A new vertical missile launch system

Abstract

This utility model relates to the field of automation control technology and discloses a new vertical missile launch device, including a main component, a vertical launcher, a placement frame fixed to the top of the vertical launcher, a missile placed inside the placement frame, and an adjustment component disposed on the placement frame, including an adjustment member, the adjustment member including an adjustment plate, a first gear fixed to one side of the adjustment plate, a support plate sleeved on the outside of the first gear, the first gear and the support plate being rotatably connected by a rotating shaft, a gear ring sleeved on the outside of the first gear, the gear ring meshing with the first gear, and the gear ring and the support plate being rotatably connected by a rotating shaft. The beneficial effects of this utility model are: it can flexibly change the size of the launch unit according to new missiles of different sizes, making it compatible with various types of missiles, whether small precision strike missiles or large long-range strategic missiles, providing suitable launch space.

Description

Technical Field

[0001] This utility model relates to the field of automation control technology, and in particular to a new vertical missile launch device. Background Technology

[0002] In modern warfare, vertical launch systems for missiles have become mainstream equipment due to their advantages such as rapid response, immediate launch without complicated aiming angles, omnidirectional launch capability to strike targets in different directions, and the ability to launch multiple missiles in succession to form a firepower output. They are effectively integrated into the combat system and enhance the offensive and defensive capabilities of the combat platform. However, under current technology, the size of their launch units is fixed. This was initially for the convenience of standardized production, installation and debugging. However, with the rapid development of missile technology and the continuous emergence of new missiles, this fixed setting is difficult to adapt to missiles of different sizes, which affects combat effectiveness. Utility Model Content

[0003] The purpose of this section is to outline some aspects of embodiments of the present invention and to briefly describe some preferred embodiments. Simplifications or omissions may be made in this section, as well as in the abstract and title of this application, to avoid obscuring the purpose of these documents; however, such simplifications or omissions should not be construed as limiting the scope of the present invention.

[0004] In view of the problems existing in the above and / or existing new missile vertical launch systems, this utility model is proposed.

[0005] Therefore, the problem that this utility model aims to solve is that the launch unit size of the missile vertical launch device is fixed. Originally, this was to facilitate standardized production, installation and debugging. However, due to the development of missile technology and the emergence of new missiles, this fixed setting is difficult to adapt to missiles of different sizes, which affects the combat effectiveness.

[0006] To solve the above-mentioned technical problems, the present invention provides the following technical solution: a new missile vertical launch device, which includes a main body assembly and an adjustment assembly. The main body assembly includes a vertical launcher, and a placement frame is fixed on the top of the vertical launcher. A missile is placed inside the placement frame. The adjustment component is disposed on the placement frame. The adjustment component includes an adjustment element, which includes an adjustment plate. A first gear is fixed on one side of the adjustment plate. A support plate is sleeved on the outside of the first gear. The first gear and the support plate are rotatably connected by a rotating shaft. A gear ring is sleeved on the outside of the first gear. The gear ring meshes with the first gear. The gear ring and the support plate are rotatably connected by a rotating shaft.

[0007] As a preferred embodiment of the new missile vertical launch device of this utility model, the adjustment component further includes a driving component, the driving component includes a second gear, the second gear is rotatably connected to the top of the support plate through a rotating shaft, and a rack is provided on one side of the second gear, the second gear and the rack meshing.

[0008] In a preferred embodiment of the new missile vertical launch device of this utility model, a slide rod is fixed to one end of the rack, a support frame is sleeved on the outside of the slide rod, and the support frame and the slide rod are slidably connected.

[0009] As a preferred embodiment of the new missile vertical launch device of this utility model, wherein: a movable column is fixed to one end of the rack, a positioning sleeve is movably connected to the outside of the movable column, a first spring is fixed to one end of the movable column, and one end of the first spring is fixed to the inner wall of the positioning sleeve.

[0010] In a preferred embodiment of the new missile vertical launch device of this utility model, a drive rod is fixed to one end of the positioning sleeve, a drive bar is fixed to one side of the drive rod, a drive plate is sleeved on the outside of the drive bar, and the drive bar and the drive plate are movably connected.

[0011] In a preferred embodiment of the new missile vertical launch device of this utility model, a positioning frame is sleeved on the outer side of the drive plate, the positioning frame and the drive plate are movably connected, a second spring is fixed on the inner wall of the positioning frame, and one end of the second spring is fixed to the bottom of the drive plate.

[0012] As a preferred embodiment of the new missile vertical launch device of this utility model, the adjustment component further includes a limiting member, the limiting member including a limiting plate, the limiting plate being fixed to one side of the positioning frame, a limiting block being provided on one side of the limiting plate, a moving strip being fixed on one side of the limiting block, a positioning tube being sleeved on the outside of the moving strip, and the positioning tube and the moving strip being movably connected.

[0013] As a preferred embodiment of the new missile vertical launch device of this utility model, a compression plate is sleeved on the outside of the moving bar, a third spring is fixed on one side of the compression plate, one end of the third spring is fixed to the inner wall of the positioning tube, and a connecting plate is sleeved on the outside of the positioning tube.

[0014] In a preferred embodiment of the new missile vertical launch device of this utility model, a movable block is fixed on one side of the gear ring, a threaded rod is inserted into the top of the movable block, and the movable block and the threaded rod are threadedly connected.

[0015] In a preferred embodiment of the new missile vertical launch device of this utility model, a fixing plate is sleeved on the outer side of the threaded rod, and the fixing plate and the threaded rod are threadedly connected.

[0016] The beneficial effects of this utility model are: it can flexibly change the size of the launch unit according to the different sizes of new missiles, so that it can be compatible with various types of missiles, whether it is a small precision strike missile or a large long-range strategic missile, there is a suitable launch space. Attached Figure Description

[0017] To more clearly illustrate the technical solutions of the embodiments of this utility model, the drawings used in the description of the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort. Among them: Figure 1 This is an overall structural diagram of the new vertical missile launch system.

[0018] Figure 2 For the new vertical launch system of missiles Figure 1 Enlarged view of the structure at point A in the middle.

[0019] Figure 3 This is a diagram of the first spring structure of the new vertical missile launch system.

[0020] Figure 4 This is a structural diagram of the second gear of the new vertical launch missile system.

[0021] Figure 5 This is a structural diagram of the adjustment plate for the new vertical launch system for missiles.

[0022] Figure 6 This is a structural diagram of the drive rod for the new vertical missile launch system.

[0023] Figure 7 This is a structural diagram of the limiting block for the new vertical missile launch system. Detailed Implementation

[0024] To make the above-mentioned objectives, features and advantages of this utility model more apparent and understandable, the specific embodiments of this utility model will be described in detail below with reference to the accompanying drawings.

[0025] Many specific details are set forth in the following description in order to provide a full understanding of the present invention. However, the present invention may also be implemented in other ways different from those described herein. Those skilled in the art can make similar extensions without departing from the spirit of the present invention. Therefore, the present invention is not limited to the specific embodiments disclosed below.

[0026] Secondly, the term "an embodiment" or "embodiment" as used herein refers to a specific feature, structure, or characteristic that may be included in at least one implementation of the present invention. The phrase "in one embodiment" appearing in different places in this specification does not necessarily refer to the same embodiment, nor is it a single or selective embodiment that excludes other embodiments.

[0027] Example 1 Reference Figures 1 to 7 This is the first embodiment of the present invention. This embodiment provides a new missile vertical launch device. The new missile vertical launch device includes a main body component 100 and an adjustment component 200. The two work together to flexibly change the size of the launch unit to be compatible with new missiles of different sizes, providing adaptation space for various types of missiles such as small precision strike missiles and large long-range strategic missiles.

[0028] The main component 100 includes a vertical launcher 101, a placement frame 102 fixed to the top of the vertical launcher 101, and a missile 103 disposed inside the placement frame 102.

[0029] The vertical launcher 101 serves as the basic platform for launching the missile 103. It relies on internal devices to ensure that the missile 103 can be launched vertically according to the program. The vertical launcher 101 is existing technology, so it will not be described in detail. The placement frame 102 is located on top of the vertical launcher 101 and is used to support and position the missile 103 to ensure that the missile 103 is in an accurate position when it is ready to be launched. The missile 103 is placed in the placement frame 102 and is in a ready-to-launch state. After receiving the command, it flies to the predetermined target with the help of power to carry out the strike mission.

[0030] The adjustment assembly 200 is disposed on the placement frame 102 and includes an adjustment member 201. The adjustment member 201 includes an adjustment plate 201a. A first gear 201b is fixed on one side of the adjustment plate 201a. A support plate 201c is sleeved on the outside of the first gear 201b. The first gear 201b and the support plate 201c are rotatably connected by a rotating shaft. A gear ring 201d is sleeved on the outside of the first gear 201b. The gear ring 201d meshes with the first gear 201b. The gear ring 201d and the support plate 201c are rotatably connected by a rotating shaft.

[0031] When missiles 103 of different sizes need to be placed, the gear ring 201d is rotated. At this time, the gear ring 201d can drive the first gear 201b to rotate. The rotation of the first gear 201b can drive the adjusting plate 201a to move. When the adjusting plate 201a moves, it can clamp the missiles 103 of different sizes. The support plate 201c is used to support the first gear 201b to prevent the first gear 201b from deviating when rotating.

[0032] Example 2 Reference Figures 2-7 This is the second embodiment of the present invention, which is based on the previous embodiment.

[0033] Specifically, the adjustment component 200 also includes a drive component 202, which includes a second gear 202a. The second gear 202a is rotatably connected to the top of the support disk 201c via a rotating shaft. A rack 202b is provided on one side of the second gear 202a, and the second gear 202a and the rack 202b mesh.

[0034] The outer side of the gear ring 201d has teeth that mesh with the second gear 202a. When the gear ring 201d rotates, it can drive the second gear 202a to rotate. At this time, the rotation of the second gear 202a can drive the rack 202b to move. At this time, the movement of the rack 202b can drive the other second gears 202a to rotate. When the second gears 202a rotate, they can drive the other gear rings 201d to rotate, thus enabling the simultaneous clamping of missiles 103 of different sizes.

[0035] Specifically, a slide bar 202c is fixed to one end of the rack 202b, and a support frame 202d is sleeved on the outside of the slide bar 202c. The support frame 202d and the slide bar 202c are slidably connected.

[0036] When it is necessary to move the single set of adjusting plates 201a, the rack 202b and the second gear 202a need to be separated. When the rack 202b moves, it can drive the slide rod 202c to move. At this time, the slide rod 202c can move within the support frame 202d. The support frame 202d can support the slide rod 202c and prevent it from deviating. A first groove corresponding to the support frame 202d is provided on the top of the vertical transmitter 101. The support frame 202d slides within the first groove. When the rack 202b moves, it can drive the support frame 202d to slide within the first groove, thereby supporting the support frame 202d and preventing it from deviating.

[0037] Specifically, a movable column 202e is fixed to one end of the rack 202b, a positioning sleeve 202f is movably connected to the outside of the movable column 202e, a first spring 202g is fixed to one end of the movable column 202e, and one end of the first spring 202g is fixed to the inner wall of the positioning sleeve 202f.

[0038] When the rack 202b moves, it can drive the moving column 202e to move. At this time, the positioning sleeve 202f can support the moving column 202e to prevent it from shifting. When the moving column 202e moves, it can apply a squeezing force to the first spring 202g. After the size adjustment is completed, the missile 103 is loaded and the rack 202b is released. The rebound force of the first spring 202g can drive the moving column 202e back to its original position, thus clamping the missile 103 and waiting for launch.

[0039] Specifically, a drive rod 202h is fixed to one end of the positioning sleeve 202f, a drive bar 202i is fixed to one side of the drive rod 202h, a drive plate 202j is sleeved on the outside of the drive bar 202i, and the drive bar 202i and the drive plate 202j are movably connected.

[0040] An inclined guide groove is provided on the drive plate 202j. When it is necessary to separate the rack 202b and the second gear 202a, the drive plate 202j is moved. The movement of the drive plate 202j can drive the guide groove to move and squeeze the drive bar 202i to move. The movement of the drive bar 202i can drive the drive rod 202h to move. At this time, the movement of the drive rod 202h can drive the rack 202b and the second gear 202a to separate.

[0041] Specifically, a positioning frame 202k is sleeved on the outer side of the drive plate 202j. The positioning frame 202k and the drive plate 202j are movably connected. A second spring 202l is fixed on the inner wall of the positioning frame 202k. One end of the second spring 202l is fixed to the bottom of the drive plate 202j.

[0042] The positioning frame 202k is fixed to the top of the vertical transmitter 101. The positioning frame 202k can support the drive plate 202j and prevent the drive plate 202j from shifting. When the drive plate 202j is moved, a squeezing force can be applied to the second spring 202l. The rebound force of the second spring 202l can drive the drive plate 202j back to its original position.

[0043] Specifically, the adjustment component 200 also includes a limiting component 203, which includes a limiting plate 203a. The limiting plate 203a is fixed to one side of the positioning frame 202k. A limiting block 203b is provided on one side of the limiting plate 203a. A moving strip 203c is fixed on one side of the limiting block 203b. A positioning tube 203d is sleeved on the outside of the moving strip 203c. The positioning tube 203d and the moving strip 203c are movably connected.

[0044] A limiting groove corresponding to the limiting block 203b is provided on the limiting plate 203a. The limiting groove is set as an inclined surface. When the drive plate 202j moves, it can drive the limiting block 203b to move on one side of the limiting plate 203a. The setting of the limiting plate 203a can prevent the force of the second spring 202l from driving the drive plate 202j back to its original position. When it is necessary to release the limitation on the drive plate 202j, the moving bar 203c is moved. At this time, the moving bar 203c can drive the limiting block 203b and the limiting plate 203a to separate, thereby releasing the limitation on the drive plate 202j. Then, the force of the second spring 202l can drive the drive plate 202j back to its original position. The setting of the positioning tube 203d can support the moving bar 203c and prevent the moving bar 203c from shifting.

[0045] Example 3 Reference Figures 1 to 7 This is the third embodiment of the present invention, which is based on the first two embodiments.

[0046] Specifically, a pressing plate 203e is sleeved on the outside of the moving strip 203c, a third spring 203f is fixed on one side of the pressing plate 203e, one end of the third spring 203f is fixed to the inner wall of the positioning tube 203d, and a connecting plate 203g is sleeved on the outside of the positioning tube 203d.

[0047] When the moving bar 203c moves, it can drive the extrusion plate 203e to move. At this time, the movement of the extrusion plate 203e can apply a compressive force to the third spring 203f. At this time, the limiting block 203b and the limiting plate 203a separate, thereby releasing the limitation on the drive plate 202j. When the moving bar 203c is released, the rebound force of the third spring 203f can drive the limiting block 203b and the limiting plate 203a to re-engage. The connecting plate 203g is fixed to one side of the drive plate 202j. The positioning tube 203d can be supported by the setting of the connecting plate 203g.

[0048] Specifically, a movable block 203h is fixed on one side of the gear ring 201d, and a threaded rod 203i is inserted into the top of the movable block 203h. The movable block 203h and the threaded rod 203i are threadedly connected.

[0049] After the individual gear ring 201d is moved, the threaded rod 203i is rotated to make it move and engage with the fixed plate 203j, thereby limiting the movement of the gear ring 201d. The moving block 203h is used to support the threaded rod 203i.

[0050] Specifically, a fixing plate 203j is sleeved on the outer side of the threaded rod 203i, and the fixing plate 203j and the threaded rod 203i are threadedly connected.

[0051] The fixing plate 203j is fixed to the top of the vertical transmitter 101. A fixing groove corresponding to the threaded rod 203i is provided on the fixing plate 203j. By rotating the threaded rod 203i into the fixing groove, the gear ring 201d can be limited.

[0052] In use, if missiles 103 of different sizes need to be placed and multiple sets of adjusting plates 201a need to be operated simultaneously to clamp the missiles, the gear ring 201d can be rotated directly. The rotation of the gear ring 201d drives the first gear 201b meshing with it to rotate, and the rotation of the first gear 201b drives the adjusting plate 201a to move. At the same time, the rotation of the gear ring 201d will also drive the second gear 202a to rotate, and the rotation of the second gear 202a will drive the rack 202b meshing with it to move. The movement of the rack 202b will then drive the other second gears 202a to rotate, and in turn drive the other gear rings 201d to rotate, so that multiple sets of adjusting plates 201a can move simultaneously to prepare for clamping missiles 103 of different sizes.

[0053] If only a single adjusting plate 201a needs to be moved and adjusted, the drive plate 202j is operated first. Pushing the drive plate 202j causes it to move, which in turn causes its inclined guide groove to press against the drive bar 202i, causing it to move. The movement of the drive bar 202i causes the drive rod 202h to move, which in turn causes the rack 202b to move, thus separating the rack 202b from the second gear 202a.

[0054] When the rack 202b moves, it will drive the slide bar 202c to slide within the support frame 202d. The support frame 202d slides within the first groove at the top of the vertical launcher 101, providing support for the support frame 202d and preventing it from shifting. At the same time, the rack 202b drives the moving column 202e to move. The moving column 202e moves within the positioning sleeve 202f. The movement of the moving column 202e applies a squeezing force to the first spring 202g. After completing the above adjustment operation, the missile 103 is placed in the appropriate position within the placement frame 102.

[0055] If only one set of adjusting plates 201a is adjusted, releasing the push on the drive plate 202j will cause the second spring 202l to return the drive plate 202j to its original position. For the moving column 202e, the first spring 202g will return it to its original position, thereby allowing the adjusting plate 201a to clamp the missile 103 and await subsequent launch commands. If a single gear ring 201d is moved and adjusted, the corresponding threaded rod 203i can be rotated to move the threaded rod 203i toward the fixed plate 203j until the threaded rod 203i rotates into the corresponding fixed groove on the fixed plate 203j, thereby limiting the movement of the gear ring 201d and preventing it from moving accidentally.

[0056] If further adjustments to the adjustment device are required, and the limitation on the drive plate 202j needs to be released, pull the moving bar 203c. The moving bar 203c moves, causing the limiting block 203b to separate from the limiting groove on the limiting plate 203a. The limiting groove is an inclined surface. The limiting plate 203a originally prevented the drive plate 202j from returning to its original position under the action of the second spring 202l, thereby releasing the limitation on the drive plate 202j. When the moving bar 203c is released, the rebound force of the third spring 203f causes the limiting block 203b and the limiting plate 203a to re-engage, restoring the limitation state on the drive plate 202j, so that the corresponding adjustment operation can be performed again according to the needs next time.

[0057] It should be noted that the above embodiments are only used to illustrate the technical solution of this utility model and are not intended to limit it. Although this utility model has been described in detail with reference to preferred embodiments, those skilled in the art should understand that modifications or equivalent substitutions can be made to the technical solution of this utility model without departing from the spirit and scope of the technical solution of this utility model, and all such modifications or substitutions should be covered within the scope of the claims of this utility model.

Claims

1. A novel vertical launch system for missiles, characterized in that: It includes a main body component (100) and an adjustment component (200), wherein: The main component (100) includes a vertical launcher (101), a placement frame (102) is fixed on the top of the vertical launcher (101), and a missile (103) is placed inside the placement frame (102). The adjustment component (200) is disposed on the placement frame (102). The adjustment component (200) includes an adjustment member (201), which includes an adjustment piece (201a). A first gear (201b) is fixed on one side of the adjustment piece (201a). A support plate (201c) is sleeved on the outside of the first gear (201b). The first gear (201b) and the support plate (201c) are rotatably connected by a rotating shaft. A gear ring (201d) is sleeved on the outside of the first gear (201b). The gear ring (201d) meshes with the first gear (201b). The gear ring (201d) and the support plate (201c) are rotatably connected by a rotating shaft.

2. The new vertical missile launcher as described in claim 1, characterized in that: The adjustment assembly (200) further includes a drive component (202), which includes a second gear (202a). The second gear (202a) is rotatably connected to the top of the support disk (201c) via a rotating shaft. A rack (202b) is provided on one side of the second gear (202a), and the second gear (202a) and the rack (202b) mesh.

3. The new vertical missile launcher as described in claim 2, characterized in that: One end of the rack (202b) is fixed with a slide rod (202c), and a support frame (202d) is sleeved on the outside of the slide rod (202c). The support frame (202d) and the slide rod (202c) are slidably connected.

4. The new vertical missile launcher as described in claim 3, characterized in that: One end of the rack (202b) is fixed with a movable column (202e), and a positioning sleeve (202f) is movably connected to the outside of the movable column (202e). One end of the movable column (202e) is fixed with a first spring (202g), and one end of the first spring (202g) is fixed to the inner wall of the positioning sleeve (202f).

5. The new vertical missile launcher as described in claim 4, characterized in that: One end of the positioning sleeve (202f) is fixed with a drive rod (202h), and a drive bar (202i) is fixed on one side of the drive rod (202h). A drive plate (202j) is sleeved on the outside of the drive bar (202i), and the drive bar (202i) and the drive plate (202j) are movably connected.

6. The new vertical missile launcher as described in claim 5, characterized in that: A positioning frame (202k) is sleeved on the outside of the drive plate (202j). The positioning frame (202k) and the drive plate (202j) are movably connected. A second spring (202l) is fixed on the inner wall of the positioning frame (202k). One end of the second spring (202l) is fixed to the bottom of the drive plate (202j).

7. The new vertical missile launcher as described in claim 6, characterized in that: The adjustment component (200) further includes a limiting member (203), which includes a limiting plate (203a). The limiting plate (203a) is fixed to one side of the positioning frame (202k). A limiting block (203b) is provided on one side of the limiting plate (203a). A moving strip (203c) is fixed on one side of the limiting block (203b). A positioning tube (203d) is sleeved on the outside of the moving strip (203c). The positioning tube (203d) and the moving strip (203c) are movably connected.

8. The new vertical missile launcher as described in claim 7, characterized in that: The moving strip (203c) is fitted with a pressing plate (203e) on the outside. A third spring (203f) is fixed on one side of the pressing plate (203e). One end of the third spring (203f) is fixed to the inner wall of the positioning tube (203d). A connecting plate (203g) is fitted on the outside of the positioning tube (203d).

9. The new vertical missile launcher as described in claim 7 or 8, characterized in that: A movable block (203h) is fixed on one side of the gear ring (201d), and a threaded rod (203i) is inserted into the top of the movable block (203h). The movable block (203h) and the threaded rod (203i) are threadedly connected.

10. The new vertical missile launcher as described in claim 9, characterized in that: A fixing plate (203j) is sleeved on the outside of the threaded rod (203i), and the fixing plate (203j) and the threaded rod (203i) are threadedly connected.

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