Airborne thrower of unmanned aerial vehicle
By designing a lightweight UAV-borne launcher, the problems of complex structure and large size in existing technologies have been solved, achieving the effect of lightweight UAV loading and smooth ammunition delivery.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-04-23
- Publication Date
- 2026-03-20
AI Technical Summary
Existing UAV-borne launchers are complex in structure and large in size, resulting in excessive burden on UAVs during flight and making it difficult to load and launch munitions smoothly.
A simple and compact UAV-borne launcher was designed, including a launch tube, a launching assembly, a clamping assembly, and a control mechanism. The launcher throws the ammunition by connecting the internal components through a through hole, and uses carbon fiber material to reduce weight.
It enables lightweight loading of drones and smooth munition dropping, reduces the weight of drones, and simplifies the assembly process.
Smart Images

Figure CN224013873U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to unmanned aerial vehicle throws and drops technical field especially unmanned aerial vehicle airborne thrower. BACKGROUND
[0002] With the development of technology, the unmanned aerial vehicle is used more and more frequently in the scene of shooting, observation, etc. In shooting, investigation, it can also be thrown and dropped through the unmanned aerial vehicle.
[0003] However, the common unmanned aerial vehicle on the market does not have an external control port, so the types of various throwers are few. If you want to achieve the throwing and dropping of a certain ammunition, you need to load the thrower on the unmanned aerial vehicle. The unmanned aerial vehicle airborne thrower in the prior art has a complex structure and a large size, which makes the flight burden of the unmanned aerial vehicle too heavy, and it is difficult to successfully complete the loading of the thrower and the throwing and dropping of the ammunition. UTILITY MODEL CONTENT
[0004] The utility model aims at providing an unmanned aerial vehicle airborne thrower, which has a simple structure, a small size, can reduce the carrying weight of the unmanned aerial vehicle, and make the unmanned aerial vehicle airborne thrower successfully complete the loading and the ammunition successfully complete the throwing and dropping.
[0005] The utility model provides an unmanned aerial vehicle airborne thrower, which comprises a thrower main body.
[0006] The thrower main body comprises a cartridge, which is a barrel-shaped structure for placing ammunition.
[0007] The thrower main body further comprises a plurality of throw assemblies, each of which comprises an external part, a connecting part and an internal part. The external part is located on the outside of the cartridge. The connecting part is used to connect the external part and the internal part. The internal part is connected to the inside of the cartridge through a through hole and is used to throw out the ammunition.
[0008] The thrower main body comprises a base, and the cartridge and the throw assemblies are mounted on the base.
[0009] Preferably, the thrower main body further comprises a clamping assembly.
[0010] The clamping assembly comprises a circular-arc-shaped groove, which is formed in the end of the connecting part.
[0011] Further preferably, the connecting part comprises a connecting rod, a pin shaft and a pin shaft cap.
[0012] One end of the connecting rod is connected to the clamping assembly, and the other end of the connecting rod is connected to the internal part.
[0013] The connecting rod is connected with the external part through the pin shaft and the pin shaft cap.
[0014] Further preferably, a locking mechanism is further included, which is installed on the base;
[0015] One end of the locking mechanism is connected with the clamping assembly.
[0016] Preferably, a control mechanism is further included, which is located below the base;
[0017] The control mechanism includes a switch, a charge-discharge module, a light-sensitive module, a voltage boosting module, a single-chip microcomputer and a power supply.
[0018] Further preferably, an upper cover is installed at the bottom end of the control mechanism.
[0019] Further preferably, the upper cover is fixed on the unmanned aerial vehicle through screws.
[0020] Further preferably, the throwing assembly is provided with two.
[0021] Further preferably, the two arc-shaped grooves are both semicircular arc-shaped grooves.
[0022] Preferably, the material of the unmanned aerial vehicle onboard throwing device is carbon fiber.
[0023] Beneficial effects:
[0024] The technical scheme of the utility model discloses the ammunition is placed in the cartridge cylinder, when needing to throw, the throwing assembly is opened, wherein the built-in part connected in the cartridge cylinder interior through the through hole can throw the ammunition, the unmanned aerial vehicle onboard throwing device is simple in structure, small in size, can reduce the carrying weight of the unmanned aerial vehicle, makes the unmanned aerial vehicle onboard throwing device complete loading and ammunition successfully complete throwing. BRIEF DESCRIPTION OF DRAWINGS
[0025] In order to more clearly illustrate the specific embodiment of the utility model or the technical scheme in the prior art, the following will briefly introduce the drawings needed to be used in the specific embodiment or the prior art description, and obviously, the drawings in the following description are some embodiments of the utility model, and for those skilled in the art, other drawings can also be obtained according to these drawings without creative labor.
[0026] Figure 1 It is the overall structure front view of the utility model;
[0027] Figure 2 It is the overall structure plan view of the utility model;
[0028] Figure 3The whole structure use state schematic view of the utility model.
[0029] Mark explanation:
[0030] 1: cartridge; 2: external part; 3: connecting part; 301: connecting rod; 302: pin shaft; 303: pin shaft cap; 4: internal part; 5: through hole; 6: clamping assembly; 7: locking mechanism; 8: upper cover; 9: base. DETAILED DESCRIPTION
[0031] The technical scheme of the utility model will be described below in conjunction with embodiments, obviously, the described embodiments are part of the embodiments of the utility model, not all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by the ordinary skilled in the art without making creative labor belong to the protection scope of the utility model.
[0032] In the description of the utility model, it is understood that the orientation or position relationship indicated by the terms "center", "longitudinal", "transverse", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise" and the like is based on the orientation or position relationship shown in the drawings, and is only for the convenience of describing the utility model and simplifying the description, and does not indicate or imply that the indicated device or element must have a particular orientation, be constructed and operated in a particular orientation, and therefore cannot be understood as a limitation on the utility model.
[0033] In addition, the terms "first", "second" are only for the purpose of description, and cannot be understood as indicating or implying relative importance or implicitly indicating the number of the indicated technical features. Therefore, the features defined with "first", "second" can explicitly or implicitly include one or more of the features. In the description of the utility model, the meaning of "multiple" is two or more than two, unless otherwise explicitly and specifically limited. In addition, the terms "mounting", "connecting", "connecting" should be broadly understood, for example, it can be fixedly connected, or it can be detachably connected, or integrally connected; it can be mechanically connected, or it can be electrically connected; it can be directly connected, or it can be indirectly connected through an intermediate medium, or it can be the communication between two elements. For the ordinary skilled in the art, the specific meaning of the above terms in the utility model can be understood according to the specific circumstances.
[0034] As Figures 1 to 3As shown, the utility model provides a kind of unmanned aerial vehicle airborne thrower, it includes thrower main part, thrower main part includes cartridge 1, cartridge 1 is bucket structure, for placing ammunition. Thrower main part further includes throw component, throw component is provided with multiple, throw component includes external part 2, connecting piece 3 and internal part 4, external part 2 is located the outside of cartridge 1, connecting piece 3 is used to connect external part 2 and internal part 4, internal part 4 is connected to the inside of cartridge 1 by through-hole 5, for throwing ammunition. Thrower main part includes base 9, cartridge 1 and throw component are all installed on base 9.
[0035] The technical scheme of the utility model places ammunition in cartridge 1, when needing to throw, throw component opens, wherein internal part 4 connected in the inside of cartridge 1 by through-hole 5 can throw ammunition, the unmanned aerial vehicle airborne thrower simple structure, volume is smaller, can reduce the carrying weight of unmanned aerial vehicle, so that unmanned aerial vehicle airborne thrower successfully completes loading and ammunition successfully completes throwing.
[0036] Thrower main part further includes clamping assembly 6, clamping assembly 6 includes circular-arc groove, and circular-arc groove is set up in the end of connecting piece 3.
[0037] Connecting piece 3 includes connecting rod 301, pin shaft 302 and pin shaft cap 303, one end of connecting rod 301 is connected with clamping assembly 6, the other end of connecting rod 301 is connected with internal part 4, and connecting rod 301 is connected with external part 2 by pin shaft 302 and pin shaft cap 303.
[0038] The unmanned aerial vehicle airborne thrower further includes locking mechanism 7, and the locking mechanism 7 is installed on the base 9. One end of the locking mechanism 7 is connected with the clamping assembly 6.
[0039] The unmanned aerial vehicle airborne thrower further includes a control mechanism, which is located below the base 9. Specifically, as shown in Figure 1 The control mechanism is located inside the base 9. The control mechanism includes a switch, a charge-discharge module, a photosensitive module, a voltage booster, a single-chip microcomputer, and a power supply. Specifically, the working principle of the unmanned aerial vehicle airborne thrower is to convert the received optical signal into an electrical signal to drive the throw component to open and realize the throwing function of a certain ammunition through program code.
[0040] The bottom end of the control mechanism is provided with an upper cover 8. The upper cover 8 is fixed on the unmanned aerial vehicle by screws. That is, the entire unmanned aerial vehicle airborne thrower is fixed on the unmanned aerial vehicle by screws, and the assembly method is simple and fast.
[0041] The throw component is provided with two. The two circular-arc grooves are both semicircular-arc grooves. Specifically, in this embodiment, as shown in Figure 2 The two semicircular-arc grooves together form a complete circle, and the specific size matches the size of the ammunition to be assembled.
[0042] The material of the UAV airborne throwing device is carbon fiber.
[0043] Finally, it should be noted that: the above embodiments are only used to illustrate the technical solutions of the present application, but not limited to them; although the present application has been described in detail with reference to the foregoing embodiments, those skilled in the art should understand that: it can still modify the technical solutions recorded in the foregoing embodiments, or make equivalent replacement for part or all of the technical features; and these modifications or replacements do not make the essence of the corresponding technical solutions deviate from the scope of the technical solutions of the embodiments of the present application.
Claims
1. An airborne launcher for unmanned aerial vehicles (UAVs), characterized in that, include: The main body of the launcher; The main body of the launcher includes a munition-holding tube, which is a barrel-shaped structure used to hold munitions; The main body of the thrower also includes a throwing assembly, which is provided in multiple ways. The throwing assembly includes an external component, a connecting component, and an internal component. The external component is located on the outside of the ammunition loading tube. The connecting component is used to connect the external component and the internal component. The internal component is connected to the inside of the ammunition loading tube through a through hole for throwing the ammunition. The main body of the launcher includes a base, and the projectile container and the launching assembly are both mounted on the base.
2. The UAV-borne launcher according to claim 1, characterized in that, The main body of the launcher also includes a clamping assembly.
3. The UAV-borne launcher according to claim 2, characterized in that, The connector includes a connecting rod, a pin, and a pin cap; One end of the connecting rod is connected to the clamping assembly, and the other end of the connecting rod is connected to the built-in component; The connecting rod is connected to the external component via the pin and pin cap.
4. The UAV-borne launcher according to claim 2, characterized in that, It also includes a locking mechanism, which is mounted on the base; One end of the locking mechanism is connected to the clamping assembly.
5. The UAV-borne launcher according to claim 1, characterized in that, It also includes a control mechanism located below the base; The control mechanism includes a switch, a charging / discharging module, a photosensitive module, a boost module, a microcontroller, and a power supply.
6. The UAV-borne launcher according to claim 5, characterized in that, The bottom of the control mechanism is fitted with a top cover.
7. The UAV-borne launcher according to claim 6, characterized in that, The top cover is fixed to the drone with screws.
8. The UAV-borne launcher according to claim 2, characterized in that, There are two throwing components.
9. The UAV-borne launcher according to claim 1, characterized in that, The drone-borne launcher is made of carbon fiber.