CN213620242U - Mounting device of unmanned aerial vehicle primary and secondary machine - Google Patents
Mounting device of unmanned aerial vehicle primary and secondary machine Download PDFInfo
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- CN213620242U CN213620242U CN202022457143.9U CN202022457143U CN213620242U CN 213620242 U CN213620242 U CN 213620242U CN 202022457143 U CN202022457143 U CN 202022457143U CN 213620242 U CN213620242 U CN 213620242U
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Abstract
The utility model discloses a carry device of unmanned aerial vehicle primary and secondary machine sets up on the primary machine of unmanned aerial vehicle primary and secondary machine, carry device is including setting up the cabin body and at least one rotation on the primary machine set up the internal pivot in cabin, the cabin body has the hatch door that can open and close, it is provided with a plurality of mount pad to connect in the pivot, the mount pad is used for connecting the submachine of unmanned aerial vehicle primary and secondary machine can release the submachine. Because the submachine is hidden in the cabin body of the mother machine, the primary and secondary unmanned aerial vehicles have higher concealment, the battlefield viability of the primary and secondary unmanned aerial vehicles is greatly improved, and the submachine is put in by using the mounting seats in sequence when the tasks are executed, so that the submachine can execute a plurality of tasks.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, concretely relates to carry device of unmanned aerial vehicle primary and secondary machine.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, has the advantages of small volume, low requirement on the operation environment, strong battlefield viability and the like compared with a manned aircraft, and has very important significance on the future air combat. The cluster intelligent swarm is a development direction of the unmanned aerial vehicle, and the unmanned aerial vehicle intelligent cluster technology has systematic high viability due to the fact that a plurality of unmanned aerial vehicles coordinate with each other to fight.
For example, chinese patent CN106741939B discloses a multi-rotor unmanned aerial vehicle mother-son aircraft system, which comprises a mother aircraft, N child aircraft, and N electromagnetic adsorption devices, where N is a natural number greater than 1; wherein, be provided with the iron sheet above the frame platform of submachine, electromagnetic adsorption device installs arbitrary rotor below of mother's machine and with the motor shaft fixed connection of this rotor, adsorb the iron sheet on the submachine through electromagnetic adsorption device, make submachine and mother adsorb and become an organic whole.
But current primary and secondary machine carry device is external device, and the disguise is low, has seriously influenced unmanned aerial vehicle's battlefield viability, and can only carry out single task.
SUMMERY OF THE UTILITY MODEL
In view of this, the utility model provides a carry device of unmanned aerial vehicle primary and secondary machine to solve above-mentioned technical problem.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a carry device of unmanned aerial vehicle primary and secondary machine, sets up on the primary machine of unmanned aerial vehicle primary and secondary machine, carry the device including setting up cabin body and at least one rotation on the primary machine set up the internal pivot in cabin, the cabin body has the hatch door that can open and close, it is provided with a plurality of mount pad to connect in the pivot, the mount pad is used for connecting the submachine of unmanned aerial vehicle primary and secondary machine can release the submachine.
Further, the hatch door comprises a left cover and a right cover, and the left cover and the right cover are respectively pivoted on the mother machine through hinges.
Furthermore, the hatch door also comprises a plurality of lock catches, and after the left cover and the right cover are closed, the lock catches are locked to keep the hatch door in a closed state.
Further, the mounting device is arranged at the bottom of the mother machine.
Furthermore, the submachine placed on the mounting seat is in a folding storage state.
Furthermore, the rotating shafts are arranged in three numbers, and the three rotating shafts are arranged in the cabin body in parallel.
Furthermore, three mounting seats are arranged on the rotating shaft.
Further, the submachine is four rotor unmanned aerial vehicle.
Further, the main engine adopts an electric-injection double-cylinder steam/heavy oil engine.
Further, the parent machine adopts a high wing load airfoil design.
According to the above technical solution, the utility model has the advantages that:
1. because the submachine is hidden in the cabin body of the master machine, the master machine and the slave machine of the unmanned aerial vehicle have higher concealment, and the battlefield viability of the master machine and the slave machine of the unmanned aerial vehicle is greatly improved;
2. when the tasks are executed, the sub-machines are sequentially thrown in by using the mounting seats, so that the sub-machines can execute a plurality of tasks.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this application, are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification.
Fig. 1 is a schematic perspective view of the present invention.
Fig. 2 is a schematic view of a partial structure of the present invention.
Fig. 3 is a schematic structural view of the interior of the cabin of the present invention.
Fig. 4 is another schematic structural diagram of the interior of the cabin of the present invention.
Fig. 5 is a schematic structural view of the slave unit of the present invention.
List of reference numerals: the device comprises a main machine 1, a left cover 2, a right cover 3, a hinge 4, a lock catch 5, a sub machine 6, a rotating shaft 7, a mounting seat 8 and a cabin 9.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention will be described in further detail with reference to the following embodiments and accompanying drawings. The exemplary embodiments and descriptions of the present invention are provided to explain the present invention, but not to limit the present invention.
Referring to fig. 1 to 5, a mounting device for a primary and secondary unmanned aerial vehicle shown in fig. 1, 2, 3 and 4 is arranged on a primary unmanned aerial vehicle 1, the mounting device comprises a cabin 9 arranged on the primary unmanned aerial vehicle 1 and at least one rotating shaft 7 rotatably arranged in the cabin 9, the cabin 9 has a door capable of being opened and closed, a plurality of mounting seats 8 are connected to the rotating shaft 7, a secondary unmanned aerial vehicle 6 of the primary and secondary unmanned aerial vehicle is connected to the mounting seats 8, when the sub-machine 6 is released, the cabin door is opened, then the rotating shaft 7 rotates to adjust the ejection direction, then the mounting seat 8 ejects the sub-machine 6, as the sub-machines 6 are hidden in the cabin body 9 of the main machine 1, the unmanned primary and secondary machines have higher concealment, the battlefield viability of the unmanned primary and secondary machines is greatly improved, when executing a task, the slave units 6 are sequentially loaded by the mounting base 8, so that the slave units 6 can execute a plurality of tasks.
As shown in fig. 2 and 3, the mounting device is arranged at the bottom of the main machine 1, the cabin door comprises a left cover 2, a right cover 3 and a plurality of lock catches 5, the left cover 2 and the right cover 3 are respectively pivoted on the main machine 1 through hinges 4, the female end and the sub end of each lock catch 5 are respectively arranged on the left cover 2 and the right cover 3, and after the left cover 2 and the right cover 3 are both closed, the female end and the sub end of each lock catch 5 are locked to keep the cabin door in a closed state.
As shown in fig. 3, three rotating shafts 7 are provided, the three rotating shafts 7 are arranged in the cabin 9 in parallel, and each rotating shaft 7 is provided with three mounting seats 8, so that the mother machine 1 can carry 9 the rack machine 6 to perform remote reconnaissance and accurate percussion tasks.
As shown in fig. 4 and 5, the slave unit 6 placed on the mounting seat 8 is in a folded storage state.
In this embodiment, the slave units 6 are grouped into "swarm" and the master unit 1 independently completes the task after the task is released over the air.
In this embodiment, the sub-machine 6 is a quad-rotor unmanned aerial vehicle.
In the embodiment, the main engine 1 can select an electric injection double-cylinder steam/heavy oil engine, so that stable work of various environments is ensured.
In this embodiment, the main engine 1 is designed to have a high wing load airfoil profile, and the wind resistance is 7-level.
In this embodiment, the parent machine 1 can carry two loads simultaneously for a single flight, and has an automatic fault handling capability based on a safe system redundancy design.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not intended to limit the present invention, and it will be apparent to those skilled in the art that various modifications and variations can be made in the embodiments of the present invention. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (10)
1. The utility model provides a carry device of unmanned aerial vehicle primary and secondary machine sets up on primary machine (1) of unmanned aerial vehicle primary and secondary machine, a serial communication port, carry the device including setting up cabin body (9) and at least one rotation setting on primary machine (1) are in pivot (7) in the cabin body (9), cabin body (9) have the hatch door that can open and close, it is provided with a plurality of mount pad (8) to connect on pivot (7), mount pad (8) are used for connecting sub-machine (6) of unmanned aerial vehicle primary and secondary machine can release sub-machine (6).
2. The mounting device of the unmanned aerial vehicle son-mother machine according to claim 1, wherein the cabin door comprises a left cover (2) and a right cover (3), and the left cover (2) and the right cover (3) are respectively pivoted on the mother machine (1) through hinges (4).
3. The mounting device of the unmanned aerial vehicle primary and secondary aircraft according to claim 2, wherein the cabin door further comprises a plurality of lock catches (5), and after the left cover (2) and the right cover (3) are both closed, the lock catches (5) are locked to keep the cabin door in a closed state.
4. The mounting device of unmanned aerial vehicle primary and secondary aircraft according to any one of claims 1-3, characterized in that the mounting device is arranged at the bottom of the primary aircraft (1).
5. The mounting device of the primary and secondary unmanned aerial vehicle units according to any one of claims 1 to 3, wherein the secondary units (6) placed on the mounting base (8) are in a folded storage state.
6. The mounting device of an unmanned aerial vehicle primary and secondary aircraft according to any one of claims 1 to 3, wherein the number of the rotating shafts (7) is three, and the three rotating shafts (7) are arranged in parallel in the cabin (9).
7. The mounting device of unmanned aerial vehicle primary and secondary aircraft according to any one of claims 1-3, characterized in that, be provided with three mount pads (8) on pivot (7).
8. The mounting device of a son and mother unmanned aerial vehicle of claim 1, wherein the son aircraft (6) is a quad-rotor unmanned aerial vehicle.
9. The mounting device of the unmanned aerial vehicle son-mother machine according to claim 1, wherein the mother machine (1) adopts an electronic injection double-cylinder gasoline/heavy oil machine.
10. The mounting arrangement of a drone parent and a drone parent according to claim 1, characterised in that the parent (1) is of high wing load wing profile design.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022457143.9U CN213620242U (en) | 2020-10-29 | 2020-10-29 | Mounting device of unmanned aerial vehicle primary and secondary machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022457143.9U CN213620242U (en) | 2020-10-29 | 2020-10-29 | Mounting device of unmanned aerial vehicle primary and secondary machine |
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| CN213620242U true CN213620242U (en) | 2021-07-06 |
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| CN202022457143.9U Active CN213620242U (en) | 2020-10-29 | 2020-10-29 | Mounting device of unmanned aerial vehicle primary and secondary machine |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113386962A (en) * | 2021-07-13 | 2021-09-14 | 北京航空航天大学 | Primary and secondary formula unmanned aerial vehicle system that can release recovery in air |
| CN114537676A (en) * | 2022-03-03 | 2022-05-27 | 哈尔滨工业大学重庆研究院 | Fuel cell primary and secondary unmanned aerial vehicle |
-
2020
- 2020-10-29 CN CN202022457143.9U patent/CN213620242U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113386962A (en) * | 2021-07-13 | 2021-09-14 | 北京航空航天大学 | Primary and secondary formula unmanned aerial vehicle system that can release recovery in air |
| CN114537676A (en) * | 2022-03-03 | 2022-05-27 | 哈尔滨工业大学重庆研究院 | Fuel cell primary and secondary unmanned aerial vehicle |
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