CN215664013U - Unmanned aerial vehicle's carry mechanism - Google Patents
Unmanned aerial vehicle's carry mechanism Download PDFInfo
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- CN215664013U CN215664013U CN202023196335.5U CN202023196335U CN215664013U CN 215664013 U CN215664013 U CN 215664013U CN 202023196335 U CN202023196335 U CN 202023196335U CN 215664013 U CN215664013 U CN 215664013U
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- fixedly connected
- unmanned aerial
- aerial vehicle
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Abstract
The utility model discloses a mounting mechanism of an unmanned aerial vehicle, which comprises an unmanned aerial vehicle body, wherein the middle part of the bottom end of the unmanned aerial vehicle body is fixedly connected with a fixed plate, the middle part of the fixed plate is provided with a mounting groove, two sides of the mounting groove are respectively provided with a groove, the mounting groove is internally detachably connected with a mounting plate, the mounting plate is internally provided with a long groove, the middle part of the long groove is provided with a circular groove, the circular groove extends to the surface of the mounting plate and is rotatably connected with a circular plate, and the middle part of the circular plate is fixedly connected with a handle. Simple structure, convenient operation and worth popularizing and using.
Description
Technical Field
The utility model relates to the technical field of mounting mechanisms, in particular to a mounting mechanism of an unmanned aerial vehicle.
Background
A drone is an unmanned aircraft that is operated with a radio remote control device and self-contained program control, 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, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
The prior art is used for unmanned carry mechanism installation and dismantlement mode tradition, and the dismouting is got up more loaded down with trivial details, influences unmanned aerial vehicle's availability factor, needs to improve.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the defects in the prior art, and provides a mounting mechanism of an unmanned aerial vehicle.
In order to achieve the purpose, the utility model adopts the following technical scheme: a mounting mechanism of an unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein a fixed plate is fixedly connected to the middle of the bottom end of the unmanned aerial vehicle body, a mounting groove is formed in the middle of the fixed plate, grooves are formed in two sides of the mounting groove, a mounting plate is detachably connected to the inside of the mounting groove, an elongated groove is formed in the mounting plate, a circular groove is formed in the middle of the elongated groove, extends to the surface of the mounting plate and is rotatably connected with a circular plate, a handle is fixedly connected to the middle of the circular plate, a sliding barrel is fixedly connected to the middle of each of two sides of the elongated groove, a return spring is fixedly connected to the inside of the sliding barrel, a sliding rod is fixedly connected to the other side of the return spring, the other end of the sliding rod extends out of the sliding barrel and is fixedly connected with a rope, a first connecting rod is fixedly connected to the outer surface of the sliding rod, and a second connecting rod is fixedly connected to one side, close to the sliding barrel, of the first connecting rod, the second connecting rod extends to two ends of the elongated slot and is fixedly connected with a connecting plate, the middle of the outer surface of the connecting plate is fixedly connected with a cylinder, and the bottom end surface of the mounting plate is fixedly connected with a hanging hook.
As a further description of the above technical solution:
the surface of the slide bar is in smooth contact with the inner side wall of the slide cylinder.
As a further description of the above technical solution:
the other end of the rope is fixedly connected with the side surface of the circular plate.
As a further description of the above technical solution:
the groove is matched with the cylinder for use.
As a further description of the above technical solution:
the sliding rod can move in the sliding barrel for a distance equal to the length of the cylinder.
As a further description of the above technical solution:
and the side surface of the second connecting rod is in smooth contact with the inner side wall of the long groove.
The utility model has the following beneficial effects:
compared with the prior art, this portable multi-functional administrative affairs management device, through having set up the mounting groove, a groove, the mounting panel, the elongated slot, the circular slot, the plectane, the slide cartridge, reset spring, the slide bar, the rope, the head rod, the second connecting rod, structural member such as connecting plate and cylinder, it rotates to rotate the handle plectane, the rope is to the side motion, the pulling slide bar is close to the plectane, make reset spring tensile, head rod and second connecting rod pulling connecting plate move to the elongated slot inside simultaneously, then the cylinder breaks away from the recess, can take off the mounting panel from the unmanned aerial vehicle body fast, utilize the same principle can install the mounting panel fast, moreover, the steam generator is simple in structure, and convenient operation is worth using widely.
Drawings
Fig. 1 is a side view of a mounting mechanism of an unmanned aerial vehicle according to the present invention;
fig. 2 is a sectional view of a mounting plate of a mounting mechanism of an unmanned aerial vehicle according to the present invention;
fig. 3 is a side view of a mounting plate of a mounting mechanism of an unmanned aerial vehicle according to the present invention.
Illustration of the drawings:
1. an unmanned aerial vehicle body; 2. a fixing plate; 3. a groove; 4. mounting a plate; 5. a handle; 6. hanging a hook; 7. a cylinder; 8. a circular groove; 9. a circular plate; 10. a rope; 11. a second connecting rod; 12. a long groove; 13. A slide bar; 14. a slide cylinder; 15. a return spring; 16. a first connecting rod; 17. a connecting plate; 11. a second connecting rod; 18. and (4) mounting the groove.
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.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc., indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention; the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance, and furthermore, unless otherwise explicitly stated or limited, the terms "mounted," "connected," and "connected" are to be construed broadly and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Referring to fig. 1-3, the utility model provides a mounting mechanism of an unmanned aerial vehicle, comprising: including unmanned aerial vehicle body 1, the bottom middle part fixedly connected with fixed plate 2 of unmanned aerial vehicle body 1, mounting groove 18 has been seted up at the middle part of fixed plate 2, cooperation mounting panel 4 realizes dismantling of mounting panel 4 and connects, recess 3 has all been seted up to the both sides of mounting groove 18, cooperation cylinder 7 realizes the rigidity of mounting panel 4, the inside of mounting groove 18 can be dismantled and is connected with mounting panel 4, the inside of mounting panel 4 has seted up elongated slot 12, circular slot 8 has been seted up at the middle part of elongated slot 12, realize the rotation of plectane 9, circular slot 8 extends to the surface of mounting panel 4, and the rotation is connected with plectane 9, the middle part fixedly connected with handle 5 of plectane 9, the equal fixedly connected with slide cartridge 14 in the middle part of both sides of elongated slot 12, the position of fixed reset spring 15, and the direction of injectd slide bar 13, the inside fixedly connected with reset spring 15 of slide cartridge 14, realize slide bar 13, plectane 9 handle 5, The automatic resetting of components such as a reset spring 15, a cylinder 7 and the like is convenient, the mounting plate 4 is convenient to detach and mount, the other side of the reset spring 15 is fixedly connected with a sliding rod 13, the directional movement of the cylinder 7 is realized, the other end of the sliding rod 13 extends out of a sliding barrel 14 and is fixedly connected with a rope 10, the sliding rod 13 can be moved through the rotation of a circular plate 9, the outer surface of the sliding rod 13 is fixedly connected with a first connecting rod 16, the cylinder 7 is driven to move through the movement of the sliding rod 13, one side of the first connecting rod 16, which is close to the sliding barrel 14, is fixedly connected with a second connecting rod 11, the cylinder 7 is driven to move through the movement of the sliding rod 13, the second connecting rod 11 extends to two ends of a long groove 12 and is fixedly connected with a connecting plate 17, the cylinder 7 is driven to move through the movement of the sliding rod 13, the cylinder 7 is fixedly connected with the middle part of the outer surface of the connecting plate 17, and the bottom end surface of the mounting plate 4 is fixedly connected with a hanging hook 6, be used for unmanned aerial vehicle body 1 to use the carry function.
The surface of the slide bar 13 is in smooth contact with the inner side wall of the slide cylinder 14, and the moving direction of the slide bar 13 is limited. The other end of the rope 10 is fixedly connected with the side surface of the circular plate 9, and the rope 10 is moved by the rotation of the circular plate 9, so that the sliding rod 13 is driven to move. Recess 3 and cylinder 7 cooperation are used, realize the removable connection of mounting panel 4. The slide 13 is movable inside the slide 14 by a distance equal to the length of the cylinder 7, ensuring that the cylinder 7 can be completely detached from the groove 3 by rotating the circular plate 9. The side surface of the second connecting rod 11 is in smooth contact with the inner side wall of the long groove 12, the moving direction of the cylinder 7 is limited, and the mounting and positioning accuracy of the mounting plate 4 is improved.
The working principle is as follows: when needing to dismantle, rotate handle 5, make plectane 9 rotate, plectane 9 drives rope 10 to one side motion when rotating, consequently rope 10 pulling slide bar 13 moves to plectane one side, make reset spring 15 tensile, slide bar 13 drives head rod 16 and second connecting rod 11 and moves to plectane 9 one side simultaneously, pulling connecting plate 17 moves to elongated slot 12 inside, so cylinder 7 breaks away from recess 3, can take off mounting panel 4 from unmanned aerial vehicle body 1 fast this moment, then loosen handle 5, reset spring 15 resets, cylinder 7 resets, but utilize same principle to install mounting panel 4 fast.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments or portions thereof without departing from the spirit and scope of the utility model.
Claims (6)
1. The utility model provides an unmanned aerial vehicle's carry mechanism, includes unmanned aerial vehicle body (1), its characterized in that: the unmanned aerial vehicle is characterized in that a fixed plate (2) is fixedly connected to the middle of the bottom end of the unmanned aerial vehicle body (1), a mounting groove (18) is formed in the middle of the fixed plate (2), grooves (3) are formed in two sides of the mounting groove (18), a mounting plate (4) is detachably connected to the inside of the mounting groove (18), an elongated slot (12) is formed in the inside of the mounting plate (4), a circular slot (8) is formed in the middle of the elongated slot (12), the circular slot (8) extends to the surface of the mounting plate (4) and is rotatably connected with a circular plate (9), a handle (5) is fixedly connected to the middle of the circular plate (9), sliding cylinders (14) are fixedly connected to the middle of two sides of the elongated slot (12), a reset spring (15) is fixedly connected to the inside of the sliding cylinder (14), a sliding rod (13) is fixedly connected to the other side of the reset spring (15), and the other end of the sliding rod (13) extends out of the sliding cylinder (14), and fixedly connected with rope (10), the surface fixedly connected with head rod (16) of slide bar (13), one side fixedly connected with second connecting rod (11) that head rod (16) is close to slide cartridge (14), second connecting rod (11) extend to the both ends of elongated slot (12) to fixedly connected with connecting plate (17), the surface middle part fixedly connected with cylinder (7) of connecting plate (17), the bottom surface fixedly connected with carry of mounting panel (4) colludes (6).
2. The unmanned aerial vehicle mounting mechanism of claim 1, wherein: the surface of the slide rod (13) is in smooth contact with the inner side wall of the slide cylinder (14).
3. The unmanned aerial vehicle mounting mechanism of claim 1, wherein: the other end of the rope (10) is fixedly connected with the side surface of the circular plate (9).
4. The unmanned aerial vehicle mounting mechanism of claim 1, wherein: the groove (3) is matched with the cylinder (7) for use.
5. The unmanned aerial vehicle mounting mechanism of claim 1, wherein: the movable distance of the slide rod (13) in the slide cylinder (14) is equal to the length of the cylinder (7).
6. The unmanned aerial vehicle mounting mechanism of claim 1, wherein: the side surface of the second connecting rod (11) is in smooth contact with the inner side wall of the long groove (12).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023196335.5U CN215664013U (en) | 2020-12-24 | 2020-12-24 | Unmanned aerial vehicle's carry mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023196335.5U CN215664013U (en) | 2020-12-24 | 2020-12-24 | Unmanned aerial vehicle's carry mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215664013U true CN215664013U (en) | 2022-01-28 |
Family
ID=79949730
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202023196335.5U Active CN215664013U (en) | 2020-12-24 | 2020-12-24 | Unmanned aerial vehicle's carry mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215664013U (en) |
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2020
- 2020-12-24 CN CN202023196335.5U patent/CN215664013U/en active Active
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