Typical warhead-fuze collaborative weapon system

Abstract

The invention discloses a typical warhead-fuze collaborative weapon system, and belongs to the technical field of ammunition fuze, the typical warhead-fuze collaborative weapon system comprises a shell, a fuze module, a guidance cabin, a warhead, a detonation module and a fuel cabin are arranged in the shell, the fuze module is located at one end of the shell, the fuel cabin is located at the other end of the shell, and the warhead is located in the middle of the shell; the guidance cabin is located between the fuze module and the warhead, and the detonation module is located between the warhead and the fuel cabin. According to the typical warhead-fuze collaborative weapon system, the collaborative performance is optimized, and efficient collaboration among the warhead, the fuze module and the explosion tube is achieved through innovative module arrangement and connection design; the environmental adaptability is improved, structural strengthening and adaptability design are carried out on key modules of the system for high-altitude, high-temperature and other complex combat environments, and reliable operation of the system is ensured; and through the heat insulation design and multi-layer protection, the isolation performance of the warhead and the fuel cabin is improved, and accidental explosion caused by heat transfer is prevented.

Description

Technical Field

[0001] The present invention relates to the technical field of detection equipment, and in particular to a typical warhead-fuze coordinated weapon system. Background Art

[0002] In the existing technology, with the continuous development of modern military technology, the design of warheads and fuzes has become a key factor in the development of weapon systems. In the existing technology, the designs of warheads and fuzes are mostly independently developed and lack systematic collaborative design, which may lead to problems such as fuze trigger failure and unstable performance in actual combat.

[0003] The prior art has the following deficiencies: (1) The design of the warhead and fuze lacks comprehensive optimization, and the synergy between the two cannot be fully utilized.

[0004] (2) It has poor adaptability to combat environments and cannot work stably in complex environments.

[0005] (3) Safety and reliability are not high enough, and the risk of false triggering and functional failure is high.

[0006] Therefore, there is an urgent need for a design method that can improve the coordinated performance between the warhead and the fuze. Summary of the invention

[0007] The purpose of the present invention is to provide a typical warhead-fuze coordinated weapon system, optimize the coordinated performance, and realize efficient coordination between the warhead, the fuze module and the explosive tube through innovative module layout and connection design; improve environmental adaptability, and structurally strengthen and adapt the key modules of the system for complex combat environments such as high altitude and high temperature to ensure reliable operation of the system; enhance safety, and improve the isolation between the warhead and the fuel tank through thermal insulation design and multi-layer protection to prevent accidental explosion caused by heat transfer.

[0008] To achieve the above-mentioned objectives, the present invention provides a typical warhead-fuze coordinated weapon system, comprising an outer shell, wherein a fuze module, a guidance cabin, a warhead, a detonation module and a fuel tank are arranged inside the outer shell, the fuze module is located at one end of the outer shell, the fuel tank is located at the other end of the outer shell, the warhead is located in the middle of the outer shell, the guidance cabin is located between the fuze module and the warhead, and the detonation module is located between the warhead and the fuel tank.

[0009] Preferably, the warhead comprises a prefabricated fragmentation explosion tube, the interior of the prefabricated fragmentation explosion tube is filled with explosive charge, a conical explosive cover is provided at one end of the charge close to the guidance cabin, a central explosion tube is provided at the center of the charge, and the central explosion tube is coaxially arranged with the prefabricated fragmentation explosion tube.

[0010] Preferably, the prefabricated fragmentation explosion tube is made of a high-strength alloy material, prefabricated fragments are distributed inside the tube wall, and the prefabricated fragmentation explosion tube is electrically connected to the central explosion tube and the fuse module.

[0011] Preferably, the fuze module includes an environment sensing unit and a control unit.

[0012] Preferably, the fuel tank is of layered sealing design, the space between the fuel tank and the warhead is filled with thermal insulation material, and the detonation module is located at the center of the thermal insulation material.

[0013] Therefore, the present invention adopts the above-mentioned typical warhead-fuze coordinated weapon system, which has the following beneficial effects: (1) Optimizing synergy performance: Through innovative module layout and connection design, efficient synergy between the warhead, fuze module and explosive tube is achieved; (2) Improving environmental adaptability: In view of complex combat environments such as high altitude and high temperature, the key modules of the system are structurally strengthened and designed for adaptability to ensure reliable operation of the system; (3) Enhanced safety: Through thermal insulation design and multi-layer protection, the isolation between the warhead and the fuel tank is improved to prevent accidental explosion caused by heat transfer.

[0014] The technical solution of the present invention is further described in detail below through the accompanying drawings and embodiments. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 It is a schematic diagram of the structure of a typical warhead-fuze coordinated weapon system of the present invention.

[0016] Reference numerals 1. Fuze module; 2. Guidance cabin; 3. Prefabricated fragmentation explosion tube; 4. Central explosion tube; 5. Charge; 6. Detonation module; 7. Fuel tank; 8. Casing. DETAILED DESCRIPTION

[0017] The technical solution of the present invention is further described below through the accompanying drawings and embodiments.

[0018] Unless otherwise defined, the technical terms or scientific terms used in the present invention should be understood by people with ordinary skills in the field to which the present invention belongs. The words "first", "second" and similar words used in the present invention do not indicate any order, quantity or importance, but are only used to distinguish different components. "Include" or "comprise" and similar words mean that the elements or objects appearing before the word include the elements or objects listed after the word and their equivalents, without excluding other elements or objects. "Connect" or "connected" and similar words are not limited to physical or mechanical connections, but may include electrical connections, whether direct or indirect. "Up", "down", "left", "right" and the like are only used to indicate relative positional relationships. When the absolute position of the described object changes, the relative positional relationship may also change accordingly.

[0019] like Figure 1 As shown, the present invention provides a typical warhead-fuze coordinated weapon system, including a shell 8, inside which are arranged a fuze module 1, a guidance cabin 2, a warhead, an initiation module 6 and a fuel tank 7. The fuze module 1 is located at one end of the shell 8, and the fuze module 1 includes an environmental sensing unit and a control unit. The fuze module 1 is used for target detection, data analysis and explosion triggering control. The fuze module 1 can adapt to a variety of combat environments, including high altitude and high temperature conditions, to ensure the reliability of the environmental sensing unit and the control module.

[0020] The fuel tank 7 is located at the other end of the outer shell 8. The fuel tank 7 is a layered sealing design, which provides power for the system to support flight or guidance, and is used to ensure the stability of the power supply of the weapon system in a high temperature and high pressure environment. The warhead is located in the middle of the outer shell 8, installed in the core part of the weapon system, and is used to store the explosive device and work in conjunction with the fuze module 1. The warhead includes a prefabricated fragmentation explosion tube 3, which is used to achieve directional killing or explosion effects under the control of the fuze.

[0021] The prefabricated fragmentation explosion tube 3 is filled with a charge 5. When the charge 5 explodes, it releases huge energy in a very short time, causing the surrounding medium to be strongly impacted and compressed. A conical charge cover is provided at one end of the charge 5 close to the guidance cabin 2. The conical charge cover can focus the energy generated by the explosion of the charge 5 to effectively damage the target. A central explosion tube 4 is provided at the center of the charge 5. The central explosion tube 4 is coaxially arranged with the prefabricated fragmentation explosion tube 3 to enhance the explosion power and cooperate with the warhead to achieve multi-point strikes.

[0022] The prefabricated fragmentation explosion tube 3 is made of high-strength alloy material, and prefabricated fragments are distributed inside the tube wall to achieve directional explosion and improve killing accuracy. The prefabricated fragmentation explosion tube 3 is electrically connected to the central explosion tube 4 and the fuze module 1 to achieve directional killing or explosion effect under the control of the fuze module 1.

[0023] The guidance cabin 2 is located between the fuze module 1 and the warhead, and the detonation module 6 is located between the warhead and the fuel cabin 7. The fuel cabin 7 and the warhead are filled with heat insulation material, and the detonation module 6 is located at the center of the heat insulation material. The heat insulation material is used to prevent heat transfer between the explosive device and the fuel to ensure the safety of the system. The detonation module 6 can trigger the warhead charge 5 to explode at the most appropriate time point according to the predetermined combat requirements.

[0024] Embodiment 1 The shell 8 of the prefabricated fragmentation explosion tube 3 is made of high-strength titanium alloy, and the prefabricated fragments are made of tungsten alloy. The shell 8 of the central explosion tube 4 is made of nickel-based high-temperature alloy, and the outer packaging material of the charge 5 is made of polymer composite material. The warhead's explosive cover material is copper, and the shell 8 of the fuze module 1 is made of magnesium-aluminum alloy. The environmental sensing unit uses a pressure sensor and a laser ranging element, and the laser ranging element uses an aluminum alloy shell 8 and high-temperature resistant optical glass. The detonation module 6 uses a miniature high-energy electric spark initiator.

[0025] Embodiment 2 The shell 8 of the prefabricated fragmentation explosion tube 3 is made of aluminum-lithium alloy, and the prefabricated fragments are made of high-density ceramic material. The shell 8 of the central explosion tube 4 is made of titanium-aluminum intermetallic compound, and the outer packaging material of the charge 5 is made of aramid fiber composite material. The charge liner of the warhead is made of polyimide material. The shell 8 of the fuze module 1 is made of carbon fiber reinforced composite material, the environmental perception unit is made of infrared thermal imaging sensor and ultrasonic distance sensor, and the infrared sensor lens is made of germanium material. The detonation module 6 uses a laser detonator.

[0026] Embodiment 3 The shell 8 of the prefabricated fragmentation explosion tube 3 is made of high-strength stainless steel, and the prefabricated fragments are made of beryllium copper alloy. The shell 8 of the central explosion tube 4 is made of ceramic-based composite materials, and the outer packaging material of the charge 5 is made of polymer thermosetting resin. The charge liner of the warhead is made of aluminum alloy. The shell 8 of the fuze module 1 is made of titanium alloy, the environmental perception unit uses a MEMS air pressure sensor and a millimeter wave radar, and the shell 8 of the millimeter wave radar is made of polyamide plastic. The detonation module 6 uses an electronic ignition system with high-temperature resistant tungsten electrodes.

[0027] Embodiment 4 The shell 8 of the prefabricated fragmentation explosion tube 3 is made of high-strength composite ceramic material, and the prefabricated fragments are made of nickel-cobalt alloy. The shell 8 of the central explosion tube 4 is made of titanium-zirconium alloy, and the outer packaging material of the charge 5 is made of liquid crystal polymer. The charge liner of the warhead is made of tungsten alloy. The shell 8 of the fuze module 1 is made of high-strength aramid fiber composite material, the environmental perception unit uses a radar altimeter and a magnetic sensor, and the radar altimeter uses a special aluminum alloy shell 8. The detonation module 6 uses an explosive electromagnetic detonator.

[0028] Embodiment 5 The shell 8 of the prefabricated fragmentation explosion tube 3 is made of nickel-based alloy, and the prefabricated fragments are made of tempered ceramics. The shell 8 of the central explosion tube 4 is made of stainless steel composite material, and the outer packaging material of the charge 5 is made of multi-layer polyethylene film. The warhead's explosive cover is made of tantalum. The shell 8 of the fuze module 1 is made of polycarbonate material, the environmental perception unit uses a multifunctional environmental monitoring sensor and a short-wave infrared ranging sensor, and the short-wave infrared ranging element uses silicon-based coated glass. The detonation module 6 uses a mechanically triggered detonator.

[0029] Embodiment 6 The shell 8 of the prefabricated fragmentation explosion tube 3 is made of steel alloy, and the prefabricated fragments are made of high-hardness tungsten steel material. The shell 8 of the central explosion tube 4 is made of aluminum-magnesium alloy, and the outer packaging material of the charge 5 is made of special silicone rubber. The charge liner of the warhead is made of titanium alloy. The shell 8 of the fuze module 1 is made of ceramic composite material, the environmental perception unit uses a piezoelectric vibration sensor and a laser scanning ranging sensor, and the shell 8 of the laser scanning module is made of aluminum oxide coating. The detonation module 6 uses a piezoelectric crystal to trigger the detonation device.

[0030] Therefore, the present invention adopts the above-mentioned typical warhead-fuze coordinated weapon system to optimize the coordinated performance, and realizes efficient coordination between the warhead, the fuze module and the explosive tube through innovative module layout and connection design; improves environmental adaptability, and structurally strengthens and adapts the key modules of the system for complex combat environments such as high altitude and high temperature to ensure reliable operation of the system; enhances safety, and improves the isolation between the warhead and the fuel tank through thermal insulation design and multi-layer protection to prevent accidental explosions caused by heat transfer.

[0031] Finally, it should be noted that the above embodiments are only used to illustrate the technical solution of the present invention rather than to limit it. Although the present invention has been described in detail with reference to the preferred embodiments, those skilled in the art should understand that they can still modify or replace the technical solution of the present invention with equivalents, and these modifications or equivalent replacements cannot cause the modified technical solution to deviate from the spirit and scope of the technical solution of the present invention.

Claims

1. A typical warhead-fuze coordinated weapon system, characterized in that: It includes an outer shell, inside which are arranged a fuze module, a guidance cabin, a warhead, a detonation module and a fuel tank. The fuze module is located at one end of the outer shell, the fuel tank is located at the other end of the outer shell, the warhead is located in the middle of the outer shell, the guidance cabin is located between the fuze module and the warhead, and the detonation module is located between the warhead and the fuel tank.

2. A typical warhead-fuze coordinated weapon system according to claim 1, characterized in that: The warhead includes a prefabricated fragmentation blasting tube, which is filled with explosives. A conical explosive cover is provided at one end of the charge close to the guidance cabin, and a central blasting tube is provided at the center of the charge. The central blasting tube is coaxially arranged with the prefabricated fragmentation blasting tube.

3. A typical warhead-fuze coordinated weapon system according to claim 2, characterized in that: The prefabricated fragmentation explosion tube is made of high-strength alloy material, and prefabricated fragments are distributed inside the tube wall. The prefabricated fragmentation explosion tube is electrically connected to the central explosion tube and the fuze module.

4. A typical warhead-fuze coordinated weapon system according to claim 1, characterized in that: The fuze module includes an environment sensing unit and a control unit.

5. A typical warhead-fuze coordinated weapon system according to claim 1, characterized in that: The fuel tank adopts a layered sealing design. The space between the fuel tank and the warhead is filled with insulation material, and the detonation module is located in the center of the insulation material.

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