CN114935285B - Interception-preventing efficient bouncing type water-entering striking missile and method - Google Patents
Interception-preventing efficient bouncing type water-entering striking missile and method Download PDFInfo
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- CN114935285B CN114935285B CN202210569068.6A CN202210569068A CN114935285B CN 114935285 B CN114935285 B CN 114935285B CN 202210569068 A CN202210569068 A CN 202210569068A CN 114935285 B CN114935285 B CN 114935285B
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
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Abstract
The invention provides an interception-preventing efficient bouncing type water-entering striking missile and a method thereof, and belongs to the field of military missiles. Solves the problem that the existing water-entering hit missile is easily intercepted by an enemy defense system in the air or under water. The device comprises a missile body, a missile body head load reducing device, a head impact transmission rod, a transmission control device, a transmission device and a bouncing springboard; when the missile body head load-reducing device of the missile impacts the water surface, the missile body head load-reducing device is transmitted to the bouncing springboard through the head impact transmission rod and the transmission device to enable the bouncing springboard to be opened, and when the bouncing springboard beats the water surface, the missile finishes one-time forward sliding by means of water surface reverse thrust; after the missile leaves the water surface, the transmission control device enables the transmission device to restore to the original position through the return spring to enable the bouncing springboard to be closed, and one water surface sliding period of the missile is completed; repeating the sliding process to realize that the missile slides forward towards the target on the near water surface; when the transmission control device receives the sensor signal, the missile enters water to strike. The invention is suitable for high-speed sudden-prevention weapons near the water surface.
Description
Technical Field
The invention belongs to the field of military missiles, and particularly relates to an interception-preventing efficient bouncing type water-entering striking missile and a method.
Background
Along with the construction of the large-scale warfleet area defense system by the naval countries, the construction of the high-altitude anti-conductor system and the underwater anti-submarine system is highly valued, and the large-scale warhead anti-submarine system brings great attack limit to missiles which singly rely on the high-altitude and high-speed maneuvering advantages or adopt an underwater launching mode for sudden prevention.
By means of the missile weapon for concealing and burst prevention in the near water surface space, the weapons of the missile weapon for concealing and burst prevention in the near water surface space can be greatly utilized for attack by utilizing the weakness that an air and underwater defense system cannot be effectively connected in the near water surface space, and the aim of the technology of the missile crossing the water-air medium is focused by the navy in China. The near water surface burst-proof missile fully utilizes the natural weakness that the detection range cannot be fully covered in the near water surface space (5 m above and below the water surface) of the enemy warhead defending system, and performs near water burst-proof attack by means of a continuous bouncing mode, thereby being a brand-new near water surface combat attack mode of the missile.
The near-water space burst-prevention weapon is a necessary trend of future attack-prevention and defense countermeasure development, and the currently proposed near-water high-speed burst-prevention weapon attack mode controls the springboard to open and close through the ranging sensor so as to jump and fly on the water surface. Because the missile flies at a high speed suddenly and the springboard is opened and closed with accurate time control, a brand new interception-preventing high-efficiency bouncing type water-entering striking missile is needed to be designed to solve the problems.
Disclosure of Invention
The invention aims to provide an anti-interception high-efficiency bouncing type water-entering hit missile so as to solve the problem that the existing water-entering hit missile is easily intercepted by an enemy defense system in the air or under water.
In order to achieve the above purpose, the technical scheme of the invention is realized as follows:
the utility model provides an anti-interception high-efficient spring type water-entering hit missile, includes missile body, the head of missile body load-reducing device, head impact transfer pole, transmission controlling means, transmission and spring springboard, transmission controlling means and transmission all set up in the inside of missile body, and the head of missile body load-reducing device sets up in the outside of missile body, has seted up the sliding tube in the head central point of missile body, the head of missile body load-reducing device is connected in the one end of head impact transfer pole, and the other end of head impact transfer pole passes sliding tube and is articulated with transmission, spring springboard sets up in the opening part of missile body bottom, and spring springboard's one end articulates in the bottom of missile body, and the other end is connected with transmission; the transmission control device comprises a controller, a sensor and an execution part, wherein the sensor and the execution part are electrically connected with the controller, and the sensor is used for receiving a missile approaching target and a tail end water entering signal;
when the missile body head carrier of the missile impacts the water surface, the generated water surface reverse thrust is transmitted to the bouncing springboard through the head impact transmission rod and the transmission device to open the bouncing springboard, and when the bouncing springboard beats the water surface, the missile finishes one-time forward sliding by means of the water surface reverse thrust; after the missile leaves the water surface, the transmission control device enables the transmission device to restore to the original position through the return spring to enable the bouncing springboard to be closed, and one water surface sliding period of the missile is completed; after the previous period of sliding is completed, the missile body head carrier of the missile impacts the water surface again, and the sliding process is repeated, so that the missile can move forward towards the target in the near water surface; when the transmission control device receives the sensor signal, the controller of the transmission control device controls the action of the executing component to keep the transmission device fixed, so that the bouncing springboard is in a closed state when the tail end of the missile enters water, and the missile enters water to strike.
Still further, transmission includes first transfer line, second transfer line and fixed pivot, fixed pivot is fixed in the missile bullet body, and the one end of first transfer line is articulated with the other end of head impact transfer line, and the other end is articulated with the one end of second transfer line, and the other end of second transfer line is articulated with the spring springboard, is equipped with the sliding tray at the middle part of first transfer line, cooperates fixed pivot in the sliding tray.
Still further, transmission controlling means still includes transmission control pole and transmission control cover, actuating part is the direct-acting electromagnet, and transmission control cover one end is the open end, and the other end is the blind end, and the blind end of transmission control cover is connected with the missile body, and the one end of transmission control pole is articulated through the pivot with the other end of first transmission pole and the one end of second transmission pole, and the other end of transmission control pole stretches into in the open end of transmission control cover, reset spring sets up in transmission control cover inside, reset spring one end and the other end fixed connection of transmission control pole, and the other end is fixed on the closed end of transmission control cover, the direct-acting electromagnet sets up in transmission control cover, has seted up the pinhole on the transmission control pole, the action of controller control direct-acting electromagnet, and when the direct-acting electromagnet was cut off, the ejector pin of direct-acting electromagnet stretches out and cooperates the position that limits the transmission control pole with the pinhole on the transmission control pole, and when the direct-acting electromagnet was circular telegram, the ejector pin of direct-acting electromagnet is retracted, releases the restriction to the transmission control pole.
Furthermore, a plurality of groups of pulleys which are convenient for the head impact transmission rod to move are uniformly arranged in the sliding tube.
Furthermore, a buffer cushion for buffering the impact of the missile head load reducer on the missile body is arranged at the head of the missile body.
Still further, the cushion pad is disposed around the sliding tube.
Further, the projectile head load carrier is of a disc structure.
Furthermore, a hinge seat connected with one end of the bouncing springboard is arranged on the inner wall of the bottom of the missile body.
Furthermore, the head impact transmission rod is hinged with the first transmission rod, the bouncing springboard is hinged with the hinge seat at the bottom of the missile body, and the second transmission rod is hinged with the bouncing springboard through pins.
The invention provides a working method of an interception-preventing efficient bouncing type water-entering striking missile, which comprises the following steps:
when the missile strikes the water surface, strong impact force is transmitted to the transmission device through the head impact transmission rod, one end of the first transmission rod connected with the head impact transmission rod is acted by force first, a clockwise moment is generated and starts to rotate towards the tail of the missile body around the fixed rotating shaft, and the fixed rotating shaft slides to the top of the chute from the bottom of the chute; the first transmission rod drives the second transmission rod to move through the rotating shaft, the second transmission rod is stressed to move towards the lower part of the missile body, the second transmission rod drives the bouncing springboard to open and form a supporting mode, and the bouncing springboard enables the missile to slide forwards by means of strong reverse thrust of the water surface;
after the missile leaves the water surface, the transmission control device receives a stress signal, and after the supporting process of the bouncing springboard is finished, the transmission control rod is recovered to an initial position through the reset spring, and the transmission control rod drives the rotating shaft to recover the transmission device to an initial state, so that the transmission device is recovered to the initial state, meanwhile, the bouncing springboard is closed, and the head impact transmission rod is retracted along the sliding pipe, so that the missile completes a water surface bouncing period;
after the previous period of sliding is completed, the missile body head carrier of the missile impacts the water surface again, and the sliding process is repeated, so that the missile can move forward towards the target in the near water surface;
after the missile passes through a plurality of water surface sliding processes, the controller receives signals of the sensors, a control instruction is executed after the last sliding process is finished, the controller enables the transmission control rod to be fixed by controlling the ejector rod of the direct-acting electromagnet to extend out of the pin hole of the transmission control rod, meanwhile, the rotating shaft is also kept fixed, the transmission of head water collision impact force by the transmission device is stopped, the transmission device is not affected by the impact force transmitted by the head impact transmission rod when the missile impacts the water surface again, and meanwhile, the bouncing springboard is kept closed, so that the missile achieves the purpose of high-speed water entering and high-efficiency striking at the tail end.
Compared with the prior art, the anti-interception high-efficiency bouncing type water-entering striking missile has the following advantages:
(1) The invention creates the anti-interception high-efficiency bouncing type water-entering striking missile, which can jump on the water surface, and has reasonable and effective structural device;
(2) The anti-interception high-efficiency bouncing type water-entering striking missile is a mode that the missile head contacts the water surface to generate load to push the rotation and movement of the connecting rod to achieve ejection, and the missile instantly opens and closes at the instant of water contact by bouncing the springboard, so that high-speed flying in the near water surface is achieved.
(2) The missile provided by the invention flies in the air, the near-water surface sliding jump prevention mode is converted, when the head of the missile impacts the water surface, strong impact force is transmitted to the bouncing springboard through the transmission structure, and the bouncing springboard is opened and closed at the moment of the head of the missile touching the water, so that the missile finishes one-time forward sliding jump by means of strong reverse thrust of the water surface; striking the water surface again after the previous period of sliding is completed, and repeating the sliding process to realize that the missile slides forward towards the target on the near water surface; when the transmission control device receives a signal close to the water entering at the tail end of the target and transmits the signal to the transmission controller, the transmission structure is controlled by the controller to be kept fixed, so that the bouncing springboard is in a closed state when the tail end of the missile enters water, and further, the battle mode of high-speed hidden burst prevention at the near water surface and high-speed water entering and high-efficiency battle at the tail end is realized, and the battle efficiency is considerable.
(3) The space near the water surface belongs to radar monitoring blind areas, the interception-preventing high-efficiency bouncing type water-entering striking missile can avoid detection of enemy radars, the enemy defense system is broken through at a high speed, and the scheme of the missile on the sliding of the near water surface has good feasibility.
Drawings
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the invention and do not constitute an undue limitation on the invention. In the drawings:
FIG. 1 is a schematic diagram of the overall structure of an anti-interception high-efficiency bouncing type water-entering striking missile according to an embodiment of the invention;
FIG. 2 is a schematic diagram of a projectile head downloader for an anti-interception efficient bouncing type water-entry-hit projectile according to an embodiment of the invention;
FIG. 3 is a schematic diagram of a transmission device when a bouncing springboard of an anti-interception high-efficiency bouncing type water-entering beating missile is closed according to an embodiment of the invention;
FIG. 4 is a schematic diagram of a transmission device when a bouncing springboard of an anti-interception high-efficiency bouncing type water-entering beating missile is opened according to an embodiment of the invention;
FIG. 5 is a schematic diagram of a transmission control device for preventing interception and efficient bouncing of a water-entering hit missile according to an embodiment of the present invention;
FIG. 6 is a schematic diagram of the installation positions of a controller and a direct-acting electromagnet of an anti-interception high-efficiency bouncing type water-entering striking missile according to an embodiment of the invention;
FIG. 7 is a schematic diagram of an arrangement of a transmission control rod, a transmission control sleeve and a return spring of an anti-interception efficient bouncing type water-entering striking missile according to an embodiment of the invention;
FIG. 8 is a schematic diagram of a bouncing jump board structure of an anti-interception efficient bouncing type water-entering hitting missile according to an embodiment of the invention;
FIG. 9 is a schematic diagram of a principle of a near water surface ski jump of an anti-interception efficient bouncing type water-entry-hit missile according to an embodiment of the present invention;
fig. 10 is a graph of a trajectory of an anti-interception high-efficiency bouncing type water-entry-hit missile according to an embodiment of the present invention.
Reference numerals illustrate:
1. a missile body; 2. a projectile head load reducer; 3. a head impact transfer lever; 4. a cushion pad; 5. bouncing springboard; 6. a sliding tube; 7. a pin; 8. fixing the rotating shaft; 9. a sliding groove; 10. a rotating shaft; 11. a transmission control lever; 12. a transmission device; 12-1, a first transmission rod; 12-2, a second transmission rod; 13. a controller; 14. a pulley; 15. a return spring; 16. a pin hole; 17. a transmission control sleeve; 18. and a direct-acting electromagnet.
Detailed Description
The technical scheme of the invention will be clearly and completely described below with reference to the accompanying drawings.
1-10, an anti-interception efficient bouncing type water-entering striking missile comprises a missile body 1, a missile body head load-reducing device 2, a head impact transmission rod 3, a transmission control device, a transmission device 12 and a bouncing springboard 5, wherein the transmission control device and the transmission device 12 are arranged inside the missile body 1, the missile body head load-reducing device 2 is arranged outside the missile body 1, a sliding tube 6 is arranged in the center of the head of the missile body 1, the missile body head load-reducing device 2 is connected to one end of the head impact transmission rod 3, the other end of the head impact transmission rod 3 passes through the sliding tube 6 and is hinged with the transmission device 12, the bouncing springboard 5 is arranged at an opening at the bottom of the missile body 1, one end of the bouncing springboard 5 is hinged at the bottom of the missile body 1, and the other end of the bouncing springboard 5 is hinged with a second transmission rod 12-2 of the transmission device 12 through a pin; the transmission control device comprises a controller 13, a sensor and an execution part, wherein the execution part is a direct-acting electromagnet 18, the sensor and the direct-acting electromagnet 18 are electrically connected with the controller 13, the sensor is used for receiving a missile approaching target and a tail end water entering signal, and the sensor can be integrated into the controller;
when the missile body head carrier 2 of the missile impacts the water surface, the generated water surface reverse thrust is transmitted to the bouncing springboard 5 through the head impact transmission rod 3 and the transmission device 12 to open the bouncing springboard 5, and the missile finishes one-time forward sliding by means of the water surface reverse thrust when the bouncing springboard 5 beats the water surface; after the missile leaves the water surface, the transmission control device enables the transmission device 12 to restore to the original position through the return spring 15 to enable the bouncing springboard 5 to be closed, and one water surface sliding period of the missile is completed; after the previous period of sliding is completed, the missile body head carrier 2 of the missile impacts the water surface again, and the sliding process is repeated, so that the missile can move forward towards the target in the near water surface; when the transmission control device receives the sensor signal, the controller 13 of the transmission control device controls the action of the executing component to keep the transmission device 12 fixed, so that the bouncing springboard 5 is in a closed state when the tail end of the missile enters water, and the missile enters water to strike.
An anti-interception high-efficiency bouncing type water-entering striking missile, wherein the head of the missile generates strong impact force when contacting water, and the impact load is utilized and transmitted to a ski-jump board, so that the missile can fly in a ski-jump way on the water surface.
According to the fight scheme of the missile on the near water surface sliding jump, the missile belongs to a radar monitoring blind area in the near water surface space, can avoid enemy radar detection, breaks through an enemy defense system at a high speed, and has high fight prevention efficiency and perfect enemy detection avoidance.
The transmission device 12 comprises a first transmission rod 12-1, a second transmission rod 12-2 and a fixed rotating shaft 8, wherein the fixed rotating shaft 8 is fixed in the missile body 1, one end of the first transmission rod 12-1 is hinged with the other end of the head impact transmission rod 3, the other end of the first transmission rod is hinged with one end of the second transmission rod 12-2, the other end of the second transmission rod 12-2 is hinged with the bouncing springboard 5, a sliding groove 9 is formed in the middle of the first transmission rod 12-1, the fixed rotating shaft 8 is matched in the sliding groove 9, and the middle of the first transmission rod 12-1 can be moved through the sliding groove 9 to change the position of the fixed rotating shaft 8 relative to the first transmission rod 12-1.
The missile impacts the water surface, strong impact force is transmitted to the transmission device through the head impact transmission rod 3, one end of the first transmission rod 12-1 connected with the head impact transmission rod 3 is acted by force first, clockwise moment is generated to start rotating towards the tail of the missile around the fixed rotating shaft 8, and the fixed rotating shaft 8 slides to the top of the sliding groove 9 from the bottom of the sliding groove 9; the first transmission rod 12-1 drives the second transmission rod 12-2 through the rotating shaft 10, the second transmission rod 12-2 is stressed to move downwards, the second transmission rod 12-2 drives the bouncing springboard 5 to support, and the missile slides forwards by means of strong reverse thrust on the water surface.
The transmission control device further comprises a transmission control rod 11 and a transmission control sleeve 17, one end of the transmission control sleeve 17 is an open end, the other end of the transmission control sleeve 17 is a closed end, the closed end of the transmission control sleeve 17 is connected with the missile body 1, one end of the transmission control rod 11 is hinged with the other end of the first transmission rod 12-1 and one end of the second transmission rod 12-2 through a rotating shaft 10, the other end of the transmission control rod 11 stretches into the open end of the transmission control sleeve 17, a return spring 15 is arranged in the transmission control sleeve 17, one end of the return spring 15 is fixedly connected with the other end of the transmission control rod 11, the other end of the return spring is fixed on the closed end of the transmission control sleeve 17, a direct-acting electromagnet 18 is arranged in the transmission control sleeve 17, a pin hole 16 is formed in the transmission control rod 11, the controller 13 controls the action of the direct-acting electromagnet 18, when the direct-acting electromagnet 18 is powered off, a push rod of the direct-acting electromagnet stretches out to limit the position of the transmission control rod 11 in a matched mode, when the direct-acting electromagnet 18 is powered on, the push rod of the direct-acting electromagnet is retracted, and the limit of the transmission control rod 11 is released, and the direct-acting electromagnet 18 is in a direct-acting state in the direct-acting state, and the direct-acting electromagnet is not limited in the direct-acting state.
When the missile hits the water surface, the transmission control rod 11 is in a telescopic state and can stretch along with the rotation of the transmission device 12; after the missile leaves the water surface, the transmission control device receives stress information of the transmission control rod 11, after the supporting process of the bouncing springboard 5 is completed, the transmission control rod 11 is recovered to an initial position through the reset spring 15, the transmission control rod 11 drives the rotating shaft 10 to recover the transmission device 12 to an initial state, then the bouncing springboard 5 is closed, the head impact transmission rod 3 is retracted along the sliding tube 6, and the water surface bouncing process of the missile is completed; when the missile approaches the target and sends out a terminal water entering signal, the terminal water entering signal is transmitted to the controller 13, the controller 13 receives the signal and controls the ejector rod of the direct-acting electromagnet 18 to be inserted into the pin hole 16 of the transmission control rod 11, the transmission device 12 keeps fixed when the next missile impacts the water surface, the transmission control rod 11 and thus the rotating shaft are also kept fixed, the transmission device 12 does not rotate and move, the spring springboard 5 at the terminal water entering stage is in a closed state, and the missile enters water at a high speed to perform high-efficiency striking.
A plurality of groups of pulleys 14 which are convenient for the head impact transfer rod 3 to move are uniformly arranged in the sliding tube 6. So set up, reduce frictional force when making things convenient for head impact transfer lever 3 round trip to move.
The head of the missile body 1 is provided with a buffer cushion 4 for buffering the impact of the missile body 1 by the missile body head load reducing device 2. The cushion pad 4 is arranged around the sliding tube 6, is arranged to provide a buffer for the head downloader 2 to strike the missile body, and can transmit the impact force to the head impact transmission rod 3 through the missile body head downloader 2.
The projectile head carrier 2 is of a disc structure, and is the first contact part of a missile striking water surface, and the head carrier strikes the water surface and is subjected to the action of water surface thrust reaction and generates axial impact force.
A hinge seat connected with one end of the bouncing springboard 5 is arranged on the inner wall of the bottom of the missile body 1. The head impact transmission rod 3 is hinged with the first transmission rod 12-1, the bouncing springboard 5 is hinged with a hinge seat at the bottom of the missile body 1, and the second transmission rod 12-2 is hinged with the bouncing springboard 5 through pins 7.
A working method for preventing interception and efficient bouncing type water-entering striking guided missiles specifically comprises the following steps:
when the missile strikes the water surface, strong impact force is transmitted to the transmission device 12 through the head impact transmission rod 3, one end of the first transmission rod 12-1 connected with the head impact transmission rod 3 is acted by force first, clockwise moment is generated and starts to rotate towards the tail of the missile around the fixed rotating shaft 8, and the fixed rotating shaft 8 slides to the top of the chute from the bottom of the chute; the first transmission rod 12-1 drives the second transmission rod 12-2 to move through the rotating shaft 10, the second transmission rod 12-2 is stressed to move downwards to the projectile body, the second transmission rod 12-2 drives the bouncing springboard 5 to open and form a supporting mode, and the bouncing springboard 5 enables the projectile to slide forwards by means of strong reverse thrust on the water surface;
after the missile leaves the water surface, the transmission control device receives a stress signal, after the supporting process of the bouncing springboard 5 is completed, the transmission control rod 11 is recovered to the initial position through the reset spring 15, the transmission control rod 11 drives the rotating shaft 10 to recover the transmission device 12 to the initial state, so that the transmission device 12 is recovered to the initial state, meanwhile, the bouncing springboard 5 is closed, the head impact transmission rod 3 is retracted along the sliding tube 6, and the missile completes a water surface sliding period;
after the head of the missile impacts the water surface, impact force is instantaneously transmitted to the bouncing springboard 5 through the transmission device 12, so that the missile obtains forward jumping acting force at the initial stage of water impact, and the near-water jumping flight is realized. The missile continuously flies forward in a sliding way, avoids monitoring by an enemy radar, and breaks through an enemy defense system at a high speed;
after the previous period of sliding is completed, the missile body head carrier 2 of the missile impacts the water surface again, and the sliding process is repeated, so that the missile can move forward towards the target in the near water surface;
after the missile passes through a plurality of water surface sliding processes, the controller 13 receives signals of the sensors, a control instruction is executed after the last sliding process is finished, the controller 13 enables the transmission control rod 11 to be kept fixed by controlling the ejector rod of the direct-acting electromagnet to extend out and be inserted into the pin hole 16 of the transmission control rod 11, meanwhile, the rotating shaft 10 is kept fixed, the transmission of head water collision impact force by the transmission device 12 is stopped, the transmission device 12 is not affected by the impact force transmitted by the head impact transmission rod 3 when the missile impacts the water surface again, meanwhile, the bouncing springboard 5 is kept closed, and then the missile achieves the aim of high-speed water entering and high-efficiency striking at the tail end.
The damage effect of target striking by the end of the bouncing type water-entering striking missile is multiple times of that of the marine explosion to the naval vessel, and the fight efficiency of the missile can be effectively ensured.
Claims (8)
1. An anti-interception high-efficiency bouncing type water-entering striking missile is characterized in that: the missile body comprises a missile body (1), a missile body head load reducing device (2), a head impact transmission rod (3), a transmission control device, a transmission device (12) and a bouncing springboard (5), wherein the transmission control device and the transmission device (12) are arranged in the missile body (1), the missile body head load reducing device (2) is arranged outside the missile body (1), a sliding tube (6) is arranged in the center of the head of the missile body (1), the missile body head load reducing device (2) is connected with one end of the head impact transmission rod (3), the other end of the head impact transmission rod (3) penetrates through the sliding tube (6) to be hinged with the transmission device (12), the bouncing springboard (5) is arranged at an opening at the bottom of the missile body (1), one end of the bouncing springboard (5) is hinged with the bottom of the missile body (1), and the other end of the bouncing springboard is connected with the transmission device (12); the transmission control device comprises a controller (13), a sensor and an execution part, wherein the sensor and the execution part are electrically connected with the controller (13), and the sensor is used for receiving a missile approaching target and a tail end water entering signal;
when the missile body head carrier (2) of the missile hits the water surface, the generated water surface reverse thrust is transmitted to the bouncing springboard (5) through the head impact transmission rod (3) and the transmission device (12) to enable the bouncing board (5) to be opened, and when the bouncing board (5) beats the water surface, the missile finishes one-time forward sliding by means of the water surface reverse thrust; after the missile leaves the water surface, the transmission control device enables the transmission device (12) to restore to the original position through the return spring (15) to enable the bouncing springboard (5) to be closed, and one water surface sliding period of the missile is completed; after the previous period of sliding is completed, the missile body head carrier (2) of the missile impacts the water surface again, and the sliding process is repeated, so that the missile can slide forward towards the target on the near water surface; when the transmission control device receives a sensor signal, a controller (13) of the transmission control device controls an executing component to act so that the transmission device (12) is kept fixed, and the bouncing gangway (5) is in a closed state when the tail end of the missile enters water, so that the missile enters water to strike;
the transmission device (12) comprises a first transmission rod (12-1), a second transmission rod (12-2) and a fixed rotating shaft (8), wherein the fixed rotating shaft (8) is fixed in the missile body (1), one end of the first transmission rod (12-1) is hinged with the other end of the head impact transmission rod (3), the other end of the first transmission rod is hinged with one end of the second transmission rod (12-2), the other end of the second transmission rod (12-2) is hinged with the bouncing springboard (5), a sliding groove (9) is formed in the middle of the first transmission rod (12-1), and the sliding groove (9) is matched with the fixed rotating shaft (8);
the transmission control device also comprises a transmission control rod (11) and a transmission control sleeve (17), the execution part is a direct-acting electromagnet (18), one end of the transmission control sleeve (17) is an open end, the other end is a closed end, the closed end of the transmission control sleeve (17) is connected with the missile body (1), one end of the transmission control rod (11) is hinged with the other end of the first transmission rod (12-1) and one end of the second transmission rod (12-2) through a rotating shaft (10), the other end of the transmission control rod (11) stretches into the open end of the transmission control sleeve (17), a return spring (15) is arranged in the transmission control sleeve (17), one end of the return spring (15) is fixedly connected with the other end of the transmission control rod (11), the other end of the return spring is fixedly arranged on the closed end of the transmission control sleeve (17), the direct-acting electromagnet (18) is arranged in the transmission control sleeve (17), a pin hole (16) is formed in the transmission control rod (11), the controller (13) controls the action of the direct-acting electromagnet (18), when the direct-acting electromagnet (18) is powered off, the direct-acting electromagnet (16) stretches out of the transmission control rod (11) and is matched with the direct-acting electromagnet (11) when the direct-acting electromagnet is powered on the straight-acting electromagnet (16), releasing the limit on the transmission control lever (11).
2. The interception-preventing high-efficiency bouncing type water-entering hit missile according to claim 1, wherein: a plurality of groups of pulleys (14) which are convenient for the head impact transfer rod (3) to move are uniformly arranged in the sliding tube (6).
3. The interception-preventing high-efficiency bouncing type water-entering hit missile according to claim 1, wherein: the head of the missile body (1) is provided with a buffer pad (4) for buffering the impact of the missile body head load reducing device (2) on the missile body (1).
4. An interception efficient bouncing type water-entering hit missile according to claim 3, wherein: the cushion pad (4) is arranged around the sliding tube (6).
5. The interception-preventing high-efficiency bouncing type water-entering hit missile according to claim 1, wherein: the projectile head load-reducing device (2) is of a disc structure.
6. The interception-preventing high-efficiency bouncing type water-entering hit missile according to claim 1, wherein: the inner wall of the bottom of the missile body (1) is provided with a hinge seat connected with one end of a bouncing springboard (5).
7. The anti-interception efficient bouncing water-entering hit missile of claim 6, wherein: the head impact transmission rod (3) is hinged with the first transmission rod (12-1), the bouncing springboard (5) is hinged with a hinge seat at the bottom of the missile body (1), and the second transmission rod (12-2) is hinged with the bouncing springboard (5) through pins (7).
8. The method for operating an anti-interception high-efficiency bouncing type water-entering hit missile according to claim 1, wherein the method comprises the following steps: the method specifically comprises the following steps:
when the missile strikes the water surface, strong impact force is transmitted to a transmission device (12) through a head impact transmission rod (3), one end of the first transmission rod (12-1) connected with the head impact transmission rod (3) is acted by force first, a clockwise moment is generated and starts to rotate towards the tail of the missile body around a fixed rotating shaft (8), and the fixed rotating shaft (8) slides to the top of a chute from the bottom of the chute; the first transmission rod (12-1) drives the second transmission rod (12-2) to move through the rotating shaft (10), the second transmission rod (12-2) is stressed to move towards the lower part of the missile body, the second transmission rod (12-2) drives the bouncing springboard (5) to open and form a supporting mode, and the bouncing springboard (5) enables the missile to jump forward by means of strong reverse thrust of the water surface;
after the missile leaves the water surface, the transmission control device receives a stress signal, after the supporting process of the bouncing springboard (5) is finished, the transmission control rod (11) is recovered to an initial position through the reset spring (15), the transmission control rod (11) drives the rotating shaft (10) to recover the transmission device (12) to an initial state, the transmission device (12) is recovered to the initial state, meanwhile, the bouncing springboard (5) is closed, the head impact transmission rod (3) is retracted along the sliding pipe (6), and the missile finishes a water surface bouncing period;
after the previous period of sliding is completed, the missile body head carrier (2) of the missile impacts the water surface again, and the sliding process is repeated, so that the missile can slide forward towards the target on the near water surface;
after the missile passes through a plurality of water surface sliding processes, the controller (13) receives signals of the sensors, a control instruction is executed after the last sliding process is finished, the controller (13) enables the transmission control rod (11) to be kept fixed by controlling the ejector rod of the direct-acting electromagnet to extend out of the pin hole (16) of the transmission control rod (11), meanwhile, the rotating shaft (10) also keeps fixed, the transmission of the head water collision impact force by the transmission device (12) is stopped, the transmission device (12) is not affected by the impact force transmitted by the head impact transmission rod (3) when the missile impacts the water surface again, meanwhile, the bouncing springboard (5) keeps closed, and the missile achieves the end high-speed water entering striking target.
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