CN109823554B - Unmanned aerial vehicle flies accuse cabin modularization quick assembly disassembly structure - Google Patents
Unmanned aerial vehicle flies accuse cabin modularization quick assembly disassembly structure Download PDFInfo
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Abstract
The invention discloses a modularized quick dismounting structure of an unmanned aerial vehicle flight control cabin, which comprises an empty cabin and a flight control box, wherein the flight control box is clamped in the empty cabin, the top of the flight control box is provided with two GPS seats, the outer side surface of the flight control box is provided with an antenna seat, the two sides of the flight control box are provided with sliding rails, a power plug and a signal plug are arranged in a front panel, the unmanned aerial vehicle body is provided with the empty cabin capable of placing the flight control box, the power socket, the signal socket and the sliding groove are arranged in the empty cabin, the flight control box and the empty cabin are quickly installed and separated through the sliding rail and the sliding groove, the power plug and the signal plug are automatically aligned to be matched with the power socket and the signal socket, complicated operation is not needed, the unmanned aerial vehicle can be matched with various flight control systems through modularization of the flight control cabin, and the application range of the unmanned aerial vehicle can be increased; the design of the plug-in and plug-out type can realize quick installation and replacement, shorten the time for quickly and continuously executing the unmanned aerial vehicle flight task, save the cost and improve the economic benefit.
Description
Technical Field
The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a modularized rapid dismounting structure of a flight control cabin of an unmanned aerial vehicle.
Background
The unmanned aerial vehicle is characterized by small volume, low cost, convenient use, accuracy and the like, and is widely used for tracking, positioning, communication, telemetering, information acquisition and other tasks, a flight control subsystem of the unmanned aerial vehicle is a core system of the unmanned aerial vehicle for completing the whole flight processes of taking off, flying in the air, executing tasks, returning to the ground and recycling and the like, and for most unmanned aerial vehicles, the general flight control is not used, but the unmanned aerial vehicle has a emphasis in the application field of industrial unmanned aerial vehicles, and different flight controls are replaced according to different requirements.
The existing unmanned aerial vehicle flight control cabin modularization quick assembly disassembly structure technology has the following problems: most of the existing unmanned aerial vehicles on the market are provided with fixed flight control systems, which is equivalent to the unmanned aerial vehicle which can only finish fixed tasks in specific environments, the functions are single, and the existing unmanned aerial vehicle has no standard modular design, so that the use efficiency and the application expansion capacity of the unmanned aerial vehicle are low, and meanwhile, the manufacturing and use costs of the existing unmanned aerial vehicle are high.
Disclosure of Invention
The invention aims to provide a modularized quick dismounting structure of an unmanned aerial vehicle flight control cabin, which aims to solve the problems of low application expansion capacity and high manufacturing and use costs of a fixed flight control system and the use efficiency in the background technology.
In order to achieve the above purpose, the present invention provides the following technical solutions: the utility model provides an unmanned aerial vehicle flies to control cabin modularization quick assembly disassembly structure, includes the blank room and flies to control the box, the joint is provided with the accuse box that flies in the blank room, the top of the accuse box that flies is provided with the GPS seat, and flies to control the lateral surface of box and be provided with signal receiving device, all be provided with the slide rail on the left and right sides face of the accuse box that flies, and all be provided with the screw thread fixed orifices on the left and right sides face of the accuse box that flies, the intermediate position department of the medial surface of the accuse box that flies is provided with signal plug, signal plug's left and right sides all is provided with supplementary joint piece, intermediate position department in the blank room is provided with signal socket, signal socket's left and right sides all is provided with power socket, two the outside of power socket all is provided with supplementary joint groove, the left and right sides of blank room all is provided with the snap-in plate, and the outside of two snap-in plates all is provided with the spout, and the outside of two snap-in plates all is provided with the division round pin.
Preferably, the GPS seat comprises a base, a connecting rod and a positioning device, wherein the base is arranged at the bottom of the GPS seat, the connecting rod is arranged on the base, and the positioning device is arranged at the top end of the connecting rod.
Preferably, the signal receiving device comprises a hinge fixing head, a mounting plate and an antenna rod, wherein the hinge fixing head is arranged on the mounting plate, and the antenna rod is arranged on the hinge fixing head.
Preferably, the two GPS seats are provided, and the sizes and shapes of the two GPS seats are the same, and the two signal receiving devices are provided, and the sizes and shapes of the two signal receiving devices are the same.
Preferably, the four slide rails are arranged in total, the lengths and the shapes of the four slide rails are the same, the slide rails are distributed on the left side surface and the right side surface of the flight control box in pairs, the shapes and the sizes of the two power plugs are the same, and the shapes and the sizes of the two auxiliary clamping blocks are the same.
Preferably, the shape and the size of the two fastening plates are the same, the specification and the shape of the two indexing pins are the same, and the size and the shape of the two power sockets are the same.
Preferably, the four sliding grooves are formed in total, the lengths and the shapes of the four sliding grooves are the same, and the sliding grooves are distributed on the inner side face of the buckling plate in pairs.
Preferably, the two hinge fixing heads have the same size and shape, the two mounting plates are made of stainless steel 303, and the two antenna rods have the same size and shape.
Compared with the prior art, the invention provides a modularized quick dismounting structure of an unmanned aerial vehicle flight control cabin, which has the following beneficial effects: the invention is provided with a flight control box capable of enabling a machine body and a flight control cabin to be plugged and unplugged and separated based on the existing unmanned aerial vehicle, simultaneously enabling the machine body and the flight control cabin to be disassembled and assembled conveniently and rapidly, enabling the unmanned aerial vehicle to be capable of replacing different flight control systems, the flight control box of the modularized rapid disassembly structure of the unmanned aerial vehicle flight control cabin is provided with two GPS seats at the top, an antenna seat is arranged on the outer side surface, sliding rails are arranged on two sides of the flight control box, a power plug and a signal plug are arranged in the front panel, an empty cabin of the flight control box can be placed in the opening of the machine body of the unmanned aerial vehicle, the power socket, the signal socket and the sliding groove are arranged in the empty cabin, the flight control box and the empty cabin are quickly installed and separated through the sliding rail and the sliding groove, in the installation process, the power plug and the signal plug are automatically aligned to be matched with the power socket and the signal socket without complicated operation, and meanwhile, the flight control box is fixed in the empty cabin through the indexing pin, so that the stability of flight is ensured, the unmanned aerial vehicle can be matched with various flight control systems through modularization of the flight control cabin, and the weight application range of the unmanned aerial vehicle is increased; the design of the plug-in and plug-out separation type can realize quick installation and replacement of the flight control box, shorten the time for quick and continuous execution of the unmanned aerial vehicle flight task, save the cost and improve the economic benefit.
Drawings
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate and together with the embodiments of the invention and do not constitute a limitation to the invention, and in which:
fig. 1 is a schematic structural diagram of a modular quick assembly disassembly structure of a flight control cabin of an unmanned aerial vehicle;
FIG. 2 is a schematic view of an empty cabin according to the present invention;
FIG. 3 is a schematic view of a GPS base according to the present invention;
fig. 4 is a schematic diagram of a signal receiving apparatus according to the present invention;
In the figure: 1. a power plug; 2. a signal plug; 3. an auxiliary clamping block; 4. a flight control box; 5. a GPS seat; 6. a threaded fixing hole; 7. a signal receiving device; 8. a slide rail; 9. a buckling plate; 10. a signal jack; 11. a power socket; 12. an auxiliary clamping groove; 13. a chute; 14. an empty cabin; 15. an indexing pin; 51. a base; 52. a connecting rod; 53. a positioning device; 71. a hinge fixing head; 72. a mounting plate; 73. an antenna mast.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
Referring to fig. 1-4, the present invention provides a technical solution: the utility model provides an unmanned aerial vehicle flight control cabin modularization quick assembly disassembly structure, includes air chamber 14 and flight control box 4, its characterized in that: the air conditioner comprises an air conditioner box (4) clamped in an air conditioner box (14), GPS seats (5) are arranged at the top of the air conditioner box (4), signal receiving devices (7) are arranged on the outer side faces of the air conditioner box (4), sliding rails (8) are arranged on the left side face and the right side face of the air conditioner box (4), threaded fixing holes (6) are arranged on the left side face and the right side face of the air conditioner box (4), signal plugs (2) are arranged at the middle position of the inner side face of the air conditioner box (4), power plugs (1) are arranged on the left side and the right side of the signal plugs (2), auxiliary clamping blocks (3) are arranged on the outer sides of the two power plugs (1), signal sockets (10) are arranged at the middle position of the air conditioner box (14), power sockets (11) are arranged on the left side and the right side of the two power sockets (11), clamping grooves (12) are arranged on the left side and the right side of the air conditioner box (14), sliding grooves (13) are arranged on the inner sides of the two clamping plates (9), and indexing pins (15) are arranged on the outer sides of the two clamping plates (9).
Further, the GPS seat 5 includes base 51, connecting rod 52 and positioner 53, and the bottom of GPS seat 5 is provided with base 51, is provided with connecting rod 52 on the base 51, and connecting rod 52 is convenient for to positioner 53's installation and change, and connecting rod 52's top is provided with positioner 53, is convenient for fix a position unmanned aerial vehicle to the operator of being convenient for controls it.
Further, the signal receiving apparatus 7 includes a hinge fixing head 71, a mounting plate 72, and an antenna mast 73, the hinge fixing head 71 is provided on the mounting plate 72, and the antenna mast 73 is provided on the hinge fixing head 71.
Further, the two GPS seats 5 are arranged in total, the sizes and the shapes of the two GPS seats 5 are the same, and the current position can be accurately positioned, so that the performance of the equipment can be optimized, the two signal receiving devices 7 are arranged in total, the sizes and the shapes of the two signal receiving devices 7 are the same, the capability of receiving and transmitting signals of the equipment can be enhanced, and the practicability of the equipment is provided.
Further, four slide rails 8 are arranged in total, the lengths and the shapes of the four slide rails 8 are the same, the slide rails 8 are distributed on the left side surface and the right side surface of the flight control box 4 in pairs, and the flight control cabin can be well fixed, so that the stability of the equipment is effectively improved, the shapes and the sizes of the two power plugs 1 are the same, the shapes and the sizes of the two auxiliary clamping blocks 3 are the same, the equipment is convenient to manufacture, and the manufacturing efficiency is improved.
Further, the shape and the size of the two buckling plates 9 are the same, the specification and the shape of the two indexing pins 15 are the same, the size and the shape of the two power sockets 11 are the same, the installation of the flight control box 4 is facilitated, the flight control box 4 can be further fixed by utilizing the indexing pins 15, and firm and reliable connection between the flight control box 4 and the empty cabin 14 is ensured.
Further, the four sliding grooves 13 are formed in total, the lengths and the shapes of the four sliding grooves 13 are the same, the sliding grooves 13 are distributed on the inner side faces of the buckling plates 9 in pairs, and the flight control cabin 4 is convenient to slidingly mount through the sliding rails 8 and the sliding grooves 13, so that the purpose of quickly mounting and replacing the flight control box can be achieved.
Further, the two hinge fixing heads 71 are identical in size and shape, the two mounting plates 72 are made of stainless steel 303, and the stainless steel 303 is easy to process, so that the manufacturing efficiency of the device can be improved, the manufacturing cost can be saved, and the two antenna rods 73 are identical in size and shape, so that the antenna rods 73 are convenient to install and replace.
The working principle and the using flow of the invention are as follows: after the invention is installed, a user firstly checks whether the external appearance of the invention is complete or not, confirms that the invention is in a state capable of working normally, then moves the invention to a position required to be used by the user, then installs the flight control box 4 into the air cabin 14 at the tail of the unmanned aerial vehicle required to be used, and the flight control box 4 and the air cabin 14 are installed and separated quickly through the sliding rail 8 and the sliding groove 13, in the installation process, the power plug 1 and the signal plug 2 on the flight control box 4 are automatically aligned to be matched with the power jack 11 and the signal jack 10 in the air cabin 14, other complicated operations are not required, meanwhile, the auxiliary clamping block 3 arranged on the flight control box 4 can be automatically aligned to be clamped into the auxiliary clamping groove 12 in the air cabin 14, and the air cabin 14 can be fixed through the index pin 15, so that the firm connection between the air cabin 14 and the flight control box 4 is ensured, after the installation is completed, the GPS seat 5 and the signal receiving device 7 can be utilized to receive and feed back information, and an operator can perform various remote control and remote control tasks and the like through radio control.
Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides an unmanned aerial vehicle flies accuse cabin modularization quick assembly disassembly structure, includes air chamber (14) and flies accuse box (4), its characterized in that: the intelligent elevator is characterized in that a flight control box (4) is clamped in the empty cabin (14), a GPS seat (5) is arranged at the top of the flight control box (4), a signal receiving device (7) is arranged on the outer side face of the flight control box (4), sliding rails (8) are arranged on the left side face and the right side face of the flight control box (4), screw thread fixing holes (6) are arranged on the left side face and the right side face of the flight control box (4), a signal plug (2) is arranged at the middle position of the inner side face of the flight control box (4), a power plug (1) is arranged on the left side and the right side of the signal plug (2), auxiliary clamping blocks (3) are arranged on the outer sides of the two power plugs (1), a signal jack (10) is arranged at the middle position of the inside of the empty cabin (14), power jacks (11) are arranged on the left side and the right side of the two power jacks (11), auxiliary clamping grooves (12) are arranged on the outer sides of the two power jacks (11), buckling blocks (9) are arranged on the left side and the right side and the two buckling blocks (9) are arranged on the inner sides of the two buckling blocks (9), and the two buckling blocks (9) are arranged on the outer sides of the empty cabin (9);
The GPS seat (5) comprises a base (51), a connecting rod (52) and a positioning device (53), wherein the base (51) is arranged at the bottom of the GPS seat (5), the connecting rod (52) is arranged on the base (51), and the positioning device (53) is arranged at the top end of the connecting rod (52);
The utility model discloses a power plug, including four slide rails (8), two power plug (1), auxiliary clamping block (3), slide rail (8) are provided with four altogether, and the length and the shape of four slide rails (8) are the same, slide rail (8) two liang distributes on the left and right sides face of flight control box (4), two the shape and the size of power plug (1) are the same, two the shape and the size of auxiliary clamping block (3) are the same.
2. The unmanned aerial vehicle flight control cabin modularization quick assembly disassembly structure according to claim 1, wherein: the signal receiving device (7) comprises a hinge fixing head (71), a mounting plate (72) and an antenna rod (73), wherein the hinge fixing head (71) is arranged on the mounting plate (72), and the antenna rod (73) is arranged on the hinge fixing head (71).
3. The unmanned aerial vehicle flight control cabin modularization quick assembly disassembly structure according to claim 1, wherein: the GPS seats (5) are provided with two, the sizes and the shapes of the two GPS seats (5) are the same, the signal receiving devices (7) are provided with two, and the sizes and the shapes of the two signal receiving devices (7) are the same.
4. The unmanned aerial vehicle flight control cabin modularization quick assembly disassembly structure according to claim 1, wherein: the shape and the size of the two buckling plates (9) are the same, the specification and the shape of the two indexing pins (15) are the same, and the size and the shape of the two power supply sockets (11) are the same.
5. The unmanned aerial vehicle flight control cabin modularization quick assembly disassembly structure according to claim 1, wherein: the sliding grooves (13) are formed in four, the lengths and the shapes of the four sliding grooves (13) are the same, and the sliding grooves (13) are distributed on the inner side face of the buckling plate (9) in pairs.
6. The unmanned aerial vehicle flight control cabin modularization quick assembly disassembly structure according to claim 2, wherein: the size and the shape of the two hinge fixing heads (71) are the same, the size and the shape of the two mounting plates (72) are the same, the two mounting plates (72) are both made of stainless steel 303, and the size and the shape of the two antenna rods (73) are the same.
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| CN201910261106.XA CN109823554B (en) | 2019-04-02 | 2019-04-02 | Unmanned aerial vehicle flies accuse cabin modularization quick assembly disassembly structure |
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| CN201910261106.XA CN109823554B (en) | 2019-04-02 | 2019-04-02 | Unmanned aerial vehicle flies accuse cabin modularization quick assembly disassembly structure |
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| CN112455675A (en) * | 2020-12-11 | 2021-03-09 | 重庆工程职业技术学院 | Modularized water unmanned aerial vehicle |
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