Missile launcher

Abstract

The utility model discloses a missile launcher, relates to missile launching equipment technical field, said missile launcher includes: base, pitching subassembly and rotating device, be equipped with the support frame of height adjustable on the base, the pitching subassembly is equipped with the support frame top end and can rotate up and down around its top end, and the rotating device is equipped with the rotating device. A hoop assembly for installing a missile is arranged on one side of the pitching assembly, the rotating device is arranged at the bottom end of the supporting frame and can rotate in the circumferential direction of the supporting frame, and a height-adjustable seat is arranged on the rotating device. According to the missile launcher, the pitching angle of a missile and the height of the launcher are adjusted through the pitching assembly, the direction and the height of the seat are adjusted through the rotating device, operation of personnel of different body types can be met, angle and height adjustment is convenient, man-machine operation is convenient, and practicability is improved.

Description

Technical Field

[0001] The utility model relates to the technical field of missile launching equipment, in particular to a missile launching rack. Background Art

[0002] A missile launch system refers to a special device used to support missiles and determine their direction, prepare for launch, and implement launches. In recent years, in order to improve the mobility of missile weapon systems, many modern missile launchers are also missile transportation equipment. The most common of these is the missile launcher used to suspend and launch missiles on aircraft. Currently, missiles with a launch weight of less than 25kg are mostly launched by a launcher or directly carried on the shoulder to complete the launch mission. Before the missile is carried on the shoulder or launched by a tripod, it is often necessary to conduct multiple rounds of remote control launches through the missile launcher, and then transition to shoulder or tripod launch after the missile launch is stable.

[0003] However, the launcher height, seat height and direction of existing missile launchers are not easy to adjust, making it difficult to meet the needs of personnel of different body sizes, resulting in inconvenience in human-machine operation. Utility Model Content

[0004] The embodiment of the utility model provides a missile launcher to solve the technical problem in the related art that the existing missile launcher is difficult to meet the needs of people with different body shapes, resulting in inconvenience in human-machine operation.

[0005] The utility model provides a missile launcher, comprising:

[0006] A base, wherein a height-adjustable support frame is provided on the base;

[0007] A pitch assembly, which is arranged at the top of the support frame and can rotate up and down around the top of the support frame, and a hoop assembly for mounting the missile is provided on one side of the pitch assembly;

[0008] A rotating device is arranged at the bottom end of the support frame and can rotate along the circumferential direction thereof, and a height-adjustable seat is arranged on the rotating device.

[0009] In some embodiments, the pitch assembly includes:

[0010] A pitching machine, the pitching machine is arranged at the top of the support frame, and a corresponding adapter flange is arranged on one side of the pitching machine;

[0011] A cradle is arranged on both sides of the pitching machine, and the middle part of the cradle is rotatably connected to the adapter flange, and the cradle can rotate up and down around the pitching machine.

[0012] In some embodiments, the pitch assembly further comprises:

[0013] A first telescopic rod is arranged at the bottom end of the pitch machine and is slidably connected to the top end of the support frame. A top screw is correspondingly arranged on one side of the top end of the support frame in the vertical direction, and a locking pin is arranged on the other side. The top screw cooperates with the locking pin to adjust the height of the first telescopic rod.

[0014] In some embodiments, a protective plate is further provided on the top of the cradle.

[0015] In some embodiments, the rotating device further comprises:

[0016] A support, one end of which is disposed at the bottom end of the support frame, and the other end of which extends to the outside of the support frame and is connected to the seat;

[0017] An azimuth adjuster is disposed below the support and is used to adjust the rotational azimuth of the support.

[0018] In some embodiments, a slide groove is further provided under the support, a second telescopic rod is provided in the slide groove, a top end of the second telescopic rod is connected to the seat, and the second telescopic rod can slide along the length direction of the slide groove.

[0019] In some embodiments, the orientation adjuster comprises:

[0020] A slewing support, the slewing support is arranged below the support;

[0021] A latch seat, the latch seat being arranged at one side of the slewing support, and a spring being arranged inside the latch seat;

[0022] A latch, the latch being arranged in the middle of the spring and sliding along the length direction of the latch seat;

[0023] A limit platform is arranged below the latch seat, and the latch is engaged with the limit platform.

[0024] In some embodiments, a slot is provided on the latch seat, and a pin is provided on the top of the latch, and the pin is engaged with the slot.

[0025] In some embodiments, an adjustment handle is further provided under the seat.

[0026] In some embodiments, the support frame comprises:

[0027] Three universally adjustable foot cups, each of which is arranged on the base;

[0028] A triangular support arm, wherein one leg of the triangular support arm is correspondingly connected to one of the universally adjustable foot cups;

[0029] A support rod is vertically arranged on the top of the triangular support arm.

[0030] The beneficial effects brought by the technical solution provided by the utility model include:

[0031] The embodiment of the utility model provides a missile launcher, which includes: a base, a pitch assembly and a rotating device, the base is provided with a height-adjustable support frame, the pitch assembly is provided at the top of the support frame and can rotate up and down around the top of the support frame, a hoop assembly for installing missiles is provided on one side of the pitch assembly, the rotating device is provided at the bottom of the support frame and can rotate along its circumferential direction, and a height-adjustable seat is provided on the rotating device. The missile launcher of the utility model adjusts the pitch angle of the missile and the height of the launcher through the pitch assembly, and adjusts the orientation and height of the seat through the rotating device, which can meet the needs of people of different body shapes to operate, and the angle and height are easy to adjust, the human-machine operation is convenient, and one machine can be used for multiple purposes, thereby improving its practicality. BRIEF DESCRIPTION OF THE DRAWINGS

[0032] 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.

[0033] Figure 1 A schematic diagram of the structure of a missile launcher provided by an embodiment of the utility model;

[0034] Figure 2 A schematic diagram of the structure of a pitch assembly provided in an embodiment of the utility model;

[0035] Figure 3 A schematic diagram of the structure of a rotating device provided in an embodiment of the utility model;

[0036] Figure 4 A schematic cross-sectional view of a rotating device provided in an embodiment of the utility model;

[0037] Figure 5 A schematic diagram of the overall structure of the azimuth adjuster provided in an embodiment of the utility model;

[0038] Figure 6 A schematic diagram of the specific structure of the azimuth adjuster provided in the embodiment of the utility model;

[0039] Reference numerals:

[0040] 1. Base; 11. Support frame; 111. Universal adjustment foot cup; 112. Triangular support arm; 113. Support rod;

[0041] 2. Pitch assembly; 21. Clamp assembly; 22. Pitch machine; 221. Adapter flange; 23. Cradle; 231. Protective plate; 24. First telescopic rod; 241. Top screw; 242. Locking pin;

[0042] 3. Rotating device; 31. Seat; 311. Adjusting handle; 32. Support; 321. Slide; 3211. Second telescopic rod; 33. Azimuth adjuster; 331. Rotating support; 332. Latch seat; 3321. Spring; 3322. Slot; 333. Latch; 3331. Pin; 334. Limiting table. 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 creative work are within the scope of protection of the utility model.

[0044] The embodiment of the utility model provides a missile launcher, which can solve the technical problem in the related art that the existing missile launcher is difficult to meet the needs of people with different body shapes, resulting in inconvenience in human-machine operation.

[0045] Figure 1 A missile launcher provided by an embodiment of the utility model comprises: a base 1, a pitch assembly 2 and a rotating device 3, wherein the base 1 is provided with a height-adjustable support frame 11, the pitch assembly 2 is arranged at the top of the support frame 11 and can rotate up and down around its top, a hoop assembly 21 for mounting a missile is provided on one side of the pitch assembly 2, the rotating device 3 is arranged at the bottom of the support frame 11 and can rotate along its circumferential direction, and a height-adjustable seat 31 is provided on the rotating device 3.

[0046] The missile launcher of the utility model is provided with a base, a pitch assembly and a rotating device. The base is provided with a height-adjustable support frame. The pitch assembly is provided at the top of the support frame and can rotate up and down around the top of the support frame. A hoop assembly for installing missiles is provided on one side of the pitch assembly. The rotating device is provided at the bottom of the support frame and can rotate along its circumferential direction. A height-adjustable seat is provided on the rotating device. The missile launcher of the utility model adjusts the pitch angle of the missile and the height of the launcher through the pitch assembly, and adjusts the orientation and height of the seat through the rotating device, which can meet the needs of people of different body shapes to operate. The angle and height are easy to adjust, and the human-machine operation is convenient, which improves the practicality and versatility. The launcher as a whole can also be disassembled for easy transportation, which reduces the use and manufacturing costs.

[0047] As an optional implementation, in a utility model embodiment, see Figure 1 and Figure 2 As shown, the pitch assembly 2 includes: a pitch machine 22 and a cradle 23, the pitch machine 22 is arranged at the top of the support frame 11, one side of the pitch machine 22 is correspondingly provided with an adapter flange 221, the cradle 23 is arranged on both sides of the pitch machine 22, and the middle part of the cradle 23 is rotatably connected to the adapter flange 221, the cradle 23 can rotate up and down around the pitch machine 22, the pitch machine 22 is fixed to the top of the support frame 11, the clamp assembly 21 is four clamps, and each two clamps The clamp is arranged on one side of the cradle 23 for installing the missile, and the cradle 23 is a bilaterally symmetrical structure. A corresponding adapter flange 221 is provided on one side of the pitch machine 22. A fixing frame is provided in the middle of one side of the cradle 23. The fixing frame is rotatably connected to one of the adapter flanges 221. The cradle 23 can rotate up and down around the pitch machine 22 through the adapter flange 221. The up and down rotation of the cradle 23 further drives the missile to rotate up and down, thereby realizing the adjustment of the missile launch angle.

[0048] As an optional implementation, in a utility model embodiment, see Figure 3 and Figure 4 As shown, the pitch assembly 2 also includes: a first telescopic rod 24, which is arranged at the bottom end of the pitch machine 22 and is slidably connected to the top of the support frame 11, one side of the top of the support frame 11 is correspondingly provided with a top screw 241 in the vertical direction, and the other side is provided with a locking pin 242, the top screw 241 and the locking pin 242 cooperate to adjust the height of the first telescopic rod 24, the top screw 241 can move in the vertical direction of the support frame 11, and a plurality of pin holes are provided inside the first telescopic rod 24 in the vertical direction, the locking pin 242 is engaged with the pin holes, and when the first telescopic rod 24 slides upward, the top screw is moved upward in the vertical direction of the support frame 11 241, the top screw 241 is used to support the first telescopic rod 24 until the first telescopic rod 24 rises to a preset height, and then the locking pin 242 is pressed to engage with the pin hole to fix the current position of the first telescopic rod 24. When the first telescopic rod 24 slides downward, the locking pin 242 is first pressed to disconnect the locking pin 242 from the pin hole, and then the top screw 241 is moved downward along the vertical direction of the support frame 11 until the first telescopic rod 24 drops to a preset height or the first telescopic rod 24 is completely retracted into the support frame 11. The height of the pitch mechanism 22 can be adjusted through this structure, and the operation is simple.

[0049] As an optional implementation, in a utility model embodiment, see Figure 1 As shown, a protective plate 231 is also provided on the top of the cradle 23. The protective plate 231 is used to protect the operator and prevent the wake of the missile from hurting the operator during the missile launch. The protective plate 231 is made of transparent tempered glass or acrylic plate material, which is convenient for the operator to aim at the target.

[0050] As an optional implementation, in a utility model embodiment, see Figure 3 As shown, the rotating device 3 also includes: a support 32 and an azimuth adjuster 33, one end of the support 32 is arranged at the bottom end of the support frame 11, and the other end extends to the outside of the support frame 11 and is connected to the seat 31, the azimuth adjuster 33 is arranged below the support 32, and is used to adjust the rotation azimuth of the support 32, the seat 31 is connected to the bottom end of the support frame 11 through the support 32, and the support 32 is rotated along the circumferential direction of the support frame 11 through the azimuth adjuster 33, the support 32 further drives the seat 31 to rotate along the circumferential direction of the support frame 11, so as to realize the adjustment of the azimuth of the seat 31.

[0051] As an optional implementation, in a utility model embodiment, see Figure 3 As shown, a slide groove 321 is further provided below the support 32, and a second telescopic rod 3211 is provided in the slide groove 321. The top end of the second telescopic rod 3211 is connected to the seat 31, and the second telescopic rod 3211 can slide along the length direction of the slide groove 321. The slide groove 321 is arranged below the support 32 in the vertical direction and is fixedly connected thereto, and an adjustment hole and an adjustment bolt are provided on the slide groove 321. When the second telescopic rod 3211 slides outward along the length direction of the slide groove 321, the adjustment bolt is first loosened to extend the second telescopic rod 3211, and the second telescopic rod 3211 drives the seat 31 away from the support frame. 11, until the second telescopic rod 3211 is adjusted to a preset length, tighten the adjusting bolt to fix the current position of the second telescopic rod 3211, when the second telescopic rod 3211 slides inward along the length direction of the slide slot 321, first loosen the adjusting bolt to shorten the second telescopic rod 3211, and the second telescopic rod 3211 drives the seat 31 to approach the support frame 11, until the second telescopic rod 3211 is adjusted to a preset length, tighten the adjusting bolt to fix the current position of the second telescopic rod 3211, and the distance between the seat 31 and the support frame 11 can be adjusted through this structure, which can be suitable for operation by people of different body shapes.

[0052] As an optional implementation, in a utility model embodiment, see Figure 4 and Figure 6As shown, the orientation adjuster 33 includes: a swivel support 331, a latch seat 332, a latch 333 and a limit platform 334, the swivel support 331 is arranged below the support 32, the latch seat 332 is arranged on one side of the swivel support 331, a spring 3321 is arranged inside the latch seat 332, the latch 333 is arranged in the middle of the spring 3321, and the latch 333 slides along the length direction of the latch seat 332, the limit platform 334 is arranged below the latch seat 332, the latch 333 is clamped with the limit platform 334, the swivel support 331 is provided with a bearing and can rotate along the circumferential direction of the support frame 11, then the swivel support 331 drives the support 32 to further drive the seat 31 along the support frame 11 Rotate in the circumferential direction. When the seat 31 needs to be rotated, lift the pin 333 to make its bottom end away from the limit platform 334. When the personnel perform the launching operation, the swivel support 331 and the support frame 11 are in a rotatable state, and the operator can adjust the orientation of the seat 31 at any time. When the seat 31 does not rotate and needs to be fixed, press the pin 333 downward to make the bottom end of the pin 333 protrude from the pin seat 332 and be stuck in the limit platform 334. At this time, the pin 333 limits the rotation of the swivel support 331 and fixes the position of the seat 31. When the pin 333 is lifted and away from the limit platform 334, the swivel support 331 can be rotated along the circumferential direction of the support frame 11 to adjust the orientation of the seat 31.

[0053] As an optional implementation, in a utility model embodiment, see Figure 5 and Figure 6 When the cam 332 is in the unlock state, the locking cam 333 is in the unlock state, and the locking cam 333 is in the unlock state.

[0054] As an optional implementation, in a utility model embodiment, see Figure 3As shown, an adjustment handle 311 is further provided under the seat 31, and the adjustment handle 311 is used to adjust the height of the seat 31, so that the seat 31 can be operated by people of different heights, thereby improving the practicality of the utility model.

[0055] As an optional implementation, in a utility model embodiment, see Figure 1 and Figure 6 As shown, the support frame 11 includes: three universal adjustment foot cups 111, a triangular support arm 112 and a support rod 113, each of the universal adjustment foot cups 111 is arranged on the base 1, one leg of the triangular support arm 112 is connected to a corresponding universal adjustment foot cup 111, the support rod 113 is arranged on the top of the triangular support arm 112 in the vertical direction, the universal adjustment foot cup 111 is fixedly connected to the base 1, a screw is vertically provided at the middle of the universal adjustment foot cup 111, one leg of the triangular support arm 112 is connected to a corresponding screw of the universal adjustment foot cup 111, and the connection height of each leg and the screw is adjustable, so the overall height of the support frame 11 is also adjustable, and the triangular support arm 112 is used to support the support rod 113 and the pitch assembly 2, while ensuring the stability and horizontality of the support rod 113 and the pitch assembly 2.

[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. A missile launcher, characterized in that: include: A base (1), wherein the base (1) is provided with a height-adjustable support frame (11); A pitch assembly (2), the pitch assembly (2) being arranged at the top end of the support frame (11) and being capable of rotating up and down around the top end thereof, and a hoop assembly (21) for mounting a missile being arranged on one side of the pitch assembly (2); A rotating device (3) is arranged at the bottom end of the support frame (11) and can rotate along the circumferential direction thereof, and a height-adjustable seat (31) is arranged on the rotating device (3).

2. The missile launcher according to claim 1, characterized in that: The pitch assembly (2) comprises: A pitching machine (22), the pitching machine (22) being arranged at the top end of the support frame (11), and a corresponding adapter flange (221) being arranged on one side of the pitching machine (22); A cradle (23) is provided on both sides of the pitching machine (22), and the middle part of the cradle (23) is rotatably connected to the adapter flange (221), and the cradle (23) can rotate up and down around the pitching machine (22).

3. The missile launcher according to claim 2, characterized in that: The pitch assembly (2) further comprises: A first telescopic rod (24), the first telescopic rod (24) being arranged at the bottom end of the pitch machine (22) and being slidably connected to the top end of the support frame (11), a top screw (241) being arranged on one side of the top end of the support frame (11) in a vertical direction, and a locking pin (242) being arranged on the other side, the top screw (241) and the locking pin (242) cooperating to adjust the height of the first telescopic rod (24).

4. The missile launcher according to claim 2, characterized in that: A protective plate (231) is also provided at the top of the cradle (23).

5. The missile launcher according to claim 1, characterized in that: The rotating device (3) further comprises: A support (32), one end of the support (32) being arranged at the bottom end of the support frame (11), and the other end of the support (32) extending to the outside of the support frame (11) and connected to the seat (31); An azimuth adjuster (33), the azimuth adjuster (33) being arranged below the support (32) and being used for adjusting the rotational azimuth of the support (32).

6. The missile launcher according to claim 5, characterized in that: A slide groove (321) is also provided below the support (32), and a second telescopic rod (3211) is provided in the slide groove (321). The top end of the second telescopic rod (3211) is connected to the seat (31), and the second telescopic rod (3211) can slide along the length direction of the slide groove (321).

7. The missile launcher according to claim 5, characterized in that: The azimuth regulator (33) comprises: A slewing support (331), wherein the slewing support (331) is disposed below the support (32); A latch seat (332), the latch seat (332) being arranged on one side of the rotary support (331), and a spring (3321) being arranged inside the latch seat (332); A latch (333), wherein the latch (333) is disposed in the middle of the spring (3321), and the latch (333) slides along the length direction of the latch seat (332); A limiting platform (334) is provided below the latch seat (332), and the latch (333) is engaged with the limiting platform (334).

8. The missile launcher according to claim 7, characterized in that: The latch seat (332) is provided with a slot (3322), the top of the latch (333) is provided with a pin (3331), and the pin (3331) is engaged with the slot (3322).

9. The missile launcher according to claim 1, characterized in that: An adjustment handle (311) is also provided below the seat (31).

10. The missile launcher according to claim 1, characterized in that: The support frame (11) comprises: Three universally adjustable foot cups (111), each of the universally adjustable foot cups (111) being arranged on the base (1); A triangular support arm (112), wherein a support leg of the triangular support arm (112) is correspondingly connected to one of the universally adjustable foot cups (111); A support rod (113), wherein the support rod (113) is arranged at the top of the triangular support arm (112) in a vertical direction.

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