Automatic hand grenade throwing device carried by unmanned aerial vehicle

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, and particularly discloses an automatic hand grenade throwing device carried by an unmanned aerial vehicle. The damping mechanism comprises a damping box, four limiting rods, damping springs, a damping plate and a buffering mechanism, the damping box is installed at the top end of the damping frame, the four limiting rods are installed at the four corners of the interior of the damping box respectively, and the outer surfaces of the limiting rods are sleeved with the damping springs; the shock absorption plate drives the shock absorption frame to move up and down through the elasticity of the shock absorption springs, the shock absorption effect can be achieved on shock generated when the unmanned aerial vehicle flies, then the shock can be buffered and absorbed again through the elasticity of the elastic pieces matched with repulsive force generated by the same magnetic poles of the magnetic blocks, and the shock absorption effect is improved. And finally, repeated springback can be inhibited through the damping characteristic of the buffer, so that the stability of the hand grenade in the ejection process is improved, and the ejection accuracy of the hand grenade is also ensured.

Description

Technical Field

[0001] The utility model belongs to the technical field of unmanned aerial vehicles, and in particular relates to an automatic grenade throwing device carried by an unmanned aerial vehicle. Background Art

[0002] A hand grenade is a small hand-thrown ammunition that can be used for both offense and defense. It is also a widely used and large-volume ammunition. It can kill living targets and destroy tanks and armored vehicles. Drones are becoming more and more commonly used in the military field. They can perform tasks such as reconnaissance and strikes. Because of their mobility and flexibility and the advantage of non-contact combat, they are one of the driving forces for the birth of new combat modes. Therefore, combining drones with the classic weapon system of hand grenades not only retains the powerful killing effectiveness of grenades, but also gives them unprecedented remote control capabilities.

[0003] In the Chinese patent with publication number CN107514933B, a drone grenade throwing device is mentioned, which overcomes the limitation of manual throwing, expands the flexibility of use, improves safety, takes into account the safety issues in the grenade throwing process, and ensures the safety of the grenade throwing process through the cooperation of the safety release mechanism and the magazine door unlocking mechanism; however, the bomb placement tube in the bomb throwing device is directly installed on the drone's bracket. This rigid connection cannot effectively buffer or offset these unstable factors when the drone encounters airflow disturbances and self-swaying during flight. Therefore, the grenade is not only affected by the preset ejection force at the moment of ejection, but also additionally bears the dynamic influence from the shaking of the drone, which greatly challenges the stability of the grenade during the ejection process. The lack of stability directly leads to the difficulty in predicting the ejection trajectory of the grenade, thereby reducing its ejection accuracy, which may cause deviations when hitting the target, affecting the overall combat effect;

[0004] In addition, during the use of the grenade launching device, since the grenade placement tube is directly and fixedly installed on the drone's bracket, the angle of the grenade during the ejection process is fixed and difficult to adjust, which in turn limits the application scope of the grenade. It is difficult to flexibly adjust the ejection angle to meet combat needs in different terrain conditions and when facing a variety of targets, reducing its practicality. Utility Model Content

[0005] The purpose of the utility model is to provide an automatic grenade throwing device carried by a drone to solve the problems raised in the above background technology.

[0006] In order to achieve the above purpose, the utility model provides the following technical solutions:

[0007] An automatic grenade throwing device carried by an unmanned aerial vehicle comprises:

[0008] shock mount;

[0009] A shock absorbing mechanism, the shock absorbing mechanism comprising a shock absorbing box, a limiting rod, a shock absorbing spring, a shock absorbing plate and a buffer mechanism, the shock absorbing box is mounted on the top of the shock absorbing frame, four limiting rods are provided, and the four limiting rods are respectively installed at the four inner corners of the shock absorbing box, the shock absorbing spring is sleeved on the outer surface of the limiting rod, the shock absorbing plate is installed between the middle parts of the outer surfaces of the four limiting rods, and two buffer mechanisms are provided, and the two buffer mechanisms are respectively installed at the top and bottom of the shock absorbing plate;

[0010] The adjusting mechanism is installed at the lower part of the outer wall of the shock-absorbing frame, and the adjusting mechanism can adjust the throwing angle of the grenade.

[0011] Preferably, a drone bracket is installed on the top of the shock absorbing mechanism, an automatic grenade throwing bin is installed on the inner side of the adjusting mechanism, and an electric bin door is installed at the bottom end of the automatic grenade throwing bin.

[0012] Preferably, the shock absorbing frame is configured as an H-shaped structure, and the top end of the shock absorbing frame passes through the bottom end of the shock absorbing box and is installed on the bottom end of the shock absorbing plate.

[0013] Preferably, the buffer mechanism includes a buffer, a buffer plate, an elastic sheet and a magnetic block. Two buffer plates are provided, and the opposite surfaces of the two buffer plates are respectively installed on the top of the shock-absorbing plate and the box wall of the shock-absorbing box. The buffer is installed between the middle parts of the opposite surfaces of the two buffer plates. A plurality of elastic sheets and magnetic blocks are provided, and a plurality of elastic sheets are respectively installed on the four sides of the opposite surfaces of the two buffer plates, and a plurality of magnetic blocks are respectively installed at the four corners of the opposite surfaces of the two buffer plates.

[0014] Preferably, the plurality of elastic sheets are all configured as arc-shaped structures, and the opposite surfaces of two adjacent elastic sheets are in contact with each other, and the magnetic poles of the magnetic blocks mounted on the two buffer plates are the same.

[0015] Preferably, the adjustment mechanism includes an adjustment frame, an adjustment shaft, an adjustment gear, a protective cover, an electric push rod and an adjustment rack. The adjustment frame is installed on the upper outer surface of the automatic grenade throwing bin. Two of the adjustment shafts, adjustment gears, protective covers, electric push rods and adjustment racks can be provided. The two adjustment shafts are respectively installed on both sides of the outer wall of the adjustment frame, the two adjustment gears are respectively installed on the outer surfaces of the two adjustment shafts, the two protective covers are respectively installed on the opposite sides of the two adjustment shafts, the two electric push rods are respectively installed on the top ends of the two protective covers, and the two adjustment racks are respectively installed on the output ends of the two electric push rods.

[0016] Preferably, the side surface of the adjustment frame is arranged as a T-shaped structure, and the outer surface of the adjustment gear is meshed with the outer surface of the adjustment rack.

[0017] Preferably, the distance between the top end of the electric push rod and the bottom end of the shock absorbing box is greater than the height of the buffer, and the bottom end of the adjusting rack passes through the lower wall of the protective cover.

[0018] Compared with the prior art, the beneficial effects of the utility model are:

[0019] (1) The utility model sets a shock absorbing mechanism at the bottom end of the UAV bracket. The shock absorbing plate drives the shock absorbing frame to move up and down through the elasticity of the shock absorbing spring, which can reduce the vibration of the UAV during flight. Then, the elasticity of the elastic sheet cooperates with the repulsive force generated by the magnetic block due to the same magnetic poles, which can buffer and reduce the vibration again. Finally, the damping characteristics of the buffer can suppress repeated rebound, thereby improving the stability of the grenade during ejection and ensuring the accuracy of the grenade ejection.

[0020] (2) The utility model provides an adjustment mechanism on the outer surface of the shock-absorbing frame, and the adjustment rack can be pushed and pulled by the extension and retraction of the electric push rod. Then, the adjustment rack is driven by the meshing transmission between the adjustment rack and the adjustment gear to rotate the automatic grenade ejection chamber, thereby adjusting the angle of the grenade during the ejection process, thereby expanding the application range of the grenade, so that the ejection device can flexibly adjust the ejection angle to meet combat needs under different terrain conditions and facing various targets. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] Figure 1 It is a three-dimensional diagram of the utility model;

[0022] Figure 2 It is a cross-sectional view of the shock absorbing mechanism of the utility model;

[0023] Figure 3 It is a three-dimensional diagram of the buffer mechanism of the utility model;

[0024] Figure 4 It is a three-dimensional diagram of the adjustment mechanism of the utility model;

[0025] In the figure: 1. shock-absorbing frame; 2. shock-absorbing mechanism; 3. drone rack; 4. adjustment mechanism; 5. automatic grenade throwing chamber; 6. electric chamber door;

[0026] 21. shock-absorbing box; 22. limit rod; 23. shock-absorbing spring; 24. shock-absorbing plate; 25. buffer mechanism;

[0027] 251, buffer; 252, buffer plate; 253, elastic sheet; 254, magnetic block;

[0028] 41. Adjustment frame; 42. Adjustment shaft; 43. Adjustment gear; 44. Protective cover; 45. Electric push rod; 46. Adjustment rack. DETAILED DESCRIPTION

[0029] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in 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.

[0030] Embodiment 1:

[0031] See also Figure 1 - Figure 4 As shown, a grenade automatic throwing device carried by a drone comprises:

[0032] Shock mount 1;

[0033] The shock absorbing mechanism 2 includes a shock absorbing box 21, a limiting rod 22, a shock absorbing spring 23, a shock absorbing plate 24 and a buffer mechanism 25. The shock absorbing box 21 is installed at the top of the shock absorbing frame 1. Four limiting rods 22 are provided, and the four limiting rods 22 are respectively installed at the four inner corners of the shock absorbing box 21. The shock absorbing spring 23 is sleeved on the outer surface of the limiting rod 22. The shock absorbing plate 24 is installed between the middle parts of the outer surfaces of the four limiting rods 22. Two buffer mechanisms 25 are provided, and the two buffer mechanisms 25 are respectively installed at the top and bottom of the shock absorbing plate 24;

[0034] The adjusting mechanism 4 is installed at the lower part of the outer wall of the shock absorbing frame 1, and the adjusting mechanism 4 can adjust the throwing angle of the grenade.

[0035] Depend on Figure 1 - Figure 3 It can be seen that a drone rack 3 is installed on the top of the shock absorbing mechanism 2, an automatic grenade throwing chamber 5 is installed on the inner side of the adjusting mechanism 4, and an electric chamber door 6 is installed on the bottom of the automatic grenade throwing chamber 5;

[0036] The buffer mechanism 25 includes a buffer 251, a buffer plate 252, an elastic sheet 253 and a magnetic block 254. Two buffer plates 252 are provided, and the opposite surfaces of the two buffer plates 252 are respectively installed on the top of the shock absorbing plate 24 and the box wall of the shock absorbing box 21. The buffer 251 is installed between the middle parts of the opposite surfaces of the two buffer plates 252. There are a plurality of elastic sheets 253 and a plurality of magnetic blocks 254, and the plurality of elastic sheets 253 are respectively installed on the four sides of the opposite surfaces of the two buffer plates 252, and the plurality of magnetic blocks 254 are respectively installed at the four corners of the opposite surfaces of the two buffer plates 252.

[0037] As can be seen from the above, first, the drone bracket 3 is installed on the drone, so that the entire throwing device can be carried by the drone. When the drone encounters airflow disturbance and self-swaying during flight, the shock-absorbing plate 24 drives the shock-absorbing frame 1 to move up and down on the limit rod 22, and then the elasticity of the shock-absorbing spring 23 can be used to dampen the vibration caused by the shaking. At the same time, the elastic deformation of the arc-shaped elastic sheet 253 and the repulsive force generated by the magnetic block 254 due to the same magnetic poles can be used to buffer and dampen the vibration of the grenade automatic throwing bin 5 again. Finally, the damping characteristics of the buffer 251 can suppress the repeated rebound of the shock-absorbing spring 23, which can effectively buffer or offset these unstable factors, thereby improving the stability of the grenade during the ejection process, making the ejection trajectory of the grenade predictable, and avoiding deviations when hitting the target, thereby ensuring the accuracy of the grenade ejection and improving the overall combat effect.

[0038] Specifically, refer to Figure 1 - Figure 3 As shown, the shock absorber frame 1 is configured as an H-shaped structure, and the top end of the shock absorber frame 1 passes through the bottom end of the shock absorber box 21 and is installed on the bottom end of the shock absorber plate 24; a plurality of elastic sheets 253 are configured as arc structures, and the opposite surfaces of two adjacent elastic sheets 253 contact each other, and the magnetic poles of the magnetic blocks 254 installed on the two buffer plates 252 are the same.

[0039] As can be seen from the above, the H-shaped shock absorbing frame 1 can enhance its structural strength, and the installation between the shock absorbing frame 1 and the shock absorbing plate 24 enables the shock absorbing frame 1 to perform shock absorbing operation as the shock absorbing plate 24 moves; the arc-shaped elastic sheet 253 can have a certain deformation buffering ability, and the same magnetic poles make the magnetic blocks 254 on the two buffer plates 252 generate repulsive forces against each other.

[0040] Embodiment 2:

[0041] refer to Figure 4 As shown, the adjustment mechanism 4 includes an adjustment frame 41, an adjustment shaft 42, an adjustment gear 43, a protective cover 44, an electric push rod 45 and an adjustment rack 46. The adjustment frame 41 is installed on the upper outer surface of the grenade automatic throwing chamber 5. Two adjustment shafts 42, adjustment gears 43, protective cover 44, electric push rod 45 and adjustment rack 46 can be provided. Two adjustment shafts 42 are respectively installed on both sides of the outer wall of the adjustment frame 41, two adjustment gears 43 are respectively installed on the outer surfaces of the two adjustment shafts 42, two protective covers 44 are respectively installed on the opposite sides of the two adjustment shafts 42, two electric push rods 45 are respectively installed on the top ends of the two protective covers 44, and two adjustment racks 46 are respectively installed on the output ends of the two electric push rods 45.

[0042] As can be seen from the above, when it is necessary to throw a grenade, the electric push rod 45 can be started, and the push-pull movement of the adjustment rack 46 can be achieved through the extension and retraction of the electric push rod 45. At this time, by adjusting the meshing transmission between the rack 46 and the adjustment gear 43, the adjustment shaft 42 drives the adjustment frame 41 to rotate, so that the adjustment frame 41 drives the automatic grenade throwing chamber 5 to rotate stably, and the angle of the grenade during the ejection process can be adjusted, thereby expanding the application range of the grenade. When the angle of the automatic grenade throwing chamber 5 is adjusted, the electric chamber door 6 can be opened, so that the automatic grenade throwing chamber 5 throws the grenade inside out, so that the throwing device can flexibly adjust the ejection angle to meet combat needs under different terrain conditions and facing diverse targets, and also improves the practical performance of the throwing device.

[0043] Preferably, reference Figure 4 As shown, the side of the adjustment frame 41 is set as a T-shaped structure, and the outer surface of the adjustment gear 43 is meshed with the outer surface of the adjustment rack 46; the distance between the top end of the electric push rod 45 and the bottom end of the shock absorber box 21 is greater than the height of the buffer 251, and the bottom end of the adjustment rack 46 passes through the lower wall of the protective cover 44.

[0044] As can be seen from the above, the contact area between the adjustment frame 41 and the automatic grenade throwing chamber 5 can be increased, so that the adjustment frame 41 and the automatic grenade throwing chamber 5 are firmly connected, and the adjustment gear 43 can be driven to rotate by the adjustment rack 46; the electric push rod 45 is placed within the buffering range of the buffer 251 and does not contact the shock absorber box 21, so as not to affect the buffering of the buffer 251, and the protective cover 44 can limit and protect the adjustment rack 46.

[0045] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. An automatic grenade throwing device carried by an unmanned aerial vehicle, characterized in that: include: Shock mount (1); A shock absorbing mechanism (2), the shock absorbing mechanism (2) comprising a shock absorbing box (21), a limiting rod (22), a shock absorbing spring (23), a shock absorbing plate (24) and a buffer mechanism (25), the shock absorbing box (21) being mounted on the top end of the shock absorbing frame (1), four limiting rods (22) being provided, and the four limiting rods (22) being respectively installed at the four inner corners of the shock absorbing box (21), the shock absorbing spring (23) being sleeved on the outer surface of the limiting rod (22), the shock absorbing plate (24) being installed between the middle parts of the outer surfaces of the four limiting rods (22), and two buffer mechanisms (25) being provided, and the two buffer mechanisms (25) being respectively installed at the top end and the bottom end of the shock absorbing plate (24); An adjusting mechanism (4) is installed on the lower part of the outer wall of the shock absorbing frame (1), and the adjusting mechanism (4) can adjust the throwing angle of the grenade.

2. The automatic grenade throwing device carried by an unmanned aerial vehicle according to claim 1, characterized in that: The top end of the shock absorbing mechanism (2) is provided with a drone rack (3), the inner side of the adjusting mechanism (4) is provided with an automatic grenade throwing chamber (5), and the bottom end of the automatic grenade throwing chamber (5) is provided with an electric chamber door (6).

3. The automatic grenade throwing device carried by an unmanned aerial vehicle according to claim 2, characterized in that: The shock absorbing frame (1) is configured as an H-shaped structure, and the top end of the shock absorbing frame (1) passes through the bottom end of the shock absorbing box (21) and is installed on the bottom end of the shock absorbing plate (24).

4. The automatic grenade throwing device carried by an unmanned aerial vehicle according to claim 1, characterized in that: The buffer mechanism (25) comprises a buffer (251), a buffer plate (252), an elastic sheet (253) and a magnetic block (254); two buffer plates (252) are provided, and the opposite surfaces of the two buffer plates (252) are respectively installed on the top of the shock absorbing plate (24) and the box wall of the shock absorbing box (21); the buffer (251) is installed between the middle parts of the opposite surfaces of the two buffer plates (252); a plurality of elastic sheets (253) and a plurality of magnetic blocks (254) are provided, and the plurality of elastic sheets (253) are respectively installed on the four sides of the opposite surfaces of the two buffer plates (252); and a plurality of magnetic blocks (254) are respectively installed on the four corners of the opposite surfaces of the two buffer plates (252).

5. The automatic grenade throwing device carried by an unmanned aerial vehicle according to claim 4, characterized in that: The plurality of elastic sheets (253) are all arranged in an arc-shaped structure, and the opposite surfaces of two adjacent elastic sheets (253) are in contact with each other, and the magnetic poles of the magnetic blocks (254) mounted on the two buffer plates (252) are the same.

6. The automatic grenade throwing device carried by an unmanned aerial vehicle according to claim 1, characterized in that: The adjusting mechanism (4) comprises an adjusting frame (41), an adjusting shaft (42), an adjusting gear (43), a protective cover (44), an electric push rod (45) and an adjusting rack (46). The adjusting frame (41) is mounted on the upper portion of the outer surface of the automatic grenade throwing chamber (5). Two of the adjusting shaft (42), the adjusting gear (43), the protective cover (44), the electric push rod (45) and the adjusting rack (46) can be provided. The two adjusting shafts (42) are respectively mounted on both sides of the outer wall of the adjusting frame (41). The two adjusting gears (43) are respectively mounted on the outer surfaces of the two adjusting shafts (42). The two protective covers (44) are respectively mounted on the opposite sides of the two adjusting shafts (42). The two electric push rods (45) are respectively mounted on the top ends of the two protective covers (44). The two adjusting racks (46) are respectively mounted on the output ends of the two electric push rods (45).

7. The automatic grenade throwing device carried by an unmanned aerial vehicle according to claim 6, characterized in that: The side surface of the adjustment frame (41) is arranged as a T-shaped structure, and the outer surface of the adjustment gear (43) is meshed with the outer surface of the adjustment rack (46).

8. The automatic grenade throwing device carried by an unmanned aerial vehicle according to claim 6, characterized in that: The distance between the top end of the electric push rod (45) and the bottom end of the shock absorbing box (21) is greater than the height of the buffer (251), and the bottom end of the adjusting rack (46) penetrates the lower wall of the protective cover (44).

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