CN210852956U

CN210852956U - Unmanned aerial vehicle nacelle structure convenient to installation and firm

Info

Publication number: CN210852956U
Application number: CN201921612477.XU
Authority: CN
Inventors: 田志; 田凯; 王翊赫
Original assignee: Tianjin Hanyu Haode Technology Development Co ltd
Current assignee: Tianjin Hanyu Haode Technology Development Co ltd
Priority date: 2019-09-26
Filing date: 2019-09-26
Publication date: 2020-06-26
Anticipated expiration: 2029-09-26

Abstract

The utility model discloses an unmanned aerial vehicle nacelle structure convenient to installation and firm, including the connecting block, connecting block upper end fixed mounting has the connection piece, connecting block lower extreme fixed mounting has the inserted block, connection piece and inserted block and connecting block structure as an organic whole, connecting block lower extreme fixed mounting has the base, the fixed slot that is provided with in base upper end, slot and inserted block looks adaptation, the base upper end is located the fixed orifices that is provided with in slot one side, base lower extreme fixed mounting has the revolving stage, revolving stage lower extreme fixedly connected with cabin top. This unmanned aerial vehicle nacelle structure convenient to installation and firm adopts connecting block, connection piece and inserted block integral structure, makes overall structure more firm, and be provided with on the base with the slot of inserted block looks adaptation, connect the back connecting block and closely laminate with the base, will improve the steadiness of this nacelle greatly, overall structure is simple simultaneously, is convenient for realize, and low in cost is convenient for save the cost.

Description

Unmanned aerial vehicle nacelle structure convenient to installation and firm

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle nacelle structure convenient to installation and firm.

Background

The unmanned aerial vehicle is an unmanned aerial vehicle controlled by a radio remote control device or an onboard computer program control system, has a simple structure and low use cost, can complete the task executed by a piloted plane, is more suitable for the task which is not suitable to be executed by the piloted plane, and has great effects on emergency and early warning in emergencies.

Along with the continuous development of scientific and technological and unmanned aerial vehicle technique, people can utilize unmanned aerial vehicle to carry out the work that is difficult to accomplish before a lot, unmanned aerial vehicle simple structure, use cost are low, not only can accomplish the task of someone's pilot plane execution, be more applicable to the task that someone's aircraft should not execute, it is emergent in emergency, the early warning has very big effect, the nacelle is the important part of unmanned aerial vehicle work, but current unmanned aerial vehicle nacelle installation difficulty, it is unstable after the installation simultaneously, easily cause article to drop and cause the loss.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an unmanned aerial vehicle nacelle structure convenient to installation and firm to propose the installation difficulty in solving above-mentioned background art, unstable after the installation simultaneously, easily cause article to drop and cause the problem of loss.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle nacelle structure convenient to installation and firm, includes the connecting block, connecting block upper end fixed mounting has the connection piece, connecting block lower extreme fixed mounting has the inserted block, connection piece and inserted block and connecting block integrated structure as an organic whole, connecting block lower extreme fixed mounting has the base, the fixed slot that is provided with in base upper end, slot and inserted block looks adaptation, the base upper end is located the fixed orifices that is provided with in slot one side, base lower extreme fixed mounting has the revolving stage, revolving stage lower extreme fixedly connected with cabin top, both ends fixed mounting has the bulkhead about the cabin top, the fixed stopper that is provided with of bulkhead inner wall, the activity of bulkhead left end is provided with set screw, set screw passes the bulkhead and extends to the stopper right-hand.

Preferably, the lower end of the connecting block is movably provided with a fixed vertical rod, the fixed vertical rod penetrates through the connecting block and extends to the lower part of the connecting block, the upper end and the lower end of the fixed vertical rod are fixedly provided with limiting rings, and the upper end of the base is fixedly provided with a fixing hole.

Preferably, the diameter of the fixing hole is larger than that of the limiting ring, an elastic sheet is movably mounted inside the fixing hole, a spring is fixedly connected to the lower end of the elastic sheet, and the lower end of the spring is fixedly connected to the bottom of the fixing hole.

Preferably, the inside spring one side movable mounting that is located of fixed orifices has the latch, the lower extreme fixedly connected with ejector pin of latch left end, ejector pin left end fixedly connected with button, the button passes the base and extends to the base side.

Preferably, the upper end of the elastic sheet is flush with the upper end face of the base.

Preferably, the lower end of the cabin roof is fixedly provided with a cabin body, the side surface of the cabin body is fixedly provided with a limiting groove, and the limiting groove is matched with the limiting block

Preferably, the upper end opening of the limiting groove is larger than the lower end opening.

Compared with the prior art, the beneficial effects of the utility model are that: the unmanned aerial vehicle pod structure convenient to mount and stable adopts an integrated structure of the connecting block, the connecting sheet and the inserting block, so that the overall structure is more stable, the upper end of the base is provided with the inserting groove matched with the inserting block, and the connecting block is tightly attached to the base after connection, so that the stability of the pod is greatly improved;

according to the unmanned aerial vehicle pod structure convenient to mount and stable, during mounting, the mounting can be completed only by inserting the inserting block into the inserting groove matched with the inserting block and reinforcing the fixing vertical rod to be refined, the mounting speed is greatly improved, the mounting is convenient, the bulkhead and the pod body are of detachable structures, multiple purposes are facilitated, and meanwhile, the bulkhead and the pod body are provided with the limiting blocks and the limiting grooves matched with each other, so that the mounting time is greatly shortened while the stability is improved, and the mounting is convenient;

this unmanned aerial vehicle nacelle structure convenient to installation and firm, overall structure is simple, is convenient for realize, and low in cost is convenient for save the cost.

Drawings

FIG. 1 is a schematic view of the split structure of the present invention;

fig. 2 is a schematic view of the structure of the belt cabin of the present invention;

FIG. 3 is a schematic view of a structure of a cargo hold of the present invention;

fig. 4 is a schematic view of the structure of the elastic sheet of the present invention.

In the figure: 1. connecting blocks; 2. connecting sheets; 3. fixing the vertical rod; 4. a limiting ring; 5. inserting a block; 6. a base; 7. a slot; 8. a fixing hole; 9. a button; 10. a rotating table; 11. a cabin roof; 12. a bulkhead; 13. a limiting block; 14. a set screw; 15. a cabin body; 16. a limiting groove; 17. a spring plate; 18. a spring; 19. clamping teeth; 20. and a push rod.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-4, the present invention provides a technical solution: the utility model provides an unmanned aerial vehicle nacelle structure convenient to installation and firm, including connecting

block

1, 1 upper end fixed mounting of connecting block has

connection piece

2, 1 lower extreme fixed mounting of connecting block has inserted block 5, connection piece 2 and inserted block 5 and connecting block 1 structure as an organic whole, 1 lower extreme fixed mounting of connecting block has

base

6, 6 upper ends of base are fixed and are provided with slot 7,

slot

7 and 5 looks adaptations of inserted block, 6 upper ends of base are located slot 7 one side and fix and are provided with

fixed orifices

8, 6 lower extreme fixed mounting of base has revolving

stage

10, 10 lower extreme fixedly connected with cabin roof 11 of revolving stage, both ends fixed mounting has bulkhead 12 about cabin roof 11, the fixed stopper 13 that is provided with of bulkhead 12 inner wall, the activity of bulkhead 12 left end is provided with set screw 14, set screw 14 passes bulkhead 12 and extends to 13 right.

Further, 1 lower extreme movable mounting of connecting block has fixed montant 3, and fixed montant 3 runs through connecting block 1 and extends to connecting block 1 below, and fixed spacing ring 4 that is provided with in both ends about fixed montant 3, and fixed orifices 8 have been seted up to 6 upper ends of base, sets up spacing ring 4 and can fix fixed montant 3 on connecting block 1, avoids fixed montant 3 to drop the loss, simultaneously easy to assemble.

Further, the diameter of the fixing hole 8 is larger than that of the limiting ring 4, the elastic sheet 17 is movably mounted inside the fixing hole 8, the lower end of the elastic sheet 17 is fixedly connected with a spring 18, the lower end of the spring 18 is fixedly connected to the bottom of the fixing hole 8, and the elastic sheet 17 and the spring 18 are mounted and dismounted conveniently.

Further, the inside spring 18 one side movable mounting that is located of fixed orifices 8 has latch 19, the lower extreme fixedly connected with ejector pin 20 of the 19 left ends of latch, 20 left end fixedly connected with buttons 9 of ejector pin, and buttons 9 pass base 6 and extend to the 6 sides of base, and latch 19 can be fixed montant 3 inside base 6, has improved the steadiness of installation greatly.

Furthermore, the upper end of the elastic sheet 17 is flush with the upper end face of the base 6, and the elastic sheet 17 can completely eject the fixing vertical rod 3 during disassembly, so that the disassembly is convenient.

Further, a cabin body 15 is fixedly arranged at the lower end of the cabin roof 11, a limiting groove 16 is fixedly arranged on the side face of the cabin body 15, the limiting groove 16 is matched with the limiting block 13, and the installation stability of the cabin body 15 is greatly improved when the cabin body 15 is conveniently installed by installing the limiting groove 16 and the limiting block 13.

Furthermore, the opening at the upper end of the limiting groove 16 is larger than the opening at the lower end, so that the installation of the cabin body 15 is facilitated.

The working principle is as follows: firstly, fix connecting block 1 in the bottom of the unmanned aerial vehicle through connection piece 2, then align the slot 7 of base 6 upper end with inserted block 5 and rotate to inserted block 5 and insert inside slot 7 completely, fixed montant 3 is to it with fixed orifices 8 this moment, then press fixed montant 3, fixed montant 3 can take shell fragment 17 block at latch 19 lower extreme, press button 9 during the dismantlement and can trigger spring 18 and pop out fixed montant 3, then reverse rotation base 6 accomplishes the dismantlement, installation cabin 15 is at first unloaded set screw 14, then insert the spacing groove 16 of cabin 15 along stopper 13, then installation set screw 14 accomplishes the installation of cabin 15.

It should be finally noted that the above only serves to illustrate the technical solution of the present invention, and not to limit the scope of the present invention, and that simple modifications or equivalent replacements performed by those skilled in the art to the technical solution of the present invention do not depart from the spirit and scope of the technical solution of the present invention.

Claims

1. The utility model provides an unmanned aerial vehicle nacelle structure convenient to installation and firm, includes the connecting block, its characterized in that: connecting block upper end fixed mounting has the connection piece, connecting block lower extreme fixed mounting has the inserted block, connection piece and inserted block and connecting block integrated configuration, connecting block lower extreme fixed mounting has the base, the fixed slot that is provided with in base upper end, slot and inserted block looks adaptation, the base upper end is located the fixed orifices that is provided with in slot one side, base lower extreme fixed mounting has the revolving stage, revolving stage lower extreme fixedly connected with cabin top, both ends fixed mounting has the bulkhead about the cabin top, the fixed stopper that is provided with of bulkhead inner wall, the activity of bulkhead left end is provided with set screw, set screw passes the bulkhead and extends to the stopper right-hand member.

2. An easily installable and stable pod structure for unmanned aerial vehicles according to claim 1, wherein: the connecting block lower extreme movable mounting has fixed montant, fixed montant through connection piece extends to the connecting block below, the fixed spacing ring that is provided with in both ends about the fixed montant, the fixed orifices of having seted up in base upper end.

3. An easily installable and stable pod structure for unmanned aerial vehicles according to claim 2, wherein: the diameter of the fixing hole is larger than that of the limiting ring, an elastic sheet is movably mounted inside the fixing hole, a spring is fixedly connected to the lower end of the elastic sheet, and the lower end of the spring is fixedly connected to the bottom of the fixing hole.

4. An easily installable and stable pod structure for unmanned aerial vehicles according to claim 3, wherein: the spring is arranged in the fixed hole, the spring is movably arranged on one side of the fixed hole, the lower end of the left end of the clamp is fixedly connected with a push rod, the left end of the push rod is fixedly connected with a button, and the button penetrates through the base and extends to the side face of the base.

5. An easily installable and stable pod structure for unmanned aerial vehicles according to claim 3, wherein: the upper end of the elastic sheet is flush with the upper end face of the base.

6. An easily installable and stable pod structure for unmanned aerial vehicles according to claim 1, wherein: the cabin top lower extreme is fixed and is provided with the cabin body, cabin body side is fixed and is provided with the spacing groove, the spacing groove and stopper looks adaptation.

7. An easily installable and stable pod structure for unmanned aerial vehicles according to claim 6, wherein: the upper end opening of the limiting groove is larger than the lower end opening.