A grenade launching pod for unmanned aerial vehicles

Abstract

The utility model provides a kind of shrapnel launch pod for unmanned aerial vehicle, it is related to unmanned aerial vehicle load technical field, including unmanned aerial vehicle host computer and storage box, storage box is installed in the bottom end of unmanned aerial vehicle host computer, storage box is equipped with storage bin, the side of storage box is movably installed with rotary cover, one end of storage bin is equipped with waiting bin, the inside of storage bin is slidably installed with push plate, a plurality of springs are installed on push plate, a plurality of springs are connected with the side of storage bin, a plurality of shrapnel bodies are placed in storage bin, one shrapnel body in storage bin close to push plate is pasted with push plate, adjacent shrapnel body is pasted with each other, the bottom end of waiting bin is equipped with outlet, the bottom corner position of storage box is installed with a plurality of foot pads, a plurality of flight wings are installed on unmanned aerial vehicle host computer.The device reduces the time interval of air strike, reduces multiple to and fro flight, can effectively reduce the task cycle of unmanned aerial vehicle, reduces battle preparation time and improves task completion efficiency.

Description

Technical Field

[0001] This utility model belongs to the field of unmanned aerial vehicle (UAV) payload technology, and more specifically, it relates to a grenade launching pod for UAVs. Background Technology

[0002] With the development of drone technology, drones have been widely used in various fields such as military, rescue, and surveying. In military applications, the combat capabilities of drones have gradually attracted attention, especially in air strikes. As a high-explosive, wide-range weapon, grenades have significant advantages in specific tactical environments.

[0003] Based on the above, the inventors have discovered the following problems: In the use of existing UAV grenade pods, most pods carry one or two grenades, requiring frequent grenade loading, which increases the time interval between air strikes and requires multiple round trips. Especially in rapid response and emergency missions, this increases the mission cycle of the UAV and reduces combat preparation time and mission completion efficiency.

[0004] Therefore, in view of this, we have studied and improved the existing structure and its shortcomings, and provided a grenade launching pod for UAVs in order to achieve a more practical purpose. Utility Model Content

[0005] The purpose and effectiveness of this utility model's grenade launching pod for unmanned aerial vehicles are achieved through the following specific technical means:

[0006] A grenade launching pod for unmanned aerial vehicles (UAVs) includes a UAV main unit and a storage box. The storage box is installed at the bottom of the UAV main unit and has a storage compartment. A rotating cover is movably installed on one side of the storage box. A waiting compartment is located at one end of the storage compartment. A push plate is slidably installed inside the storage compartment. Several springs are installed on the push plate and connected to one side of the storage compartment. Several grenade bodies are placed inside the storage compartment. One grenade body in the storage compartment, closest to the push plate, is in contact with the push plate. Adjacent grenade bodies are in contact with each other. An exit is located at the bottom of the waiting compartment. Several foot pads are installed at the bottom corners of the storage box. Several flight wings are installed on the UAV main unit.

[0007] Furthermore, a rotating disk is rotatably installed inside the waiting compartment via a rotating shaft, and a pair of arc-shaped plates are installed on the rotating disk, with openings formed at the two adjacent corner positions of the pair of arc-shaped plates.

[0008] Furthermore, the diameter of the opening matches the outlet.

[0009] Furthermore, the spring is provided in at least three sets.

[0010] Furthermore, a servo motor is installed on one side of the storage box, and the output end of the servo motor is connected to the rotating disk via a coupling. The servo motor is also connected to the main power supply of the UAV.

[0011] Furthermore, the storage box has a pair of slots on one side of the rotating cover.

[0012] Furthermore, a pair of mounting blocks are installed at both ends of the storage box and the rotating cover, and one end of the rotating cover is rotatably connected to one mounting block of the storage box via a rotating shaft.

[0013] Furthermore, a locking bolt is installed on one end of the rotating cover mounting block, and the locking bolt is threadedly connected to a mounting block on the storage box.

[0014] Compared with the prior art, the present invention has the following beneficial effects:

[0015] The use of the waiting compartment allows for the placement of multiple grenade launchers. The grenade launchers fall from the exit position, leaving the waiting compartment empty. A spring drives a pusher plate to move the grenade launchers, with the foremost grenade launcher moving into the waiting compartment and awaiting launch. Launching multiple grenades at once can significantly reduce the time interval between air strikes, avoiding the waste of multiple round trips. Especially in rapid response and emergency missions, it can effectively reduce the mission cycle of UAVs, reduce combat preparation time, and improve mission completion efficiency.

[0016] A servo motor drives a rotating disk, which in turn rotates an arc-shaped plate. The arc-shaped plate separates the waiting compartment from the storage compartment, with the opening and exit coinciding. The grenade body falls off, facilitating the launch of multiple grenades and reducing mission cycle time.

[0017] By rotating the locking bolt to disengage it from the mounting block on the storage box, and then rotating the rotating cover, the grenade body can be installed in the storage compartment, reducing combat preparation time and improving mission completion efficiency. Attached Figure Description

[0018] Figure 1 This is a three-dimensional schematic diagram of a grenade launching pod for unmanned aerial vehicles (UAVs) according to this utility model.

[0019] Figure 2 This is a schematic diagram of the explosion of a grenade launching pod for unmanned aerial vehicles (UAVs) according to this utility model.

[0020] Figure 3 This is a cross-sectional schematic diagram of a grenade launching pod for unmanned aerial vehicles (UAVs) according to this utility model.

[0021] Figure 4 This is a bottom-view schematic diagram of a grenade launching pod for a drone according to this utility model.

[0022] In the diagram, the correspondence between component names and drawing numbers is as follows:

[0023] 1. UAV main unit; 2. Flight wing; 3. Storage box; 4. Rotating cover; 5. Storage compartment; 6. Waiting compartment; 7. Push plate; 8. Spring; 9. Exit; 10. Slot; 11. Rotating disk; 12. Curved plate; 13. Opening; 14. Servo motor; 15. Locking bolt; 16. Grenade body; 17. Mounting block; 18. Foot pad. Detailed Implementation

[0024] The embodiments of this utility model will be described in further detail below with reference to the accompanying drawings and examples. The following examples are for illustrative purposes only and should not be construed as limiting the scope of this utility model.

[0025] In the description of this utility model, unless otherwise stated, "a plurality of" means two or more; the terms "upper," "lower," "left," "right," "inner," "outer," "front end," "rear end," "head," "tail," etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings, and are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation, and therefore should not be construed as a limitation of this utility model. In addition, the terms "first," "second," "third," etc., are used for descriptive purposes only and should not be construed as indicating or implying relative importance.

[0026] In the description of this utility model, it should be noted that, unless otherwise explicitly specified and limited, the terms "connected" and "linked" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.

[0027] Example:

[0028] As attached Figure 1 To be continued Figure 4 As shown:

[0029] This utility model provides a grenade launching pod for unmanned aerial vehicles (UAVs), including a UAV main unit 1 and a storage box 3. The storage box 3 is installed at the bottom of the UAV main unit 1. The storage box 3 has a storage compartment 5. A rotating cover 4 is movably installed on one side of the storage box 3. A waiting compartment 6 is provided at one end of the storage compartment 5. A push plate 7 is slidably installed inside the storage compartment 5. Several springs 8 are installed on the push plate 7 and connected to one side of the storage compartment 5. Several grenade bodies 16 are placed inside the storage compartment 5. One grenade body 16 in the storage compartment 5 closest to the push plate 7 is in contact with the push plate 7. Adjacent grenade bodies 16 are in contact with each other. An outlet 9 is provided at the bottom of the waiting compartment 6. Several foot pads 18 are installed at the bottom corners of the storage box 3. The foot pads 18 protect the storage box 3 when the human-machine host 1 lands. Several flight wings 2 are installed on the drone host 1. Multiple grenade bodies 16 can be placed in the waiting compartment 6. The grenade bodies 16 fall from the outlet 9. When the waiting compartment 6 is empty, the spring 8 drives the push plate 7 to move the grenade bodies 16. The foremost grenade body 16 moves into the waiting compartment 6 and waits to be launched. Launching multiple grenades at once can greatly reduce the time interval of air strikes and avoid the waste of multiple flights. Especially in rapid response and emergency missions, it can effectively reduce the mission cycle of the drone and improve combat preparation time and mission completion efficiency.

[0030] The waiting compartment 6 is equipped with a rotating disk 11 that is rotatably mounted on a rotating shaft. A pair of arc-shaped plates 12 are mounted on the rotating disk 11, and openings 13 are formed at the two adjacent corners of the pair of arc-shaped plates 12.

[0031] The diameter of the opening 13 matches that of the outlet 9.

[0032] The spring 8 is provided in at least 3 sets, and the 3 sets of springs 8 exert a pushing force on the push plate.

[0033] A servo motor 14 is installed on one side of the storage box 3. The output end of the servo motor 14 is connected to the rotating disk 11 via a coupling. The servo motor 14 is electrically connected to the UAV host 1. The servo motor 14 drives the rotating disk 11 to rotate, and the rotating disk 11 drives the arc plate 12 to rotate. The arc plate 12 separates the waiting compartment 6 from the storage compartment 5. The opening 13 coincides with the outlet 9, which facilitates the falling of the grenade body 16 and the launch of multiple grenade bodies 16, thus reducing the mission cycle.

[0034] The storage box 3 has a pair of slots 10 on one side of the rotating cover 4.

[0035] The storage box 3 and the rotating cover 4 are each equipped with a pair of mounting blocks 17 at both ends. One end of the rotating cover 4 is rotatably connected to one mounting block 17 of the storage box 3 via a rotating shaft.

[0036] The rotating cover 4 has a locking bolt 15 installed on one end of the mounting block 17. The locking bolt 15 is threadedly connected to a mounting block 17 on the storage box 3. By rotating the locking bolt 15, it can be disengaged from the mounting block 17 on the storage box 3. By rotating the rotating cover 4, the grenade body 16 can be installed in the storage compartment 5, which reduces combat preparation time and improves mission completion efficiency.

[0037] The specific usage and function of this embodiment are as follows:

[0038] First, check the integrity of the device. Only use it after confirming it is intact. During use, first disengage the device from the mounting block 17 on the storage box 3 by rotating the locking bolt 15. Then, rotate the rotating cover 4 to install the grenade body 16 into the storage compartment 5. Tighten the locking bolt 15 to secure the rotating cover 4 to the storage box 3. The flight wing 2 drives the drone host 1 to take off. The drone host 1 controls the servo motor 14 to rotate the rotating disk 11. The rotating disk 11 rotates the arc-shaped plate 12, which separates the waiting compartment 6 from the storage compartment 5. The opening 13 is connected to... With nine outlets overlapping, the grenade body 16 falls from outlet 9, leaving the waiting chamber 6 empty. Spring 8 drives push plate 7 to move the grenade body 16, with the foremost grenade body 16 moving into the waiting chamber 6 and waiting to be launched. Launching multiple grenades at once can significantly reduce the time interval between air strikes and avoid the waste of multiple round trips. Especially in rapid response and emergency missions, it can effectively reduce the mission cycle of UAVs, reduce combat preparation time, and improve mission completion efficiency. This device has a novel overall design and simple structure, and is therefore worthy of widespread promotion and use.

[0039] The embodiments of this utility model are given for illustrative and descriptive purposes only, and are not intended to be exhaustive or to limit the utility model to the forms disclosed. Many modifications and variations will be apparent to those skilled in the art. The embodiments were chosen and described in order to better illustrate the principles and practical applications of this utility model, and to enable those skilled in the art to understand this utility model and design various embodiments with various modifications suitable for a particular purpose.

Claims

1. A grenade launching pod for unmanned aerial vehicles, comprising a main unmanned aerial vehicle (1) and a storage box (3), characterized in that: The storage box (3) is installed at the bottom of the drone host (1). The storage box (3) is provided with a storage compartment (5). A rotating cover (4) is movably installed on one side of the storage box (3). A waiting compartment (6) is provided at one end of the storage compartment (5). A push plate (7) is slidably installed inside the storage compartment (5). Several springs (8) are installed on the push plate (7). Several springs (8) are connected to one side of the storage compartment (5). Several grenade bodies (16) are placed inside the storage compartment (5). One grenade body (16) near the push plate (7) in the storage compartment (5) is in contact with the push plate (7). Adjacent grenade bodies (16) are in contact with each other. An outlet (9) is provided at the bottom of the waiting compartment (6). Several foot pads (18) are installed at the bottom corner of the storage box (3). Several flight wings (2) are installed on the drone host (1).

2. The grenade launching pod for UAV as claimed in claim 1, wherein: The waiting compartment (6) is equipped with a rotating disk (11) that is rotatably mounted on a rotating shaft. A pair of arc-shaped plates (12) are mounted on the rotating disk (11), and openings (13) are formed at the two adjacent corners of the pair of arc-shaped plates (12).

3. The grenade launching pod for UAV as claimed in claim 2 wherein: The diameter of the opening (13) matches that of the outlet (9).

4. The grenade launching pod for UAV as claimed in claim 3 wherein: The spring (8) is provided in at least 3 sets.

5. The grenade launching pod for UAV as claimed in claim 4 wherein: A servo motor (14) is installed on one side of the storage box (3). The output end of the servo motor (14) is connected to the rotating disk (11) via a coupling. The servo motor (14) is electrically connected to the UAV host (1).

6. The grenade launching pod for UAVs of claim 1, wherein: The storage box (3) has a pair of slots (10) on one side of the rotating cover (4).

7. The grenade launching pod for UAV as claimed in claim 6 wherein: Both ends of the storage box (3) and the rotating cover (4) are equipped with a pair of mounting blocks (17), and one end of the rotating cover (4) is rotatably connected to one mounting block (17) of the storage box (3) via a rotating shaft.

8. The grenade launching pod for UAV as claimed in claim 7 wherein: A locking bolt (15) is installed on a mounting block (17) at one end of the rotating cover (4), and the locking bolt (15) is threadedly connected to a mounting block (17) on the storage box (3).

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