pad; 31 is a magnetic recoil motor, 32 is a paper gasket, 33 is a safety sheet, and 34 is an electronic timing ignition module; 41 is an isolation ball, 42 is a ball cover, 43 is a ball seat, 44 is a detonating tube, 45 is a centrifuge, 46 is an open ring, 47 is a safety pin, 48 is a shear pin, 49 is a flame detonator, 410 is a centrifugal spring; reference numeral 51 denotes a gasket, 52 denotes a reinforcing cap, 53 denotes a squib case, and 54 denotes a squib.
Detailed Description
The invention is further described with reference to the accompanying drawings.
With reference to fig. 1 and 2, the invention relates to a highly reliable artillery artificial hail suppression and rain enhancement bomb time detonator, which comprises a detonator body 1, a delay powder timing ignition mechanism 2 arranged at the front end of the detonator body 1, an electronic timing ignition mechanism 3 arranged in the cavity of the detonator body, a ball rotor safety and safety relief mechanism 4 and a detonator 5, wherein a sixth-step stepped hole is formed downwards from the top surface of the front end of the detonator body, and is respectively a first-step hole, a second-step hole, a third-step hole, a fourth-step hole, a fifth-step hole and a sixth-step hole from front to back, the delay powder timing ignition mechanism 2 is arranged in the first-step hole and the second-step hole, the third-step hole is used as a fire transmission channel, the electronic timing ignition mechanism 3 is arranged in the fourth-step hole and the fifth-step hole, the ball rotor safety and safety relief mechanism 4 is adjacent to the electronic timing ignition mechanism 3, the ball safety and safety relief mechanism 4 and the detonator 5 are both arranged in the sixth-step hole, the front end of the booster 5 is adjacent to the ball rotor safety and relief mechanism 4, and the rear end is used as a fuse output end for detonating explosive charge of the artificial hail suppression and rain enhancement bomb containing silver iodide.
The delay powder timing ignition mechanism 2 comprises a cover plate 21, a firing pin 22, a delay body 23 and an adjusting pad 24, wherein the delay body 23 is of a delay tubular structure. The cover plate 21 is positioned in a first-step hole at the front end of the fuse body 1 and seals the fuse body 1, the firing pin 22, the delay body 23 and the adjusting pad 24 are filled in a second-step hole from top to bottom, the lower surface of the cover plate 21 is attached to the upper surface of the firing pin 22, the needle point of the firing pin 22 is close to the upper surface of the delay body 23, the lower surface of the delay body 23 is attached to the upper surface of the adjusting pad 24, and the lower surface of the adjusting pad 24 is attached to the hole bottom of the second-step hole.
The flange of the striker 22 is changed from a conventional annular flange to a discrete point flange, so as to reduce the flange shearing area and ensure the reliable flange shearing.
A circle of first flange is arranged at the bottom of the circumferential outer wall of the delay body 23 and tightly attached to the inner wall of the second stepped hole, so that radial positioning is realized; meanwhile, an annular cavity is formed between the delay body 23 and the inner wall of the second-stage hole, so that the pressure is prevented from being out of control and increasing rapidly after the delay agent is combusted to generate a gaseous product, the combustion time of the delay agent is stable, and the timing precision of the delay agent timing ignition mechanism 2 is improved.
The electronic timing ignition mechanism 3 comprises a paper gasket 32, a magnetic recoil motor 31, a safety disc 33 and an electronic timing ignition module 34 consisting of an electric ignition head and a timer which are sequentially arranged from top to bottom; the paper gasket 32 and the magnetic recoil motor 31 are filled in the fourth-step hole, the safety disc 33 and the electronic timing ignition module 34 are arranged in the fifth-step hole, the lower surface of the magnetic recoil motor 31 is attached to the upper surface of the safety disc 33, and the upper surface of the safety disc 33 is attached to the upper surface of the fifth-step hole. The electronic timing ignition module 34 realizes the functions of capacitive energy storage, timing, driving ignition and ignition, and is the prior art.
The paper gasket 32 is provided with a first central fire transfer hole, a second central fire transfer hole is arranged on a magnetic core of the magnetic recoil motor 31, a third central fire transfer hole is arranged on the safety plate 33, the first central fire transfer hole, the second central fire transfer hole and the third central fire transfer hole are communicated with the same diameter to form a central fire transfer channel, the front end of the central fire transfer channel is connected with the third-order hole, and the rear end of the central fire transfer channel is communicated with the flame detonator 49.
The safety and safety release mechanism 4 comprises a ball rotor consisting of an isolation ball 41 and two detonating tubes 44, a ball cover 42 which contains the ball rotor and has an open back end, a ball seat 43 which closes the open back end of the ball cover 42, and a flame detonator 49 which is positioned at the front end of the central axis of the ball cover, wherein a cylindrical cavity is arranged between the upper surface of the flame detonator 49 and the lower surface of the safety plate 33 and is used for containing a magnetic core which sits backwards in the motor, the lower surface of the flame detonator 49 is adjacent to the isolation ball 41, a cylindrical hole is arranged between the flame detonator 49 and the isolation ball 41 on the ball cover 42 and is used as a detonating channel after fuse release, a movement gap is arranged between the ball rotor and the inner wall of a cavity formed by the ball cover 42 and the ball seat 43, the detonating tubes 44 are symmetrically arranged on the two side axes of the center of the isolation ball 41, the two detonating tubes 44 are communicated by the detonating channel, and the centrifugal tubes 45 and the centrifugal spring 410 which are tightly attached to the isolation ball 41 are symmetrically arranged on the two sides of the front axis of the isolation ball 41 along the radial direction The centrifugal safety mechanism is characterized in that two axially symmetrical sides above the ball seat 43 and below the isolating ball 41 are provided with a split ring 46 tightly attached to the ball seat 43 on one side, a safety pin hole is formed in the ball seat 43 on the other side, a safety pin 47 is inserted into the safety pin hole, the safety pin 47 tightly attached to the isolating ball 41, a shear hole is formed in the transverse center line of the safety pin 47 from one side of the ball seat 43, the shear hole penetrates through the safety pin 47 to the ball seat 43, a shear pin 48 is inserted, and the split ring 46 is opposite to the safety pin 47.
The safety and safety relief mechanism 4 of the ball rotor is provided with a triple safety mechanism of a centrifuge 45, a split ring 46 and a safety pin 47, so that the assembly accuracy is ensured, and the safety is improved.
The booster 5 comprises a gasket 51, a reinforcing cap 52, a booster 54 and a booster shell 53, wherein the reinforcing cap 52 is arranged on the top surface of the booster shell 53, the reinforcing cap and the booster shell form a explosive loading cavity, the booster 54 is arranged in the explosive loading cavity, and the gasket 51 is arranged between the ball seat 43 and the reinforcing cap 52. The washer 51 is made of aluminum.
The washer 51 between the ball seat 43 and the reinforcing cap 52 can buffer the recoil impact of the safety pin 47 during firing, and prevent the safety pin 47 from being restored after the safety is released.
The two timing ignition mechanisms, namely the delay powder timing ignition mechanism 2 and the electronic timing ignition mechanism 3 are mutually independent, the output of the two timing ignition mechanisms can reliably ignite the flame detonator 49, and the two timing ignition mechanisms are structurally connected in series and functionally connected in parallel, so that the reliability is improved, and the ignition failure rate quantification requirement below one in thousandth can be met.
The working process of the time fuse for the high-reliability antiaircraft gun artificial hail suppression and rain enhancement bomb is as follows.
Under the condition of assembly, the isolating ball 41 is locked by the safety pin 47, the split ring 46 and the pair of the centrifugal pieces 45 and cannot rotate to be in a dislocation state, at the moment, even if the flame detonator 49 in the ball rotor safety and release safety mechanism 4 is accidentally fired and exploded, the detonating tube 44 and the detonating tube 5 cannot be ignited due to the existence of the safety pin 47 and the isolating ball 41, the detonator body has a complete structure, and no dangerous rupture disc flies out, so that the explosion-proof safety of the detonator is ensured. After the safety and safety release mechanism 4 of the ball rotor is installed in the fuze body, the ball rotor can be prevented from being assembled into a safety release state by adopting a mode of visual observation and toggle check from a central hole at the tail part of the ball seat 43, and the phenomena of missing assembly and assembly error of the ball rotor and 'dead' of the ball rotor due to impurities, hard edges, burrs and other redundancies are prevented. In addition, the safety pin 47 is secured by the shear pin 48, the centrifugal rotor 45 is secured by the corresponding centrifugal spring 410, the magnetic core of the magnetic recoil motor 31 is secured by the safety plate 33, and the striker 22 is secured by the flange thereon. These securing elements (features) bring the respective secured elements into the assembled state.
The drop impact, the transportation vibration and the accidental rolling generated during the service handling do not cause the shear pin 48 to be cut off by accidental shearing, the split ring to be thrown (opened) accidentally, the centrifugal pin 45 not to release the ball rotor, the magnetic core of the magnetic recoil motor 31 not to cut the safety disc 33, and the flange on the firing pin 22 not to be cut off, and the safety pin 47, the split ring 46 and the pair of centrifugal pins 45 constitute a redundant safety of the explosion-proof member, namely the isolation ball 41. The isolating ball 41 is locked by the safety pin 47, the split ring 46 and the centrifuge 45, can not be rotated correctly and is in a dislocation explosion-proof state during assembly, and the safety of the fuse in a service processing stage is ensured.
When the shot is shot, under the action of the recoil force, the safety pin 47 of the recoil safety mechanism recoils to cut the shear pin 48, and the first locking of the ball rotor is released; meanwhile, the firing pin 22 in the delay powder timing ignition mechanism sits backwards, the flange on the firing pin is cut off, the delay body 23 is punctured, and the delay body starts timing work. The magnetic core recoil led by the magnetic recoil motor shears the safety sheet 33, the magnetic recoil motor generates electricity, the electric energy is stored in an electronic timing ignition module 34 in the electronic timing ignition mechanism 3, and the timing is started. The projectile moves in the chamber to approach the muzzle, the overload of the recoil is gradually reduced, the centrifugal force generated by the high-speed rotation of the projectile overcomes the friction force generated by the recoil to throw the two petals of the split ring 46 away along the middle weak part, the centrifugal pin 45 also compresses the centrifugal spring 410 to be withdrawn outwards, and thus the ball rotor is released. After the projectile flies out of the muzzle, the ball rotor, i.e. the isolation ball 41 and the detonating tube 44 therein overcome the friction torque under the action of the centrifugal torque and gradually rotate forward under the participation of the gyro torque, the explosion sequence is aligned, the fuse is relieved, and the projectile is in a state of being fired. The projectile flies a safe distance corresponding to the time that the ball rotor is rotating, and the fuse achieves delayed arming (e.g., 15 m away from the muzzle for a 37 mm caliber antiaircraft gun). After a period of time, if the delay powder timing ignition mechanism 2 finishes working firstly, flame is output, the flame detonator 49 is ignited through the central fire transmission hole arranged on the magnetic core of the magnetic recoil motor 31, the flame detonator 49 ignites the detonating tube 44 on one side of the ball rotor 41, the detonating tube 44 ignites the detonating tube on the other side, then the detonating tube is ignited, and the detonating powder 54 ignites the projectile to finish the detonation work; if the electronic timing ignition mechanism 3 finishes working first, the electric ignition head can also output flame to ignite the flame detonator 49, and the subsequent detonating and detonating processes are the same as the above. As described above, the delay charge timing ignition mechanism 2 and the electronic timing ignition mechanism 3 are redundantly provided in parallel. Any one set of the explosive burns out, and the other set of the explosive is exploded. And if one set fails to ignite, the other set is used as a backup to finish the preset ignition. The two timing ignition mechanisms are all in ignition failure, and are events with small probability. According to experience, the probability of accidental failure of one path of ignition mechanism is estimated to be about 1%, and the probability of failure of both paths of ignition mechanisms is about 1% multiplied by 1% =0.01%, namely one ten thousandth. On the premise of ensuring the production quality, the failure rate of the fuse safety and safety relief mechanism and the fuse detonation sequence is almost 0, so that the failure rate of the fuse action is considered to be possibly controlled below one ten thousandth. Under the condition of detonator misfire, the unexploded pellet can fall to the ground at high speed to generate kinetic energy damage. The timing expectation values of the two timing ignition mechanisms are set to be 15 s or 9 s or 12 s (according to the order requirement). The delay powder timing ignition mechanism 2 has larger timing error which can reach +/-3 s. And the timing error of the electronic timing ignition mechanism 3 is smaller within +/-10 ms.
The fuze guide and explosion transfer medicine meets the sensitivity requirements of GJB373B-2019 'fuze safety design rule' on the guide and explosion transfer medicine, and can ensure that the accidental fire cannot be caused to cause premature explosion under the assembly condition, during the service treatment and in the launching process.
If the detonator accidentally misfires in the air, such as if the ball rotor safety and arming mechanism 4 is not armed or not fully armed (meaning that the ball rotors are not aligned or not fully aligned), the fired detonator 49 can still be initiated by the two-way timing ignition mechanism, but the detonator is in a self-disabling state, at which time the formed unexploded charge is safe. If the two timing ignition mechanisms of the fuze accidentally misfire in the air, but the safety and safety release mechanism 4 of the ball rotor is relieved, namely the ball rotor is aligned, at the moment, because the fuze does not have an instantaneous trigger mechanism, accidental ignition explosion cannot happen at the moment of landing. And in the process of falling to the ground, the structure of the detonator head can be damaged, and even if the detonator delay powder timing ignition mechanism 2 is not ignited before and is ignited when falling to the ground, the detonator delay powder timing ignition mechanism can also fail due to the damage of the head structure because of the existence of the delay action, the accidental ignition action can not occur any more, and the formed unexplosive powder is also safe.
Claims (9)
1. The utility model provides a high reliability antiaircraft gun artificial hail suppression and rain enhancement bullet time detonator which characterized in that: comprises a fuse body (1), a delay powder timing ignition mechanism (2) positioned at the front end of the fuse body (1), an electronic timing ignition mechanism (3) arranged in a cavity of the fuse body, a ball rotor safety and relief mechanism (4) and a detonating tube (5), wherein a sixth-order stepped hole is formed downwards from the top surface of the front end of the fuse body (1), and is respectively a first-order hole, a second-order hole, a third-order hole, a fourth-order hole, a fifth-order hole and a sixth-order hole from front to back, the delay powder timing ignition mechanism (2) is arranged in the first-order hole and the second-order hole, the third-order hole is used as a igniting channel, the electronic timing ignition mechanism (3) is arranged in the fourth-order hole and the fifth-order hole, the ball rotor safety and relief mechanism (4) is adjacent to the electronic timing ignition mechanism (3), and the ball rotor safety and relief mechanism (4) and the detonating tube (5) are both arranged in the sixth-order hole, the front end of the booster tube (5) is adjacent to the ball rotor safety and relief mechanism (4), and the rear end of the booster tube is used as a fuse output end and is used for detonating explosive charges of the artificial hail-suppression rain-enhancement bomb containing silver iodide.
2. The highly reliable artillery artificial hail suppression and rain enhancement bomb time fuse as recited in claim 1, wherein: the delay powder timing ignition mechanism (2) comprises a cover plate (21), a firing pin (22), a delay body (23) and an adjusting pad (24), wherein the cover plate (21) is positioned in a first-step hole in the front end of the fuze body (1) and seals the fuze body (1), the firing pin (22), the delay body (23) and the adjusting pad (24) are filled in a second-step hole from top to bottom, the lower surface of the cover plate (21) is attached to the upper surface of the firing pin (22), the needle point of the firing pin (22) is close to the upper surface of the delay body (23), the lower surface of the delay body (23) is attached to the upper surface of the adjusting pad (24), and the lower surface of the adjusting pad (24) is attached to the bottom of the second-step hole.
3. The highly reliable artillery artificial hail suppression and rain enhancement bomb time fuse as recited in claim 2, wherein: the flange of the striker pin (22) is a discrete point flange.
4. The highly reliable artillery artificial hail suppression and rain enhancement bomb time fuse as recited in claim 2, wherein: a circle of first flange is arranged at the bottom of the circumferential outer wall of the delay body (23), and the first flange is tightly attached to the inner wall of the second-step hole to realize radial positioning; meanwhile, an annular cavity is formed between the delay body (23) and the inner wall of the second-step hole, so that the pressure is prevented from being out of control and increasing rapidly after the delay agent is combusted to generate a gaseous product, the combustion time of the delay agent is stable, and the timing precision of the delay agent timing ignition mechanism (2) is improved.
5. The highly reliable artillery artificial hail suppression and rain enhancement bomb time fuse as recited in claim 1, wherein: the electronic timing ignition mechanism (3) comprises a paper gasket (32), a magnetic recoil motor (31), a safety disc (33) and an electronic timing ignition module (34) consisting of an electric ignition head and a timer, which are sequentially arranged from top to bottom; the paper gasket (32) and the magnetic recoil motor (31) are filled in the fourth-step hole, the safety disc (33) and the electronic timing ignition module (34) are arranged in the fifth-step hole, the lower surface of the magnetic recoil motor (31) is attached to the upper surface of the safety disc (33), and the upper surface of the safety disc (33) is attached to the upper surface of the fifth-step hole.
6. The highly reliable artillery artificial hail suppression and rain enhancement bomb time fuse as recited in claim 5, wherein: be equipped with first center biography fire hole on paper gasket (32), magnetism recoil motor (31) magnetic core and be equipped with the center of second and pass the fire hole, be equipped with the center of third and pass the fire hole on insurance piece (33), first center passes fire hole, the center of second and the center of third and passes the fire hole and communicate with the footpath and constitute central biography fire passageway, central biography fire passageway front end and third rank jogged joint, the rear end accesss to flame detonator (49).
7. The highly reliable artillery artificial hail suppression and rain enhancement bomb time fuse as recited in claim 5, wherein: the safety and safety relief mechanism (4) of the ball rotor comprises a ball rotor consisting of an isolation ball (41) and two detonating tubes (44), a ball cover (42) accommodating the ball rotor and having an open rear end, a ball seat (43) closing the open rear end of the ball cover (42), and a flame detonator (49) positioned at the front end of the central axis of the ball cover, wherein a cylindrical cavity is formed between the upper surface of the flame detonator (49) and the lower surface of a safety disc (33) and used for accommodating a magnetic core of a backseat in a motor, the lower surface of the flame detonator (49) is adjacent to the isolation ball (41), a cylindrical hole is formed between the flame detonator (49) and the isolation ball (41) on the ball cover (42), and is used as a detonating passage after fuse relief is relieved, a movement gap is formed between the ball rotor and the inner wall of the cavity formed by the ball cover (42) and the ball seat (43), and the detonating tubes (44) are symmetrically arranged on the two side axes of the ball center of the isolation ball (41), the two detonating tubes (44) are communicated by a detonating channel, centrifugal safety mechanisms tightly attached to the isolating ball (41) are symmetrically arranged on two sides of the front axis of the isolating ball (41) along the radial direction, each centrifugal safety mechanism consists of a centrifugal element (45) and a centrifugal spring (410), a split ring (46) tightly attached to the ball seat (43) is arranged on one side of the two sides below the isolating ball (41) and symmetrically arranged on the axis above the ball seat (43), a safety pin hole is formed in the other side of the two sides of the isolating ball (41), a safety pin (47) is inserted into the safety pin hole, the safety pin (47) tightly attached to the isolating ball (41), a shear hole is formed in the transverse center line of the safety pin (47) from one side of the ball seat (43), the shear hole penetrates through the safety pin (47) to the ball seat (43), a shear pin (48) is inserted, and the opening of the split ring (46) is opposite to the safety pin (47).
8. The highly reliable artillery artificial hail suppression and rain enhancement projectile time fuse as claimed in claim 7, wherein: the booster (5) comprises a gasket (51), a reinforcing cap (52), booster powder (54) and a booster shell (53), the reinforcing cap (52) is arranged on the top surface of the booster shell (53), the booster powder and the booster shell form a powder loading cavity, the booster powder (54) is arranged in the powder loading cavity, and the gasket (51) is arranged between the ball seat (43) and the reinforcing cap (52).
9. The highly reliable artillery artificial hail suppression and rain enhancement projectile time fuse as claimed in claim 8, wherein: a gasket (51) between the ball seat (43) and the reinforcing cap (52) can buffer the recoil impact of the safety pin (47) during launching, and prevent the safety pin (47) from resetting after the safety is relieved.
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| CN202110801787.1A CN113587748B (en) | 2021-07-15 | 2021-07-15 | High-reliability artillery artificial hail-suppression rain-enhancement bomb time fuse |
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| CN202110801787.1A CN113587748B (en) | 2021-07-15 | 2021-07-15 | High-reliability artillery artificial hail-suppression rain-enhancement bomb time fuse |
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| CN113587748B CN113587748B (en) | 2023-04-07 |
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Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB191502724A (en) * | 1913-11-19 | 1917-06-28 | Cie Forges Et Acieries Marine | Multiple Effect Fuse for Artillery Projectiles. |
| WO1987001192A1 (en) * | 1985-08-22 | 1987-02-26 | Oregon Etablissement Für Patentverwertung | Double-action fuse for missiles |
| CN2856919Y (en) * | 2006-01-17 | 2007-01-10 | 刘影晨 | 37mm artificial hail-suppression rainfall bomb |
| CN106338224A (en) * | 2016-10-27 | 2017-01-18 | 南京理工大学 | Time detonating fuse of antiaircraft gun hail-suppression precipitation increasing bomb |
| CN109506527A (en) * | 2018-11-20 | 2019-03-22 | 南京理工大学 | Hail mitigation increases the electromechanical time fuse of rain bullet |
| CN210833274U (en) * | 2019-10-23 | 2020-06-23 | 湖南亿能电子科技有限公司 | Electronic trigger fuse test system |
| CN112066826A (en) * | 2020-08-19 | 2020-12-11 | 南京理工大学 | Mechanical trigger fuse for small-caliber rotary shell warhead |
| CN112082434A (en) * | 2020-08-19 | 2020-12-15 | 南京理工大学 | Electromechanical trigger fuse for bullet of aerial rotating rocket projectile |
-
2021
- 2021-07-15 CN CN202110801787.1A patent/CN113587748B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB191502724A (en) * | 1913-11-19 | 1917-06-28 | Cie Forges Et Acieries Marine | Multiple Effect Fuse for Artillery Projectiles. |
| WO1987001192A1 (en) * | 1985-08-22 | 1987-02-26 | Oregon Etablissement Für Patentverwertung | Double-action fuse for missiles |
| CN2856919Y (en) * | 2006-01-17 | 2007-01-10 | 刘影晨 | 37mm artificial hail-suppression rainfall bomb |
| CN106338224A (en) * | 2016-10-27 | 2017-01-18 | 南京理工大学 | Time detonating fuse of antiaircraft gun hail-suppression precipitation increasing bomb |
| CN109506527A (en) * | 2018-11-20 | 2019-03-22 | 南京理工大学 | Hail mitigation increases the electromechanical time fuse of rain bullet |
| CN210833274U (en) * | 2019-10-23 | 2020-06-23 | 湖南亿能电子科技有限公司 | Electronic trigger fuse test system |
| CN112066826A (en) * | 2020-08-19 | 2020-12-11 | 南京理工大学 | Mechanical trigger fuse for small-caliber rotary shell warhead |
| CN112082434A (en) * | 2020-08-19 | 2020-12-15 | 南京理工大学 | Electromechanical trigger fuse for bullet of aerial rotating rocket projectile |
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| CN113587748B (en) | 2023-04-07 |
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