CN214608094U - Many rotors high load unmanned aerial vehicle - Google Patents
Many rotors high load unmanned aerial vehicle Download PDFInfo
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- CN214608094U CN214608094U CN202120494756.1U CN202120494756U CN214608094U CN 214608094 U CN214608094 U CN 214608094U CN 202120494756 U CN202120494756 U CN 202120494756U CN 214608094 U CN214608094 U CN 214608094U
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Abstract
The utility model discloses a multi-rotor high-load unmanned aerial vehicle, which comprises a multi-rotor unmanned aerial vehicle, a hoisting hanging ring, a cargo container unit, a landing auxiliary unit and a landing auxiliary unit installation part; the lifting hanging rings are symmetrically arranged on two sides of the multi-rotor unmanned aerial vehicle, and the cargo container unit for loading cargos can be detachably lifted at the bottom of the multi-rotor unmanned aerial vehicle through the lifting hanging rings; descending auxiliary unit sets up in many rotor unmanned aerial vehicle's top through descending auxiliary unit installation department, and descending auxiliary unit is connected with many rotor unmanned aerial vehicle's flight control system signal transmission, and descending auxiliary unit is used for carrying out the vision to ground and listens and apart from measuring and transmit data result to flight control system. The utility model provides a pair of many rotors high load unmanned aerial vehicle has high load and the stable, reliable advantage of load.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, especially, relate to a many rotors high load unmanned aerial vehicle.
Background
Unmanned aerial vehicle cargo air transportation can solve current land transportation long-range, with high costs scheduling problem, and single freight transportation efficiency is than higher, but current unmanned aerial vehicle's load carrying capacity is subject to the effective volume of packing box, leads to adopting the cost that unmanned aerial vehicle consumed in the transportation goods also bigger, consequently, improves the payload space then can reduce unmanned aerial vehicle cost of transportation to a certain extent. In order to solve the problem, the utility model discloses a many rotors high load unmanned aerial vehicle has high load and the stable, reliable advantage of load.
Disclosure of Invention
The purpose of the invention is as follows: in order to overcome the not enough of existence among the prior art, the utility model provides a many rotors high load unmanned aerial vehicle has high load and the stable, reliable advantage of load.
The technical scheme is as follows: in order to achieve the purpose, the utility model discloses a multi-rotor high-load unmanned aerial vehicle, which comprises a multi-rotor unmanned aerial vehicle, a hoisting hanging ring, a cargo container unit, a landing auxiliary unit and a landing auxiliary unit installation part; the two hoisting hanging rings are symmetrically arranged on two sides of the multi-rotor unmanned aerial vehicle, and the cargo container unit for loading cargos is detachably hoisted to the bottom of the multi-rotor unmanned aerial vehicle through the hoisting hanging rings; the descending auxiliary unit sets up in many rotor unmanned aerial vehicle's top through descending auxiliary unit installation department, and descends auxiliary unit and many rotor unmanned aerial vehicle's flight control system signal transmission and be connected, the descending auxiliary unit is used for carrying out vision to ground and listens and apart from measuring and transmit data result to flight control system.
Furthermore, the cargo container unit comprises a hard cargo carrying box and two elastic cargo carrying bags symmetrically arranged on two sides of the hard cargo carrying box, the hard cargo carrying box is detachably hoisted through a hoisting hanging ring, and the elastic cargo carrying bags are detachably connected with the hard cargo carrying box.
Furthermore, a flanging is arranged at the outer end of the box opening of the hard cargo carrying box, the hoisting hanging ring is of a U-shaped structure, the hoisting hanging ring is hooked with the flanging, and two end parts of the hoisting hanging ring are hinged with the side face of the body of the multi-rotor unmanned aerial vehicle; the opening of the elastic cargo carrying bag is butted with a hard port box, and the top of the hard port box and the side surface butted with the opening of the elastic cargo carrying bag are provided with openings; the outer end of the opening at the top is provided with a hook, and the hard port box is hung at the box opening of the hard cargo carrying box through the hook.
Further, a handle is arranged on the side face of the hard port box.
Furthermore, a bottom support frame for supporting the bottom of the elastic cargo carrying bag is arranged at the bottom of the hard port box, and a side protection frame for limiting and protecting the side surface of the elastic cargo carrying bag is arranged on the side surface of the hard port box;
the bottom support frame comprises a bottom fixing rod fixedly arranged at the bottom of the hard port box and bottom support rods arranged and connected to the same length side of the bottom fixing rod; the side protection frame comprises a side main protection rod fixedly arranged on the side surface of the hard port box and branch protection rods which are arranged and connected to the upper side of the side main protection rod in the same length; the bottom support rod, the side main guard rod and the support guard rod are telescopic rod structures which are positioned through positioning screws.
Further, the descending auxiliary unit includes camera and the distance sensor who is connected with many rotor unmanned aerial vehicle's flight control system respectively, the camera is the gesture setting on descending auxiliary unit installation department downwards with the distance sensor respectively.
Has the advantages that: the utility model discloses a many rotors high load unmanned aerial vehicle, beneficial effect is: the utility model carries cargo by combining the hard cargo carrying box and the elastic cargo carrying bag, and can load more cargoes according to the elastic expansion function of the elastic cargo carrying bag, thereby greatly improving the loading capacity of the unmanned aerial vehicle; in addition, support elasticity through the end support frame and carry the bag bottom and carry out spacing protection to elasticity through side protection frame and carry the bag side, can improve unmanned aerial vehicle and carry cargo aircraft's stability, reliability of flying.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
fig. 2 is a schematic view of the cargo conveyance unit in a partially disassembled state.
Detailed Description
The present invention will be further described with reference to the accompanying drawings.
As shown in the attached figure 1, the multi-rotor high-load unmanned aerial vehicle comprises a multi-rotor unmanned aerial vehicle 1, a hoisting hanging ring 2, a cargo container unit 3, a landing auxiliary unit 4 and a landing auxiliary unit installation part 5; the two hoisting hanging rings 2 are symmetrically arranged on two sides of the multi-rotor unmanned aerial vehicle 1, and the cargo container unit 3 for loading cargos is detachably hoisted to the bottom of the multi-rotor unmanned aerial vehicle 1 through the hoisting hanging rings 2; descending auxiliary unit 4 sets up in many rotor unmanned aerial vehicle 1's top through descending auxiliary unit installation department 5, and descends auxiliary unit 4 and is connected with many rotor unmanned aerial vehicle 1's flight control system signal transmission, descending auxiliary unit 4 is used for carrying out vision to ground and listens and apart from measuring and transmit data result to flight control system. More specifically, the cargo container unit 3 includes a hard cargo box 31 and two elastic cargo bags 32 symmetrically disposed on two sides of the hard cargo box 31, the hard cargo box 31 is detachably hoisted by the hoisting hanging ring 2, and the elastic cargo bags 32 are detachably connected to the hard cargo box 31. The utility model discloses a stereoplasm carries packing box 31 and elasticity and carries cargo bag 32 and combine together and carry cargo, carries cargo bag 32 according to the elasticity inflation effect that has of elasticity, can load more goods to improve unmanned aerial vehicle's load-carrying capacity greatly.
As shown in fig. 2, a turned edge 310 is arranged at the outer end of the opening of the hard cargo carrying box 31, the hoisting hanging ring 2 is of a U-shaped structure, the hoisting hanging ring 2 is hooked with the turned edge 310, and two end parts of the hoisting hanging ring 2 are hinged to the side surface of the body of the multi-rotor unmanned aerial vehicle 1; the mouth of the elastic cargo carrying bag 32 is butted with a hard port box 32.1, and the top of the hard port box 32.1 and the side surface butted with the mouth of the elastic cargo carrying bag 32 are provided with openings 321; the outer end of the opening 321 at the top has a hook 322, and the hard port box 32.1 is hung at the box mouth of the hard cargo box 31 by the hook 322. The elastic cargo carrying bag 32 and the hard cargo carrying box 31 are convenient to assemble and disassemble, and loading and unloading are convenient.
More specifically, the side of the hard port box 32.1 is provided with a handle 323, so that the use convenience is improved.
It is worth noting that the bottom of the hard port box 32.1 is provided with a bottom support frame 33 which supports the bottom of the elastic cargo carrying bag 32, and the side of the hard port box 32.1 is provided with a side protection frame 34 which carries out limiting protection on the side of the elastic cargo carrying bag 32, so that the stability and reliability of cargo carrying flight of the unmanned aerial vehicle can be improved.
The bottom support frame 33 comprises a bottom fixing rod 331 fixedly arranged at the bottom of the hard port box 32.1 and bottom support rods 332 arranged and connected to the same length side of the bottom fixing rod 331; the side protection frame 34 comprises a side main protection rod 341 fixedly arranged on the side surface of the hard port box 32.1 and a branch protection rod 342 connected with the side main protection rod 341 on the upper side in the same length; the bottom support rod 332, the side main protection rod 341 and the support protection rod 342 are telescopic rod structures positioned by positioning screws, and can adjust the support length and the protection height according to the expansion degree of the elastic cargo carrying bag 32 after loading the cargo, so that the protection reliability is ensured.
Descending auxiliary unit 4 includes camera 41 and the distance sensor 42 of being connected with many rotor unmanned aerial vehicle 1's flight control system respectively, camera 41 and distance sensor 42 are gesture setting on descending auxiliary unit installation department 5 down respectively, and wherein, camera 41 carries out the vision to ground and listens, and distance sensor 42 carries out distance measurement to ground.
The above description is only a preferred embodiment of the present invention, and it should be noted that: for those skilled in the art, without departing from the principle of the present invention, several improvements and modifications can be made, and these improvements and modifications should also be considered as the protection scope of the present invention.
Claims (6)
1. The utility model provides a many rotors high load unmanned aerial vehicle which characterized in that: the multi-rotor unmanned aerial vehicle comprises a multi-rotor unmanned aerial vehicle (1), a hoisting hanging ring (2), a cargo container unit (3), a landing auxiliary unit (4) and a landing auxiliary unit installation part (5); the two hoisting hanging rings (2) are symmetrically arranged on two sides of the multi-rotor unmanned aerial vehicle (1), and the cargo container unit (3) used for loading cargos is detachably hoisted to the bottom of the multi-rotor unmanned aerial vehicle (1) through the hoisting hanging rings (2); descending auxiliary unit (4) set up in the top of many rotor unmanned aerial vehicle (1) through descending auxiliary unit installation department (5), and descend auxiliary unit (4) and the flight control system signal transmission of many rotor unmanned aerial vehicle (1) and be connected, descending auxiliary unit (4) are used for carrying out vision to ground and listen and apart from measuring and transmit data result to flight control system.
2. A multi-rotor high-load drone according to claim 1, characterized in that: the cargo carrying container unit (3) comprises a hard cargo carrying box (31) and two elastic cargo carrying bags (32) symmetrically arranged on two sides of the hard cargo carrying box (31), the hard cargo carrying box (31) can be detachably hoisted through the hoisting hanging ring (2), and the elastic cargo carrying bags (32) are detachably connected with the hard cargo carrying box (31).
3. A multi-rotor high-load drone according to claim 2, characterized in that: the outer end of the box opening of the hard cargo carrying box (31) is provided with a turned edge (310), the hoisting hanging ring (2) is of a U-shaped structure, the hoisting hanging ring (2) is hooked with the turned edge (310), and two end parts of the hoisting hanging ring (2) are hinged with the side face of the body of the multi-rotor unmanned aerial vehicle (1); the mouth of the elastic cargo carrying bag (32) is butted with a hard port box (32.1), and the top of the hard port box (32.1) and the side surface butted with the mouth of the elastic cargo carrying bag (32) are provided with openings (321); the outer end of the opening (321) at the top is provided with a hook (322), and the hard port box (32.1) is hung at the box opening of the hard cargo box (31) through the hook (322).
4. A multi-rotor high-load drone according to claim 3, characterized in that: a handle (323) is arranged on the side surface of the hard port box (32.1).
5. A multi-rotor high-load drone according to claim 3, characterized in that: the bottom of the hard port box (32.1) is provided with a bottom support frame (33) for supporting the bottom of the elastic cargo carrying bag (32), and the side surface of the hard port box (32.1) is provided with a side protection frame (34) for limiting and protecting the side surface of the elastic cargo carrying bag (32);
the bottom support frame (33) comprises a bottom fixing rod (331) fixedly arranged at the bottom of the hard port box (32.1) and bottom support rods (332) arranged and connected to the same length side of the bottom fixing rod (331); the side protection frame (34) comprises a side main protection rod (341) fixedly arranged on the side surface of the hard port box (32.1) and branch protection rods (342) which are connected with the side main protection rod (341) in an arrayed manner and on the upper side of the same length; the bottom support rod (332), the side main guard rod (341) and the support guard rod (342) are telescopic rod structures which are positioned through positioning screws.
6. A multi-rotor high-load drone according to claim 1, characterized in that: descending auxiliary unit (4) are including camera (41) and distance sensor (42) of being connected with the flight control system of many rotor unmanned aerial vehicle (1) respectively, camera (41) and distance sensor (42) are respectively and set up on descending auxiliary unit installation department (5) down the gesture.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120494756.1U CN214608094U (en) | 2021-03-05 | 2021-03-05 | Many rotors high load unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120494756.1U CN214608094U (en) | 2021-03-05 | 2021-03-05 | Many rotors high load unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214608094U true CN214608094U (en) | 2021-11-05 |
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ID=78393897
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120494756.1U Active CN214608094U (en) | 2021-03-05 | 2021-03-05 | Many rotors high load unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214608094U (en) |
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2021
- 2021-03-05 CN CN202120494756.1U patent/CN214608094U/en active Active
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