CN211810298U - Unmanned aerial vehicle field take-off and landing platform - Google Patents
Unmanned aerial vehicle field take-off and landing platform Download PDFInfo
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- CN211810298U CN211810298U CN202020353707.1U CN202020353707U CN211810298U CN 211810298 U CN211810298 U CN 211810298U CN 202020353707 U CN202020353707 U CN 202020353707U CN 211810298 U CN211810298 U CN 211810298U
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Abstract
The utility model discloses an open-air platform that takes off and land of unmanned aerial vehicle, including the platform that takes off and land, the bolted connection of platform bottom takes off and land has folding device, the bolted connection of folding device bottom has first bracing piece, the track groove has been seted up to first bracing piece outer wall, the inside joint of first bracing piece has the telescopic link, telescopic link bottom fixedly connected with inserts native base, telescopic link top outer wall welding has the locking lever, locking lever outer wall threaded connection has the locking head, the inside through connection of folding device has folding locker. This unmanned aerial vehicle platform that takes off and land in the field, when needs use unmanned aerial vehicle in the field, with first bracing piece pull-up, perpendicular to folding device rotates folding locker, with first bracing piece locking, will insert soil base angle simultaneously and insert mud ground, meadow, gobi etc. when the soil unevenness, the pulling locking lever makes the telescopic link pull out, will take off and land platform adjustment level, after finishing using, rotate folding locker, make first bracing piece fold portable.
Description
Technical Field
The utility model relates to a platform technical field that takes off and land specifically is an open-air platform that takes off and land of unmanned aerial vehicle.
Background
The unmanned plane is called unmanned plane for short, and is called UAV in English, and is an unmanned aerial vehicle operated by using a radio remote control device and a self-contained program control device. Unmanned aerial vehicles are in fact a general term for unmanned aerial vehicles, and can be defined from a technical perspective as follows: unmanned fixed wing aircraft, unmanned VTOL aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned paravane, etc. Compared with manned aircraft, it has the advantages of small volume, low cost, convenient use, low requirement on the operational environment, strong battlefield viability and the like. Since the unmanned aircraft has important significance for future air battles, the research and development work of the unmanned aircraft is carried out in all major military countries in the world. 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.
In the field operation of the existing rotor unmanned aerial vehicle and the existing vertical take-off and landing unmanned aerial vehicle, a horizontal platform with a certain area is needed for ensuring the attitude level of the unmanned aerial vehicle in the take-off and landing stage; and the huge wind-force that the rotor produced rolls up debris such as sand, soil, grass, branch, rubbish on ground easily, reaches on unmanned aerial vehicle's the paddle or the fuselage, causes the flight accident.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle field take-off and landing platform to solve the problem that proposes among 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 open-air platform that takes off and land of unmanned aerial vehicle, includes the platform that takes off and land, the bolted connection of platform bottom takes off and land has folding device, the bolted connection of folding device bottom has first bracing piece, the track groove has been seted up to first bracing piece outer wall, the inside joint of first bracing piece has the telescopic link, telescopic link bottom fixedly connected with inserts native base, telescopic link top outer wall welding has the locking lever, locking lever outer wall threaded connection has the locking head, the inside through connection of folding device has folding locker.
In a preferred embodiment: the lifting platform bottom and the folding device top are both provided with external threads, and nuts are connected through threads, so that the lifting platform is convenient to install and disassemble.
In a preferred embodiment: the locking rod is externally provided with a thread matched with the locking head, and the locking rod is fixed through the locking head 8.
In a preferred embodiment: a track matched with the telescopic rod is arranged in the first supporting rod, and the platform can be kept horizontal on the undulating ground.
In a preferred embodiment: the folding device is internally provided with a notch matched with the folding locker for folding the foot rest and being convenient to carry.
In a preferred embodiment: the width of the track groove is larger than the width of the cross section of the locking rod, and friction is reduced.
Compared with the prior art, the beneficial effects of the utility model are that:
1. this unmanned aerial vehicle platform that takes off and land in the field, telescopic link bottom fixedly connected with inserts native base, is convenient for insert the land in adverse circumstances such as earth, sand, meadow, gobi and uses.
2. This open-air platform that takes off and land of unmanned aerial vehicle, the inside through connection telescopic link of first bracing piece when on undulating surface, through the adjustment telescopic link height, makes the platform that takes off and land reach the level.
3. This open-air platform that takes off and land of unmanned aerial vehicle, folding device bottom bolted connection first bracing piece through the first bracing piece of pulling, makes first bracing piece folding, portable
Drawings
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle field take-off and landing platform.
Fig. 2 is a cross-sectional view of a first support rod in an unmanned aerial vehicle field take-off and landing platform.
Fig. 3 is a cross-sectional view of a folding device in an unmanned aerial vehicle field take-off and landing platform.
In the figure: the device comprises a lifting platform 1, a folding device 2, a first supporting rod 3, a telescopic rod 4, a soil inserting bottom corner 5, a track groove 6, a locking rod 7, a locking head 8 and a folding locker 9.
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. 1-3, in the embodiment of the present invention, an unmanned aerial vehicle field take-off and landing platform comprises a take-off and landing platform 1, wherein the take-off and landing platform 1 is made of a flat and smooth composite material, so as to provide a flat take-off and landing platform for an airplane and prevent external impurities from entering the airplane, the take-off and landing platform 1 and one end of a folding device 2 are both provided with external threads and are connected with nuts through threads, so as to be conveniently assembled and disassembled, the bottom of the take-off and landing platform 1 is bolted with the folding device 2, the bottom of the folding device 2 is bolted with a first support rod 3, the outer wall of the first support rod 3 is provided with a track groove 6, the first support rod 3 is internally provided with a track matched with a telescopic rod 4, the platform can be kept horizontal on a rough ground, the inside of the first support rod 3 is clamped with a telescopic rod 4, the bottom of the, be convenient for insert earth, improve life, 6 radiuses in track groove are greater than locking lever 7 radiuses, reduce friction, and 4 top outer wall welding of telescopic link have locking lever 7, and 7 outer wall threaded connection of locking lever have locking head 8, and folding device 2 is inside to be offered the notch with folding locker 9 formula that matches for it is folding with the foot rest, portable, folding device 2 inside through connection has folding locker 9.
The utility model discloses a theory of operation is: when needs use unmanned aerial vehicle in the field, 3 are drawn up first bracing piece, make first bracing piece perpendicular to folding device 2, rotate folding locker 9, make folding locker 9 move inwards, the first bracing piece 3 of chucking, lock first bracing piece 3, insert soil base angle 5 simultaneously in the adverse circumstances such as muddy ground, sand, meadow, gobi, when the land unevenness, pulling locking lever 7 makes telescopic link 4 move down, when reaching the level, rotate locking head 8, make locking head 8 move inwards. The telescopic rod 4 is fixed, the lifting platform is adjusted to be horizontal, after the lifting platform is used, the folding locker 9 is rotated, the folding locker 9 is enabled to move outwards, the first supporting rod 3 is pulled down simultaneously, and the first supporting rod 3 is enabled to be folded, so that the lifting platform is convenient to carry.
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 invention.
Claims (6)
1. The utility model provides an open-air platform that takes off and land of unmanned aerial vehicle, includes platform (1) that takes off and land, its characterized in that, platform (1) bottom bolted connection has folding device (2), folding device (2) bottom bolted connection has first bracing piece (3), track groove (6) have been seted up to first bracing piece (3) outer wall, the inside joint of first bracing piece (3) has telescopic link (4), telescopic link (4) bottom fixedly connected with inserts native base (5), telescopic link (4) top outer wall welding has locking lever (7), locking lever (7) outer wall threaded connection has locking head (8), folding device (2) inside through connection has folding locker (9).
2. The unmanned aerial vehicle field take-off and landing platform of claim 1, wherein the bottom of the take-off and landing platform (1) and the top of the folding device (2) are both provided with external threads, and nuts are connected through the threads.
3. The unmanned aerial vehicle field take-off and landing platform of claim 1, wherein the locking rod (7) is externally provided with a thread matched with the locking head (8).
4. The unmanned aerial vehicle field take-off and landing platform of claim 1, wherein a track matched with the telescopic rod (4) is formed inside the first supporting rod (3).
5. The unmanned aerial vehicle field take-off and landing platform of claim 1, wherein the folding device (2) is internally provided with a notch matched with the folding locker (9).
6. An unmanned aerial vehicle field take-off and landing platform according to claim 1, wherein the width of the track groove (6) is greater than the width of the cross section of the locking rod (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020353707.1U CN211810298U (en) | 2020-03-19 | 2020-03-19 | Unmanned aerial vehicle field take-off and landing platform |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020353707.1U CN211810298U (en) | 2020-03-19 | 2020-03-19 | Unmanned aerial vehicle field take-off and landing platform |
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| Publication Number | Publication Date |
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| CN211810298U true CN211810298U (en) | 2020-10-30 |
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| CN202020353707.1U Active CN211810298U (en) | 2020-03-19 | 2020-03-19 | Unmanned aerial vehicle field take-off and landing platform |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113650797A (en) * | 2021-08-27 | 2021-11-16 | 广东电网有限责任公司 | Unmanned aerial vehicle patrols and examines operation platform |
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2020
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113650797A (en) * | 2021-08-27 | 2021-11-16 | 广东电网有限责任公司 | Unmanned aerial vehicle patrols and examines operation platform |
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