CN215043774U

CN215043774U - Geological exploration unmanned aerial vehicle of universal joint angle modulation

Info

Publication number: CN215043774U
Application number: CN202121393246.1U
Authority: CN
Inventors: 王野; 邰贺; 杨静; 陈闯; 赵昕
Original assignee: Individual
Current assignee: Individual
Priority date: 2021-06-23
Filing date: 2021-06-23
Publication date: 2021-12-07
Anticipated expiration: 2031-06-23

Abstract

The utility model discloses a geological exploration unmanned aerial vehicle of universal joint angle modulation, including unmanned aerial vehicle main part, infrared prospecting ware, first wing, second wing are all installed to unmanned aerial vehicle main part both sides symmetry, unmanned aerial vehicle main part bottom has seted up accomodates the chamber, accomodate the intracavity and install the universal joint, the universal joint includes the first connecting piece of fixed mounting in accomodating the intracavity, first connecting piece is kept away from unmanned aerial vehicle main part one end and is articulated to be fixed with steering member one end, steering member other end is articulated to be fixed with the second connecting piece, fixed mounting has infrared prospecting ware on the second connecting piece, infrared surveying ware swing joint accomodates the chamber; accomodate infrared reconnaissance ware through setting up the chamber of accomodating in unmanned aerial vehicle main part bottom, fix infrared reconnaissance ware through fixing the universal joint of accomodating the intracavity, the rotation that the universal joint can be nimble is favorable to improving the mobility of device, improves the practicality of device, is favorable to improving the use ageing of device.

Description

Geological exploration unmanned aerial vehicle of universal joint angle modulation

Technical Field

The utility model relates to an unmanned aerial vehicle field especially relates to a geological exploration unmanned aerial vehicle of universal joint angle modulation.

Background

The unmanned plane is called unmanned plane for short, and is an unmanned aerial vehicle operated by radio remote control equipment and a self-contained program control device. Unmanned aerial vehicles are in fact a general term for unmanned aerial vehicles, and can be defined from a technical perspective as follows: unmanned fixed wing aircraft, unmanned VTOL aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned paravane, etc. Compared with manned aircraft, it has the advantages of small volume, low cost, convenient use, low requirement on the operational environment, strong battlefield viability and the like.

Along with the development of science and technology, unmanned aerial vehicle is widely applied to various trades, if in geological exploration, unmanned aerial vehicle mainly plays the effect such as exploration vein, oil well, but current geological exploration type unmanned aerial vehicle, exploration equipment often the snap-on unmanned aerial vehicle, and the angle is difficult to adjust, greatly reduced the speed of unmanned aerial vehicle exploration, reduced geological exploration efficiency, for this reason we propose the geological exploration unmanned aerial vehicle of universal joint angle modulation.

Disclosure of Invention

In order to overcome the not enough of prior art, the utility model provides a geological exploration unmanned aerial vehicle of universal joint angle modulation is favorable to improving the mobility of surveying equipment, improves exploration efficiency, is favorable to improving the practicality of device, improves the use ageing of device.

In order to solve the technical problem, the utility model provides a following technical scheme: the utility model provides a geological exploration unmanned aerial vehicle of universal joint angle modulation, includes unmanned aerial vehicle main part, infrared reconnaissance ware, first wing, second wing are installed to the equal symmetry in unmanned aerial vehicle main part both sides, unmanned aerial vehicle main part bottom has been seted up and has been accomodate the chamber, accomodate the intracavity and install the universal joint, the universal joint includes fixed mounting in the first connecting piece of accomodating the intracavity, first connecting piece is kept away from unmanned aerial vehicle main part one end and is articulated to be fixed with steering piece one end, the articulated fixed mounting of steering piece other end has the second connecting piece, fixed mounting has infrared reconnaissance ware on the second connecting piece, infrared reconnaissance ware swing joint accomodates the chamber.

Preferably, the top of the unmanned aerial vehicle main body is far away from one end of the first wing and is fixedly provided with a control block, and the control block is fixedly provided with a plurality of steering paddles distributed at equal intervals.

Preferably, unmanned aerial vehicle main part top middle part fixed mounting has the parachute, the inner chamber has been seted up at unmanned aerial vehicle main part top, parachute swing joint inner chamber.

Preferably, the parachute is made of nylon and is fixedly provided with a folding framework inside.

Preferably, a plurality of rollers are installed at the bottom of the unmanned aerial vehicle main body, the number of the rollers is even, and the rollers are symmetrical to each other.

Preferably, unmanned aerial vehicle main part bottom fixed mounting has a plurality of telescope tubes, equal swing joint has the liter telescopic link in the telescope tube, gyro wheel fixed mounting is in rise telescopic link bottom.

Preferably, a loop bar is fixedly mounted at the inner top of the telescopic pipe, a limiting plate is fixedly mounted at the top of the telescopic pipe, the limiting plate is movably connected with the inner bottom of the telescopic pipe, a damping spring is sleeved on the loop bar, and the bottom of the damping spring is attached to the top of the limiting plate.

Preferably, unmanned aerial vehicle main part material is carbon fiber, and its surface electroplates has the wearing layer.

Compared with the prior art, the utility model discloses the beneficial effect that can reach is:

1. the infrared detector is stored through the storage cavity arranged at the bottom of the unmanned aerial vehicle main body, and the infrared detector is fixed through the universal joint fixed in the storage cavity, so that the universal joint can flexibly rotate, the mobility of the device is improved, the practicability of the device is improved, and the use timeliness of the device is improved;

2. through setting up at the control block and the steering oar at unmanned aerial vehicle main part top, the direction of being convenient for control unmanned aerial vehicle main part is favorable to improving the practicality of device, improves the mobility of unmanned aerial vehicle main part to improve exploration efficiency, through will turning to the oar by same control block control, be favorable to improving the use ageing of device, the nature controlled of the hoisting device of being convenient for.

Drawings

FIG. 1 is a front view of the overall structure of the present invention;

FIG. 2 is a schematic view of the landing state structure of the present invention;

FIG. 3 is a top view of the overall structure of the present invention;

FIG. 4 is a schematic view of the structure at A shown in FIG. 1 according to the present invention;

FIG. 5 is a schematic view of the internal structure of the telescopic tube of the present invention;

wherein: 1. an unmanned aerial vehicle main body; 2. a first airfoil; 3. a second airfoil; 4. a control block; 5. a steering paddle; 6. an inner cavity; 7. a telescopic sleeve; 8. lifting and shrinking the rod; 9. a roller; 10. an infrared detector; 11. a parachute; 12. a universal joint; 13. a first connecting member; 14. a steering member; 15. a second connecting member; 16. a limiting plate; 17. a loop bar; 18. a damping spring; 19. a receiving cavity.

Detailed Description

In order to make the technical means, the creation features, the achievement purposes and the functions of the invention easy to understand, the invention is further explained below with reference to the specific embodiments, but the following embodiments are only the preferred embodiments of the invention, not all. Based on the embodiments in the implementation, other embodiments obtained by those skilled in the art without any creative work belong to the protection scope of the present invention. The experimental methods in the following examples are conventional methods unless otherwise specified, and materials, reagents and the like used in the following examples are commercially available unless otherwise specified.

Example (b):

as shown in fig. 1-5, the utility model provides a geological exploration unmanned aerial vehicle of universal joint angle modulation, including unmanned aerial vehicle main part 1, infrared prospecting ware 10, first wing 2, second wing 3 are all installed to unmanned aerial vehicle main part 1 both sides symmetry, unmanned aerial vehicle main part 1 bottom has seted up accomodates the chamber 19, accomodate the intracavity and install universal joint 12, universal joint 12 includes first connecting piece 13 of fixed mounting in accomodating the chamber 19, first connecting piece 13 keeps away from unmanned aerial vehicle main part 1 one end and articulates and is fixed with steering member 14 one end, steering member 14 other end articulates and is fixed with second connecting piece 15, fixed mounting has infrared prospecting ware 10 on second connecting piece 15, infrared prospecting ware 10 swing joint accomodates the chamber 19;

accomodate infrared reconnaissance ware 10 through setting up accomodate the chamber 19 in unmanned aerial vehicle main part 1 bottom, fix infrared reconnaissance ware 10 through fixing the universal joint 12 of accomodating in the chamber 19, the rotation that the universal joint 12 can be nimble is favorable to improving the mobility of device, improves the practicality of device, is favorable to improving the use prescription of device.

As shown in fig. 3, the embodiment also discloses that a control block 4 is fixedly mounted at one end of the top of the main body 1 of the unmanned aerial vehicle, which is far away from the first wing 2, and a plurality of steering paddles 5 which are distributed at equal intervals are fixedly mounted on the control block 4;

through setting up at the control block 4 and the steering oar 5 at 1 top of unmanned aerial vehicle main part, the direction of being convenient for control unmanned aerial vehicle main part 1 is favorable to the practicality of improving the device, improves the mobility of unmanned aerial vehicle main part 1 to improve exploration efficiency, through will turning to oar 5 and being controlled by same control block 4, be favorable to improving the use ageing of device, the nature controlled of the hoisting device of being convenient for.

As shown in fig. 2 and fig. 3, the embodiment further discloses that a parachute 11 is fixedly installed in the middle of the top of the main body 1 of the unmanned aerial vehicle, an inner cavity 6 is formed in the top of the main body 1 of the unmanned aerial vehicle, and the parachute 11 is movably connected with the inner cavity 6;

through setting up parachute 11 at 1 top of unmanned aerial vehicle main part, be convenient for protect unmanned aerial vehicle main part 1, reduce unmanned aerial vehicle main part 1's descending speed, be favorable to improving the practicality of device, through setting up at the inner chamber 6 at 1 top of unmanned aerial vehicle main part, be convenient for place parachute 11, further improve the use ageing of device.

As shown in fig. 2, the embodiment further discloses that the parachute 11 is made of nylon, and a folding framework is fixedly installed inside the parachute;

establish to nylon through with parachute 11, be favorable to improving parachute 11's intensity, be favorable to improving the practicality of device, through setting up at the inside folding skeleton of parachute 11, be convenient for carry out reutilization to parachute 11, be favorable to reducing the use cost of device.

As shown in fig. 1 and 2, the present embodiment further discloses that a plurality of rollers 9 are installed at the bottom of the main body 1 of the unmanned aerial vehicle, the number of the rollers 9 is even, and the rollers are symmetrical to each other;

through setting up gyro wheel 9 in 1 bottoms of unmanned aerial vehicle main part, be convenient for take off for unmanned aerial vehicle main part 1 and provide power, be favorable to improving device's practicality, improve device's use ageing.

As shown in fig. 1 and fig. 2, the embodiment further discloses that a plurality of telescopic pipes 7 are fixedly installed at the bottom of the main body 1 of the unmanned aerial vehicle, telescopic pipes 7 are movably connected with telescopic rods 8, and the rollers 9 are fixedly installed at the bottoms of the telescopic rods 8;

install telescopic tube 7 in unmanned aerial vehicle main part 1 bottom to telescopic link 8, be convenient for fix gyro wheel 9, and can raise the height of unmanned aerial vehicle main part 1, protect infrared reconnaissance ware 10.

As shown in fig. 5, the embodiment further discloses that a loop bar 17 is fixedly installed at the top inside the telescopic tube 7, a limit plate 16 is fixedly installed at the top of the telescopic rod 8 inside the telescopic tube 7, the limit plate 16 is movably connected to the bottom inside the telescopic tube 7, a damping spring 18 is sleeved on the loop bar 17, and the bottom of the damping spring 18 is attached to the top of the limit plate 16;

through setting up loop bar 17 in telescopic tube 7, be convenient for install damping spring 18, support damping spring 18 limiting plate 16, make the liter telescopic rod 8 can be in telescopic tube 7 internalization, be favorable to when falling to the ground at unmanned aerial vehicle main part 1, cushion, be favorable to improving the use prescription of device.

As shown in fig. 1-3, the embodiment further discloses that the main body 1 of the unmanned aerial vehicle is made of carbon fiber, and the surface of the main body is plated with a wear-resistant layer;

establish to the carbon fiber through with unmanned aerial vehicle main part 1, be favorable to improving unmanned aerial vehicle main part 1 intensity, and can reduce the dead weight, be convenient for take off, be favorable to improving the practicality of device, through electroplating at the wearing layer on unmanned aerial vehicle main part 1 surface, be favorable to protecting unmanned aerial vehicle main part 1, improve the life of device.

In the present disclosure, unless expressly stated or limited otherwise, the first feature "on" or "under" the second feature may comprise direct contact between the first and second features, or may comprise contact between the first and second features not directly. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.

The foregoing shows and describes the general principles, essential features, and advantages of the invention. It should be understood by those skilled in the art that the present invention is not limited by the above embodiments, and the description in the above embodiments and the description is only preferred examples of the present invention, and is not intended to limit the present invention, and that the present invention can have various changes and modifications without departing from the spirit and scope of the present invention, and these changes and modifications all fall into the scope of the claimed invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims

1. The utility model provides a geological exploration unmanned aerial vehicle of universal joint angle modulation, includes unmanned aerial vehicle main part (1), infrared reconnaissance ware (10), first wing (2), second wing (3), its characterized in that are installed to the equal symmetry in unmanned aerial vehicle main part (1) both sides: unmanned aerial vehicle main part (1) bottom has been seted up and has been accomodate chamber (19), accomodate and install universal joint (12) in chamber (19), universal joint (12) are including first connecting piece (13) of fixed mounting in accomodating chamber (19), first connecting piece (13) are kept away from that unmanned aerial vehicle main part (1) one end is articulated to be fixed with steering gear (14) one end, the articulated fixed mounting of steering gear (14) other end has second connecting piece (15), fixed mounting has infrared reconnaissance ware (10) on second connecting piece (15), chamber (19) are accomodate to infrared reconnaissance ware (10) swing joint.

2. The unmanned aerial vehicle for geological exploration with adjustable universal joint angle as claimed in claim 1, wherein: the unmanned aerial vehicle main part (1) top is kept away from first wing (2) one end fixed mounting and is had control block (4), fixed mounting has steering oar (5) that a plurality of equidistance distribute on control block (4).

3. The unmanned aerial vehicle for geological exploration with adjustable universal joint angle as claimed in claim 1, wherein: unmanned aerial vehicle main part (1) top middle part fixed mounting has parachute (11), inner chamber (6) have been seted up at unmanned aerial vehicle main part (1) top, parachute (11) swing joint inner chamber (6).

4. The unmanned aerial vehicle for geological exploration with adjustable universal joint angle of claim 3, wherein: parachute (11) material is nylon, and its inside fixed mounting has folding skeleton.

5. The unmanned aerial vehicle for geological exploration with adjustable universal joint angle as claimed in claim 1, wherein: a plurality of rollers (9) are installed to unmanned aerial vehicle main part (1) bottom, roller (9) quantity is the even number, and its symmetry each other.

6. The unmanned aerial vehicle for geological exploration with adjustable universal joint angle of claim 5, wherein: unmanned aerial vehicle main part (1) bottom fixed mounting has a plurality of telescopic tube (7), equal swing joint has telescopic rod (8) in telescopic tube (7), gyro wheel (9) fixed mounting is in telescopic rod (8) bottom.

7. The unmanned aerial vehicle for geological exploration with adjustable universal joint angle of claim 6, wherein: top fixed mounting has loop bar (17) in telescopic tube (7), it has limiting plate (16) to rise telescopic tube (8) top and be located telescopic tube (7) internal fixed mounting, bottom in limiting plate (16) swing joint telescopic tube (7), damping spring (18) have been cup jointed on loop bar (17), damping spring (18) bottom and limiting plate (16) top laminating.

8. The unmanned aerial vehicle for geological exploration with adjustable universal joint angle as claimed in claim 1, wherein: unmanned aerial vehicle main part (1) material is carbon fiber, and its surface electroplates has the wearing layer.