TWM562820U - Unmanned aerial vehicles with buffer device - Google Patents

Abstract

A drone with a buffer device is used to solve the problem that the conventional drone cannot meet the combat demand mainly based on defense or attack. The system includes: a body having a carrier body and a plurality of spiral wings; and a buffer device coupled by a first plate body and a second plate body, the first plate body and the second plate body There are several buffer groups in between, and the second plate body is connected to the carrier body.

Description

Drone with buffer

This creation is about a drone, especially a cushioning device that allows the drone to be used for combat or attack-based combat demanders.

In recent years, drones have been widely used in various fields, such as aerial photography, investigation, scientific research, geological surveys, and the military to search or kill from things... and so on. Among them, national defense is a very important part for all countries; at present, national defense in the face of foreign invading targets, such as weapons, personnel such as sea, land and air, will be loaded with weapons in a drone ( For example: firearms, projectors or patching nets to defend or attack to deal with various foreign invading targets.

However, when the weapon is launched, it usually produces a momentary retreat force, which is the recoil force. The rear seat force causes the next launching action to be untargeted, which greatly affects the accuracy of the shooting. Moreover, the rear seat force is too The big drone will even cause the drone to lose balance and fall, thus causing the conventional drone to fail to meet the combat demand based on defense or attack.

In view of this, the conventional drones still have the need to improve.

In order to solve the above problems, the purpose of the present invention is to provide a drone with a buffer device, which is provided with a buffer device between the fuselage and the weapon, so that when the drone launches a weapon, the cushioning device can reduce the recoil force. By.

The following directionality or its similar terms, such as "before", "after", "on" (top), "lower", "inside", "outside", "side", etc., mainly refer to the direction of the additional schema, and each directionality or its approximate language is only used to assist in the interpretation and understanding of the creation. The embodiments are not intended to limit the creation.

The unmanned aerial vehicle with a buffer device comprises: a body having a carrier body and a plurality of spiral wings; and a buffer device coupled by a first plate body and a second plate body, the first There is a plurality of buffer groups between the plate body and the second plate body, and the second plate body is connected to the carrier body.

Accordingly, the drone of the present invention has a buffer device mainly between the fuselage and a weapon, and the buffer device has a plurality of buffer groups, so that the weapon carried by the drone is launched by the launching station. The generated recoil can be absorbed by each of the buffer groups, so that the shaking of the body can be greatly reduced, thereby preventing the body from losing balance and falling, and also improving the accuracy of the shooting again.

Each of the buffer groups has two seat plates, each of which has a plurality of receiving holes, each of the receiving holes receiving an elastic body, and each of the elastic bodies protrudes from the upper surface of the two seats . In this way, the elastic body can be respectively abutted against the first plate body and the second plate body.

Wherein, the receiving holes of the two seat plates are arranged correspondingly. Thus, the function of each of the elastic bodies is easily accommodated in each of the receiving holes.

Wherein, the elastic system is placed in the same receiving hole with two coherences. Thus, it has the effect of improving the assembly convenience of each of the elastic body and the two seat plates.

Each of the elastic systems is formed into a ring shape, and each of the seat plates of the buffer group is a first seat plate and a second seat plate. Thus, the structure is simple and easy to manufacture and assemble, and has the effect of reducing manufacturing cost and improving assembly convenience.

The receiving holes of the first seat plate and the second seat plate are correspondingly disposed. Thus, the function of each of the elastic bodies is easily accommodated in each of the receiving holes.

The first extending member and the second extending member respectively extend through the elastic body, and the two ends of the first extending member respectively The two ends of the first plate are correspondingly and combined, and the two ends of the second plate are respectively corresponding to and combined with the two ends of the second plate. Thus, it is effective to avoid the detachment of each of the elastic bodies from the two seat plates.

The first plate body has a plurality of through holes, and each of the through holes penetrates the upper surface of the upper surface of the first plate body. Thus, it has the effect of reducing the overall weight of the cushioning device.

Wherein, the second plate body has a plurality of through holes, each of the through holes penetrating through the upper surface of the second plate body. Thus, it has the effect of reducing the overall weight of the cushioning device.

There is further included a connecting member, a surface of the connecting member is coupled to the second plate by a plurality of positioning rods, and the other surface of the connecting member has a latching portion. In this way, it has the effect of improving the assembly smoothness when the connecting member and the cushioning device are combined.

[this creation]

1‧‧‧ body

11‧‧‧ Vehicle body

12‧‧‧ spiral wings

13‧‧‧ First Joint Department

2‧‧‧buffering device

21‧‧‧ first board

211‧‧‧ Second Joint Department

212‧‧‧First assembly hole

213‧‧‧through hole

22‧‧‧Second plate

221‧‧‧Second assembly hole

222‧‧‧through hole

23‧‧‧Buffering group

231a‧‧‧ first board

231b‧‧‧Second board

232‧‧‧ Elastomers

233a‧‧‧First piercing

233b‧‧‧Second piercing

234‧‧‧ accommodating holes

3‧‧‧Connecting parts

31‧‧‧ Positioning rod

32‧‧‧ Positioning parts

33‧‧‧Card Department

W‧‧‧Weapons

W1‧‧‧ guns

W2‧‧‧ gun net

Fig. 1 is an exploded perspective view of a preferred embodiment of the present invention.

Fig. 2 is an exploded perspective view showing an embodiment of the cushioning device of the present invention.

Figure 3: An exploded perspective view of the buffer set of this creation.

Figure 4: A use case diagram of a preferred embodiment of the present invention in combination with a gun.

Figure 5: A use case diagram of a preferred embodiment of the present invention in combination with a gun net.

In order to make the above and other objects, features and advantages of the present invention more comprehensible, the preferred embodiments of the present invention are described in detail below with reference to the accompanying drawings. ""Unmanned Aerial Vehicle" (UAV), which can be used as a defense or attack-based combat demand, but not limited to it, in the technical field of this creation. Those with ordinary knowledge can understand.

Referring to FIG. 1 , a preferred embodiment of the present invention includes a body 1 and a buffer device 2 . The buffer device 2 is located in the body 1 and a weapon W. between.

The airframe 1 has a carrier body 11 and a plurality of spiral wings 12. The plurality of spiral wings 12 are preferably located around the carrier body 11. The plurality of spiral wings 12 provide the vehicle body 11 with the power of movement. The carrier body 11 can have a plurality of first bonding portions 13 , and the plurality of first bonding portions 13 are preferably located within the range of the plurality of spiral wings 12 . In particular, the fuselage 1 can be any unmanned aerial vehicle (UAV) construction, and the present invention is not limited to the drawings.

Referring to Figures 1 and 2, the buffer device 2 has a first plate body 21 and a second plate body 22, the first plate body 21 is connected to the carrier body 11, and the second plate body 22 is connected. The weapon W. In detail, the first board body 21 may have a plurality of second joint portions 211, and the plurality of second joint portions 211 are located around the first board body 21, and the plurality of second joint portions 211 preferably correspond to The plurality of first joint portions 13 having the body 11 allow the plurality of second joint portions 211 to be combined with the plurality of first joint portions 13 respectively.

The first board body 21 has a first assembly hole 212. The first assembly hole 212 extends through the upper surface of the first board body 21, and the first assembly hole 212 is preferably located at the center of the board body 21. In addition, the first plate body 21 can also have a plurality of through holes 213. The through holes 213 extend through the upper surface of the first plate body 21, and the plurality of through holes 213 can be used to reduce the overall weight of the buffer device 2. The size, shape and position of the plurality of through holes 213 are not limited in this creation.

The second board 22 is located between the body 1 and the first board 21, and the second board 22 has a plurality of second assembly holes 221, and the plurality of second assembly holes 221 extend through the second board. The second assembly holes 221 are preferably aligned with the first assembly holes 212 of the first plate body 21 . In addition, the second plate body 22 can also have a plurality of through holes 222 extending through the upper surface of the second plate body 22, and the plurality of through holes 222 can be used to relieve the buffer device 2 The overall weight, the size, shape and position of the plurality of through holes 222 are not limited in this creation.

Referring to FIGS. 2 and 3 , the buffer device 2 has a plurality of buffer groups 23 , and the plurality of buffer groups 23 are located between the first plate body 21 and the second plate body 22 . In this embodiment, each of the buffer groups 23 has a first seat plate 231a, a second seat plate 231b, and a plurality of elastic bodies 232. The first seat plate 231a may be coupled to the second block in a locking manner. The plate body 22 and the second seat plate 231b may be coupled to the first plate body 21 in a locking manner. Each of the first seat plate 231a and the second seat plate 231b has a plurality of accommodating holes 234. The accommodating holes 234 of the first seat plate 231a and the second seat plate 231b are preferably disposed correspondingly. The body 232 is disposed in each of the accommodating holes 234, and each of the elastic bodies 232 is preferably annular, and the elastic body 232 is preferably disposed in the same accommodating hole 234. 232 protrudes from the upper surface of the first seat plate 231a and the second seat plate 231b, so that the elastic bodies 232 can respectively abut the first plate body 21 and the second plate body 22.

Each of the buffering members 23 can also have a first extending member 233a and a second extending member 233b. The first extending member 233a and the second extending member 233b extend through the elastic body 232. The two ends of the second extending plate 231b are corresponding to and coupled with the two ends of the second seat plate 231b. The elastic body 232 can be prevented from being separated from the two seat plates 231a and 231b, and each of the buffer groups 23 has a better shock absorbing effect. The number of the buffer groups 23 is preferably six, so that the buffer device 2 can have a better cushioning effect.

Referring to FIG. 1 , the drone of the present invention may further include a connecting member 3 connected between the buffer device 2 and the weapon W. One surface of the connecting member 3 has a plurality of positioning rods 31, and each of the positioning rods 31 can pass through the first assembly hole 212 of the first plate body 21 and the plurality of second assembly holes 221 of the second plate body 22, and The connecting member 3 is coupled to the second plate 22 by a positioning member 32.

The other surface of the connecting member 3 has a latching portion 33, and the latching portion 33 is available. In combination with various weapons W, the weapon W can be coupled to the connector 3. As shown in Fig. 4, the latch portion 33 can be coupled to a gun branch W1, or as shown in Fig. 5, the latch portion 33 can be coupled to a gun net W2.

Referring to FIG. 4 , each of the second joint portions 211 of the first plate body 21 can be respectively coupled to each of the first joint portions 13 of the carrier body 11 , and each of the positioning rods 31 of the connector member 3 . Each of the second assembly holes 221 of the second plate body 22 is coupled and positioned by the positioning member 32, and the firearm W1 is coupled to the latching portion 33 of the connecting member 3, so that the buffer device 2 is located at the machine. Between body 1 and the gun W1. In this way, when the firearm W1 generates a recoil force due to the launch, the rear seat force is transmitted to each of the elastic bodies 232 via the plurality of positioning rods 31 and the second plate body 22, and each of the elastic bodies 232 can be Absorbing the recoil force, so that the recoil force can be prevented from being transmitted to the fuselage 1 and the shaking of the fuselage 1 can be greatly reduced; thereby, the fuselage 1 can be prevented from losing balance and falling, and can be lifted The accuracy of shooting again.

In summary, the drone of the present invention has a buffer device between the fuselage and a weapon, and the buffer device has a plurality of buffer groups, so that the weapon carried by the drone is The recoil generated by the launch can be absorbed by each buffer group, so that the shaking of the fuselage can be greatly reduced, thereby preventing the fuselage from losing balance and falling, and also improving the accuracy of another shot. .

Although the present invention has been disclosed by the above-described preferred embodiments, it is not intended to limit the present invention, and it is still within the spirit and scope of the present invention to make various changes and modifications to the above embodiments. The technical scope of the protection is created, so the scope of protection of this creation is subject to the definition of the patent application scope attached.

Claims (10)

A UAV with a buffer device includes: a body having a carrier body and a plurality of spiral wings; and a buffer device coupled by a first plate body and a second plate body, the first plate body And a plurality of buffer groups between the second plate body, the second plate body being connected to the carrier body. The unmanned aerial vehicle with a buffer device according to the first aspect of the invention, wherein each of the buffer groups has two seats, each of the two plates has a plurality of receiving holes, each of the receiving holes receiving An elastomer, each of which protrudes from a lower surface of the two seat plates. The unmanned aerial vehicle with a buffer device according to claim 2, wherein each of the receiving holes of the two seat plates is disposed correspondingly. The unmanned aerial vehicle with a buffer device according to claim 2, wherein the elastic system is placed in the same receiving hole with two coherences. The unmanned aerial vehicle with a buffer device according to claim 2, wherein each of the elastic systems is formed in a ring shape, and the seat plates of each of the buffer groups are a first seat plate and a second seat plate, respectively. The unmanned aerial vehicle with a buffer device according to claim 5, wherein each of the receiving holes of the first seat plate and the second seat plate is disposed correspondingly. The unmanned aerial vehicle with a cushioning device according to claim 6, further comprising a first extending member and a second extending member, wherein the first extending member and the second extending member are each extending An elastic body, the two ends of the first extending member are corresponding to and coupled to the two ends of the first seat plate, and the two ends of the second extending member respectively correspond to the two ends of the second seat plate and are combined . The unmanned aerial vehicle with a buffer device according to claim 1, wherein the first plate body has a plurality of through holes, each of the through holes penetrating the upper surface of the upper surface of the first plate body. The unmanned aerial vehicle with a buffer device according to claim 1, wherein the second plate body has a plurality of through holes, each of the through holes penetrating through the upper surface of the second plate body. A drone having a cushioning device according to any one of claims 1 to 9, wherein A connector is included, a surface of the connector is coupled to the second plate by a plurality of positioning rods, and the other surface of the connector has a latch portion.