CN217624072U

CN217624072U - Integral type unmanned aerial vehicle frame

Info

Publication number: CN217624072U
Application number: CN202222075006.8U
Authority: CN
Inventors: 张永钢; 郭咏
Original assignee: Jiangsu Icarus Electric Uav General Technology Co ltd
Current assignee: Jiangsu Icarus Intelligent Technology Co ltd
Priority date: 2022-08-09
Filing date: 2022-08-09
Publication date: 2022-10-21
Anticipated expiration: 2032-08-09

Abstract

The utility model provides an integral type unmanned aerial vehicle frame, including the unmanned aerial vehicle frame, the extension rod, collar and second bolt, the angular welding such as unmanned aerial vehicle frame side surface has a plurality of branches, the specification such as extension rod is provided with a plurality ofly, a plurality of extension rods activity respectively are inserted and are established in a plurality of branches, the draw-in groove has all been seted up to the inside left and right-hand member of a plurality of extension rods, the inside relative inboard of a plurality of extension rods all is fixed with spacing spring, a plurality of spacing spring other ends are fixed mutually with a plurality of extension rods respectively, specifications such as second bolt are provided with a plurality ofly, original device connecting rod and installation pole length are fixed have been solved in this design, can not carry out length adjustment's problem according to the unmanned aerial vehicle frame in-service behavior, the utility model discloses rational in infrastructure, the practicality is good for the unmanned aerial vehicle frame is whole can carry out length adjustment according to the in-service behavior.

Description

Integral type unmanned aerial vehicle frame

Technical Field

The utility model relates to an integral type unmanned aerial vehicle frame belongs to unmanned aerial vehicle equipment technical field.

Background

Along with scientific and technological's continuous development and progress, the unmanned aerial vehicle technique is also at quick development and maturity, and most unmanned aerial vehicle's frame forms for distributed equipment at present for can take place the deviation phenomenon when assembling the unmanned aerial vehicle frame, can discount greatly when leading to unmanned aerial vehicle to use.

Chinese patent No.: CN214296419U, an integral type unmanned aerial vehicle frame has been mentioned, the device utilizes the ring flange, peg graft pole and spliced eye, adopt ring flange one and two connecting rod and the installation pole of connecting rod and flange dish, be convenient for to the equipment of connecting rod and installation pole, the peg graft pole is pegged graft in the inside of spliced eye, not only be convenient for to the concatenation between two ring flanges, improve the stability that connecting rod and installation pole are connected simultaneously, but the device connecting rod is fixed with installation pole length, can not carry out length adjustment according to the unmanned aerial vehicle frame in-service use condition, an integral type unmanned aerial vehicle frame is urgently needed now and the problem that the aforesaid appears is solved.

SUMMERY OF THE UTILITY MODEL

Not enough to prior art exists, the utility model aims at providing an integral type unmanned aerial vehicle frame to solve the problem that proposes in the above-mentioned background, the utility model discloses rational in infrastructure, the practicality is good for the unmanned aerial vehicle frame is whole can carry out length adjustment according to the in-service use condition.

In order to achieve the above purpose, the present invention is realized by the following technical solution: the utility model provides an integral type unmanned aerial vehicle frame, includes unmanned aerial vehicle frame, extension rod, collar and second bolt, angular welding such as unmanned aerial vehicle frame side surface has a plurality of branches, the specification such as extension rod is provided with a plurality ofly, and is a plurality of the extension rod activity is respectively inserted and is established in a plurality of branches, and is a plurality of the draw-in groove has all been seted up to the inside left and right ends of extension rod, and is a plurality of the inside relative inboard of extension rod all is fixed with spacing spring, and is a plurality of the spacing spring other end is fixed mutually with a plurality of extension rods respectively, specifications such as second bolt are provided with a plurality ofly, and is a plurality of second bolt head runs through a plurality of extension rods respectively and is located a plurality of draw-in grooves, and is a plurality of all be provided with spacing piece, a plurality of in the draw-in groove the extension rod other end all welds fixed connection piece, the specification such as collar is provided with a plurality ofly.

Further, the bolt heads of the second bolts are respectively fixed with the plurality of limiting sheets.

Furthermore, a plurality of the relative inboard of spacing piece all is provided with anti-skidding line, and the both ends are supported tightly respectively with a plurality of extension rods about the anti-skidding line in many places.

Furthermore, a plurality of arc-shaped grooves are formed in the relative outer sides of the fixed connecting blocks, and a plurality of mounting rings are clamped in the arc-shaped grooves respectively.

Further, the fixed connecting blocks are fixedly connected with the mounting rings through a plurality of first bolts.

The utility model has the advantages that: the utility model discloses an integral type unmanned aerial vehicle frame, because of the utility model discloses added branch, extension rod, collar, fixed connection piece, first bolt, second bolt, spacing piece, anti-skidding line and spacing spring, improved through our design and the in-service use shows, can make the unmanned aerial vehicle frame whole can carry out length adjustment according to the in-service use condition, and adjust comparatively swiftly convenient.

Drawings

Other features, objects and advantages of the invention will become more apparent upon reading of the detailed description of non-limiting embodiments with reference to the following drawings:

fig. 1 is a schematic cross-sectional view of the integral structure of an integrated unmanned aerial vehicle frame according to the present invention;

fig. 2 is a schematic perspective view of a strut of the integrated unmanned aerial vehicle frame of the present invention;

fig. 3 is a schematic perspective view of a limiting plate of the integrated unmanned aerial vehicle frame of the present invention;

in the figure: the unmanned aerial vehicle comprises an unmanned aerial vehicle frame 1, a support rod 2, an extension rod 3, a mounting ring 4, a fixed connecting block 5, a first bolt 6, a second bolt 7, a limiting piece 8, an anti-skid pattern 9, a clamping groove 10 and a limiting spring 11.

Detailed Description

In order to make the utility model realize, the technical means, the creation characteristics, the achievement purpose and the efficacy are easy to understand and understand, the utility model is further explained by combining the specific implementation mode.

Referring to fig. 1-3, the present invention provides a technical solution: the utility model provides an integral type unmanned aerial vehicle frame, including unmanned aerial vehicle frame 1, extension rod 3, collar 4 and second bolt 7, angle welding such as 1 side surface of unmanned aerial vehicle frame has a plurality of branches 2, extension rod 3 isotacticity is provided with a plurality ofly, a plurality of extension rod 3 activity is respectively inserted and is established in a plurality of branches 2, draw-in groove 10 has all been seted up to the inside left and right-hand member of a plurality of extension rod 3, a plurality of extension rod 3 inside relative inboards all are fixed with limiting spring 11, a plurality of limiting spring 11 other ends are fixed mutually with a plurality of extension rods 3 respectively, the isotacticity of second bolt 7 is provided with a plurality ofly, a plurality of second bolt 7 bolt heads run through a plurality of extension rod 3 respectively and are located a plurality of draw-in grooves 10, all be provided with spacing piece 8 in a plurality of draw-in grooves 10, a plurality of extension rod 3 other ends all weld fixed connection piece 5, collar 4 isotacticity is provided with a plurality ofly, original device connecting rod and collar length are fixed according to this design has been solved, can not carry out the problem that length adjustment according to the unmanned aerial vehicle frame in-service behavior.

As a first embodiment of the present invention: the bolt heads of the second bolts 7 are fixed with the limiting pieces 8 respectively, the anti-skid patterns 9 are arranged on the inner sides of the limiting pieces 8, the anti-skid patterns 9 are tightly abutted to the left end and the right end of the extension rods 3 respectively, and the plurality of limiting pieces 8 are enabled to be more stable to abut against the extension rods 3 through the added anti-skid patterns 9.

The arc wall has all been seted up in the relative outside of a plurality of fixed connection blocks 5, a plurality of collars 4 block respectively and establish in a plurality of arc walls, through the arc wall of seting up, make a plurality of fixed connection blocks 5 and a plurality of collars 4 laminating department area bigger, through 6 fixed connection of a plurality of first bolts between a plurality of fixed connection blocks 5 and a plurality of collars 4, through a plurality of first bolts 6 that add, the installation between a plurality of fixed connection blocks 5 and a plurality of collars 4 of being convenient for is fixed.

As a second embodiment of the present invention: when needs adjust 1 whole length of unmanned aerial vehicle frame, only need unscrew a plurality of second bolts 7, make a plurality of spacing pieces 8 and then remove toward opposite direction in a plurality of draw-in grooves 10, and then make a plurality of spacing pieces 8 not contact with a plurality of extension rods 3, then can a plurality of extension rods 3 of manual push-and-pull, a plurality of extension rods 3 will remove in a plurality of branch 2 (when a plurality of extension rods 3 are at the interior tensile removal of a plurality of branch 2, a plurality of spacing springs 11 are with being stretched, when a plurality of extension rods 3 are at the interior relative movement of a plurality of branch 2, a plurality of spacing springs 11 will be extruded and compressed, and is swift convenient, adjust the completion back, screw up a plurality of second bolts 7, make a plurality of spacing pieces 8 and then relative movement in a plurality of draw-in grooves 10, support both ends to tightly and can accomplish the regulation of extension rods 3 about it with a plurality of extension rods 3, antiskid line 9 through the interpolation, make a plurality of spacing pieces 8 withstand a plurality of extension rods 3 more firm.

The basic principles and the main features of the invention and the advantages of the invention have been shown and described above, it will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, but that the invention may be embodied in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.

Claims

1. The utility model provides an integral type unmanned aerial vehicle frame, includes unmanned aerial vehicle frame (1), extension rod (3), collar (4) and second bolt (7), its characterized in that: the side surface of the unmanned aerial vehicle frame (1) is welded with a plurality of supporting rods (2) at equal angles, a plurality of extension rods (3) are arranged in an equal-specification mode, the extension rods (3) are movably inserted into the supporting rods (2) respectively, clamping grooves (10) are formed in the left end and the right end of the inner part of each extension rod (3), limiting springs (11) are fixed on the inner opposite inner sides of the inner parts of the extension rods (3), and the other ends of the limiting springs (11) are fixed with the extension rods (3) respectively;

specification such as second bolt (7) is provided with a plurality ofly, and is a plurality of second bolt (7) bolt head runs through a plurality of extension rod (3) respectively and is located a plurality of draw-in grooves (10), and is a plurality of all be provided with spacing piece (8) in draw-in groove (10), it is a plurality of extension rod (3) other end all welds fixed connection piece (5), specification such as collar (4) is provided with a plurality ofly.

2. The integrated drone rack of claim 1, wherein: the bolt heads of the second bolts (7) are respectively fixed with the limiting pieces (8).

3. The integrated drone rack of claim 2, wherein: a plurality of the limiting pieces (8) are provided with anti-skid lines (9) on the inner sides relative to each other, and the anti-skid lines (9) at a plurality of positions are respectively abutted against the left end and the right end of the extension rods (3).

4. The integrated drone rack of claim 1, wherein: a plurality of arc-shaped grooves are formed in the relative outer sides of the fixed connecting blocks (5), and the mounting rings (4) are clamped in the arc-shaped grooves respectively.

5. The integrated drone rack of claim 1, wherein: the fixed connecting blocks (5) are fixedly connected with the mounting rings (4) through a plurality of first bolts (6).