CN216186138U

CN216186138U - Primary and secondary unmanned aerial vehicle release recovery unit

Info

Publication number: CN216186138U
Application number: CN202122478210.XU
Authority: CN
Inventors: 王裕雯
Original assignee: Individual
Current assignee: Individual
Priority date: 2021-10-14
Filing date: 2021-10-14
Publication date: 2022-04-05
Anticipated expiration: 2031-10-14

Abstract

The utility model discloses a release and recovery device for a primary-secondary unmanned aerial vehicle, which comprises a square cabin box, a steering engine fixing frame, a steering engine body and a square cabin cover, and is characterized in that: the square cabin box is characterized in that a steering engine fixing frame is in threaded connection with the outer wall of one side of the square cabin box, a steering engine body is in clamping connection with the inside of the steering engine fixing frame, connection contact blocks are arranged on two sides of the outer wall of the steering engine body, and the steering engine body is in mutual contact with the top end of the steering engine fixing frame through the connection contact blocks; the utility model can execute a plurality of tasks, such as power inspection, road detection and the like, when a rescue task is carried out, the primary machine carries the secondary machine to reach the area required by the task, but the area is narrow or the environment is severe, when the six rotor unmanned aerial vehicles can not reach, the secondary machine can play a role and can search and rescue in a large area, one unmanned aerial vehicle is not enough and the other unmanned aerial vehicle is carried, at the moment, the two unmanned aerial vehicles can separately execute the task, and the primary idea of task planning of the multiple unmanned aerial vehicles is basically realized.

Description

Primary and secondary unmanned aerial vehicle release recovery unit

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a release and recovery device for a primary unmanned aerial vehicle and a secondary unmanned aerial vehicle.

Background

Unmanned aerial vehicles serve as emerging industries with emerging features, the popularity is continuously increased in recent years, and because the application range is very wide, the unmanned aerial vehicles are vigorously developed in various countries, at present, for example, the unmanned aerial vehicles in the Xinjiang province have high stability and convenient maneuverability, and the long-endurance and large-combat radius excellent single-machine performances of rainbow unmanned aerial vehicles;

however, the unmanned aerial vehicle release and recovery device does not have the multi-machine coordination capability, and unmanned aerial vehicle formation products such as high and huge unmanned aerial vehicle formation performance are also produced in recent years, but the unmanned aerial vehicle formation device has the defects of complex use and maintenance, harsh use environment, poor practicability and the like, unmanned aerial vehicle cluster coordination in the real sense is not realized, and the use requirement of future clustered unmanned aerial vehicles is not met, so that the release and recovery device for the primary and secondary unmanned aerial vehicles is provided to solve the problems in the prior art.

SUMMERY OF THE UTILITY MODEL

Aiming at the problems, the utility model aims to provide a release and recovery device for a primary-secondary unmanned aerial vehicle, and the release and recovery device for the primary-secondary unmanned aerial vehicle solves the problems of complex use and maintenance, harsh use environment and poor practicability.

In order to realize the purpose of the utility model, the utility model is realized by the following technical scheme: primary and secondary unmanned aerial vehicle release recovery unit, including square cabin box, steering wheel mount, steering wheel body and square cabin cover, its characterized in that: the square cabin cover is characterized in that a steering engine fixing frame is connected to the outer wall of one side of the square cabin box in a threaded mode, a steering engine body is connected to the inner clamping mode of the steering engine fixing frame, connection contact blocks are arranged on two sides of the outer wall of the steering engine body, the steering engine body is mutually abutted to the top end of the steering engine fixing frame through the connection contact blocks, an output end head is installed on the steering engine body, the top end of the output end head penetrates through one side of the square cabin cover, the top end of the output end head is fixedly connected with the square cabin cover, and the square cabin cover is arranged on the top end of the square cabin box.

The further improvement lies in that: the bottom middle part of the square cabin box is fixedly provided with an extension platform through two first fixing bolts, and the bottom end of the extension platform is fixedly connected with two copper columns.

The further improvement lies in that: two the bottom of copper post is run through and is provided with well board on the female machine, and two well board fixed connection on the bottom of copper post and the female machine, extend the platform and be connected with well board on the female machine through two copper posts.

The further improvement lies in that: the steering wheel fixing frame is characterized in that the outer wall of one side of the steering wheel fixing frame is fixedly connected to the shelter box through a second fixing bolt, four connecting and mounting holes are formed in the steering wheel fixing frame in a penetrating mode, and the four connecting and mounting holes are symmetrically formed in the steering wheel fixing frame through the central axis of the steering wheel fixing frame.

The further improvement lies in that: the square cabin box and the square cabin cover are both made of epoxy resin plates, the inner side wall of the square cabin box is bonded with sponge, and a hole site matched with the extension platform is formed in the bottom of the square cabin box.

The utility model has the beneficial effects that: the six-rotor unmanned aerial vehicle can execute multiple tasks such as power inspection, road detection and the like, and if the rescue task is carried out, the host machine carries the submachine to reach an area required by the task, but the area is narrow or the environment is severe, and the submachine can play a role when the six-rotor unmanned aerial vehicle cannot reach; when searching and rescuing in a large area, one unmanned aerial vehicle is not enough, and another unmanned aerial vehicle is carried, so that two unmanned aerial vehicles can separately execute tasks, and the preliminary idea of multi-unmanned aerial vehicle task planning is basically realized.

Drawings

Fig. 1 is a schematic front view of the present invention.

FIG. 2 is a schematic side view of the present invention.

Fig. 3 is a schematic structural diagram of a steering engine fixing frame elevation part of the utility model.

Fig. 4 is a control flow chart of the present invention.

Wherein: 1. a shelter box; 2. a first fixing bolt; 3. an extension platform; 4. a copper pillar; 5. a master upper center plate; 6. a second fixing bolt; 7. a steering engine fixing frame; 8. connecting the mounting holes; 9. a steering engine body; 10. connecting the contact block; 11. an output end; 12. a square hatch cover.

Detailed Description

In order to further understand the present invention, the following detailed description will be made with reference to the following examples, which are only used for explaining the present invention and are not to be construed as limiting the scope of the present invention.

Example one

According to the drawings of fig. 1-3, the release and recovery device for the primary and secondary unmanned aerial vehicles is provided in the embodiment, and comprises a square cabin box 1, a steering engine fixing frame 7, a steering engine body 9 and a square cabin cover 12, wherein the steering engine fixing frame 7 is in threaded connection with the outer wall of one side of the square cabin box 1, the steering engine body 9 is in clamping connection with the steering engine body 7, the two sides of the outer wall of the steering engine body 9 are respectively provided with a connecting contact block 10, the steering engine body 9 is in mutual contact with the top end of the steering engine fixing frame 7 through the connecting contact block 10, the steering engine body 9 is provided with an output end 11, the top end of the output end 11 penetrates through one side of the square cabin cover 12, the top end of the output end 11 is fixedly connected with the square cabin cover 12, the square cabin cover 12 is arranged at the top end of the square cabin box 1, and the steering engine body 9 drives the square cabin cover 12 through the output end 11 when a submachine is needed, the square hatch 12 is opened so that the sub-machine in the square box 1 is operated and used.

The bottom middle part of shelter box 1 has extension platform 3 through two first fixing bolt 2 fixed mounting, and extension platform 3's bottom fixedly connected with two copper posts 4 will extend platform 3 and mother machine and go up well core plate 5 and be connected through two copper posts 4 that set up.

The bottom ends of the two copper columns 4 are provided with a mother machine upper central plate 5 in a penetrating mode, the bottom ends of the two copper columns 4 are fixedly connected with the mother machine upper central plate 5, the extension platform 3 is connected with the mother machine upper central plate 5 through the two copper columns 4, and the device is connected with the mother machine through the arranged mother machine upper central plate 5.

One side outer wall of steering wheel mount 7 passes through second fixing bolt 6 fixed connection at square cabin box 1, and four connection mounting holes 8 have been seted up in the inside run-through of steering wheel mount 7, and four connection mounting holes 8 all use the axis of steering wheel mount 7 to set up as the symmetry, carry out fixed mounting steering wheel mount 7 through the second fixing bolt 6 that sets up to improve the stability of fixed mounting steering wheel mount 7.

The square cabin box 1 and the square cabin cover 12 are both made of epoxy resin plates, the sponge is adhered to the inner side wall of the square cabin box 1, hole sites matched with the extension platforms 3 are formed in the bottom of the square cabin box 1, the square cabin box 1 and the square cabin cover 12 are made of epoxy resin plates, and therefore the strength is guaranteed to be sufficient, and meanwhile the weight is light.

During the use, at first will extend platform 3 and install the bottom of square cabin box 1 through two first fixing bolt 2, and be connected the center of well core plate 5 and female quick-witted body on the female machine, secondly place the aircraft inside of square cabin box 1, later the female machine carries out flight work when, when needs the aircraft to carry out work, through the steering wheel body 9 that sets up, like this when needs use the aircraft, steering wheel body 9 drives square cabin cover 12 through output end 11, open square cabin cover 12, thereby make the aircraft in the square cabin box 1 work and use, primary and secondary unmanned aerial vehicle releases recovery unit just so and has accomplished the use.

Example two

According to fig. 4, the present embodiment provides a mother-son unmanned aerial vehicle controlled release method, which includes the following steps:

the method comprises the following steps: firstly, a director determines the task of the unmanned aerial vehicle flying, and before the flying task starts, post personnel should make preparations for flying in an inner field and an outer field;

step two: after flight preparation is finished, post personnel of the internal field and the external field report to a commander, and then an operator of the external field logs in a specific remote controller account;

step three: after a commander issues a takeoff work command, an operator in an interior controls a platform to send a control command to a master machine firstly, so that the master machine can normally take off under the full-automatic control of the platform, a planned air route is installed for flight work, and the master machine hovers at a specified position;

step four: an operator controls the steering engine body 9 to rotate, the shelter cover 12 is rotated to be opened, then the platform sends a take-off instruction to the flight control of the submachine, so that the submachine finishes a take-off action in the shelter box 1, and the release of the submachine is realized;

step five: the operator controls the two machines to complete tasks through the platform and then returns to a designated place, and then recovers the submachine, the master machine is controlled to hover at a designated position, and then the submachine is taken over by the field operator to recover.

In the second step, because the flight controls of the primary and secondary machines are different, the infield cloud platform needs to take over the primary and secondary machines respectively and upload the flight paths respectively.

In the fifth step, the factor aircraft flight control level precision is too high, the recovery difficulty is high directly through an aircraft control system, and when an observer in the outfield finds that the recovery of the submachine is difficult, the operator in the outfield is informed to recover the submachine.

The foregoing illustrates and describes the principles, general features, and advantages of the present invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the utility model as claimed. The scope of the utility model is defined by the appended claims and equivalents thereof.

Claims

1. Primary and secondary unmanned aerial vehicle releases recovery unit, including shelter box (1), steering wheel mount (7), steering wheel body (9) and shelter lid (12), its characterized in that: the square cabin box is characterized in that a steering engine fixing frame (7) is in threaded connection with the outer wall of one side of the square cabin box (1), a steering engine body (9) is connected to the inner clamping of the steering engine fixing frame (7), connection contact blocks (10) are arranged on two sides of the outer wall of the steering engine body (9), the steering engine body (9) is in mutual contact with the top end of the steering engine fixing frame (7) through the connection contact blocks (10), an output end (11) is installed on the steering engine body (9), the top end of the output end (11) penetrates through one side of a square cabin cover (12), the top end of the output end (11) is fixedly connected with the square cabin cover (12), and the square cabin cover (12) is arranged on the top end of the square cabin box (1).

2. The primary and secondary unmanned aerial vehicle release and recovery device of claim 1, wherein: the square cabin is characterized in that an extension platform (3) is fixedly mounted in the middle of the bottom end of the square cabin box (1) through two first fixing bolts (2), and two copper columns (4) are fixedly connected to the bottom end of the extension platform (3).

3. The primary and secondary unmanned aerial vehicle release and recovery device of claim 2, wherein: two the bottom of copper post (4) is run through and is provided with well core plate (5) on the female machine, and two well core plate (5) fixed connection on the bottom of copper post (4) and the female machine, extend platform (3) and be connected with well core plate (5) on the female machine through two copper posts (4).

4. The primary and secondary unmanned aerial vehicle release and recovery device of claim 1, wherein: the steering wheel fixing frame is characterized in that the outer wall of one side of the steering wheel fixing frame (7) is fixedly connected to the square cabin box (1) through a second fixing bolt (6), four connecting and mounting holes (8) are formed in the steering wheel fixing frame (7) in a penetrating mode, and the four connecting and mounting holes (8) are symmetrically formed in the middle axis of the steering wheel fixing frame (7).

5. The primary and secondary unmanned aerial vehicle release and recovery device of claim 1, wherein: the square cabin box (1) and the square cabin cover (12) are both made of epoxy resin plates, sponge is adhered to the inner side wall of the square cabin box (1), and hole sites matched with the extension platform (3) are formed in the bottom of the square cabin box (1).