CN211893636U - Wing protector for unmanned aerial vehicle - Google Patents
Wing protector for unmanned aerial vehicle Download PDFInfo
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- CN211893636U CN211893636U CN202020099030.3U CN202020099030U CN211893636U CN 211893636 U CN211893636 U CN 211893636U CN 202020099030 U CN202020099030 U CN 202020099030U CN 211893636 U CN211893636 U CN 211893636U
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Abstract
The utility model discloses a wing protector for unmanned aerial vehicle, including unmanned aerial vehicle main part, wing mechanism, protection casing, adjustment mechanism, knob, gear, first spring, dead lever, inside groove, tooth's socket, stop gear, fixture block, resettlement groove, second spring, draw-in groove and spout. The utility model has the advantages that: make the fixture block on the dead lever slide to the bottommost along the spout, the user presses down the knob, make the gear break away from the tooth's socket, rotate the knob after that, drive first spring and rotate, first spring rotates and drives two fixture blocks and rotate, when the fixture block reachs the position of draw-in groove, draw-in groove will be gone into to automatic block, thereby accomplish the installation, make the protection casing protect wing mechanism, afterwards, loosen pressing down to the knob, then the knob can reply to the normal position under the resilience of first spring, the gear is by the tooth's socket block again, thereby be convenient for in unmanned aerial vehicle packing transportation, form good protection to the wing position, while easy to assemble dismantles, and difficult not hard up in the use.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle wing protective equipment specifically is a wing protector for unmanned aerial vehicle belongs to unmanned aerial vehicle protection 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, traditional unmanned aerial vehicle is in the in-service use, when needs pack unmanned aerial vehicle and transport, because the fragility of unmanned aerial vehicle wing, cause the influence or even damage to the wing very easily to cause great loss, current protector is not enough to unmanned aerial vehicle's wing position protection, and when most protector uses or the installation dismantlement process is loaded down with trivial details very, or is not hard up easily during the use, all is not very convenient.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a wing protector for unmanned aerial vehicle just lies in solving above-mentioned problem, and the flexible operation is convenient for in unmanned aerial vehicle packing transportation, forms good protection to the wing position, and easy to assemble dismantlement simultaneously, and difficult not hard up in the use.
The utility model discloses a following technical scheme realizes above-mentioned purpose, a wing protector for unmanned aerial vehicle, including the unmanned aerial vehicle main part, the top of unmanned aerial vehicle main part is equipped with wing mechanism, wing mechanism's top is equipped with the protection casing, the middle part of protection casing is equipped with adjustment mechanism, adjustment mechanism includes knob, gear, first spring, dead lever, inside groove and tooth's socket, the top surface middle part of protection casing rotates to be connected with the knob, the knob extends to the inside groove inside the protection casing, and the bottom of knob is connected with the gear, the bottom of gear is connected with the first spring, the bottom of first spring is connected with the dead lever, the top of inside groove is equipped with the tooth's socket, the gear block in the tooth's socket; the wing mechanism is provided with a fixed rod, the fixed rod is provided with a wing mechanism, the wing mechanism is provided with a wing mechanism, the wing; the inside on wing mechanism top is equipped with draw-in groove with the spout.
Preferably, in order to realize when using in the unmanned aerial vehicle main part the installation of wing main part, wing mechanism is including installation pole, installation piece and wing main part, the roof of unmanned aerial vehicle main part is fixed with the installation pole, the top of installation pole is fixed with the installation piece, install on the installation piece the wing main part.
Preferably, in order to realize reasonable arrangement of the sliding grooves and the clamping grooves in use, two opposite sides of the top end of the mounting block are respectively provided with one sliding groove, and the other two opposite sides of the top end of the mounting block are respectively provided with one clamping groove.
Preferably, in order to better protect the wing main body, the whole protective cover is of a cylindrical structure with a hollow inner part and an unsealed bottom end, the top of the protective cover is of a circular plate shape, and the side wall of the protective cover is of a net shape.
Preferably, in order to conveniently limit the first spring when the adjusting mechanism is used, the adjusting mechanism further comprises a connecting rod, the connecting rod is connected to the middle of the bottom end of the gear, the bottom of the connecting rod extends to the inside of the fixing rod, and the first spring is wound on the connecting rod.
Preferably, in order to conveniently place the second spring when in use, the limiting mechanism further comprises a side plate, the fixing rod is provided with the side plate on the inner wall of the placing groove, and one side of the side plate is connected with the second spring.
Preferably, for further convenience when using the block of fixture block, the fixture block deviates from the tip of second spring is hemispherical, just the draw-in groove with spout horizontal cross-section's opening part is the loudspeaker form.
Compared with the prior art, the beneficial effects of the utility model are that: the bottom of the protective cover is manually aligned to the top of the wing mechanism, the clamping blocks on two sides of the bottom end of the fixed rod are aligned to the sliding grooves in the wing mechanism, when the clamping blocks on the fixed rod slide to the bottom end along the sliding grooves, a user manually presses the rotary knob to enable the gear to be separated from the tooth grooves, then the rotary knob is rotated, when the rotary knob is rotated, the first spring is driven to rotate, the first spring drives the fixed rod to rotate, the fixed rod drives the two clamping blocks to rotate, when the clamping blocks are extruded, the second spring contracts to drive the clamping blocks to retract into the fixed rod, the rotary knob is continuously rotated, when the clamping blocks reach the positions of the clamping grooves, the clamping blocks are automatically clamped into the clamping grooves, the mounting process is conveniently completed, the protective cover protects the wing mechanism, then the rotary knob is released from pressing the rotary knob, the rotary knob returns to the original position under the rebounding of the first, the wing protection device has the advantages that the wing protection device can well protect the wing part, is convenient to install and disassemble, and is not easy to loosen in the using process.
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 adjusting mechanism and the protecting cover shown in FIG. 1;
FIG. 3 is a schematic view of a connection structure between the adjusting mechanism and the limiting mechanism shown in FIG. 1;
FIG. 4 is a schematic view of a connection structure between the wing mechanism and the limiting 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. unmanned aerial vehicle main part, 2, wing mechanism, 21, installation pole, 22, installation piece, 23, wing main part, 3, protection casing, 4, adjustment mechanism, 41, knob, 42, gear, 43, connecting rod, 44, first spring, 45, dead lever, 46, inside groove, 47, tooth's socket, 5, stop gear, 51, fixture block, 52, resettlement groove, 53, curb plate, 54, second spring, 55, draw-in groove, 56, spout.
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 wing protector for an unmanned aerial vehicle includes an unmanned aerial vehicle body 1, the top of the unmanned aerial vehicle main body 1 is provided with a wing mechanism 2, the top of the wing mechanism 2 is provided with a protective cover 3, the middle part of the protective cover 3 is provided with an adjusting mechanism 4, the adjusting mechanism 4 comprises a knob 41, a gear 42, a first spring 44, a fixing rod 45, an inner groove 46 and a tooth groove 47, the knob 41 is rotatably connected to the middle of the top surface of the shield 3, the knob 41 extends to the inner groove 46 inside the shield 3, and the gear 42 is connected to the bottom of the knob 41, the first spring 44 is connected to the bottom of the gear 42, the fixing rod 45 is connected to the bottom of the first spring 44, the tooth slot 47 is formed in the top of the inner groove 46, and the gear 42 is clamped in the tooth slot 47; the bottom of the fixed rod 45 and the wing mechanism 2 are provided with limiting mechanisms 5, each limiting mechanism 5 comprises a clamping block 51, a placing groove 52, a second spring 54, a clamping groove 55 and a sliding groove 56, the two opposite sides of the bottom of the fixed rod 45 are respectively provided with one placing groove 52, the inner wall of the fixed rod 45 where the placing groove 52 is arranged is provided with the second spring 54, and the other end of the second spring 54 is connected with the clamping block 51; the clamping groove 55 and the sliding groove 56 are arranged inside the top end of the wing mechanism 2.
As a technical optimization scheme of the utility model, wing mechanism 2 is including installation pole 21, installation piece 22 and wing main part 23, the roof of unmanned aerial vehicle main part 1 is fixed with installation pole 21, the top of installation pole 21 is fixed with installation piece 22, install on the installation piece 22 wing main part 23.
As a technical optimization scheme of the utility model, the inside relative both sides in installation piece 22 top are equipped with one respectively spout 56, the inside other a set of relative both sides in installation piece 22 top are equipped with one respectively draw-in groove 55.
As a technical optimization scheme of the utility model, the whole of protection casing 3 is the cylinder structure that an inside hollow bottom does not seal, just the top of protection casing 3 is the disc form, and the lateral wall of protection casing 3 is netted.
As a technical optimization scheme of the utility model, adjustment mechanism 4 still includes connecting rod 43, the bottom middle part of gear 42 is connected with connecting rod 43, the bottom of connecting rod 43 extends to the inside of dead lever 45, just first spring 44 twine in connecting rod 43.
As a technical optimization scheme of the utility model, stop gear 5 still includes curb plate 53, dead lever 45 is being equipped with be equipped with on the inner wall of resettlement groove 52 department curb plate 53, one side of curb plate 53 is connected with second spring 54.
As a technical optimization scheme of the utility model, fixture block 51 deviates from second spring 54's tip is hemispherical, just draw-in groove 55 with spout 56 horizontal cross-section's opening part is the loudspeaker form.
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 be packaged and transported, a user can manually align the bottom of the protective cover 3 with the top of the mounting block 22, the fixture blocks 51 on the two sides of the bottom end of the fixing rod 45 are aligned with the sliding grooves 56 on the mounting block 22, when the fixture blocks 51 on the fixing rod 45 slide to the bottom end along the sliding grooves 56, the user manually presses the knob 41 to separate the gear 42 from the tooth grooves 47, then the knob 41 is rotated, when the knob 41 rotates, the first spring 44 is driven to rotate, the fixing rod 45 is driven to rotate by the first spring 44, the fixing rod 45 rotates to drive the two fixture blocks 51 to rotate, when the fixture blocks 51 are extruded, the second spring 54 contracts to drive the fixture blocks 51 to retract into the fixing rod 45, the knob 41 is continuously rotated, when the fixture blocks 51 reach the positions of the clamping grooves 55, the clamping grooves 55 are automatically clamped, so that the mounting process is conveniently completed, and the, when needs are dismantled, press knob 41, with the above-mentioned operation of carrying on opposite directions can, later, loosen the pressing to knob 41, then knob 41 can reply to the normal position under the resilience of first spring 44, gear 42 is by tooth's socket 47 block again to be convenient for in unmanned aerial vehicle packing transportation, form good protection to the wing position, the while is easy to assemble dismantlement, and difficult not hard up in the use, the whole use of this device of final completion.
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 (7)
1. The utility model provides a wing protector for unmanned aerial vehicle, includes unmanned aerial vehicle main part (1), its characterized in that: the top of the unmanned aerial vehicle main body (1) is provided with a wing mechanism (2), the top of the wing mechanism (2) is provided with a protective cover (3), the middle of the protective cover (3) is provided with an adjusting mechanism (4), the adjusting mechanism (4) comprises a knob (41), a gear (42), a first spring (44), a fixing rod (45), an inner groove (46) and a tooth groove (47), the middle of the top surface of the protective cover (3) is rotatably connected with the knob (41), the knob (41) extends to the inner groove (46) inside the protective cover (3), the bottom of the knob (41) is connected with the gear (42), the bottom of the gear (42) is connected with the first spring (44), the bottom of the first spring (44) is connected with the fixing rod (45), the top of the inner groove (46) is provided with the tooth groove (47), the gear (42) is engaged with the tooth groove (47); limiting mechanisms (5) are arranged at the bottom of the fixing rod (45) and on the wing mechanism (2), each limiting mechanism (5) comprises a clamping block (51), a placement groove (52), a second spring (54), a clamping groove (55) and a sliding groove (56), two sides of the bottom of the fixing rod (45), which are opposite to each other, are respectively provided with one placement groove (52), the second spring (54) is arranged on the inner wall of the fixing rod (45) where the placement groove (52) is arranged, and the other end of the second spring (54) is connected with the clamping block (51); the clamping groove (55) and the sliding groove (56) are formed in the top end of the wing mechanism (2).
2. The wing protector for an unmanned aerial vehicle of claim 1, wherein: wing mechanism (2) are including installation pole (21), installation piece (22) and wing main part (23), the roof of unmanned aerial vehicle main part (1) is fixed with installation pole (21), the top of installation pole (21) is fixed with installation piece (22), install on installation piece (22) wing main part (23).
3. The wing protector for an unmanned aerial vehicle of claim 2, wherein: the two opposite sides in the top end of the mounting block (22) are respectively provided with the sliding grooves (56), and the other two opposite sides in the top end of the mounting block (22) are respectively provided with the clamping grooves (55).
4. The wing protector for an unmanned aerial vehicle of claim 1, wherein: the whole of protection casing (3) is the cylinder structure that inside hollow bottom was not sealed, just the top of protection casing (3) is the disc form, and the lateral wall of protection casing (3) is netted.
5. The wing protector for an unmanned aerial vehicle of claim 1, wherein: the adjusting mechanism (4) further comprises a connecting rod (43), the middle of the bottom end of the gear (42) is connected with the connecting rod (43), the bottom of the connecting rod (43) extends to the inside of the fixing rod (45), and the first spring (44) is wound on the connecting rod (43).
6. The wing protector for an unmanned aerial vehicle of claim 1, wherein: the limiting mechanism (5) further comprises a side plate (53), the side plate (53) is arranged on the inner wall, where the mounting groove (52) is arranged, of the fixing rod (45), and the second spring (54) is connected to one side of the side plate (53).
7. The wing protector for an unmanned aerial vehicle of claim 1, wherein: the end part of the clamping block (51) departing from the second spring (54) is hemispherical, and the opening of the horizontal section of the clamping groove (55) and the sliding groove (56) is trumpet-shaped.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020099030.3U CN211893636U (en) | 2020-01-16 | 2020-01-16 | Wing protector for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020099030.3U CN211893636U (en) | 2020-01-16 | 2020-01-16 | Wing protector for unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN211893636U true CN211893636U (en) | 2020-11-10 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202020099030.3U Active CN211893636U (en) | 2020-01-16 | 2020-01-16 | Wing protector for unmanned aerial vehicle |
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| Country | Link |
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| CN (1) | CN211893636U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112937843A (en) * | 2021-04-21 | 2021-06-11 | 深圳市瑞可创新科技有限公司 | Aerial photography unmanned aerial vehicle with anti-falling mechanism |
| CN115847927A (en) * | 2023-02-21 | 2023-03-28 | 山西纽维尔环保科技有限公司 | Novel marking press article location device |
-
2020
- 2020-01-16 CN CN202020099030.3U patent/CN211893636U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112937843A (en) * | 2021-04-21 | 2021-06-11 | 深圳市瑞可创新科技有限公司 | Aerial photography unmanned aerial vehicle with anti-falling mechanism |
| CN115847927A (en) * | 2023-02-21 | 2023-03-28 | 山西纽维尔环保科技有限公司 | Novel marking press article location device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20220622 Address after: No. 35, Lijia, Xinchang village, Jingcheng Town, Zhushan District, Jingdezhen City, Jiangxi Province, 333000 Patentee after: Jingdezhen Tianyi Aviation Technology Co.,Ltd. Address before: 317203 98 group 1, Xinqiao village, Lei Feng Township, Tiantai County, Taizhou, Zhejiang Patentee before: Ding Wuxuan |
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| TR01 | Transfer of patent right |