Crawler-type remote control unmanned launching vehicle

Abstract

The utility model provides a crawler-type remote control unmanned launching vehicle which comprises a crawler, a bearing seat is arranged in the middle of the crawler, an adapter is arranged at the top of the bearing seat, a launching seat is detachably connected to the top of the adapter, and the launching seat is obliquely arranged during launching. The launching base used for launching the rocket projectile is detachably connected to the crawler with the remote control function, manual remote control over the crawler to launch the rocket projectile in the mountain land or the complex ground environment is facilitated, the rocket projectile launching convenience is improved, the launching base can be detached, and the rocket projectile launching cost is reduced. The carrying convenience of the launching vehicle is improved, the survival probability of individual soldiers is increased, and the launching of rocket projectiles has the advantages of high maneuverability and high flexibility.

Description

Technical Field

[0001] The utility model relates to the technical field of military unmanned launching vehicles, in particular to a tracked remote-controlled unmanned launching vehicle. Background Art

[0002] A tracked remote-controlled vehicle is a wirelessly controlled barrier-free land vehicle, which is usually used as a carrier. For example, in some situations where bomb disposal, dredging and transportation are required, relevant equipment is usually installed on the tracked remote-controlled vehicle to meet the corresponding needs. Common military equipment in the military field are tracked remote-controlled mine-clearing vehicles, tracked remote-controlled transport vehicles and tracked remote-controlled rocket launchers. Such equipment is characterized by unmanned driving, suitable for use in various road conditions, and easy to operate. According to the power type, the above tracked remote-controlled vehicles are divided into fuel engine and electric motor drive.

[0003] At present, the common rocket tracked unmanned launcher still has the following shortcomings in actual use: 1. In order to increase the amount of ammunition carried, the existing unmanned launcher usually sets the external dimensions to a larger specification, and such large-sized tracked unmanned launcher is not convenient for a single soldier to carry. For example, in the high-altitude, cold and oxygen-deficient areas of the plateau, such rocket tracked unmanned launcher has poor portability due to its large specifications; 2. The high-altitude, cold and oxygen-deficient areas of the plateau are cold and humid, resulting in poor moisture-proof effect in the launch cabin, which is prone to moisture short circuit problems.

[0004] To this end, the utility model provides a tracked remote-controlled unmanned launching vehicle. Utility Model Content

[0005] In view of the shortcomings of the prior art, the purpose of the utility model is to provide a tracked remote-controlled unmanned launching vehicle to solve the problems raised in the above-mentioned background technology. The utility model has the advantages of large ammunition carrying capacity, small space occupation, and easy carrying on plateaus. It also has the advantage that the ammunition magazine is waterproof and moisture-proof.

[0006] In order to achieve the above-mentioned purpose, the utility model is implemented through the following technical scheme: a tracked remote-controlled unmanned launching vehicle, including a tracked vehicle, a bearing seat is arranged in the middle of the tracked vehicle, a transfer seat is arranged on the top of the bearing seat, a launching seat is detachably connected to the top of the transfer seat, and the launching seat is tilted during launching.

[0007] Furthermore, the lower end face of the adapter seat and the upper end face of the bearing seat are welded and connected, a positioning sleeve is welded on the top of the adapter seat, a locking screw is passed through the outer peripheral wall of the positioning sleeve and screwed on, and a plug pile that is plugged into and matched with the positioning sleeve is welded on the bottom of the launching seat, and one end of the locking screw is used in conjunction with one side of the plug pile.

[0008] Furthermore, a magazine is provided on the top of the supporting seat, a lifting frame is provided in the magazine, a positioning frame is rotatably connected to the top of the lifting frame, two adapter seats respectively close to the two ends are rotatably connected in the positioning frame, the two adapter seats are respectively arranged close to the two ends in the positioning frame, one side of the launching seat and one side of the adapter seat are detachably connected, a control motor for controlling the rotation of the positioning frame is provided in the magazine, and a control combination for controlling the rotation of the adapter seat is provided in the positioning frame.

[0009] Furthermore, the lifting frame includes a rectangular frame and an electric telescopic rod, the electric telescopic rod is fixedly arranged in the magazine and its output shaft is fixedly connected to a position near the end of the bottom of the rectangular frame.

[0010] Furthermore, the upper end surface of the rectangular frame is welded with vertical plates close to the two ends, and the middle parts of the two ends of the positioning frame are welded with coaxial support shafts, one side of one of the vertical plates is fixedly connected to the control motor 1, and the output shaft of the control motor 1 is welded to one end of the support shaft.

[0011] Furthermore, a connecting shaft is welded on the back of the adapter through a support plate, and both ends of the connecting shaft are rotatably connected to the two sides in the positioning frame. The control combination includes a worm gear, a worm and a second control motor. The worm gear is fixedly sleeved on the connecting shaft, and a door-type plate is welded in the positioning frame. The second control motor is fixedly arranged on one side of the door-type plate and its output shaft is fixedly connected to the worm, and the worm and the worm gear are meshing.

[0012] Furthermore, a cover for sealing the magazine opening is hingedly connected to the top of the support seat, and a control motor 3 is provided at the rotation connection between the cover and the support seat. A waterproof frame located at the periphery of the magazine is welded to the top of the support seat.

[0013] Furthermore, the number of the transmitting seats on the adapter is at least two.

[0014] The beneficial effects of the utility model are as follows:

[0015] 1. The utility model detachably connects the launching seat for launching rockets to the tracked vehicle with remote control function, so as to facilitate the manual remote control of the tracked vehicle to launch rockets in mountainous areas or complex ground environments, thereby improving the convenience of rocket launching. Moreover, the launching seat can be disassembled to improve the convenience of carrying the launching vehicle, improve the probability of survival of a single soldier, and make the launching of rockets have the advantages of high mobility and high flexibility.

[0016] 2. The utility model provides a lifting frame, a positioning frame and an adapter, so that the launching seats in the magazine can be stacked. The stacked launching seats increase the ammunition carrying capacity and greatly reduce the space occupied by the magazine, thereby facilitating the design of a smaller size of the entire tracked vehicle, improving the walking stability of the launching vehicle, and facilitating a single soldier to carry the tracked vehicle loaded with rockets as a whole. By providing a control combination and a control motor, the positioning frame can be conveniently controlled to flip. The flipping function of the positioning frame can launch all the rockets in turn, and has the function of switching and launching multiple rockets in a long distance.

[0017] 3. The utility model provides a sealing cover at the mouth of the magazine, wherein the sealing cover and the bearing seat are rotatably connected, and a control motor three is provided between the sealing cover and the bearing seat. The function of the control motor three is to drive the sealing cover to open and close the magazine to prevent water from entering and getting damp in the magazine, and has the advantages of being waterproof and moisture-proof. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 This is a schematic diagram of the structure of the tracked remote-controlled unmanned launching vehicle of the utility model;

[0019] Figure 2 for Figure 1 The enlarged schematic diagram of the part "a" in the middle;

[0020] Figure 3 It is a schematic diagram of the structure of the crawler-type remote-controlled unmanned launcher after the lifting frame and the magazine are separated;

[0021] Figure 4 It is a schematic diagram of the structure of the crawler-type remote-controlled unmanned launcher after the lifting frame and the magazine are separated;

[0022] Figure 5 It is a schematic diagram of the coordination of the rectangular frame, positioning frame, control motor-adapter and launching seat of the crawler-type remote-controlled unmanned launching device of the utility model;

[0023] Figure 6 for Figure 3 Schematic diagram of the structure of the control combination.

[0024] In the figure: 1. crawler vehicle; 11. bearing seat; 111. magazine; 112. waterproof frame; 12. launching seat; 2. lifting frame; 21. rectangular frame; 211. vertical plate; 22. electric telescopic rod; 3. positioning frame; 31. supporting shaft; 32. door plate; 4. adapter seat; 41. connecting shaft; 5. control motor 1; 6. control combination; 61. worm gear; 62. worm; 63. control motor 2; 7. cover; 8. positioning sleeve; 81. locking screw; 9. pile. DETAILED DESCRIPTION

[0025] In order to make the technical means, creative features, objectives and effects achieved by the present invention easy to understand, the present invention is further described below in conjunction with specific implementation methods.

[0026] Example 1

[0027] See also Figure 1 and Figure 2 The utility model provides a technical solution: a tracked remote-controlled unmanned launching vehicle, comprising a tracked vehicle 1, a bearing seat 11 is arranged in the middle of the tracked vehicle 1, and an adapter seat 4 is arranged on the top of the bearing seat 11. The bearing seat 11 can be a structure made of welded steel structure, wherein track assemblies are installed on both sides of the bearing seat 11. The track assembly is a prior art, so the structure thereof is no longer described in detail in this technical solution. It should be noted that the driving force of the track assembly of the present application is provided by a battery and an electric motor, and the track assembly can drive the bearing seat 11 to move when started; a launching seat 12 is detachably connected to the top of the adapter seat 4, and the launching seat 12 is tilted when launching, and the tilt here refers to tilting upward relative to the horizontal plane, and the launching seat 12 can be removed. A control circuit board and a wireless communication component are built into the support base 11, which facilitates the remote control of starting and stopping the track assembly and launching rockets from the launch base 12. That is to say, the operator can use a remote controller to control the start of the track assembly and the launch of rockets from the launch base 12 through the wireless communication component and the control circuit board. After the launch base 12 and the tracked vehicle 1 are disassembled, they can be carried separately, thereby improving the convenience of carrying.

[0028] Furthermore, the lower end face of the adapter 4 is welded to the upper end face of the bearing seat 11, and the adapter 4 is a triangular plate structure, wherein the number of the adapters 4 is at least three, and a launching seat 12 is installed on each adapter 4, a positioning sleeve 8 is welded to the top of the adapter 4, and a locking screw 81 is screwed through the outer peripheral wall of the positioning sleeve 8, and a plug 9 that is plugged into and matched with the positioning sleeve 8 is welded to the bottom of the launching seat 12, and one end of the locking screw 81 is used in conjunction with one side of the plug 9, that is, after the plug 9 is inserted into the positioning sleeve 8 and then the locking screw 81 is tightened, the launching seat 12 and the adapter 4 are tightly connected, and when the locking screw 81 is loosened, the launching seat 12 can be directly removed.

[0029] To this end, the tracked remote-controlled unmanned launch vehicle proposed in this embodiment can replace the manual operation of a single soldier to launch rockets on mountainous or complex terrain, reduce the intensity of the operation of a single soldier launching rockets and the risk of exposure, and improve the speed of rocket reflection. Moreover, the above-mentioned launch seat 12 is in an exposed state, which is simpler to manufacture.

[0030] Example 2

[0031] See also Figures 3 to 6The crawler-type remote-controlled unmanned launch vehicle comprises a crawler vehicle 1, a bearing seat 11 is arranged in the middle of the crawler vehicle 1, a launch seat 12 is detachably connected to the top of the adapter seat 4, the launch seat 12 is tilted when launching, and the tilt here refers to tilting upward relative to the horizontal plane, and the launch seat 12 can be removed, wherein, crawler assemblies are installed on both sides of the bearing seat 11, and the crawler assembly is a prior art, so the present technical scheme does not describe its structure in detail, it should be noted that the driving force of the crawler assembly of the present application is provided by a battery and an electric motor, and the crawler assembly can drive the bearing seat 11 to move when it is started; the launch seat 12 is detachably connected to the top of the adapter seat 4, and the launch seat 12 is tilted when launching, and the tilt here refers to tilting upward relative to the horizontal plane, and the launch seat 12 can be removed. The control circuit board and wireless communication components are built-in in the bearing seat 11, which facilitates the remote control of the crawler assembly start and stop and the launch of rockets by the launch seat 12, that is, the operator can control the start of the crawler assembly and the launch of rockets by the launch seat 12 using the remote controller through the wireless communication components and the control circuit board.

[0032] In the present technical solution, a magazine 111 is provided on the top of the carrier 11. The magazine 111 is a cavity structure made of heat-resistant metal skin. The top of the cavity is open. A launching seat 12 is placed in the magazine 111. The launching seat 12 adopts the rocket launcher structure in the prior art and is used to launch rockets.

[0033] Furthermore, a lifting frame 2 is provided in the magazine 111, and a positioning frame 3 is rotatably connected above the lifting frame 2. The lifting frame 2 is used to control the positioning frame 3 to enter and exit the magazine 111. A control motor 5 for controlling the rotation of the positioning frame 3 is provided in the magazine 111. The specific implementation structure is that the lifting frame 2 includes a rectangular frame 21 and an electric telescopic rod 22. The electric telescopic rod 22 is fixedly provided in the magazine 111 and its output shaft is fixedly connected to the position near the end of the bottom of the rectangular frame 21. The bottom of one rectangular frame 21 corresponds to two electric telescopic rods 22. The bottom of the electric telescopic rod 22 and the bottom of the magazine 111 can be fastened and connected by bolts. The electric telescopic rod 22 is electrically connected to the control circuit board, which is convenient for remote control. The positioning frame 3 rotates to realize the flipping function. Specifically, vertical plates 211 close to the two ends are welded on the upper end surface of the rectangular frame 21, and coaxial support shafts 31 are welded in the middle of the two ends of the positioning frame 3. One side of one of the vertical plates 211 is fixedly connected to the control motor 5, and the output shaft of the control motor 5 is welded to one end of the support shaft 31, thereby the control motor 5 provides driving force for the rotation of the positioning frame 3 through the support shaft 31, wherein the control motor 5 and the control circuit board are typically connected to facilitate remote control.

[0034] Two adapters 4 are rotatably connected in the positioning frame 3, which are close to both ends. The adapter 4 is a flat plate structure. The two adapters 4 are respectively arranged close to both ends in the positioning frame 3. One side of the launch seat 12 and the adapter 4 are detachably connected. The detachable connection structure here can adopt the connection structure mentioned in Example 1. The adapter 4 is used to carry the launch seat 12. Preferably, the number of the launch seats 12 on the adapter 4 is at least two. When there are two launch seats 12 on one adapter 4, the number of the launch seats 12 on the unmanned launch vehicle is four in total, that is, it can carry four rockets. Moreover, when the adapter 4 rotates, it can drive the launch seat 12 to move and adjust the launch direction (launch inclination angle). When the adapter 4 rotates, different adapters 4 can be switched, so that all rockets can be launched. A control assembly 6 for controlling the rotation of the adapter 4 is provided in the positioning frame 3.

[0035] Specifically, a connecting shaft 41 is welded to the back of the adapter 4 through a support plate. The connecting shaft 41 is close to one end of the adapter 4. Both ends of the connecting shaft 41 are rotatably connected to the two sides in the positioning frame 3. The control assembly 6 includes a worm gear 61, a worm 62 and a second control motor 63. The worm gear 61 is fixedly sleeved on the connecting shaft 41. A door-shaped plate 32 is welded in the positioning frame 3. One positioning frame 3 corresponds to two door-shaped plates 32. The second control motor 63 is fixedly arranged on one side of the door-shaped plate 32 and its output shaft is fixedly connected to the worm 62. One door-shaped plate 32 corresponds to one second control motor 63. The second control motor 63 is also electrically connected to the control circuit board for remote control. When the second control motor 63 is started, it will drive the worm 62 to rotate, and the worm 62 is meshed with the worm gear 61, thereby driving the adapter 4 to rotate.

[0036] In this embodiment, the top of the supporting seat 11 is hingedly connected with a cover 7 for sealing the mouth of the magazine 111, and a control motor 3 is provided at the rotation connection between the cover 7 and the supporting seat 11. The control motor 3 drives the cover 7 to rotate to realize the opening and closing control of the mouth of the magazine 111. In specific implementation, a hinge seat can be welded on the top of the supporting seat 11. The control motor 3 is a bidirectional motor and is embedded in the hinge seat. The output shaft of the control motor 3 is fixedly connected to one end of the cover 7. A waterproof frame 112 located on the outer periphery of the magazine 111 is welded on the top of the supporting seat 11. When the cover 7 is covered on the waterproof frame 112, it can effectively prevent rainwater from entering the magazine 111. The waterproof frame 112 adopts a rectangular frame structure, and then a circle of sealing pad is bonded to the top of the rectangular frame.

[0037] Working principle: This working principle is described based on the technical solution of Example 2. Before using this launch vehicle, a thermal imaging detection system and a full-range image tracking system can be installed on the launch vehicle to assist in tracking the target. When in use, when a single soldier carries this launch vehicle to perform tasks in the plateau area, when the launch vehicle needs to be remotely controlled, the tracked vehicle 1 is controlled by the remote control to walk to a hidden place. When a rocket needs to be launched, first start the control motor three to open the cover 7, then control the electric telescopic rod 22 to push, and then control the control motor two 63 corresponding to the launch seat 12 in the exposed state to start, the current worm 62 drives the worm wheel 61 to rotate, and then drives the current adapter 4 to swing up. At this time, the launch seat 12 tilts upward, and after the target is locked, the launch seat 12 is controlled to launch the current rocket. After the current rocket is launched, the current adapter 4 is controlled to reset, and then the control motor one 5 is started to drive the positioning frame 3 to flip. At this time, the unfired rocket is exposed, and then another control motor two 63 is controlled to start and drive another launch seat 12 to swing up, and finally the launch seat 12 is controlled to launch to launch the remaining rockets.

[0038] In addition, it should be understood that although the present specification is described according to implementation modes, not every implementation mode contains only one independent technical solution. This description of the specification is only for the sake of clarity. Those skilled in the art should regard the specification as a whole. The technical solutions in each embodiment may also be appropriately combined to form other implementation modes that can be understood by those skilled in the art.

Claims

1. A crawler-type remote-controlled unmanned launching vehicle, comprising a crawler vehicle (1), wherein a bearing seat (11) is provided in the middle of the crawler vehicle (1), characterized in that: A transfer seat (4) is arranged on the top of the bearing seat (11), and a launching seat (12) is detachably connected to the top of the transfer seat (4), and the launching seat (12) is arranged to be tilted during launching.

2. The crawler-type remote-controlled unmanned launching vehicle according to claim 1, characterized in that: The lower end surface of the adapter seat (4) and the upper end surface of the bearing seat (11) are welded and connected, a positioning sleeve (8) is welded on the top of the adapter seat (4), a locking screw (81) is screwed through the outer peripheral wall of the positioning sleeve (8), and a plugging pile (9) that is plugged and matched with the positioning sleeve (8) is welded on the bottom of the launching seat (12), and one end of the locking screw (81) is used in conjunction with one side of the plugging pile (9).

3. The crawler-type remote-controlled unmanned launching vehicle according to claim 1, characterized in that: A magazine (111) is provided on the top of the bearing seat (11), a lifting frame (2) is provided in the magazine (111), a positioning frame (3) is rotatably connected to the top of the lifting frame (2), two adapter seats (4) respectively close to two ends are rotatably connected in the positioning frame (3), the two adapter seats (4) are respectively arranged close to two ends in the positioning frame (3), one side of the launching seat (12) and one side of the adapter seat (4) are detachably connected, a control motor (5) for controlling the rotation of the positioning frame (3) is provided in the magazine (111), and a control assembly (6) for controlling the rotation of the adapter seat (4) is provided in the positioning frame (3).

4. The crawler-type remote-controlled unmanned launching vehicle according to claim 3 is characterized in that: The lifting frame (2) comprises a rectangular frame (21) and an electric telescopic rod (22); the electric telescopic rod (22) is fixedly arranged in the magazine (111) and its output shaft is fixedly connected to a position near the end of the bottom of the rectangular frame (21).

5. The crawler-type remote-controlled unmanned launching vehicle according to claim 4, characterized in that: The upper end surface of the rectangular frame (21) is welded with vertical plates (211) near the two ends, and the middle parts of the two ends of the positioning frame (3) are welded with coaxial support shafts (31), one side of one of the vertical plates (211) is fixedly connected to the control motor (5), and the output shaft of the control motor (5) is welded to one end of the support shaft (31).

6. The crawler-type remote-controlled unmanned launching vehicle according to claim 3, characterized in that: A connecting shaft (41) is welded to the back of the adapter (4) through a support plate, and both ends of the connecting shaft (41) are rotatably connected to both sides of the positioning frame (3). The control assembly (6) comprises a worm wheel (61), a worm (62) and a second control motor (63). The worm wheel (61) is fixedly sleeved on the connecting shaft (41), and a door-shaped plate (32) is welded in the positioning frame (3). The second control motor (63) is fixedly arranged on one side of the door-shaped plate (32) and its output shaft is fixedly connected to the worm (62), and the worm (62) and the worm wheel (61) are meshed.

7. The crawler-type remote-controlled unmanned launching vehicle according to claim 3 is characterized in that: The top of the support seat (11) is hingedly connected to a cover (7) for sealing the opening of the magazine (111); a control motor 3 is provided at the rotation connection between the cover (7) and the support seat (11); and a waterproof frame (112) located on the outer periphery of the magazine (111) is welded to the top of the support seat (11).

8. The crawler-type remote-controlled unmanned launching vehicle according to claim 3, characterized in that: The number of the transmitting seats (12) on the adapter seat (4) is at least two.

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