CN212074396U

CN212074396U - Connect formula unmanned aerial vehicle wing truck soon

Info

Publication number: CN212074396U
Application number: CN202020113102.5U
Authority: CN
Inventors: 丁武轩
Original assignee: Individual
Current assignee: Dongguan Lianhao Machinery Equipment Co ltd
Priority date: 2020-01-17
Filing date: 2020-01-17
Publication date: 2020-12-04
Anticipated expiration: 2030-01-17

Abstract

The utility model discloses a connect formula unmanned aerial vehicle wing truck soon, including the connecting rod, settle a section of thick bamboo, wing mechanism, knob, pivot, second gear, slider, third gear and wing main part. The utility model has the advantages that: when unmanned aerial vehicle need fly under the environment of difference or need carry out different tasks, the user can manually rotate the knob, the knob rotates and drives third gear revolve, third gear revolve drives second gear revolve, second gear revolve rotates and drives the pivot and produces the pivoted trend, but because the pivot is spacing by two sliders, then the pivot can only be in settling a section of thick bamboo inside continuous reciprocating, when the pivot reciprocates, can drive the wing main part and reciprocate simultaneously, when the wing main part reaches suitable position, the user stall knob, thereby be convenient for freely adjust from top to bottom to unmanned aerial vehicle wing truck when using, and then be convenient for freely adjust the wing main part, make unmanned aerial vehicle's application scope can enlarge.

Description

Connect formula unmanned aerial vehicle wing truck soon

Technical Field

The utility model relates to an unmanned aerial vehicle wing equipment specifically is a connect formula unmanned aerial vehicle wing truck soon belongs to unmanned air vehicle technical field.

Background

An unmanned aircraft, referred to as "drone" for short, is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, and the application of the unmanned aerial vehicle is greatly expanded.

However, in the actual use process of the conventional unmanned aerial vehicle, because the unmanned aerial vehicle needs to perform tasks of various different types during flying, and simultaneously, the unmanned aerial vehicle may also need to fly in different environments, so that wings of the unmanned aerial vehicle generally need different flying angles, and the wing trunk of the conventional unmanned aerial vehicle is not convenient to adjust, which causes a certain degree of limitation on the application range of the unmanned aerial vehicle.

SUMMERY OF THE UTILITY MODEL

The utility model aims at providing a connect formula unmanned aerial vehicle wing truck soon in order to solve above-mentioned problem, the flexible operation is convenient for adjust unmanned aerial vehicle wing truck when using in order to be convenient for adjust the unmanned aerial vehicle wing, make unmanned aerial vehicle's application scope can enlarge.

The utility model achieves the above purpose through the following technical proposal, a rotary joint type unmanned aerial vehicle wing trunk comprises a connecting rod, a mounting cylinder is fixed on one side of the connecting rod, a wing mechanism is arranged in the connecting rod and the mounting cylinder, the wing mechanism comprises a knob, a rotating shaft, a second gear, a sliding block and a third gear, the knob is arranged in the middle of one side of the connecting rod, which is close to the mounting barrel, the bottom of the knob extends to the inside of the connecting rod, the bottom end of the knob is connected with the third gear, the rotating shaft is arranged in the mounting cylinder, the two opposite sides of the side wall of the top of the rotating shaft are respectively connected with one sliding block which is clamped on the inner wall of the mounting cylinder, and the side wall of the bottom of the rotating shaft is in threaded connection with the second gear, and the side wall of the top end of the rotating shaft is provided with a wing main body.

Preferably, in order to facilitate the installation of the whole device in use, a mounting seat is fixed to one end of the connecting rod, which is away from the mounting cylinder, and the mounting seat is in a disc shape as a whole.

Preferably, in order to conveniently adjust the connecting rod when using, the inside adjustment mechanism that is equipped with of mount pad, adjustment mechanism includes branch and spring, the inside of mount pad is equipped with branch, just it has to twine on the lateral wall of branch the spring, the bottom of spring connect in the bottom of mount pad inner chamber.

Preferably, further convenience is right when using the connecting rod is adjusted, the adjusting mechanism further comprises a first gear and a tooth groove, the top of the spring is connected with the first gear, the first gear is fixed on the side wall of the supporting rod, the top of the inner cavity of the mounting seat is provided with the tooth groove, and the first gear is clamped in the tooth groove.

Preferably, in order to facilitate the user to manually operate the knob during use, the wing mechanism further includes a sheath, the knob is in a disc shape as a whole, and the sheath is sleeved on a side wall of the knob.

Preferably, in order to facilitate the sliding blocks to be clamped with the installation cylinder in use, the wing mechanism further comprises sliding grooves, two opposite sides of the top of the inner cavity of the installation cylinder are respectively provided with one sliding groove, and the two sliding blocks are respectively clamped with the two sliding grooves.

Compared with the prior art, the beneficial effects of the utility model are that: when unmanned aerial vehicle need fly under the environment of difference or need carry out different tasks, the user can manually rotate the knob, the knob rotates and drives third gear revolve, third gear revolve drives second gear revolve, second gear revolve rotates and drives the pivot and produces the pivoted trend, but because the pivot is spacing by two sliders, then the pivot can only be in settling a section of thick bamboo inside continuous reciprocating, when the pivot reciprocates, can drive the wing main part and reciprocate simultaneously, when the wing main part reaches suitable position, the user stall knob, thereby be convenient for freely adjust from top to bottom to unmanned aerial vehicle wing truck when using, and then be convenient for freely adjust the wing main part, make unmanned aerial vehicle's application scope can enlarge.

Drawings

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

FIG. 2 is a schematic view of the connection structure of the installation cylinder and the wing mechanism shown in FIG. 1;

FIG. 3 is a schematic view of the connection structure of the connecting rod and the wing mechanism shown in FIG. 1;

FIG. 4 is a schematic view of a connection structure of the mounting base and the adjusting mechanism shown in FIG. 1;

fig. 5 is a schematic view showing the structure of the tooth grooves shown in fig. 1.

In the figure: 1. the wing mechanism comprises a connecting rod, 2, a mounting seat, 3, an adjusting mechanism, 31, a support rod, 32, a first gear, 33, a spring, 34, a tooth groove, 4, a mounting cylinder, 5, a wing mechanism, 51, a knob, 52, a sheath, 53, a rotating shaft, 54, a second gear, 55, a sliding groove, 56, a sliding block, 57, a third gear, 6 and a wing main body.

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. 1-5, a rotary joint type unmanned aerial vehicle wing trunk includes a connecting rod 1, a mounting cylinder 4 is fixed on one side of the connecting rod 1, a wing mechanism 5 is arranged in the connecting rod 1 and the mounting cylinder 4, the wing mechanism 5 comprises a knob 51, a rotating shaft 53, a second gear 54, a sliding block 56 and a third gear 57, the middle part of the connecting rod 1 near one side of the placing barrel 4 is provided with the knob 51, the bottom of the knob 51 extends to the inside of the connecting rod 1, the bottom end of the knob 51 is connected with the third gear 57, the rotating shaft 53 is arranged inside the mounting cylinder 4, the two opposite sides of the top side wall of the rotating shaft 53 are respectively connected with one sliding block 56, the sliding blocks 56 are clamped on the inner wall of the mounting barrel 4, and the second gear 54 is connected to the bottom side wall of the rotating shaft 53 in a threaded manner, and the wing main body 6 is mounted on the side wall of the top end of the rotating shaft 53.

As a technical optimization scheme of the utility model, connecting rod 1 deviates from the one end of settling a section of thick bamboo 4 is fixed with mount pad 2, the whole of mount pad 2 is discoid.

As a technical optimization scheme of the utility model, 2 inside adjustment mechanism 3 that are equipped with of mount pad, adjustment mechanism 3 includes branch 31 and spring 33, the inside of mount pad 2 is equipped with branch 31, just the winding has on the lateral wall of branch 31 spring 33, the bottom of spring 33 connect in the bottom of 2 inner chambers of mount pad.

As a technical optimization scheme of the utility model, adjustment mechanism 3 still includes first gear 32 and tooth's socket 34, the top of spring 33 is connected with first gear 32, first gear 32 is fixed in on the lateral wall of branch 31, just the top of 2 inner chambers of mount pad is equipped with tooth's socket 34, first gear 32 block in tooth's socket 34.

As a technical optimization scheme of the utility model, wing mechanism 5 still includes sheath 52, knob 51's whole is discoid, just cup jointed on knob 51's the lateral wall sheath 52.

As a technical optimization scheme of the utility model, wing mechanism 5 still includes spout 55, it is equipped with one respectively to settle 4 relative both sides in inner chamber top of a section of thick bamboo spout 55, two slider 56 blocks in two respectively spout 55.

When the utility model is used, firstly, the device is fixedly arranged at a required proper position to complete the preparation work before the device is used; when the unmanned aerial vehicle needs to fly in different environments or needs to perform different tasks, a user can manually rotate the knob 51, the knob 51 rotates to drive the third gear 57 to rotate, the third gear 57 rotates to drive the second gear 54 to rotate, the second gear 54 rotates to drive the rotating shaft 53 to generate a rotating trend, but because the rotating shaft 53 is limited by the two sliders 56, the rotating shaft 53 can only continuously move up and down in the accommodating cylinder 4, when the rotating shaft 53 moves up and down, the wing main body 6 can be driven to simultaneously move up and down, when the wing main body 6 reaches a proper position, the user stops rotating the knob 51, so that the wing trunk of the unmanned aerial vehicle can be freely adjusted up and down when the unmanned aerial vehicle is used, the wing main body 6 can be freely adjusted, meanwhile, the user can press down the mounting base 2 to enable the first gear 32 to move down to be separated from the constraint of the tooth grooves 34, then rotate mount pad 2 to drive connecting rod 1 and rotate simultaneously, and then drive wing main part 6 and rotate, when wing main part 6 reaches suitable position, loosen the hand, then spring 33 resets thereupon, makes first gear 32 block go into tooth's socket 34 again, accomplishes spacingly, makes unmanned aerial vehicle's application scope can enlarge, finally accomplishes the whole use of this device.

It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented 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 a connect formula unmanned aerial vehicle wing truck soon, includes connecting rod (1), its characterized in that: a placing barrel (4) is fixed on one side of the connecting rod (1), a wing mechanism (5) is arranged inside the connecting rod (1) and the placing barrel (4), the wing mechanism (5) comprises a knob (51), a rotating shaft (53), a second gear (54), a sliding block (56) and a third gear (57), the knob (51) is arranged in the middle of one side, close to the placing barrel (4), of the connecting rod (1), the bottom of the knob (51) extends into the inside of the connecting rod (1), the bottom end of the knob (51) is connected with the third gear (57), the rotating shaft (53) is arranged inside the placing barrel (4), two opposite sides of the top side wall of the rotating shaft (53) are respectively connected with one sliding block (56), the sliding block (56) is clamped on the inner wall of the placing barrel (4), and the second gear (54) is in threaded connection with the bottom side wall of the rotating shaft (53), and a wing main body (6) is arranged on the side wall of the top end of the rotating shaft (53).

2. The wing trunk of a swivel-joint unmanned aerial vehicle of claim 1, wherein: the connecting rod (1) deviates from one end of the mounting cylinder (4) and is fixedly provided with a mounting seat (2), and the mounting seat (2) is integrally disc-shaped.

3. The wing trunk of a swivel-joint unmanned aerial vehicle of claim 2, wherein: mount pad (2) inside adjustment mechanism (3) of being equipped with, adjustment mechanism (3) include branch (31) and spring (33), the inside of mount pad (2) is equipped with branch (31), just the winding has on the lateral wall of branch (31) spring (33), the bottom of spring (33) connect in the bottom of mount pad (2) inner chamber.

4. The wing trunk of a swivel-joint unmanned aerial vehicle of claim 3, wherein: adjustment mechanism (3) still include first gear (32) and tooth's socket (34), the top of spring (33) is connected with first gear (32), first gear (32) are fixed in on the lateral wall of branch (31), just the top of mount pad (2) inner chamber is equipped with tooth's socket (34), first gear (32) block in tooth's socket (34).

5. The wing trunk of a swivel-joint unmanned aerial vehicle of claim 1, wherein: the wing mechanism (5) further comprises a sheath (52), the knob (51) is integrally disc-shaped, and the sheath (52) is sleeved on the side wall of the knob (51).

6. The wing trunk of a swivel-joint unmanned aerial vehicle of claim 1, wherein: the wing mechanism (5) further comprises sliding grooves (55), the two opposite sides of the top of the inner cavity of the accommodating cylinder (4) are respectively provided with one sliding groove (55), and the two sliding blocks (56) are respectively clamped in the two sliding grooves (55).