CN217805233U

CN217805233U - Six wing high strength frames for unmanned aerial vehicle

Info

Publication number: CN217805233U
Application number: CN202221181574.XU
Authority: CN
Inventors: 韦志军; 黄荣; 曾俊喆
Original assignee: Guangxi Dongxiang Technology Co ltd
Current assignee: Guangxi Dongxiang Technology Co ltd
Priority date: 2022-05-17
Filing date: 2022-05-17
Publication date: 2022-11-15
Anticipated expiration: 2032-05-17

Abstract

The utility model discloses a six wing high strength frames for unmanned aerial vehicle, the reciprocating impact tunnel drilling machine comprises a machine body, the fixed a plurality of electronic jars that are provided with in the fuselage outside, it is a plurality of electronic jar top is fixed to be provided with iron buckle, a plurality of electronic jar bottom mounting is provided with down iron buckle, and is a plurality of go up iron buckle and iron buckle one end handing-over department down by hinge connection, a plurality of go up iron buckle and iron buckle other end handing-over department down by the bolt fastening, a plurality of go up iron buckle top center department and fix and be provided with the mount, the fixed block that is provided with in fuselage top center department, the fixed block outer end is fixed and is provided with a plurality of anchor braces, and a plurality of anchor braces other end fixed connection mounts, two the fixed fixer that is provided with in telescopic link center department, two the telescopic link bottom mounting is provided with the foot rest. Through the device's use, electronic jar drives the wing base, stretches out during the use, not the time spent pack up, goes up the iron buckle and passes through hinge connection with lower iron buckle, makes mount convenient to detach and installation.

Description

Six wing high strength frames for unmanned aerial vehicle

Technical Field

The utility model relates to a frame field for the unmanned aerial vehicle especially relates to a six wing high strength frames for unmanned aerial vehicle.

Background

At present unmanned aerial vehicle includes fuselage, horn and frame, and traditional frame is square positive integral type structure usually, and not only bulk strength is lower, is not convenient for accomodate when not using moreover.

Current patent (CN 207875969U) discloses an unmanned aerial vehicle frame, including control box, undercarriage, support arm, connection subplate and reinforcement, the undercarriage set up in the bottom of control box, the one end of support arm with the control box is connected, and the other end is the free end, the quantity of support arm is many, many the support arm equipartition set up in around the control box, every the free end of support arm all is equipped with one connect the subplate, adjacent two connect and pass through between the subplate the reinforcement is connected. Its simple structure, it is convenient to make, and the cost of manufacture is low, and weight is lighter, and the free end of two adjacent support arms links together through the reinforcement, has improved the structural strength of frame greatly, but also can avoid the support arm to take place the swing, has improved the stability of unmanned aerial vehicle flight greatly.

However, this device still has some problems: the device frame intensity is not enough when using for unmanned aerial vehicle is relatively poor at flight in-process stability, makes unmanned aerial vehicle the shake can appear in shooting in-process picture, and is very inconvenient.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the defects existing in the prior art and providing a high-strength frame for a six-wing unmanned aerial vehicle.

In order to realize the purpose, the utility model adopts the following technical scheme: a high-strength rack for a six-wing unmanned aerial vehicle comprises a machine body, wherein a plurality of electric cylinders are fixedly arranged on the outer side of the machine body, upper iron buckles are fixedly arranged at the top ends of the electric cylinders, lower iron buckles are fixedly arranged at the bottom ends of the electric cylinders, one ends of the upper iron buckles and one ends of the lower iron buckles are connected through hinges, and the other ends of the upper iron buckles and the lower iron buckles are fixed through bolts;

a plurality of go up the fixed mount that is provided with in iron knot top center department, fuselage top center department is fixed and is provided with the fixed block, the fixed a plurality of reinforcement frame that are provided with in fixed block outer end, and a plurality of reinforcement frame other end fixed connection mount, two the fixed fixer that is provided with in telescopic link center department, two the telescopic link bottom mounting is provided with the foot rest.

As a further description of the above technical solution:

the fixing frames and the reinforcing frame are integrated.

As a further description of the above technical solution:

the center of the bottom end of the machine body is fixedly provided with a cloud pedestal.

As a further description of the above technical solution:

the fixing frames are hexagonal.

As a further description of the above technical solution:

and the reinforcing frames and the fixing frames are umbrella-shaped.

As a further description of the above technical solution:

and anti-skidding sleeves are fixedly arranged at the front end and the rear end of each of the two foot stands.

As a further description of the above technical solution:

and a wing base is fixedly arranged at the outer end of the electric cylinder.

As a further description of the above technical solution:

the machine body is made of carbon fiber composite materials.

The utility model discloses following beneficial effect has:

in the utility model, electronic jar upper end is equipped with the iron and detains, and electronic jar lower extreme is equipped with down the iron and detains, goes up the iron and detains and detain through hinge connection with lower iron, is convenient for fix on electronic jar, goes up the iron and detains the top and be equipped with the mount, makes wholly more stable.

In the utility model, through electronic jar function, can make electronic jar drive wing base and contract, stretch out during the use, not the time spent pack up, be convenient for accomodate, occupation space is little.

Drawings

Fig. 1 is a perspective view of a high-strength frame for a six-wing unmanned aerial vehicle according to the present invention;

fig. 2 is a top view of an electric cylinder of a high-strength frame for a six-wing unmanned aerial vehicle according to the present invention;

fig. 3 is a retracted top view of an electric cylinder of a high-strength frame for a six-wing unmanned aerial vehicle according to the present invention;

fig. 4 is a perspective view of the upper iron buckle and the lower iron buckle of the high-strength frame for the six-wing unmanned aerial vehicle provided by the utility model.

Illustration of the drawings:

1. a body; 2. an electric cylinder; 3. a cloud pedestal; 4. mounting an iron buckle; 5. a wing base; 6. a fixed block; 7. a reinforcing frame; 8. a fixed mount; 9. a telescopic rod; 10. a holder; 11. a foot rest; 12. an anti-slip sleeve; 13. a lower iron buckle; 14. and (4) bolts.

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.

In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific 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 meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.

Referring to fig. 1-4, the present invention provides an embodiment: the utility model provides a six wing high strength frames for unmanned aerial vehicle, which comprises a

fuselage

1, 1 outside of fuselage is fixed to be provided with a plurality of electronic jars 2, the fixed wing base 5 that is provided with in 2 outer ends of electronic jar, electronic jar 2 drives wing base 5 and removes, stretch out during the use, not the time spent pack up, convenient to accomodate, 2 fixed being provided with in top of electronic

jar iron buckle

4, 2 bottom mounting of electronic jar are provided with down iron buckle 13, it detains 4 and 13 one end handing-over department of iron buckle down by hinge connection to go up iron, it detains 4 and 13 other end handing-over department of iron buckle down and is fixed by bolt 14, be convenient for installation and the dismantlement of mount 8.

Go up the fixed mount 8 that is provided with in 4 top center departments of iron buckle, the fixed block 6 that is provided with in 1 top center department of fuselage, the fixed a plurality of anchor strut 7 that are provided with in 6 outer ends of fixed block, and anchor strut 7 other end fixed connection mount 8, mount 8 is hexagonal shape, mount 8 makes electronic jar 2 connect stably, mount 8 and anchor strut 7 formula as an organic whole, the integral type is convenient for dismantle and the installation, make whole fuselage 1 more firm, anchor strut 7 and mount 8 are umbelliform, umbelliform makes whole fuselage 1 firm, the fixed fixer 10 that is provided with in 9 center departments of telescopic link, be convenient for fix telescopic link 9, the fixed foot rest 11 that is provided with in telescopic link 9 bottom, both ends are fixed around the foot rest 11 and are provided with antiskid cover 12.

The center of the bottom end of the machine body 1 is fixedly provided with a cloud pedestal 3, so that the camera is stabilized on the cloud pedestal.

The fuselage 1 is made of carbon fiber composite material, and the carbon fiber composite material has high specific strength, good designability, good structural dimension stability, good fatigue fracture resistance and can be integrally formed in a large area.

The working principle is as follows: during the use, through electronic jar 2 operation, make electronic jar 2 drive wing base 5 and stretch out, then with last iron buckle 4 and lower iron buckle 13 with bolt 14 fix on electronic jar 2, make mount 8 integral erection on fuselage 1, then make telescopic link 9 expand through fixer 10.

When the airplane wing fixing device is not used, the bolt 14 for fixing the upper iron buckle 4 and the lower iron buckle 13 is dismounted, the fixing frame 8 is dismounted integrally, then the electric cylinder 2 drives the wing base 5 to be retracted, and then the telescopic rod 9 is retracted through the fixer 10.

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 and variations can be made in the embodiments or in part of the technical features of the embodiments without departing from the spirit and the scope of the invention.

Claims

1. The utility model provides a six wing high strength frames for unmanned aerial vehicle, includes fuselage (1), its characterized in that: a plurality of electric cylinders (2) are fixedly arranged on the outer side of the machine body (1), upper iron buckles (4) are fixedly arranged at the top ends of the electric cylinders (2), lower iron buckles (13) are fixedly arranged at the bottom ends of the electric cylinders (2), the joints of the upper iron buckles (4) and one ends of the lower iron buckles (13) are connected through hinges, and the joints of the upper iron buckles (4) and the other ends of the lower iron buckles (13) are fixed through bolts (14);

it is a plurality of go up iron buckle (4) top center department and fix and be provided with mount (8), fuselage (1) top center department is fixed and is provided with fixed block (6), fixed block (6) outer end is fixed and is provided with a plurality of reinforcement frames (7), and a plurality of reinforcement frame (7) other end fixed connection mount (8), and two telescopic link (9) center departments are fixed and are provided with fixer (10), two telescopic link (9) bottom mounting is provided with foot rest (11).

2. The high-strength frame for the six-wing unmanned aerial vehicle according to claim 1, wherein: the fixing frames (8) and the reinforcing frame (7) are integrated.

3. The high-strength frame for the six-wing unmanned aerial vehicle according to claim 1, wherein: fuselage (1) bottom center department is fixed and is provided with cloud pedestal (3).

4. The high-strength frame for the six-wing unmanned aerial vehicle according to claim 1, wherein: the plurality of fixing frames (8) are hexagonal.

5. The high-strength frame for the six-wing unmanned aerial vehicle according to claim 1, wherein: the reinforcing frames (7) and the fixing frames (8) are umbrella-shaped.

6. The high-strength frame for the six-wing unmanned aerial vehicle according to claim 1, wherein: anti-skidding sleeves (12) are fixedly arranged at the front end and the rear end of each of the two foot stands (11).

7. The high-strength frame for the six-wing unmanned aerial vehicle according to claim 1, wherein: the outer ends of the electric cylinders (2) are fixedly provided with wing bases (5).

8. The high-strength frame for the six-wing unmanned aerial vehicle according to claim 1, wherein: the machine body (1) is made of carbon fiber composite materials.