CN212022965U - Support lifting frame of Xinjiang longitude and latitude M210V2 unmanned aerial vehicle - Google Patents

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a support and landing frame of a Dajiang longitude and latitude M210V2 unmanned aerial vehicle, which comprises an anti-skid rubber mat and a carbon fiber tube base, wherein the top end of the anti-skid rubber mat is fixedly connected with the carbon fiber tube base, the outer side of the carbon fiber tube base is fixedly connected with a second carbon fiber tube, and a first carbon fiber tube is arranged above the second carbon fiber tube, in the utility model, through the arranged fixing buckle, the carbon fiber tube support, a screw cap, the first carbon fiber tube and the anti-skid rubber mat, according to the structure of the fixing buckle of a landing frame plug, the portable advantage of plug and play is reflected, a rotating structure through a screw hole can be folded and collected when not used, certain standing space can be reduced when transportation is carried out, the standing stability can be improved by the first carbon fiber tube and the second carbon fiber tube, the anti-skid rubber mat of the carbon fiber tube base improves the friction force to the ground, the stability is enhanced.

Description

Support lifting frame of Xinjiang longitude and latitude M210V2 unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is a big jiangqing M210V2 unmanned aerial vehicle's support undercarriage.

Background

Unmanned aerial vehicle is unmanned aerial vehicle for short, and UAV is abbreviated as English, and is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer, compared with the unmanned aerial vehicle, the unmanned aerial vehicle is more suitable for tasks which are too foolproof, dirty or dangerous, and can be divided into military use and civil use according to the application field, and the application of the unmanned aerial vehicle is more extensive along with the development of the society, so that the demand for supporting landing gears of a Xinjiang longitude and latitude M210V2 unmanned aerial vehicle is increased day by day.

In the functional structure of the Xinjiang longitude and latitude M210V2 unmanned aerial vehicle, the landing gear is a product which can help the Xinjiang longitude and latitude M210V2 unmanned aerial vehicle body to support, take off and land, the Xinjiang longitude and latitude M210V2 unmanned aerial vehicle needs to be used when taking off and landing or parking, the traditional Xinjiang longitude and latitude M210V2 unmanned aerial vehicle landing scheme is that supports are additionally arranged at two sides of the body, during taking off, factors influencing the balanced taking off of the airplane, such as uneven ground, sandy land and the like, can cause the Xinjiang longitude and latitude M210V2 unmanned plane to not take off normally, thereby causing the influence on the flying work, when the unmanned plane lands, if long water pipes or stones exist on the ground, the obstacles which can affect the landing of the Xinjiang longitude and latitude M210V2 unmanned plane can affect the working position of the landing, possibly cause the Xinjiang longitude and latitude M210V2 unmanned plane to land and turn on the side, affect the safety of the flight, therefore, the supporting landing gear of the Xinjiang longitude and latitude M210V2 unmanned aerial vehicle is provided for solving the problems.

SUMMERY OF THE UTILITY MODEL

The utility model aims at providing a big jiangqing M210V2 unmanned aerial vehicle's support undercarriage to solve the problem that proposes in the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme:

the utility model provides a big jiangqing M210V2 unmanned aerial vehicle's frame that lifts that supports, includes anti-skidding cushion and carbon fiber tube base, the top fixedly connected with carbon fiber tube base of anti-skidding cushion, the outside fixedly connected with second carbon fiber tube of carbon fiber tube base, the top of second carbon fiber tube is provided with first carbon fiber tube, the inboard block in top of first carbon fiber tube has the undercarriage plug, the front end fixedly connected with carbon fiber tube support of first carbon fiber tube, and the inboard of carbon fiber tube support is provided with the headless screw of M2.

Preferably, the front end of the first carbon fiber pipe is provided with a second spiral thread, the rear end of the undercarriage plug is provided with a first spiral thread, the outer side of the first carbon fiber pipe is provided with a threaded cap, and the threaded cap is in threaded connection with the second spiral thread and the first spiral thread.

Preferably, the inner side of the undercarriage plug is fixedly connected with a fixing buckle, and the fixing buckle is located on the vertical center line of the undercarriage plug.

Preferably, the outside fixedly connected with solid fixed ring of first carbon fiber pipe, gu the outside of fixed ring is rotated and is connected with the swivel.

Preferably, the outer side of the rotating ring is fixedly connected with a threaded cylinder, the outer side of the second carbon fiber pipe is provided with threads, and the threaded cylinder is rotatably connected with the second carbon fiber pipe through the threads.

Compared with the prior art, the beneficial effects of the utility model are that:

1. the utility model discloses in, through the first carbon fiber pipe, second carbon fiber pipe, a screw thread section of thick bamboo, change and solid fixed ring that set up, the user adjusts the distance between first carbon fiber pipe and the second carbon fiber according to the service environment of difference, adjusts the distance of unmanned aerial vehicle bottom and ground contact through first carbon fiber and second carbon fiber, avoids meetting the ground of unevenness such as stone and leads to unmanned aerial vehicle's bottom and stone to bump and cause unmanned aerial vehicle's damage.

2. The utility model discloses in, through the fixed buckle that sets up, the carbon fiber tube support, the screw cap, first carbon fiber tube and anti-skidding cushion, according to the structure of the fixed buckle of undercarriage plug, the portable advantage of plug-and-play has been embodied, revolution mechanic through the screw hole, can the fifty percent discount is received when not using, can reduce certain space of standing when transporting again, first carbon fiber tube and second carbon fiber tube can improve the stability of standing, the anti-skidding cushion of carbon fiber tube base has improved the frictional force to ground, the reinforcing stability, it is four foot undercarriages to modify traditional both sides undercarriage, thereby realize adapting to more topography, improve emergent work efficiency, reinforcing aircraft stability.

Drawings

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

fig. 2 is a schematic diagram of the explosion structure of the present invention;

FIG. 3 is a schematic view of the installation structure of the present invention during folding;

fig. 4 is a schematic view of the mounting structure of the fixing ring of the present invention;

fig. 5 is a schematic view of the installation structure of the present invention in use.

In the figure: 1-landing gear plug, 2-fixing buckle, 3-M2 screw hole, 4-first spiral thread, 5-M2 headless screw, 6-carbon fiber tube bracket, 7-second spiral thread, 8-screw cap, 9-first carbon fiber tube, 10-carbon fiber tube base, 11-antiskid rubber pad, 12-second carbon fiber tube, 13-screw cylinder, 14-rotating ring and 15-fixing ring.

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, the present invention provides a technical solution:

a supporting and landing frame of a Dajiang longitude and latitude M210V2 unmanned aerial vehicle comprises an anti-skidding rubber mat 11 and a carbon fiber tube base 10, wherein the top end of the anti-skidding rubber mat 11 is fixedly connected with the carbon fiber tube base 10, the anti-skidding rubber mat 11 of the carbon fiber tube base 10 improves the friction force to the ground and enhances the stability, the outer side of the carbon fiber tube base 10 is fixedly connected with a second carbon fiber tube 12, a first carbon fiber tube 9 is arranged above the second carbon fiber tube 12, landing gear plugs 1 are clamped on the inner side of the top end of the first carbon fiber tube 9, the number of the landing gear plugs 1 is four in total, the landing gear plugs are uniformly distributed around the bottom end of the unmanned aerial vehicle, the landing gear on the two sides is modified into four-leg landing gear, the landing gear is adapted to more terrains, the emergency work efficiency is improved, the stability of the aircraft is enhanced, the carbon fiber tube support 6 is, and the inner side of the carbon fiber tube bracket 6 is provided with the M2 headless screw 5, if folding is to be carried out, the M2 screw hole 3 and the M2 headless screw 5 can be combined with the carbon fiber tube bracket 6, thereby realizing a folding effect of rotating 180 degrees by taking the M2 headless screw 5 as an axis.

The front end of the first carbon fiber pipe 9 is provided with a second spiral thread 7, the rear end of the landing gear plug 1 is provided with a first spiral thread 4, the outer side of the first carbon fiber pipe 9 is provided with a threaded cap 8, the threaded cap 8 is in threaded connection with the second spiral thread 7 and the first spiral thread 4, the first carbon fiber pipe 9 and the landing gear plug 1 can be fixedly connected together through the threaded cap 8, meanwhile, the installation and the disassembly of the device are facilitated, the inner side of the landing gear plug 1 is fixedly connected with a fixed buckle 2, the fixed buckle 2 is positioned at the vertical central line of the landing gear plug 1, the landing gear of the unmanned aerial vehicle is connected to the antenna of the large Xinjiang longitude and latitude M210V2 unmanned aerial vehicle through the landing gear plug 1, the stability of the combination of the fixed buckle 2 and the landing gear is enhanced, the outer side of the first carbon fiber pipe 9 is fixedly connected with a fixed ring 15, the outer side of the fixed, can realize spacing to change 14 through solid fixed ring 15, the outside fixedly connected with screw thread section of thick bamboo 13 of change 14, the outside of second carbon fiber pipe 12 is provided with the screw thread, and screw thread section of thick bamboo 13 rotates with second carbon fiber pipe 12 through the screw thread to be connected, can adjust the distance between second carbon fiber pipe 12 and the first carbon fiber pipe 9 through screw thread section of thick bamboo 13.

The working process is as follows: in the utility model, when in specific use, the staff clamps the landing gear plug 1 and the carbon fiber tube support 6 together, then the staff rotates the screw cap 8 clockwise, the screw cap 8 fixes the carbon fiber tube support 6 and the landing gear plug 1 together through the first spiral thread 4 and the second spiral thread 7, simultaneously the M2 headless screw 5 is inserted into the inner side of the M2 screw hole 3 inside the carbon fiber tube support 6, simultaneously the staff adjusts the distance between the first carbon fiber tube 9 and the second carbon fiber tube 12 according to the ground condition, the staff rotates the screw barrel 13, the screw barrel 13 rotates outside the fixed ring 15 through the rotating ring 14, the second carbon fiber tube 12 is far away from the first carbon fiber tube 9 through the rotation of the screw barrel 13, until the distance between the first carbon fiber tube 9 and the second carbon fiber tube 12 is proper, then the landing gear of the unmanned aerial vehicle of the Xinjiang Longitudi M210V2 is connected to the antenna of the Xinjiang Longitudi M210V2 through the landing gear plug 1, when the fixing buckle 2 is combined, the combination stability of the fixing buckle and the fixing buckle is enhanced, as shown in fig. 1, if folding is to be carried out, the M2 screw hole 3 and the combination of the M2 headless screw 5 and the carbon fiber tube bracket 6 can be realized, so that a folding effect of rotating 180 degrees by taking the M2 headless screw 5 as an axis is realized, as shown in fig. 3.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (5)

1. The utility model provides a frame is played in support of big jiangqing M210V2 unmanned aerial vehicle, includes anti-skidding cushion (11) and carbon fiber tube base (10), its characterized in that: the top fixedly connected with carbon fiber tube base (10) of anti-skidding cushion (11), the outside fixedly connected with second carbon fiber tube (12) of carbon fiber tube base (10), the top of second carbon fiber tube (12) is provided with first carbon fiber tube (9), the inboard block in top of first carbon fiber tube (9) has undercarriage plug (1), the front end fixedly connected with carbon fiber tube support (6) of first carbon fiber tube (9), and the inboard of carbon fiber tube support (6) is provided with M2 headless screw (5).

2. The supporting landing gear of a Dajiang longitude and latitude M210V2 unmanned aerial vehicle of claim 1, wherein: the front end of the first carbon fiber pipe (9) is provided with a second spiral thread (7), the rear end of the undercarriage plug (1) is provided with a first spiral thread (4), the outer side of the first carbon fiber pipe (9) is provided with a threaded cap (8), and the threaded cap (8) is in threaded connection with the second spiral thread (7) and the first spiral thread (4).

3. The supporting landing gear of a Dajiang longitude and latitude M210V2 unmanned aerial vehicle of claim 1, wherein: the inner side of the undercarriage plug (1) is fixedly connected with a fixing buckle (2), and the fixing buckle (2) is located on the vertical center line of the undercarriage plug (1).

4. The supporting landing gear of a Dajiang longitude and latitude M210V2 unmanned aerial vehicle of claim 1, wherein: the outside fixedly connected with solid fixed ring (15) of first carbon fiber pipe (9), the outside of solid fixed ring (15) is rotated and is connected with swivel (14).

5. The supporting landing gear of a Dajiang longitude and latitude M210V2 unmanned aerial vehicle as claimed in claim 4, wherein: the outer side of the rotating ring (14) is fixedly connected with a threaded cylinder (13), the outer side of the second carbon fiber pipe (12) is provided with threads, and the threaded cylinder (13) is rotatably connected with the second carbon fiber pipe (12) through the threads.

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