Anti-tank missile launching device

Abstract

The utility model discloses an antitank missile launcher relates to missile launch equipment technical field, the launcher includes side plate and a plurality of bracket subassembly, side plate is used on the vehicle-mounted equipment, a plurality of bracket subassembly is vertically arranged on the side of side plate at interval, each bracket subassembly includes frame body, barrel, locker and stopper, and the side plate is used on the vehicle-mounted equipment. The frame body is provided with a guide rail, the barrel body is provided with supporting legs, the supporting legs are arranged on the guide rail and can slide along the guide rail, the locker and the limiter are arranged on the frame body close to the guide rail, and when the supporting legs slide on the guide rail and the front ends of the supporting legs abut against the limiter, the locker locks the rear ends of the supporting legs. According to the anti-tank missile launching device, the supporting legs are fixed through the locking devices, the supporting legs are tightly held by the limiting devices, mechanical gaps are eliminated, the supporting legs are fixed in multiple directions and do not shake, hoop fixing is not needed, the quality of a missile cylinder shell is guaranteed, the missile cylinder shell can be normally used, the locking devices are easy and convenient to operate, and the anti-tank missile launching device is convenient to use. And the missile disassembling and assembling efficiency is improved.

Description

Technical Field

[0001] The utility model relates to the technical field of missile launching equipment, in particular to an anti-tank missile launching device. Background Art

[0002] In modern warfare, anti-tank missiles play a key role on the battlefield with their high hit rate, great destructive power, concealed launch, and safety for shooters. Among them, the US "Javelin" anti-tank missile has the largest equipment and the most actual combat results. As a light anti-tank missile with infrared thermal imaging self-seeking, "Javelin" can stop controlling the missile after launch. The missile uses the infrared thermal imaging seeker to lock the thermal radiation characteristics of the tank, thereby controlling itself to fly to the target, and the shooter can retreat calmly. At present, in addition to light anti-tank missiles launched by individual soldiers, vehicle-mounted launch of anti-tank missiles is also a very important means of attack. Since anti-tank missiles have no recoil when launched, the requirements for platform installation are low, and the firepower level of the vehicle can be greatly improved, so it has become an urgent need to install anti-tank missiles on vehicle platforms for launch.

[0003] In the prior art, anti-tank missiles are installed on a vehicle-mounted platform via a truss. However, the existing truss uses a clamp to fix the missile, and the clamp holding the missile tube will cause the tube and shell to deform, causing disturbances in the missile launch, affecting the normal use of the missile, and the clamp fixation makes it inconvenient to disassemble and assemble the missile. Utility Model Content

[0004] The embodiment of the utility model provides an anti-tank missile launching device to solve the technical problems in the related art that the existing truss uses a clamp to fix the missile, the clamp holding the missile tube will cause the tube body and the shell to deform, causing the missile launch disturbance, affecting the normal use of the missile, and the clamp fixation makes it inconvenient to disassemble and assemble the missile.

[0005] The utility model embodiment provides an anti-tank missile launching device, comprising:

[0006] Side panels, which are used on vehicle-mounted equipment;

[0007] A plurality of bracket assemblies are vertically spaced apart and arranged on one side of the side plate, each of the bracket assemblies comprising:

[0008] A frame body provided with a guide rail;

[0009] A cylinder body, which is provided with supporting feet, wherein the supporting feet are arranged on the guide rail and can slide along the guide rail;

[0010] The locker and the limiter are both arranged on the frame body close to the guide rail; when the support foot slides on the guide rail and the front end abuts against the limiter, the locker locks the rear end of the support foot.

[0011] In some embodiments, the locking device comprises:

[0012] A fixing seat, the fixing seat is arranged on the outer side of the top end of the frame;

[0013] A lock pin spring, the lock pin spring being arranged in the fixing seat along a horizontal direction;

[0014] A locking pin shaft, wherein the locking pin shaft passes through the locking pin spring, the top end of the locking pin shaft extends to the guide rail and can be retracted along the length direction of the fixed seat, when the supporting foot slides on the guide rail, the supporting foot slides over the top end of the locking pin shaft and compresses the locking pin spring to make the locking pin shaft move away from the guide rail, and after the locking pin spring is reset, the locking pin shaft locks the rear end of the supporting foot.

[0015] In some embodiments, the fixing base comprises:

[0016] A base, one end of which is disposed on the frame, and the other end of which extends to the outside of the frame;

[0017] A handle, which is disposed at the other end of the base and is rotatably connected thereto;

[0018] A lever, one end of which is arranged on the handle, and the other end of which extends to the locking pin shaft, and the handle drives the lever to rotate and stretch the locking pin shaft.

[0019] In some embodiments, the fixing seat further comprises:

[0020] A ball bearing is arranged at the bottom end of the locking pin shaft, and the ball bearing is located between the shifting rod and the handle.

[0021] In some embodiments, the top end of the locking pin shaft is a sloped structure.

[0022] In some embodiments, the stopper comprises:

[0023] A support, the support being arranged at the top of the frame;

[0024] A spring, wherein the spring is arranged in the support in a horizontal direction;

[0025] A limiting shaft, the limiting shaft passes through the spring and can slide along the length direction of the spring;

[0026] A limiting rod is arranged at the top end of the limiting shaft, and when the supporting foot slides on the guide rail, the front end of the supporting foot abuts against the limiting rod.

[0027] In some embodiments, the limiting rod is vertically arranged at the top end of the limiting shaft, and the limiting rod and the limiting shaft form a T-shaped structure.

[0028] In some embodiments, a flange is provided in the middle of the side panel, and the flange is connected to a rotary shaft on the vehicle body equipment, and the side panel can rotate along the circumferential direction of the rotary shaft.

[0029] In some embodiments, the guide rail is a T-shaped structure, and the shape of the supporting foot matches the guide rail.

[0030] In some embodiments, the guide rail is made of steel, and the side panels and the frame are made of aluminum alloy.

[0031] The beneficial effects brought by the technical solution provided by the utility model include:

[0032] The embodiment of the utility model provides an anti-tank missile launcher, including a side plate and a plurality of bracket assemblies, wherein the side plate is used on a vehicle-mounted device, and a plurality of bracket assemblies are vertically spaced on one side of the side plate, and each bracket assembly includes a frame, a cylinder, a locker and a stopper, wherein the frame is provided with a guide rail, and the cylinder is provided with a support foot, wherein the support foot is provided on the guide rail and can slide along the guide rail, and the locker and the stopper are both provided on the frame close to the guide rail, and when the support foot slides on the guide rail and the front end abuts against the stopper, the locker locks the rear end of the support foot. The support foot of the anti-tank missile launcher of the utility model embodiment slides on the guide rail and is fixed by the locker, and the stopper holds the support foot tightly and eliminates the mechanical gap, and fixes the support foot from multiple directions so that it does not shake, and does not need to be fixed with a clamp, thereby ensuring the quality of the missile cylinder shell, so that it can be used normally, and the locker is easy to operate, which improves the efficiency of missile disassembly and assembly. BRIEF DESCRIPTION OF THE DRAWINGS

[0033] In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings required for use in the description of the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without creative work.

[0034] Figure 1 A schematic diagram of the overall structure of an anti-tank missile launcher provided by an embodiment of the utility model;

[0035] Figure 2 A schematic diagram of the specific structure of an anti-tank missile launcher provided by an embodiment of the utility model;

[0036] Figure 3 A schematic diagram of the overall structure of the bracket assembly provided in an embodiment of the utility model;

[0037] Figure 4A schematic diagram of the specific structure of the bracket assembly provided in the embodiment of the utility model;

[0038] Figure 5 A schematic diagram of the structure of the locking device provided by the embodiment of the utility model;

[0039] Figure 6 A schematic diagram of the structure of the limiter provided in the embodiment of the utility model;

[0040] Reference numerals:

[0041] 1. Side panel; 11. Flange;

[0042] 2. Bracket assembly; 21. Frame; 211. Guide rail; 22. Cylinder; 221. Support foot; 23. Locker; 231. Fixed seat; 2311. Base; 2312. Handle; 2313. Lever; 2314. Ball bearing; 232. Lock pin spring; 233. Lock pin shaft; 24. Limiter; 241. Support; 242. Spring; 243. Limit shaft; 244. Limit rod. DETAILED DESCRIPTION

[0043] In order to make the purpose, technical solution and advantages of the embodiment of the utility model clearer, the technical solution in the embodiment of the utility model will be clearly and completely described below in conjunction with the drawings in the embodiment of the utility model. Obviously, the described embodiment is a part of the embodiment of the utility model, not all of the embodiments. Based on the embodiment of the utility model, all other embodiments obtained by ordinary technicians in this field without making creative work are within the scope of protection of the utility model.

[0044] The embodiment of the utility model provides an anti-tank missile launching device, which can solve the technical problems in the related art that the existing truss uses a clamp to fix the missile, the clamp holding the barrel missile will cause its barrel and shell to deform, causing missile launch disturbance, affecting the normal use of the missile, and the clamp fixation makes it inconvenient to disassemble and assemble the missile.

[0045] Figure 1An anti-tank missile launching device provided by an embodiment of the utility model comprises: a side panel 1 and a plurality of bracket assemblies 2, wherein the side panel 1 is used on a vehicle-mounted device, a plurality of the bracket assemblies 2 are vertically spaced apart on one side of the side panel 1, each of the bracket assemblies 2 comprises a frame 21, a cylinder 22, a locker 23 and a limiter 24, the frame 21 is provided with a guide rail 211, the cylinder 22 is provided with a supporting foot 221, the supporting foot 221 is provided on the guide rail 211 and can slide along the guide rail 211, the locker 23 and the limiter 24 are both provided on the frame 21 close to the guide rail 211, and when the supporting foot 221 slides on the guide rail 211 and the front end abuts against the limiter 24, the locker 23 locks the rear end of the supporting foot 221.

[0046] The anti-tank missile launching device of the utility model embodiment is provided with a side plate and a plurality of bracket assemblies, wherein the side plate is used on a vehicle-mounted device, and a plurality of the bracket assemblies are vertically spaced at one side of the side plate, and each of the bracket assemblies comprises a frame, a cylinder, a locker and a limiter, wherein the frame is provided with a guide rail, and the cylinder is provided with a supporting foot, and the supporting foot is provided on the guide rail and can slide along the guide rail, and the locker and the limiter are both provided on the frame close to the guide rail, and when the supporting foot slides on the guide rail, the front end of the supporting foot abuts against the limiter, and the rear end of the supporting foot is locked and fixed by the locker, and the supporting foot is fixed by the locker so that the cylinder will not be displaced, thereby ensuring the stability and safety of the missile, and at the same time, the limiter holds the supporting foot and eliminates the mechanical gap, and fixes the supporting foot from multiple directions so that it does not shake, and there is no need to use a clamp to fix it, thereby ensuring the quality of the missile cylinder shell, so that it can be used normally, and the locker is easy to operate, thereby improving the efficiency of disassembling and assembling the missile.

[0047] As an optional implementation, in a utility model implementation, see Figure 4 and Figure 5As shown, the lock 23 includes: a fixed seat 231, a lock pin spring 232 and a lock pin shaft 233, the fixed seat 231 is arranged on the outer side of the top end of the frame body 21, the lock pin spring 232 is arranged in the fixed seat 231 along the horizontal direction, the lock pin shaft 233 passes through the lock pin spring 232, the top end of the lock pin shaft 233 extends to the guide rail 211 and can be retracted along the length direction of the fixed seat 231, when the support foot 221 slides on the guide rail 211, the support foot 221 slides over the top end of the lock pin shaft 233 to compress the lock pin spring 232 to make the lock pin shaft 233 away from the guide rail 211, and the lock pin spring After the spring 232 is reset, the locking pin shaft 233 locks the rear end of the supporting foot 221. When the cylinder 22 is not installed on the guide rail 211, the top end of the locking pin shaft 233 is located on the guide rail 211. When the supporting foot 221 of the cylinder 22 slides on the guide rail 211, the supporting foot 221 pushes the top end of the locking pin shaft 233 to move the locking pin shaft 233 away from the guide rail 211 and compresses the locking pin spring 232 until the supporting foot 221 slides over the locking pin shaft 233. The locking pin spring 232 is reset and drives the locking pin shaft 233 to reset. At this time, the locking pin shaft 233 locks and fixes the rear end of the supporting foot 221.

[0048] As an optional implementation, in a utility model implementation, see Figure 5 As shown, the fixing seat 231 includes: a base 2311, a handle 2312 and a lever 2313. One end of the base 2311 is arranged on the frame 21, and the other end extends to the outside of the frame 21. The handle 2312 is arranged on the other end of the base 2311 and is rotatably connected thereto. One end of the lever 2313 is arranged on the handle 2312, and the other end extends to the locking pin shaft 233. The handle 2312 drives the lever 2313 to rotate and stretch the locking pin shaft 233. When the cylinder 22 needs to be removed from the guide rail 211, the handle 2312 is pulled along the outer direction of the frame 21, and the handle 2312 drives the lever 2313 to rotate and stretch the locking pin shaft 233. When the cylinder 22 needs to be removed from the guide rail 211, the handle 2312 is pulled along the outer side of the frame 21, and the handle 2312 drives the lever 2313 When the lever 2313 is rotated, and the lever 2313 is connected to the locking pin shaft 233, the lever 2313 further drives the locking pin shaft 233 to extend toward the outside of the frame 21, thereby unlocking the locking device 23, and allowing the supporting foot 221 to slide out of the guide rail 211. Through this structure, the rotational movement of the handle 2312 when unlocking is converted into the translational movement of the locking pin shaft 233. The locking pin shaft 233 is moved by the principle of a labor-saving lever, which amplifies the elastic force of the handle 2312, making it convenient, fast and labor-saving to unlock the locking device 23, thereby improving the efficiency of disassembly and assembly of the missile and reducing the danger of the ammunition replacement operation. At the same time, the handle 2312 is easy to grasp and convenient for personnel to operate.

[0049] As an optional implementation, in a utility model implementation, see Figure 5 As shown, the fixed seat 231 also includes: a ball 2314, which is arranged at the bottom end of the lock pin shaft 233, and the ball 2314 is located between the lever 2313 and the handle 2312. When the handle 2312 drives the lever 2313 to rotate outward, the lever 2313 drives the ball 2314 to further drive the lock pin shaft 233. The sliding friction is converted into rolling friction through the ball 2314, which further reduces the friction force and the bolt opening resistance, thereby improving the smoothness of unlocking the locker 23.

[0050] As an optional implementation, in a utility model implementation, see Figure 5 As shown, the top end of the locking pin shaft 233 is a sloped structure, and the top end of the locking pin shaft 233 is a beveled surface, which is convenient for the supporting foot 221 to push open the top end of the locking pin shaft 233, so that the locking pin shaft 233 is away from the guide rail 211 to unlock the locker 23, and when the supporting foot 221 slides over the locking pin shaft 233, the locking pin spring 232 is reset and drives the locking pin shaft 233 to reset, and then the locking pin shaft 233 locks and fixes the rear end of the supporting foot 221.

[0051] As an optional implementation, in a utility model implementation, see Figure 4 and Figure 6 As shown, the limiter 24 includes: a support 241, a spring 242, a limit shaft 243 and a limit rod 244. The support 241 is arranged at the top of the frame 21, and the spring 242 is arranged in the support 241 along the horizontal direction. The limit shaft 243 passes through the spring 242, and the limit shaft 243 can slide along the length direction of the spring 242. The limit rod 244 is arranged at the top of the limit shaft 243. When the support foot 221 slides on the guide rail 211, the front end of the support foot 221 abuts against the limit rod 244. When the front end of the support foot 221 abuts against the limit rod 244, the limit The positioning rod 244 drives the limiting shaft 243 to slide along the length direction of the support 241 and compress the spring 242, and the axial movable range of the spring 242 is 0 to 3 mm. The spring 242 provides a reaction force to the supporting foot 221, so that the limiting rod 244 can firmly hold the supporting foot 221, and buffer the thrust of the supporting foot 221 to eliminate the mechanical gap between it and the limiting rod 244, thereby ensuring that the cylinder 22 does not shake. At the same time, the vehicle-mounted equipment will generate vibration shock when driving in a field environment, and the spring 242 can absorb part of the impact to ensure that the cylinder 22 will not be impacted and collided.

[0052] As an optional implementation, in a utility model implementation, see Figure 6 As shown, the limit rod 244 is vertically arranged at the top of the limit shaft 243, the limit rod 244 and the limit shaft 243 form a T-shaped structure, the limit rod 244 is fixedly connected to the top of the limit shaft 243, and the limit rod 244 vertically protrudes from the outside of the limit shaft 243, so that the support foot 221 can abut against and push the limit shaft 243.

[0053] As an optional implementation, in a utility model implementation, see Figure 2 As shown, a flange 11 is provided in the middle of the side panel 1, and the flange 11 is connected to the rotary shaft on the vehicle body equipment. The side panel 1 can rotate along the circumferential direction of the rotary shaft. A plurality of the bracket assemblies 2 are fixed to the side panel 1 by screws at intervals, and the middle of the side panel 1 is connected to the rotary shaft on the vehicle body equipment through the flange 11. When the side panel 1 rotates along the circumferential direction of the rotary shaft, the side panel 1 drives the plurality of the bracket assemblies 2 to pitch up and down, and the pitch angle of the bracket assembly 2 can be adjusted arbitrarily to give the cylinder 22 an initial shooting direction. When driving or transporting, the bracket assembly 2 can be turned to an angle of 0 degrees, that is, parallel to the vehicle body, to reduce the height of the bracket assembly 2 and improve its stability.

[0054] As an optional implementation, in a utility model implementation, see Figure 4 As shown, the guide rail 211 is a T-shaped structure, and the shape of the supporting foot 221 matches the guide rail 211. The guide rail 211 adopts a T-shaped structure to facilitate supporting and fixing the supporting foot 221, and the supporting foot 221 slides on the guide rail 211 and along its length direction. The shape of the supporting foot 221 matches the guide rail 211 to reduce the friction between the two, improve the smoothness of the sliding of the supporting foot 221, reduce the friction loss of the guide rail 211, and extend the service life of the guide rail 211.

[0055] As an optional implementation, in a utility model implementation, see Figure 3 As shown, the guide rail 211 is made of steel, and the side panel 1 and the frame 21 are made of aluminum alloy. The guide rail 211 plays the role of matching, friction and limiting. The support foot 221 rubs against the guide rail 211 for a long time. The steel material has good toughness and plasticity, uniform material, and high structural reliability, which greatly improves the durability of the guide rail 211. The frame 21 mainly plays a load-bearing role. The use of aluminum alloy can reduce the overall weight of the bracket assembly 2. The steel guide rail and the aluminum alloy bracket are designed separately to achieve reasonable weight reduction.

[0056] In the description of the present utility model, it should be noted that the terms "upper", "lower", etc. indicate positions or positional relationships based on the positions or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific position, be constructed and operated in a specific position, and therefore cannot be understood as a limitation on the present utility model. Unless otherwise clearly specified and limited, the terms "installed", "connected", and "connected" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be an indirect connection through an intermediate medium, or it can be a connection between the two elements. For those of ordinary skill in the art, the specific meanings of the above terms in the present utility model can be understood according to the specific circumstances.

[0057] It should be noted that, in the present utility model, relational terms such as "first" and "second" are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device. In the absence of further restrictions, the elements defined by the sentence "comprise a ..." do not exclude the existence of other identical elements in the process, method, article or device including the elements.

[0058] The above description is only a specific embodiment of the present invention, so that those skilled in the art can understand or implement the present invention. Various modifications to these embodiments will be obvious to those skilled in the art, and the general principles defined herein can be implemented in other embodiments without departing from the spirit or scope of the present invention. Therefore, the present invention will not be limited to the embodiments shown herein, but will conform to the widest scope consistent with the principles and novel features of the present invention.

Claims

1. An anti-tank missile launcher, characterized in that: include: A side panel (1) for use on vehicle-mounted equipment; A plurality of bracket assemblies (2) are vertically spaced apart and arranged on one side of the side plate (1), and each of the bracket assemblies (2) comprises: A frame (21) provided with a guide rail (211); A cylinder (22) is provided with a supporting foot (221), wherein the supporting foot (221) is provided on the guide rail (211) and can slide along the guide rail (211); A locker (23) and a limiter (24) are both arranged on the frame (21) near the guide rail (211); when the support leg (221) slides on the guide rail (211) and the front end abuts against the limiter (24), the locker (23) locks the rear end of the support leg (221).

2. The anti-tank missile launcher according to claim 1, characterized in that: The locking device (23) comprises: A fixing seat (231), the fixing seat (231) being arranged on the outer side of the top end of the frame (21); A lock pin spring (232), wherein the lock pin spring (232) is arranged in the fixing seat (231) along a horizontal direction; A locking pin shaft (233), the locking pin shaft (233) passes through the locking pin spring (232), the top end of the locking pin shaft (233) extends to the guide rail (211) and can be retracted along the length direction of the fixing seat (231), when the supporting foot (221) slides on the guide rail (211), the supporting foot (221) slides over the top end of the locking pin shaft (233) to compress the locking pin spring (232) so that the locking pin shaft (233) is away from the guide rail (211), and after the locking pin spring (232) is reset, the locking pin shaft (233) locks the rear end of the supporting foot (221).

3. The anti-tank missile launcher according to claim 2, characterized in that: The fixing seat (231) comprises: A base (2311), one end of the base (2311) is arranged on the frame (21), and the other end extends to the outside of the frame (21); A handle (2312), the handle (2312) being disposed at the other end of the base (2311) and rotatably connected thereto; A lever (2313), one end of which is disposed on the handle (2312), and the other end of which extends to the lock pin shaft (233); the handle (2312) drives the lever (2313) to rotate and stretch the lock pin shaft (233).

4. The anti-tank missile launcher according to claim 3 is characterized in that: The fixing seat (231) further comprises: A ball (2314), wherein the ball (2314) is disposed at the bottom end of the lock pin shaft (233), and the ball (2314) is located between the lever (2313) and the handle (2312).

5. The anti-tank missile launcher according to claim 2, characterized in that: The top end of the locking pin shaft (233) is an inclined surface structure.

6. The anti-tank missile launcher according to claim 1, characterized in that: The stopper (24) comprises: A support (241), wherein the support (241) is disposed at the top of the frame (21); A spring (242), wherein the spring (242) is arranged in the support (241) along a horizontal direction; A limiting shaft (243), wherein the limiting shaft (243) passes through the spring (242), and the limiting shaft (243) can slide along the length direction of the spring (242); A limiting rod (244), wherein the limiting rod (244) is arranged at the top end of the limiting shaft (243), and when the supporting foot (221) slides on the guide rail (211), the front end of the supporting foot (221) abuts against the limiting rod (244).

7. The anti-tank missile launcher according to claim 6, characterized in that: The limiting rod (244) is vertically arranged at the top end of the limiting shaft (243), and the limiting rod (244) and the limiting shaft (243) form a T-shaped structure.

8. The anti-tank missile launcher according to claim 1, characterized in that: A flange (11) is provided in the middle of the side plate (1), and the flange (11) is connected to a rotary shaft on the vehicle body equipment, and the side plate (1) can rotate along the circumferential direction of the rotary shaft.

9. The anti-tank missile launcher according to claim 1, characterized in that: The guide rail (211) is a T-shaped structure, and the shape of the supporting foot (221) matches the guide rail (211).

10. The anti-tank missile launcher according to claim 1, characterized in that: The guide rail (211) is made of steel, and the side plate (1) and the frame (21) are made of aluminum alloy.

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