CN214296416U - Soft unmanned aerial vehicle frame - Google Patents

Abstract

The utility model relates to a software unmanned aerial vehicle frame, including the gasbag, the sealing plug, upper fixed ring, lower fixed ring, the horn, the hinge, the buckle, elastic rod and couple, the gasbag is cylindrical, the gasbag top is equipped with the business turn over gas pocket, be equipped with the sealing plug in the business turn over gas pocket, gasbag outer wall upper end and lower extreme are equipped with upper fixed ring and lower fixed ring respectively, upper fixed ring top is connected with many horn one end tops through the hinge respectively all around, the hinged end bottom of many horns all is equipped with the buckle, the equal horizontal installation in upper fixed ring bottom and the relative position of horn has the elastic rod. The utility model has the advantages that: this kind of software unmanned aerial vehicle frame, when not using, can pull the elastic rod and make the elastic rod extension to make the couple break away from the buckle, then fold the horn to the gasbag top, then open the sealing plug at gasbag top, emit the gas in the gasbag, can fold software unmanned aerial vehicle, conveniently accomodate and carry software unmanned aerial vehicle.

Description

Soft unmanned aerial vehicle frame

Technical Field

The utility model relates to a software unmanned aerial vehicle technical field especially relates to a software unmanned aerial vehicle frame.

Background

The soft unmanned aerial vehicle is an unmanned aerial vehicle without a hard framework, is formed by inflating an air bag, has strong loading capacity and high endurance compared with the traditional unmanned aerial vehicle, can fly at ultra-low speed and ultra-low altitude, has good elasticity, is impact-resistant and is not damaged, and can be used for aerial photography, aerial survey, remote sensing and other purposes. The unmanned soft frame is a bearing platform of the unmanned soft vehicle, and all equipment is borne by the frame, so that the quality of the unmanned aerial vehicle frame determines the quality of the unmanned aerial vehicle to a great extent. The quality of one frame is measured, and the aspects of firmness, convenience in use, reasonability in component installation and the like can be considered. However, the existing racks are often inconvenient to store and carry.

SUMMERY OF THE UTILITY MODEL

The utility model aims to solve the technical problem that a software unmanned aerial vehicle frame is provided, solve the not enough of prior art.

The utility model provides an above-mentioned technical problem's technical scheme as follows: the utility model provides a software unmanned aerial vehicle frame, includes gasbag, sealing plug, upper fixed ring, lower fixed ring, horn, hinge, buckle, elastic rod and couple, the gasbag is cylindrical, the gasbag top is equipped with the business turn over gas pocket, be equipped with in the business turn over gas pocket the sealing plug, gasbag outer wall upper end and lower extreme are equipped with respectively upper fixed ring with lower fixed ring, the upper fixed ring top passes through respectively all around hinge and many horn one end top is connected, many the hinged end bottom of horn all is equipped with the buckle, upper fixed ring bottom with the equal horizontal installation in position that the horn is relative has the elastic rod, the elastic rod is kept away from upper fixed ring's one end install with buckle matched with the couple.

The utility model has the advantages that: this kind of software unmanned aerial vehicle frame, when not using, can pull the elastic rod and make the elastic rod extension to make the couple break away from the buckle, then fold the horn to the gasbag top, then open the sealing plug at gasbag top, emit the gas in the gasbag, can fold software unmanned aerial vehicle, conveniently accomodate and carry software unmanned aerial vehicle.

Further: the elastic rod comprises a sleeve, a spring and an inner rod, the sleeve is installed at the bottom of the upper fixing ring, the spring is arranged in the sleeve, one end of the inner rod stretches into the sleeve and is connected with one end of the spring, the other end of the spring is connected with the sleeve, and the hook is installed at the other end of the inner rod.

The beneficial effects of the further scheme are as follows: the elastic rod is simple in structure and good in elastic performance.

Further: the sleeve wall surface is provided with a strip-shaped sliding hole in the axial direction of the sleeve, the outer wall of the inner rod is provided with a poke rod at the position opposite to the sliding hole, and one end, far away from the inner rod, of the poke rod penetrates through the sliding hole.

The beneficial effects of the further scheme are as follows: the inner rod can be moved in the sleeve by stirring the poke rod, the length of the elastic rod is adjusted, and the operation is convenient.

Further: and a sponge sleeve is arranged on one part of the poke rod outside the sliding hole.

The beneficial effects of the further scheme are as follows: the sponge sleeve can make a user feel more comfortable when the user stirs the poke rod.

Further: the top of the air bag is provided with a first magnet piece at the position opposite to the horn, and the top of the horn is provided with a second magnet piece.

The beneficial effects of the further scheme are as follows: when the horn rotated to the gasbag top, can fix the horn at the gasbag top through first magnet piece and the cooperation of second magnet piece to can prevent to take place to remove at the in-process horn of carrying.

Further: the outer wall of the upper fixing ring is provided with a first U-shaped handle, and the position, opposite to the first U-shaped handle, of the lower fixing ring is provided with a second U-shaped handle.

The beneficial effects of the further scheme are as follows: after software unmanned aerial vehicle is folding, first U-shaped handle is close to second U-shaped handle, when needs carry, and the first in command and the second in command are held to usable hand, conveniently carry software unmanned aerial vehicle.

Drawings

Fig. 1 is a schematic view of a soft unmanned aerial vehicle frame structure according to an embodiment of the present invention;

fig. 2 is a front view of a frame structure of a soft unmanned aerial vehicle according to an embodiment of the present invention;

FIG. 3 is an enlarged view of FIG. 2 at A;

in the figure: 1. an air bag; 11. a first magnet piece; 2. a sealing plug; 3. an upper fixing ring; 31. a first U-shaped handle; 4. a lower fixing ring; 41. a second U-shaped handle; 5. a horn; 51. a second magnet piece; 6. A hinge; 7. a retaining ring; 8. an elastic rod; 81. a sleeve; 811. a slide hole; 82. a spring; 83. an inner rod; 831. a poke rod; 832 (g); a sponge sleeve; 9. and (4) hanging hooks.

Detailed Description

The principles and features of the present invention are described below in conjunction with the following drawings, the examples given are only intended to illustrate the present invention and are not intended to limit the scope of the present invention.

Example one

As shown in fig. 1-3, a soft unmanned aerial vehicle frame, including gasbag 1, sealing plug 2, upper fixed ring 3, lower fixed ring 4, horn 5, hinge 6, buckle 7, elastic rod 8 and couple 9, gasbag 1 is cylindrical, gasbag 1 top is equipped with the business turn over gas pocket, be equipped with sealing plug 2 in the business turn over gas pocket, gasbag 1 outer wall upper end and lower extreme are equipped with upper fixed ring 3 and lower fixed ring 4 respectively, upper fixed ring 3 top is connected with many horn 5 one end tops through hinge 6 respectively all around, the hinged end bottom of many horn 5 all is equipped with buckle 7, the equal horizontal installation elastic rod 8 in the position that upper fixed ring 3 bottom and horn 5 are relative, elastic rod 8 keeps away from the one end of upper fixed ring 3 and installs couple 9 with buckle 7 matched with.

Example two

On the basis of the first embodiment, the elastic rod 8 comprises a sleeve 81, a spring 82 and an inner rod 83, the sleeve 81 is installed at the bottom of the upper fixing ring 3, the spring 82 is arranged in the sleeve 81, one end of the inner rod 83 extends into the sleeve 81 and is connected with one end of the spring 82, the other end of the spring 82 is connected with the sleeve 81, and the hook 9 is installed at the other end of the inner rod 83.

The sleeve 81 wall is equipped with bar sliding hole 811 along sleeve 81 axial direction, the position that interior pole 83 outer wall and sliding hole are relative is equipped with poker rod 831, the one end that poker rod 831 is kept away from interior pole 83 passes sliding hole 811, can make interior pole 83 remove in sleeve 81 through stirring poker rod 831, adjust the length of elastic rod 8, and convenient operation is equipped with sponge cover 832 on the part that poker rod 831 is located the sliding hole 811, sponge cover 832 can make the user feel more comfortable when stirring poker rod 831.

EXAMPLE III

On the basis of the second embodiment, the top of the air bag 1 is provided with the first magnet piece 11 at a position opposite to each horn 5, the top of each horn 5 is provided with the second magnet piece 51, when the horn 5 rotates to the top of the air bag 1, the horn 5 can be fixed at the top of the air bag 1 through the cooperation of the first magnet piece 11 and the second magnet piece 51, and therefore the horn 5 can be prevented from moving in the carrying process.

Example four

On the basis of the third embodiment, the outer wall of the upper fixing ring 3 is provided with a first U-shaped handle 31, the position of the lower fixing ring 4 opposite to the first U-shaped handle 31 is provided with a second U-shaped handle 41, when the soft unmanned aerial vehicle is folded, the first U-shaped handle 31 is close to the second U-shaped handle 41, and when the soft unmanned aerial vehicle needs to be carried, the first handle 31 and the second handle 41 can be held by hands, so that the soft unmanned aerial vehicle is convenient to carry.

In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential", and the like, indicate the orientation or positional relationship indicated based on the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.

Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In the description of the present invention, "a plurality" means at least two, e.g., two, three, etc., unless specifically limited otherwise.

In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; they may be directly connected or indirectly connected through intervening media, or they may be connected internally or in any other suitable relationship, unless expressly stated otherwise. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.

In the present application, unless expressly stated or limited otherwise, the first feature may be directly on or directly under the second feature or indirectly via intermediate members. Also, a first feature "on," "over," and "above" a second feature may be directly or diagonally above the second feature, or may simply indicate that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature may be directly under or obliquely under the first feature, or may simply mean that the first feature is at a lesser elevation than the second feature.

In the description herein, references to the description of the term "one embodiment," "some embodiments," "an example," "a specific example," or "some examples," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above are not necessarily intended to refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples. Furthermore, various embodiments or examples and features of different embodiments or examples described in this specification can be combined and combined by one skilled in the art without contradiction.

Although embodiments of the present invention have been shown and described, it is understood that the above embodiments are exemplary and should not be construed as limiting the present invention, and that variations, modifications, substitutions and alterations can be made to the above embodiments by those of ordinary skill in the art without departing from the scope of the present invention.

Claims (6)

1. The soft unmanned aerial vehicle frame is characterized by comprising an air bag (1), a sealing plug (2), an upper fixing ring (3), a lower fixing ring (4), a horn (5), a hinge (6), a retaining ring (7), an elastic rod (8) and a hook (9), wherein the air bag (1) is cylindrical, an air inlet and outlet hole is formed in the top of the air bag (1), the sealing plug (2) is arranged in the air inlet and outlet hole, the upper fixing ring (3) and the lower fixing ring (4) are respectively arranged at the upper end and the lower end of the outer wall of the air bag (1), the periphery of the top of the upper fixing ring (3) is respectively connected with the tops of one ends of the horns (5) through the hinge (6), the bottoms of hinged ends of the horns (5) are respectively provided with the retaining ring (7), and the elastic rod (8) is horizontally arranged at the bottom of the upper fixing ring (3) and the position opposite to the horn (5), one end of the elastic rod (8) far away from the upper fixing ring (3) is provided with the hook (9) matched with the retaining ring (7).

2. The unmanned aerial vehicle frame of claim 1, wherein the elastic rod (8) comprises a sleeve (81), a spring (82) and an inner rod (83), the sleeve (81) is mounted at the bottom of the upper fixing ring (3), the spring (82) is arranged in the sleeve (81), one end of the inner rod (83) extends into the sleeve (81) and is connected with one end of the spring (82), the other end of the spring (82) is connected with the sleeve (81), and the hook (9) is mounted at the other end of the inner rod (83).

3. The unmanned aerial vehicle frame of claim 2, wherein the wall surface of the sleeve (81) is provided with a strip-shaped sliding hole (811) along the axial direction of the sleeve (81), the outer wall of the inner rod (83) is provided with a poke rod (831) at a position opposite to the sliding hole, and one end of the poke rod (831), which is far away from the inner rod (83), penetrates through the sliding hole (811).

4. The unmanned aerial vehicle of claim 3, wherein a portion of the poke rod (831) outside the sliding hole (811) is provided with a sponge sleeve (832).

5. A soft unmanned aerial vehicle frame according to claim 1, wherein a first magnet piece (11) is arranged at the top of the air bag (1) opposite to each horn (5), and a second magnet piece (51) is arranged at the top of each horn (5).

6. A soft unmanned aerial vehicle frame according to claim 1, wherein the outer wall of the upper fixing ring (3) is provided with a first U-shaped handle (31), and the position of the lower fixing ring (4) opposite to the first U-shaped handle (31) is provided with a second U-shaped handle (41).

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