CN221660951U - Unmanned aerial vehicle jettison stores pylon - Google Patents

Abstract

The utility model relates to the technical field of unmanned aerial vehicle equipment, and discloses an unmanned aerial vehicle bullet hanging frame, which comprises an unmanned aerial vehicle, wherein a bullet carrying plate is fixedly connected below the unmanned aerial vehicle through a connecting rod, a bullet throwing device is arranged below the bullet carrying plate, and a protecting device is arranged on the outer surface of the bullet throwing device. The bomb is thrown through the bomb throwing device, when the bomb throwing device is used, the external control equipment can drive the clamping device to loosen the fixing strip, so that the bomb falls under the action of gravity, at the moment, the sliding strip on the back of the bomb can slide on the sliding frame, and the fuse can be pulled through the sliding of the sliding strip in cooperation with the connecting seat, so that the pushing device is pushed downwards. The bullet loading device is protected through the bottom plate below the bullet loading box, the effect of preventing the sympathetic explosion of ammunition caused by collision is achieved, the bullet loading device is loaded through the bullet loading barrel, and when the bullet loading device is used for loading a bullet, the external control equipment can drive the protection buckle to loosen, so that the protection cover at the bottom of the bullet loading barrel is opened.

Description

A drone bombing rack

Technical Field

The utility model relates to the technical field of unmanned aerial vehicle equipment, in particular to a bombing rack for an unmanned aerial vehicle.

Background Art

Unmanned aircraft is abbreviated as "UAV" in English. It is an unmanned aircraft controlled by radio remote control equipment and self-contained program control devices. UAV is actually a general term for unmanned aircraft. From a technical point of view, it can be divided into: unmanned fixed-wing aircraft, unmanned vertical take-off and landing aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned paraglider, etc. Compared with manned aircraft, it has the advantages of small size, low cost, easy use, low requirements for combat environment, and strong battlefield survivability. As unmanned aircraft are of great significance to future air combat, major military countries in the world are stepping up the development of unmanned aircraft. In November 2013, the Civil Aviation Administration of China issued the "Interim Regulations on the Management of Pilots of Civil Unmanned Aircraft Systems", and the China AOPA Association is responsible for the relevant management of civil unmanned aircraft. According to the Regulations, drone operations in mainland China can be divided into 11 categories based on the size of the aircraft and the flying airspace. Among them, only drones weighing more than 116 kilograms and airships weighing more than 4,600 cubic meters flying in integrated airspace are managed by the Civil Aviation Administration. The rest, including other flights such as the increasingly popular micro aerial photography aircraft, are managed by industry associations or are the responsibility of the operators themselves.

Taking a bombing device and a UAV numbered CN219339710U as an example, the utility model relates to the technical field of UAVs, and in particular to a bombing device and a UAV; the bombing device includes an aircraft pylon, a support plate and at least one group of bombing mechanisms, the bombing mechanism includes a delivery tube, a baffle and a transmission assembly, the delivery tube is arranged between the aircraft pylon and the support plate, the baffle is hinged on the support plate and is located at the bottom of the delivery tube, a hook is arranged on the baffle, the transmission assembly includes a linear bearing seat, a latch, a lever and a drive unit, the linear bearing seat is arranged on the support plate, the tail end of the latch passes through the linear bearing seat and is adapted to the hook, the lever is arranged at the output end of the drive unit and the lower end is adapted to the head of the latch. The bombing device of the utility model has a simple structure and light weight, and increases the types and quantities of bombs carried by the UAV through modular design, thereby increasing the bomb load and lethality of the UAV.

but:

It is unable to accelerate the ammunition when dropping it, and it will be easier for the opponent to intercept the ammunition when the drone drops the bomb, thereby weakening the lethality of the ammunition.

Utility Model Content

1. Technical issues to be solved

In view of the deficiencies in the prior art, the utility model provides a bomb-dropping rack for an unmanned aerial vehicle.

(II) Technical solution

To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a bomb-dropping rack for unmanned aerial vehicles, comprising an unmanned aerial vehicle, a bomb-loading plate fixedly connected to the lower part of the unmanned aerial vehicle via a connecting rod, a bomb-dropping device being arranged below the bomb-loading plate; the bomb-dropping device comprising: a bomb-loading seat, the bomb-loading seat being fixedly connected to the bomb-loading plate, a sliding frame fixedly connected to the front of the bomb-loading seat, a sliding bar slidably connected to the front of the sliding frame via a sliding groove, a fixing seat fixedly connected to the front of the sliding bar, a fixing sleeve fixedly installed on the front of the fixing seat, a bomb fixedly fitted on the inner surface of the fixing sleeve, a propulsion device arranged above the bomb, the propulsion device fixedly connected to the front of the sliding bar, a connecting seat arranged on the right side of the sliding bar, the connecting seat fixedly connected to the front of the bomb-dropping seat, the connecting seat connected to the pipeline of the propulsion device via a fuze, a fixing bar fixedly connected to the left side of the sliding bar, a clamping device fixedly installed on the left side of the fixing bar, and the clamping device fixedly connected to the front of the bomb-dropping seat.

Preferably, a protective device is provided on the outer surface of the bomb-dropping device; the protective device comprises: a bomb-loading box, the bomb-loading box is fixedly connected to the bottom of the bomb-loading plate, a bottom plate is fixedly connected to the bottom of the bomb-loading box, a bomb-loading tube is fixedly passed through the bottom of the bottom plate, the bomb-loading tube is fixedly connected to the bottom of the bomb-loading plate, a protective cover is hinged at the bottom of the bomb-loading tube, a protective buckle is fixedly installed on the left side of the bomb-loading tube, and the protective buckle is buckled with the protective cover. The protective device protects the ammunition loaded on the drone, and the bomb-dropping device is protected by the bomb-loading box and the bottom plate below it to prevent the ammunition from exploding due to collision. The bomb-dropping device is loaded by the bomb-loading tube, which also protects it. When the bomb-dropping device drops bombs, the external control device drives the protective buckle to loosen, so that the protective cover at the bottom of the bomb-loading tube is opened, so as to achieve the purpose of dropping bombs.

Preferably, the number of the bomb-dropping devices is six. The bombs are dropped by the bomb-dropping devices, which can act as a launcher and cooperate with the propulsion device to launch the bombs downward.

Preferably, the fuze is adapted to the propulsion device. When the bomb is dropped by the bomb dropping device, the bomb will fall and the propulsion device will pull the fuze, so that the propulsion device will be pushed downward, thereby accelerating the bomb to land.

Preferably, the number of the ammunition barrel, protective cover and protective buckle is six. When the bombing device releases the bomb, the external control device will drive the protective buckle to release, so that the protective cover at the bottom of the ammunition barrel is opened, so as to achieve the purpose of bombing.

Preferably, the bomb throwing device is arranged on the inner surface of the bomb loading tube. The bomb throwing device is loaded through the bomb loading tube, which also plays a protective role.

(III) Beneficial effects

Compared with the prior art, the utility model provides a drone bombing rack, which has the following beneficial effects:

1. This kind of drone bomb rack releases bombs through a bomb release device. The bomb release device can act as a launcher and cooperate with a propulsion device to launch the bomb downward. When in use, an external control device will drive the clamping device to loosen the fixing bar, so that the bomb falls under the action of gravity. At this time, the sliding bar on the back of the bomb will slide on the sliding rack. The sliding of the sliding bar will cooperate with the connecting seat to pull the fuse, so that the propulsion device is pushed downward, thereby accelerating the landing of the bomb.

2. This kind of drone bombing rack protects the ammunition loaded on the drone through the protective device, protects the bombing device through the bomb box and the bottom plate below it, so as to prevent the ammunition from exploding due to collision, and loads the bombing device through the bomb tube, which also plays a protective role. When the bombing device releases the bomb, the external control device will drive the protective buckle to loosen, so that the protective cover at the bottom of the bomb tube is opened to achieve the purpose of bombing. The device has a protective effect on the bombing device, can prevent serious consequences caused by collision, and can achieve the purpose of safety.

BRIEF DESCRIPTION OF THE DRAWINGS

The accompanying drawings are used to provide a further understanding of the present invention and constitute a part of the specification. Together with the embodiments of the present invention, they are used to explain the present invention and do not constitute a limitation of the present invention. In the accompanying drawings:

Figure 1 is an overall structural diagram of the utility model;

Figure 2 is a structural diagram of the bottom of the utility model;

Figure 3 is a diagram of the lower interior of the present invention;

Figure 4 is an enlarged view of point A of the present invention.

In the figure: 1. UAV; 2. Bomb-dropping device; 201. Bomb-carrying seat; 202. Sliding frame; 203. Sliding bar; 204. Fixed seat; 205. Fixed sleeve; 206. Bomb; 207. Propulsion device; 208. Connecting seat; 209. Fuze; 210. Fixed bar; 211. Clamping device; 3. Protective device; 301. Bomb-carrying box; 302. Bottom plate; 303. Bomb-carrying tube; 304. Protective cover; 305. Protective buckle; 4. Connecting rod; 5. Bomb-carrying plate.

DETAILED DESCRIPTION

The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all of the embodiments.

Example 1

As shown in FIGS. 1-4 , the utility model provides a bomb-dropping rack for a drone, including a drone 1, a bomb-loading plate 5 is fixedly connected to the drone 1 through a connecting rod 4, and a bomb-dropping device 2 is arranged below the bomb-loading plate 5;

The bomb throwing device 2 comprises: a bomb loading seat 201, the bomb loading seat 201 is fixedly connected to the bomb loading plate 5, a sliding frame 202 is fixedly connected to the front of the bomb loading seat 201, a sliding bar 203 is slidably connected to the front of the sliding frame 202 through a sliding groove, a fixing seat 204 is fixedly connected to the front of the sliding bar 203, a fixing sleeve 205 is fixedly installed on the front of the fixing seat 204, a bomb 206 is fixedly attached to the inner surface of the fixing sleeve 205, a propulsion device 207 is arranged above the bomb 206, the propulsion device 207 is fixedly connected to the front of the sliding bar 203, a connecting seat 208 is arranged on the right side of the sliding bar 203, the connecting seat 208 is fixedly connected to the front of the bomb loading seat 201, the connecting seat 208 is connected to the propulsion device 207 pipeline through a fuze 209, a fixing bar 210 is fixedly connected to the left side of the sliding bar 203, a clamping device 211 is fixedly installed on the left side of the fixing bar 210, and the clamping device 211 is fixedly connected to the front of the bomb loading seat 201. The number of bomb throwing devices 2 is six. The fuze 209 is adapted to the propulsion device 207 .

In this embodiment, the bomb 206 is dropped by the bomb dropping device 2, which can act as a launcher and cooperate with the propulsion device 207 to launch the bomb 206 downward. When in use, the external control device will drive the clamping device 211 to loosen the fixing bar 210, so that the bomb 206 falls under the action of gravity. At this time, the sliding bar 203 on the back of the bomb 206 will slide on the sliding frame 202. The sliding of the sliding bar 203 will cooperate with the connecting seat 208 to pull the fuse 209, so that the propulsion device 207 is pushed downward, thereby accelerating the landing of the bomb 206.

Example 2

As shown in Figures 1-4, based on Example 1, the utility model provides a technical solution: a protective device 3 is provided on the outer surface of the bombing device 2;

The protection device 3 includes: a bomb box 301, which is fixedly connected to the bottom of the bomb loading plate 5, a bottom plate 302 is fixedly connected to the bottom of the bomb box 301, a bomb barrel 303 is fixedly penetrated at the bottom of the bottom plate 302, the bomb barrel 303 is fixedly connected to the bottom of the bomb loading plate 5, a protection cover 304 is hinged at the bottom of the bomb barrel 303, and a protection buckle 305 is fixedly installed on the left side of the bomb barrel 303, and the protection buckle 305 is buckled with the protection cover 304. The number of the bomb barrel 303, the protection cover 304 and the protection buckle 305 is six. The bomb throwing device 2 is arranged on the inner surface of the bomb barrel 303.

In this embodiment, the protective device 3 protects the ammunition loaded on the drone 1, and the ammunition box 301 and the bottom plate 302 thereunder protect the bombing device 2 to prevent the ammunition from exploding due to collision. The bombing device 2 is loaded through the ammunition barrel 303, which also plays a protective role. When the bombing device 2 releases the bomb, the external control device drives the protective buckle 305 to loosen, so that the protective cover 304 at the bottom of the ammunition barrel 303 is opened to achieve the purpose of bombing. The device has a protective effect on the bombing device 2, can prevent serious consequences caused by collision, and can achieve the purpose of safety.

Claims (6)

1. The utility model provides an unmanned aerial vehicle jettison stores pylon, includes unmanned aerial vehicle (1), its characterized in that: the lower part of the unmanned aerial vehicle (1) is fixedly connected with a bullet loading plate (5) through a connecting rod (4), and a bullet throwing device (2) is arranged below the bullet loading plate (5);

The projectile apparatus (2) comprises: the device comprises a bullet carrying seat (201), wherein the bullet carrying seat (201) is fixedly connected with a bullet carrying plate (5), a sliding frame (202) is fixedly connected with the front surface of the bullet carrying seat (201), a sliding strip (203) is fixedly connected with a fixing seat (204) in the front surface of the sliding frame (202) through a sliding groove, a fixing sleeve (205) is fixedly arranged on the front surface of the fixing seat (204), a bomb (206) is fixedly attached to the inner surface of the fixing sleeve (205), a propelling device (207) is arranged above the bomb (206), the propelling device (207) is fixedly connected with the front surface of the sliding strip (203), a connecting seat (208) is arranged on the right side of the sliding strip (203), the connecting seat (208) is fixedly connected with a propelling device (207) through a fuse (209), a fixing strip (210) is fixedly connected with the left side of the sliding strip (203), and a clamping device (211) is fixedly arranged on the left side of the fixing strip (210), and the front surface of the bomb (211) is fixedly connected with the clamping device (211).

2. The unmanned aerial vehicle projectile projection pylon according to claim 1, wherein: the outer surface of the bullet throwing device (2) is provided with a protection device (3);

The protection device (3) comprises: the bullet carrying box comprises a bullet carrying box body (301), wherein the bullet carrying box body (301) is fixedly connected with the lower side of a bullet carrying plate (5), a bottom plate (302) is fixedly connected with the lower side of the bullet carrying box body (301), a bullet carrying barrel (303) is fixedly penetrated through the bottom of the bottom plate (302), the lower side of the bullet carrying barrel (303) is fixedly connected with the lower side of the bullet carrying plate (5), a protective cover (304) is hinged to the lower side of the bullet carrying barrel (303), a protective buckle (305) is fixedly arranged on the left side of the bullet carrying barrel (303), and the protective buckle (305) is buckled with the protective cover (304).

3. The unmanned aerial vehicle projectile projection pylon according to claim 1, wherein: the number of the projectile throwing devices (2) is six.

4. The unmanned aerial vehicle projectile projection pylon according to claim 1, wherein: the fuze (209) is matched with the propelling device (207).

5. An unmanned aerial vehicle projectile projection pylon according to claim 2, wherein: the number of the loading barrel (303), the protective cover (304) and the protective buckle (305) is six.

6. An unmanned aerial vehicle projectile projection pylon according to claim 2, wherein: the projectile throwing device (2) is arranged on the inner surface of the projectile carrying cylinder (303).