CN216035165U

CN216035165U - Measurement high-altitude aircraft for territorial space planning

Info

Publication number: CN216035165U
Application number: CN202121929447.9U
Authority: CN
Inventors: 王启鹏
Original assignee: Shenzhen Zhongming Hi Tech Information Industry Co ltd
Current assignee: Shenzhen Zhongming Hi Tech Information Industry Co ltd
Priority date: 2021-08-17
Filing date: 2021-08-17
Publication date: 2022-03-15
Anticipated expiration: 2031-08-17

Abstract

The utility model discloses a measuring high-altitude aircraft for territorial space planning, and particularly relates to the technical field of measuring equipment. According to the panoramic measuring instrument, the mounting mechanism is arranged, the second concave sliding frame is pulled downwards to drive the adjusting sliding plate to slide downwards in the first concave sliding frame, the fixing operation is performed after the adjusting sliding plate is adjusted to a specified length, the mounting screw rod drives the first spiral ring block and the second spiral ring block to be close to each other, the two first concave sliding frames rapidly clamp and fix the two sides of the panoramic measuring instrument, the panoramic measuring instrument can be suitable for rapid mounting operation of measuring equipment of different models, the mounting efficiency is higher, the measuring efficiency is effectively improved, and the left and right and up and down limiting effects after mounting ensure the stability after mounting.

Description

Measurement high-altitude aircraft for territorial space planning

Technical Field

The utility model relates to the technical field of measuring equipment, in particular to a measuring high-altitude aircraft for territorial space planning.

Background

The aircraft is an unmanned cockpit on an unmanned aircraft operated by radio remote control equipment and a self-contained program control device, and personnel at a remote control station can track, position, remotely control, telemeter and digitally transmit the unmanned cockpit through equipment such as a radar.

Among the prior art, need high altitude vehicle to carry measuring equipment to rise to appointed height and carry out ground measurement operation, because measuring equipment model width is inconsistent, comparatively troublesome in the installation, be unfavorable for installing the operation to the measuring device of different models fast, waste time and energy more, influence measurement of efficiency.

SUMMERY OF THE UTILITY MODEL

In order to overcome the defects in the prior art, the embodiment of the utility model provides the measuring high-altitude aircraft for the territorial space planning, and the measuring high-altitude aircraft can be suitable for quick installation operation of measuring equipment of different models through the installation mechanism, has higher installation efficiency, effectively improves the measuring efficiency, and has better practicability so as to solve the problems in the background art.

In order to achieve the purpose, the utility model provides the following technical scheme: a measuring high-altitude aircraft for national soil space planning comprises an unmanned aerial vehicle body, wherein an installation support plate is arranged below the unmanned aerial vehicle body, an installation groove is formed in the bottom end of the installation support plate, and an installation mechanism is arranged inside the installation groove;

installation mechanism is including setting up the inside installation lead screw of mounting groove, micro motor is installed to installation lead screw one end, the outside cover of installation lead screw is equipped with first spiral ring piece, first spiral ring piece one side is provided with second spiral ring piece, first spiral ring piece and second spiral ring piece bottom all are connected with the smooth frame of first spill, the inside regulation slide that is provided with of the smooth frame of first spill, it is provided with the smooth frame of second spill to adjust slide bottom outside, the smooth frame of first spill and the smooth frame one side embedding of second spill are provided with fastening screw, the smooth frame opposite side of second spill is provided with the support arc board.

In a preferred embodiment, the mounting screw rod is fixedly connected with the output end of the micro motor in a welding manner, and the outer part of the mounting screw rod is connected with the inner wall of the first spiral ring block through threads.

In a preferred embodiment, a panoramic measuring instrument is arranged between the two first concave sliding frames, and two limiting frames are arranged below the first concave sliding frames.

In a preferred embodiment, the outer portions of the two ends of the adjusting sliding plate are movably connected with the first concave sliding frame and the second concave sliding frame in pairs, and the inner wall threads of the first spiral ring block are opposite to the inner wall threads of the second spiral ring block.

In a preferred embodiment, a connecting bracket is arranged on one side of the micro motor, the connecting bracket and the micro motor are fixed by welding, and the cross section of the connecting bracket is in an L shape.

In a preferred embodiment, the unmanned aerial vehicle organism both sides all are provided with two sets of book shape supports, it is provided with flight blade to roll over the embedding of shape support top, it is provided with the buffer block to roll over shape support below, the buffer block bottom is provided with a plurality of buffering shell fragments, be provided with the buffering chassis below the buffering shell fragment.

In a preferred embodiment, the upper end and the lower end of the buffering elastic sheet are respectively and fixedly connected with the buffering block and the buffering chassis in pairs, and the buffering elastic sheets are arranged in a circumferential array.

The utility model has the technical effects and advantages that:

1. by arranging the mounting mechanism, the second concave sliding frame is pulled downwards to drive the adjusting sliding plate to slide downwards in the first concave sliding frame, fixing operation is carried out after the adjusting to the specified length, the mounting screw rod drives the first spiral ring block and the second spiral ring block to be close to each other, the two first concave sliding frames rapidly clamp and fix the two sides of the panoramic measuring instrument, and the two supporting arc plates carry out limiting support on the bottom of the panoramic measuring instrument, so that the mounting mechanism can be suitable for measuring equipment of different models to carry out rapid mounting operation, the mounting efficiency is higher, the measuring efficiency is effectively improved, the mounting mechanism plays a limiting role in left and right as well as up and down after mounting, the mounting stability is ensured, and the practicability is better;

2. after the unmanned aerial vehicle organism descends to ground, the buffering chassis drives a plurality of buffering shell fragments and compresses under the effect of pressure and plays the effect of buffering, can make the buffer block play the effect of buffering like this, effectively avoids causing the damage after the unmanned aerial vehicle organism descends, plays the multi-angle cushioning effect, and a plurality of buffering shell fragments are circumference array buffering, and the buffering is more even, and the buffering effect is better.

Drawings

Fig. 1 is a schematic view of the overall structure of the present invention.

FIG. 2 is a bottom view of a portion of the bottom of the mounting plate of the present invention.

FIG. 3 is a schematic view of a partial cross-sectional structure of a second spiral block according to the present invention.

Fig. 4 is a schematic perspective view of a connection portion between the buffer block and the buffer spring plate according to the present invention.

The reference signs are: 1. an unmanned aerial vehicle body; 2. mounting a support plate; 3. installing a screw rod; 4. a micro motor; 5. a first screw ring block; 6. a second screw ring block; 7. a first concave slide frame; 8. adjusting the sliding plate; 9. a second concave sliding frame; 10. fastening a screw rod; 11. supporting the arc plate; 12. a panoramic measuring instrument; 13. a limiting frame; 14. connecting a bracket; 15. a fold-shaped bracket; 16. a flight blade; 17. a buffer block; 18. a buffering elastic sheet; 19. the chassis is cushioned.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

The measurement high-altitude aircraft for the national soil space planning comprises an unmanned aerial vehicle body 1, wherein an installation support plate 2 is arranged below the unmanned aerial vehicle body 1, the bottom end of the installation support plate 2 is provided with an installation groove, and an installation mechanism is arranged in the installation groove;

installation mechanism is including setting up at the inside installation lead screw 3 of mounting groove, micro motor 4 is installed to 3 one ends of installation lead screw, the outside cover of installation lead screw 3 is equipped with first helicoid ring piece 5, first helicoid ring piece 5 one side is provided with second helicoid ring piece 6, first

helicoid ring piece

5 and 6 bottoms of second helicoid ring piece all are connected with the smooth frame 7 of first spill, the inside regulation slide 8 that is provided with of the smooth frame 7 of first spill, the outside second spill that is provided with in the smooth frame 9 of regulation slide 8 bottom, the smooth frame 9 one side embedding of the smooth frame 7 of first spill and second spill is provided with fastening screw 10, the smooth frame 9 opposite side of second spill is provided with support arc board 11.

As shown in fig. 2 and fig. 3, the output end of the mounting screw rod 3 is fixedly connected with the output end of the micro motor 4 in a welding manner, the outer portion of the mounting screw rod 3 is connected with the inner wall of the first screw ring block 5 through threads, so that the micro motor 4 is started to drive the mounting screw rod 3 to rotate, the mounting screw rod 3 drives the first screw ring block 5 to rotate under the action of the threads, and thus the first screw ring block 5 can be moved and clamped.

As shown in fig. 2, a panoramic measuring instrument 12 is arranged between the two first concave sliding frames 7, two limiting frames 13 are arranged below the first concave sliding frames 7, so that panoramic measuring operation can be performed through the panoramic measuring instrument 12, and the limiting frames 13 can enable the adjusting sliding plate 8 to move downwards to a specified position to play a limiting role, so that damage caused by overlimit use of the adjusting sliding plate 8 is prevented.

As shown in fig. 2, the outer portions of the two ends of the adjusting sliding plate 8 are movably connected with the first concave sliding frame 7 and the second concave sliding frame 9, and the inner wall threads of the first screw ring block 5 and the inner wall threads of the second screw ring block 6 are arranged oppositely, so that the adjusting sliding plate 8 can slide on the first concave sliding frame 7 and the second concave sliding frame 9, the width can be adjusted, and the measuring devices of different models can be conveniently installed and operated.

As shown in fig. 2, a connecting bracket 14 is arranged on one side of the micro motor 4, the connecting bracket 14 is fixed with the micro motor 4 by welding, and the cross section of the connecting bracket 14 is L-shaped, so that when the micro motor 4 is in use, the connecting bracket 14 can support and stabilize the micro motor 4, thus the micro motor 4 can be kept to operate stably.

As shown in fig. 1 and fig. 4, 1 both sides of unmanned aerial vehicle organism all are provided with two sets of book shape support 15, book shape support 15 top embedding is provided with flight blade 16, book shape support 15 below is provided with buffer block 17, buffer block 17 bottom is provided with a plurality of buffering shell fragments 18, buffering shell fragment 18 below is provided with buffering chassis 19, so that alright with opening two sets of book shape support 15, start flight blade 16 simultaneously and fly the operation, after unmanned aerial vehicle organism 1 descends to ground, buffering chassis 19 begins to contact ground, buffering chassis 19 drives a plurality of buffering shell fragments 18 and extrudes under the effect of pressure, a plurality of buffering shell fragments 18 atress compression play the effect of buffering, can make buffer block 17 play the effect of buffering like this, effectively avoid causing the damage after unmanned aerial vehicle organism 1 descends.

As shown in fig. 4, the upper and lower ends of the buffering elastic sheet 18 are respectively fixedly connected with the buffering block 17 and the buffering base plate 19, and the buffering elastic sheets 18 are arranged in a circumferential array manner, so that the buffering elastic sheet 18 is compressed under the action of pressure, and pressure is converted into elastic potential energy to be slowly released, thereby playing a role in buffering and being buffered in the circumferential array manner.

The working principle of the utility model is as follows: when the panoramic measuring instrument is used, the panoramic measuring instrument 12 can be placed between two first concave sliding frames 7, then the second concave sliding frame 9 can be pulled downwards to move downwards, the second concave sliding frame 9 drives the adjusting sliding plate 8 to slide downwards in the first concave sliding frame 7, then two fastening screws 10 are rotated to respectively fix the first concave sliding frame 7 and the second concave sliding frame 9 under the action of threads, so that the length of the supporting arc plate 11 can be adjusted, the micro motor 4 is started to drive the mounting screw rod 3 to rotate, the mounting screw rod 3 drives the first screw ring block 5 to move rightwards, the second screw ring block 6 moves leftwards under the action of the threads, thus the first screw ring block 5 and the second screw ring block 6 are close to each other, the first screw ring block 5 drives the first concave sliding frame 7, the first concave sliding frame 7 drives the adjusting sliding plate 8 to move rightwards, the adjusting sliding plate 8 drives the second concave sliding frame 9 to move rightwards, the smooth frame 9 of second spill drives and supports arc board 11 and remove right, and two smooth frames 7 of first spill carry out the clamping to 12 both sides of panorama measuring apparatu, and two support arc boards 11 play spacing effect to 12 bottoms of panorama measuring apparatu, can drive panorama measuring apparatu 12 by unmanned aerial vehicle organism 1 like this and rise to and carry out measurement operation after the appointed height.

The points to be finally explained are: first, in the description of the present application, it should be noted that, unless otherwise specified and limited, the terms "mounted," "connected," and "connected" should be understood broadly, and may be a mechanical connection or an electrical connection, or a communication between two elements, and may be a direct connection, and "upper," "lower," "left," and "right" are only used to indicate a relative positional relationship, and when the absolute position of the object to be described is changed, the relative positional relationship may be changed;

secondly, the method comprises the following steps: in the drawings of the disclosed embodiments of the utility model, only the structures related to the disclosed embodiments are referred to, other structures can refer to common designs, and the same embodiment and different embodiments of the utility model can be combined with each other without conflict;

and finally: the above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the utility model, and any modifications, equivalents, improvements and the like that are within the spirit and principle of the present invention are intended to be included in the scope of the present invention.

Claims

1. The utility model provides a homeland space planning is with measuring high altitude aircraft, includes unmanned aerial vehicle organism (1), its characterized in that: an installation support plate (2) is arranged below the unmanned aerial vehicle body (1), an installation groove is formed in the bottom end of the installation support plate (2), and an installation mechanism is arranged in the installation groove;

installation mechanism is including setting up inside installation lead screw (3) of mounting groove, micro motor (4) are installed to installation lead screw (3) one end, installation lead screw (3) outside cover is equipped with first screw ring piece (5), first screw ring piece (5) one side is provided with second screw ring piece (6), first screw ring piece (5) and second screw ring piece (6) bottom all are connected with first spill sliding frame (7), first spill sliding frame (7) inside is provided with adjusts slide (8), it is provided with the smooth frame of second spill (9) to adjust slide (8) bottom outside, the smooth frame of first spill (7) and the smooth frame of second spill (9) one side embedding is provided with fastening screw (10), the smooth frame of second spill (9) opposite side is provided with support arc board (11).

2. The survey high altitude aircraft for territorial space planning of claim 1, wherein: the mounting screw rod (3) is fixedly connected with the output end of the micro motor (4) in a welding mode, and the outside of the mounting screw rod (3) is connected with the inner wall of the first screw ring block (5) through threads.

3. The survey high altitude aircraft for territorial space planning of claim 1, wherein: a panoramic measuring instrument (12) is arranged between the two first concave sliding frames (7), and two limiting frames (13) are arranged below the first concave sliding frames (7).

4. The survey high altitude aircraft for territorial space planning of claim 1, wherein: the outer parts of two ends of the adjusting sliding plate (8) are respectively movably connected with the first concave sliding frame (7) and the second concave sliding frame (9) in pairs, and the threads of the inner wall of the first screw ring block (5) are opposite to the threads of the inner wall of the second screw ring block (6).

5. The survey high altitude aircraft for territorial space planning of claim 1, wherein: a connecting support (14) is arranged on one side of the micro motor (4), the connecting support (14) is fixed with the micro motor (4) in a welding mode, and the cross section of the connecting support (14) is L-shaped.

6. The survey high altitude aircraft for territorial space planning of claim 1, wherein: unmanned aerial vehicle organism (1) both sides all are provided with two sets of book shape support (15), it is provided with flight blade (16) to roll over the embedding of shape support (15) top, it is provided with buffer block (17) to roll over shape support (15) below, buffer block (17) bottom is provided with a plurality of buffering shell fragments (18), buffering shell fragment (18) below is provided with buffering chassis (19).

7. The survey high altitude aircraft for territorial space planning of claim 6, wherein: the upper end and the lower end of the buffering elastic sheet (18) are respectively and fixedly connected with the buffering block (17) and the buffering chassis (19) in pairs, and the buffering elastic sheets (18) are arranged in a circumferential array.