CN218839798U

CN218839798U - Unmanned aerial vehicle with distance measurement

Info

Publication number: CN218839798U
Application number: CN202223587090.8U
Authority: CN
Inventors: 左欢金; 左永泉
Original assignee: Guangdong Teshineng Intelligent Technology Co ltd
Current assignee: Guangdong Teshineng Intelligent Technology Co ltd
Priority date: 2022-12-30
Filing date: 2022-12-30
Publication date: 2023-04-11
Anticipated expiration: 2032-12-30

Abstract

The utility model discloses an unmanned aerial vehicle with distance measurement, the device comprises a device body, this internal fuselage and fuselage bottom of being provided with of device are provided with the mounting groove, it installs the distancer to be provided with camera and camera lower extreme in the mounting groove, the mounting groove rear end is provided with fixed cover and fixed cover internal rotation and is provided with movable cover, movable cover one side drive is installed motor and is fixed in the mounting groove, the fuselage is equipped with the inserting groove all around in cantilever and the cantilever, it is equipped with the movable rod to slide in the inserting groove, the inserting groove upper end is equipped with spacing hole, be equipped with a plurality of screw holes on the movable rod, from this, can realize the protection function that shelters from to camera and distancer, avoided camera and distancer directly to expose the problem that receives damage and pollution outside easily, can realize the length adjustment to the unmanned aerial vehicle cantilever, avoided cantilever length and screw fixed and lead to the poor problem of unmanned aerial vehicle adaptability.

Description

Unmanned aerial vehicle with distance measurement

Technical Field

The utility model relates to an unmanned aerial vehicle especially relates to an unmanned aerial vehicle with distance measurement, belongs to unmanned air vehicle technical field.

Background

Unmanned aerial vehicle is an unmanned vehicles who uses radio remote control or self program control to give first place to, and it has advantages such as small, low, the convenient to use of making fake, extensively is used for fields such as aerial reconnaissance, supervision, communication, anti-dive, electronic interference, and at present, unmanned aerial vehicle range finding often adopts ultrasonic ranging and laser range finding for confirm the distance between target and the unmanned aerial vehicle.

The publication numbers in the prior art are: CN 210707887U's utility model provides an intelligent range finding unmanned aerial vehicle, it is through setting up the casing, first motor, the revolving stage, the ring channel, laser range finder and latch mechanism, the casing effectively protects inside laser range finder, it is rotatory to start first motor and drive the revolving stage, thereby make things convenient for laser range finder to carry out the range finding to the position of difference, but it can only carry out the semi-surrounding protection to the distancer through the casing, do not possess the parcel protective capacities to camera and distancer, during non-use, its distancer still exposes outside, easily receive the influence of external force factor to lead to the distancer to appear damaging, it does not possess the length adjustment ability to the unmanned aerial vehicle cantilever simultaneously, when flight environment and demand change, it can't effectively adjust the cantilever and change the screw, this will lead to its unmanned aerial vehicle can't mismatch with the flight condition, adaptability is not good, therefore, we need upgrade and reform transform on prior art's basis.

SUMMERY OF THE UTILITY MODEL

The to-be-solved technical problem of the utility model is to provide an unmanned aerial vehicle with distance measurement, this unmanned aerial vehicle with distance measurement can realize the protect function that shelters from to camera and distancer, avoided camera and distancer direct exposure to receive the problem of damage and pollution outside easily, can realize the length adjustment to the unmanned aerial vehicle cantilever, be convenient for adapt to different demands, avoided cantilever length and screw fixed and lead to the poor problem of unmanned aerial vehicle adaptability.

In order to solve the problems, the following technical scheme is provided:

the utility model provides an unmanned aerial vehicle with distance measurement, includes the device body, this internal fuselage and fuselage bottom of being provided with of device is provided with the mounting groove, be provided with camera and camera lower extreme in the mounting groove and install the distancer, the mounting groove rear end is provided with fixed cover and fixed cover internal rotation and is provided with the movable cover, movable cover one side drive mounting has motor and motor to fix in the mounting groove, the fuselage has set up the inserting groove all around in cantilever and the cantilever, it is equipped with the movable rod to slide in the inserting groove, the inserting groove upper end is equipped with spacing hole, be equipped with a plurality of screw holes on the movable rod, the movable rod front end is fixed with the screw.

Furthermore, the bottom of the machine body is provided with two groups of supporting legs, and the two groups of supporting legs are fixedly arranged on two sides of the mounting groove.

Furthermore, lateral blocks are arranged on two sides of the fixed cover, and rotating shafts are arranged on two sides of the movable cover and rotatably inserted into the lateral blocks.

Furthermore, an upper gear is arranged on the inner side of the rotating shaft, a lower gear is meshed with the lower end of the upper gear, and the lower gear is connected with the motor.

Furthermore, a guide rod is arranged on the outer side of the movable rod and is arranged in grooves on two sides of the insertion groove in a sliding mode.

Furthermore, the position of the limiting hole corresponds to that of the threaded hole, and a bolt penetrates through the limiting hole and the threaded hole and is screwed in the limiting hole and the threaded hole.

Furthermore, a knob is arranged at the upper end of the bolt.

Compared with the prior art, the beneficial effects of the utility model reside in that:

1. the utility model discloses a be provided with fixed cover, movable cover, go up gear, lower gear and motor in the device, by motor drive gear rotation down during the use, gear and axis of rotation synchronous rotation in the drive of lower gear, the axis of rotation drives movable cover and rotates around the side piece, can realize the protective function that shelters from to camera and distancer, improves the security of camera end, has avoided camera and distancer directly to expose the problem that receives damage and pollution outside easily.

2. The utility model discloses a be provided with cantilever, inserting groove, movable rod, screw hole and bolt in the device, pulling movable rod during the use makes its lateral shifting in the inserting groove, and spacing hole corresponds with the screw hole when removing to suitable position, can be with the bolt spiro union in spacing hole and threaded hole this moment, can realize the length adjustment to the unmanned aerial vehicle cantilever, is convenient for adapt to different demands, has avoided cantilever length and screw fixed and lead to the poor problem of unmanned aerial vehicle adaptability.

Specific embodiments of the present invention are disclosed in detail with reference to the following description and the accompanying drawings, which specify the manner in which the principles of the invention may be employed. It should be understood that the embodiments of the present invention are not so limited in scope. The embodiments of the invention include many variations, modifications and equivalents within the spirit and scope of the appended claims.

Drawings

The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:

fig. 1 is a schematic view of the overall structure of an unmanned aerial vehicle with distance measurement according to the present invention;

fig. 2 is a schematic bottom view of an unmanned aerial vehicle with distance measurement according to the present invention;

fig. 3 is a partial structural exploded view of an unmanned aerial vehicle with distance measurement according to the present invention;

fig. 4 is according to the utility model discloses an unmanned aerial vehicle's cantilever structure with distance measurement decomposes view.

In the figure: 1. a device body; 2. a body; 3. supporting legs; 4. mounting grooves; 5. a camera; 6. a distance meter; 7. a fixed cover; 8. a movable cover; 9. a side block; 10. a rotating shaft; 11. an upper gear; 12. a lower gear; 13. an electric motor; 14. a cantilever; 15. inserting grooves; 16. a limiting hole; 17. a movable rod; 18. a guide rod; 19. a threaded hole; 20. a bolt; 21. a knob; 22. a propeller.

Detailed Description

In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.

As shown in fig. 1-4, the unmanned aerial vehicle with distance measurement that this embodiment provided, including device body 1, be provided with fuselage 2 and fuselage 2 bottom in the device body 1 and be provided with mounting groove 4, be provided with camera 5 and camera 5 lower extreme in the mounting groove 4 and install distancer 6, mounting groove 4 rear end is provided with fixed cover 7 and fixed cover 7 internal rotation and is provided with movable cover 8, the drive of movable cover 8 one side is installed motor 13 and is fixed in mounting groove 4, fuselage 2 is equipped with cantilever 14 all around and has seted up inserting groove 15 in cantilever 14, it is equipped with movable rod 17 to slide in inserting groove 15, inserting groove 15 upper end is equipped with spacing hole 16, be equipped with a plurality of screw holes 19 on the movable rod 17, movable rod 17 front end is fixed with screw 22.

The preferred, 2 bottoms of fuselage are provided with two sets of supporting legs 3, and two sets of supporting legs 3 are fixed to be set up in 4 both sides of mounting groove, are convenient for support and place fuselage 2.

Preferably, both sides of the fixed cover 7 are provided with side blocks 9, both sides of the movable cover 8 are provided with rotating shafts 10, and the rotating shafts 10 are rotatably inserted into the side blocks 9, so that the movable cover 8 can be rotatably installed on the inner side of the fixed cover 7, and the movable cover 8 can rotate in the fixed cover 7.

Preferably, an upper gear 11 is disposed inside the rotating shaft 10 and a lower gear 12 is engaged with a lower end of the upper gear 11, the lower gear 12 is connected to a motor 13, so that the rotating shaft 10 is driven by the motor 13 to rotate, and the movable cover 8 is driven by the rotating shaft 10 to rotate.

Preferably, the guide rod 18 is arranged outside the movable rod 17, and the guide rod 18 is slidably arranged in the grooves on the two sides of the insertion groove 15, so that the movable rod 17 can move linearly in the insertion groove 15, and the movable rod 17 is prevented from rotating and moving in the insertion groove 15.

Preferably, the position of the limiting hole 16 corresponds to the position of the threaded hole 19, and a bolt 20 is screwed into the limiting hole 16 and the threaded hole 19 so as to fix the movable rod 17.

Preferably, the bolt 20 is provided with a knob 21 at the upper end thereof for facilitating manual control of the bolt 20.

The utility model discloses an application principle and use flow: when using, at first place unmanned aerial vehicle on subaerial through supporting leg 3, then control it to take off and take and carry out the shooting and distance measurement, movable cover 8 is in the closed condition before measuring, control motor 13 work this moment, motor 13 drive lower gear 12 rotates, lower gear 12 drives gear 11 and axis of rotation 10 and rotates axis of rotation 10 and drive movable cover 8 and shrink to fixed cover 7 in, camera 5 and distancer 6 expose this moment, control motor 13 reversal and with movable cover 8 reset after the measurement is accomplished can, when the different environment of needs flight, can suitably adjust the length of cantilever 14, rotatory knob 21, it drives bolt 20 and rotates and breaks away from in spacing hole 16 and the screw hole 19, then outwards stimulate movable rod 17, make movable rod 17 reach suitable position department, this moment again with bolt 20 spiro union in spacing hole 16 and corresponding screw hole 19 can, can change propeller 22 after the regulation distance, match the cantilever 14 of different length, promote unmanned aerial vehicle power.

It should be noted that, in this document, relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.

Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. 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

1. The utility model provides an unmanned aerial vehicle with distance measurement, a serial communication port, includes device body (1), it is provided with fuselage (2) and fuselage (2) bottom and is provided with mounting groove (4) to be provided with camera (5) and camera (5) lower extreme in device body (1), mounting groove (4) rear end is provided with fixed cover (7) and fixed cover (7) internal rotation and is provided with movable cover (8), movable cover (8) one side drive is installed motor (13) and is fixed in mounting groove (4), fuselage (2) are equipped with cantilever (14) and cantilever (14) all around and have seted up inserting groove (15), it is equipped with movable rod (17) to slide in inserting groove (15), inserting groove (15) upper end is equipped with spacing hole (16), be equipped with a plurality of screw holes (19) on movable rod (17), movable rod (17) front end is fixed with screw (22).

2. The unmanned aerial vehicle with distance measurement of claim 1, characterized in that, fuselage (2) bottom is provided with two sets of supporting legs (3), and two sets of supporting leg (3) are fixed to be set up in mounting groove (4) both sides.

3. The unmanned aerial vehicle with distance measurement of claim 1, characterized in that, fixed cover (7) both sides are equipped with side piece (9), movable cover (8) both sides are equipped with axis of rotation (10) and axis of rotation (10) rotate and peg graft in side piece (9).

4. An unmanned aerial vehicle with distance measurement according to claim 3, wherein an upper gear (11) is arranged inside the rotating shaft (10) and a lower gear (12) is meshed with the lower end of the upper gear (11), and the lower gear (12) is connected with the motor (13).

5. An unmanned aerial vehicle with distance measurement according to claim 1, characterized in that, the activity pole (17) outside is provided with guide bar (18), guide bar (18) slide setting is in the recess of inserting connection slot (15) both sides.

6. The unmanned aerial vehicle with distance measurement of claim 1, characterized in that, spacing hole (16) and screw hole (19) correspond in position, run through spiro union has bolt (20) in spacing hole (16) and screw hole (19).

7. Unmanned aerial vehicle with distance measurement according to claim 6, characterized in that, the bolt (20) upper end is equipped with knob (21).