CN213620272U

CN213620272U - Unmanned aerial vehicle shell body aircraft bonnet

Info

Publication number: CN213620272U
Application number: CN202022273016.3U
Authority: CN
Inventors: 王仰龙
Original assignee: Guandian Defense Technology Co ltd
Current assignee: Guandian Defense Technology Co ltd
Priority date: 2020-10-13
Filing date: 2020-10-13
Publication date: 2021-07-06
Anticipated expiration: 2030-10-13

Abstract

The utility model provides an unmanned aerial vehicle shell body aircraft bonnet, including engine body shell, engine body shell's front side is provided with the detection instrument, engine body shell's both ends are provided with the buffer board, be connected through a plurality of buffer spring in the middle of buffer board and the engine body shell, four corners of engine body shell upper end are provided with the fixed axle, the fixed axle upper end is provided with the bracing piece, the terminal top of bracing piece is provided with the connecting axle, the lower pot head of connecting axle has fixed cover, fixed cover is connected with a plurality of connecting rods, the connecting rod is connected on the buffer ring, and the device passes through buffer board and buffer spring's design, and when unmanned aerial vehicle bumps, can effectual protection engine body shell, through the design of buffer ring to can protect every screw, increase unmanned aerial vehicle's life.

Description

Unmanned aerial vehicle shell body aircraft bonnet

Technical Field

The utility model discloses a mainly relate to unmanned air vehicle technical field, specifically be an unmanned aerial vehicle shell body aircraft bonnet.

Background

The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. Ground, on the naval vessel or mother's aircraft remote control station personnel pass through equipment such as radar, trail it, fix a position, the remote control, telemetering measurement and digital transmission, for example, the patent number is CN 201720528826.4's patent number, this patent can be intelligent independently to charge, can also avoid operating personnel plug charging plug to produce the danger of electrocuteeing simultaneously, but in unmanned aerial vehicle's use, often can make unmanned aerial vehicle in transportation or use, collide with each other or fall down with other things, this will make unmanned aerial vehicle take place to damage, and then just reduced unmanned aerial vehicle's life, unmanned aerial vehicle's use value has also been reduced.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an unmanned aerial vehicle shell body aircraft bonnet to solve the problem that proposes in the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme:

the utility model provides an unmanned aerial vehicle shell body aircraft bonnet, includes organic shell, organic shell's front side is provided with the detection instrument, organic shell's both ends are provided with the buffer board, be connected through a plurality of buffer spring in the middle of buffer board and the organic shell, four corners of organic shell upper end are provided with the fixed axle, the fixed axle upper end is provided with the bracing piece, the terminal top of bracing piece is provided with the connecting axle, the lower pot head of connecting axle has fixed cover, fixed cover is connected with a plurality of connecting rods, the connecting rod is connected on the buffer ring.

Further, four corners of the machine body shell are provided with threaded holes, and the fixed shaft is installed on the threaded holes in a threaded mode, so that the fixed shaft can be detached and is convenient to replace and carry.

Furthermore, the upper end of connecting axle is provided with detachable threaded connection's fixation nut to can realize simple convenient the screw installation.

Furthermore, the both sides of connecting axle set up the holding tank, be provided with the block subassembly in the holding tank, the block subassembly is including block piece and block spring, block spring one end is fixed in holding tank bottom, and one end is fixed on block piece to can realize simply convenient fixing the screw on the connecting axle.

Furthermore, the clamping block is of a triangular trapezoidal structure, so that the propeller can be directly inserted from the upper side without manually pressing the clamping block.

Furthermore, the upper end of the clamping block is penetrated by the stabilizing shaft, and the stabilizing shaft is fixed on the inner wall of the accommodating groove, so that the upper end of the clamping block can be fixed, and the installation is convenient.

Furthermore, the outer side of the clamping block is provided with anti-skid stripes, so that the clamping block can be better pressed, and the disassembly is realized.

Further, the upper end of detection instrument is provided with the rotation axis, the rotation axis is connected with transparent safety cover, transparent safety cover covers the detection instrument to can realize the protection of detection instrument.

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

the device passes through buffer board and buffer spring's design, when unmanned aerial vehicle bumps, can effectual protection live engine body shell, through the design of buffering circle to can protect every screw, increase unmanned aerial vehicle's life-span.

Drawings

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

FIG. 2 is an enlarged view of area A of FIG. 1;

FIG. 3 is a sectional view of the engagement assembly area of the present invention;

FIG. 4 is an enlarged view of area B of FIG. 1;

in the figure: 1. a body housing; 2. a buffer plate; 3. a buffer spring; 4. a fixed shaft; 5. a support bar; 6. a buffer ring; 7. a connecting shaft; 8. clamping the assembly; 9. fixing a nut; 10. a detector; 11. a rotating shaft; 12. a transparent protective cover; 13. a threaded hole; 71. accommodating grooves; 72. fixing a sleeve; 73. a connecting rod; 81. a clamping block; 82. a snap spring; 83. and stabilizing the shaft.

Detailed Description

In order to facilitate understanding of the present invention, the present invention will be described more fully with reference to the accompanying drawings, in which several embodiments of the present invention are shown, but the present invention can be implemented in different forms, and is not limited to the embodiments described in the text, but rather, these embodiments are provided to make the disclosure of the present invention more thorough and comprehensive.

It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may be present, and when an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present, as the terms "vertical", "horizontal", "left", "right" and the like are used herein for descriptive purposes only.

Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs, and the use of the term knowledge in the specification of the present invention is for the purpose of describing particular embodiments and is not intended to limit the present invention, and the term "and/or" as used herein includes any and all combinations of one or more of the associated listed items.

Referring to fig. 1-4, the present invention provides a technical solution: an unmanned aerial vehicle outer shell hood comprises an unmanned aerial vehicle outer shell 1, wherein a detector 10 is arranged on the front side of the unmanned aerial vehicle outer shell 1, buffer plates 2 are arranged at two ends of the unmanned aerial vehicle outer shell 1, the buffer plates 2 are connected with the middle of the unmanned aerial vehicle outer shell 1 through a plurality of buffer springs 3, fixed shafts 4 are arranged at four corners of the upper end of the unmanned aerial vehicle outer shell 1, supporting rods 5 are arranged at the upper ends of the fixed shafts 4, a connecting shaft 7 is arranged above the tail ends of the supporting rods 5, a fixed sleeve 72 is sleeved at the lower end of the connecting shaft 7, the fixed sleeve 72 is connected with a plurality of connecting rods 73, the connecting rods 73 are connected onto a buffer ring 6, in the embodiment, the unmanned aerial vehicle outer shell 1 can be effectively protected through the design of the buffer ring 6, and each propeller can be protected, increasing the life of the drone.

Please refer to fig. 1 and fig. 2, the four corners of the housing 1 are provided with screw holes 13, the fixing shaft 4 is mounted on the screw holes 13 in a screw manner, and the upper end of the connecting shaft 7 is provided with a fixing nut 9 in a detachable screw connection manner.

Please refer to fig. 2 and fig. 3, wherein the two sides of the connecting shaft 7 are provided with receiving grooves 71, the receiving grooves 71 are provided with engaging elements 8, the engaging elements 8 include engaging blocks 81 and engaging springs 82, one end of each engaging spring 82 is fixed at the bottom of the receiving groove 71, the other end of each engaging spring 82 is fixed on the engaging block 81, the engaging blocks 81 are in a triangular trapezoid structure, the upper ends of the engaging blocks 81 are penetrated by stabilizing shafts 83, the stabilizing shafts 83 are fixed on the inner walls of the receiving grooves 71, the outer sides of the engaging blocks 81 are provided with anti-slip stripes, in this embodiment, the connecting shaft 7 and the propeller are simply and conveniently installed by the design of the engaging elements 8, the engaging blocks 81 can be directly inserted into the connecting shaft 7 without pressing the engaging blocks 81, the propeller can be fixed by directly inserting the propeller into the connecting shaft 7 without pressing the engaging blocks 81, and the engaging blocks 81, and realizing disassembly.

Referring to fig. 4, the detecting instrument 10 is provided with a rotating shaft 11 at the upper end thereof, the rotating shaft 11 is connected with a transparent protecting cover 12, and the detecting instrument 10 is covered by the transparent protecting cover 12, in this embodiment, the detecting instrument 10 can be effectively protected by the transparent protecting cover 12.

The utility model discloses a concrete operation as follows:

when unmanned aerial vehicle bumps, at first the object contacts buffer board 2 earlier to protect engine body shell 1, and can further reduce the impact through buffer spring 3 between buffer board 2 and the engine body shell 1, when unmanned aerial vehicle collision position was the screw, buffer ring 6 in the screw outside can effectually support and block the striking.

The above description of the present invention is made in conjunction with the accompanying drawings, and it is obvious that the present invention is not limited by the above embodiments, and the method and the technical solution of the present invention are not substantially improved or directly applied to other occasions without improvement, and are all within the protection scope of the present invention.

Claims

1. The utility model provides an unmanned aerial vehicle shell body aircraft bonnet, includes organic shell (1), its characterized in that, the front side of engine body shell (1) is provided with detection instrument (10), the both ends of engine body shell (1) are provided with buffer board (2), be connected through a plurality of buffer spring (3) in the middle of buffer board (2) and engine body shell (1), four corners of engine body shell (1) upper end are provided with fixed axle (4), fixed axle (4) upper end is provided with bracing piece (5), the terminal top of bracing piece (5) is provided with connecting axle (7), the lower pot head of connecting axle (7) has fixed cover (72), fixed cover (72) are connected with a plurality of connecting rods (73), connecting rod (73) are connected on buffering circle (6).

2. The unmanned aerial vehicle outer housing hood according to claim 1, wherein the body housing (1) is provided with threaded holes (13) at four corners, and the fixed shaft (4) is mounted on the threaded holes (13) in a threaded manner.

3. An unmanned aerial vehicle outer housing hood according to claim 1, characterized in that the upper end of the connecting shaft (7) is provided with a detachable screwed fixing nut (9).

4. The unmanned aerial vehicle outer housing hood according to claim 1, wherein accommodating grooves (71) are formed in two sides of the connecting shaft (7), a clamping component (8) is arranged in each accommodating groove (71), each clamping component (8) comprises a clamping block (81) and a clamping spring (82), one end of each clamping spring (82) is fixed to the bottom of each accommodating groove (71), and the other end of each clamping spring is fixed to the corresponding clamping block (81).

5. The unmanned aerial vehicle outer housing hood according to claim 4, wherein the engaging block (81) is of a triangular trapezoid structure.

6. The unmanned aerial vehicle outer housing hood according to claim 4, wherein the upper end of the engaging block (81) is penetrated by a stabilizing shaft (83), and the stabilizing shaft (83) is fixed on the inner wall of the accommodating groove (71).

7. The unmanned aerial vehicle outer housing hood according to claim 4, wherein anti-slip stripes are arranged on the outer sides of the clamping blocks (81).

8. The unmanned aerial vehicle outer housing hood according to claim 1, wherein a rotating shaft (11) is arranged at the upper end of the detecting instrument (10), a transparent protective cover (12) is connected to the rotating shaft (11), and the transparent protective cover (12) covers the detecting instrument (10).