CN214824238U - Unmanned aerial vehicle field launching support - Google Patents

Abstract

The utility model belongs to the technical field of unmanned aerial vehicle equipment technique and specifically relates to indicate an unmanned aerial vehicle field transmission support. It has solved the relatively poor problem of current unmanned aerial vehicle support stability. It includes the support body, is equipped with the roof on the support body, and the one end of support body bottom articulates there is the journal angle, and the other end of support body bottom is equipped with the spliced pole, and the bottom of spliced pole has linked firmly expanding spring, and expanding spring's bottom has linked firmly the support, is equipped with the guiding mechanism that leads to the moving direction of support between support and the spliced pole. The utility model discloses a guiding mechanism drives the support and removes, changes the relative position between spliced pole and the support to support the spliced pole through expanding spring, improve the stability of placing of support, place unmanned aerial vehicle on the roof at last, do benefit to fixed transmission support, easily launch unmanned aerial vehicle, stability is high.

Description

Unmanned aerial vehicle field launching support

Technical Field

The utility model belongs to the technical field of unmanned aerial vehicle equipment technique and specifically relates to indicate an unmanned aerial vehicle field transmission support.

Background

Unmanned aerial vehicle is unmanned aircraft promptly, it is the unmanned aircraft that one kind utilizes radio remote control equipment and self-contained program control device to control, unmanned aircraft can divide into many rotors and fixed wing two kinds according to the structure, wherein fixed wing unmanned aerial vehicle is owing to have advantages such as long flight distance, the area of cruising, the flying speed is fast, flight height is high, multi-purpose in field work, for example, forest fire tours, topography survey etc. fixed wing unmanned aerial vehicle's transmission generally all needs fixed emission support, present ejection frame is only ejection angle, ejection force is adjustable, can also fold the transportation.

However, because the field terrain environment is complex, the common launching cradle cannot adapt to complex terrain, the stability of the cradle is poor, and the launching cradle cannot be fixed, so that the launching of the unmanned aerial vehicle is influenced.

Disclosure of Invention

The utility model provides an open-air transmission support of unmanned aerial vehicle does benefit to fixed transmission support, and stability is high.

In order to solve the technical problem, the utility model discloses a following technical scheme:

the utility model provides an unmanned aerial vehicle field launch support, includes the support body, be equipped with the roof on the support body, the one end of support body bottom articulates there is the journal angle, the other end of support body bottom is equipped with the spliced pole, the bottom of spliced pole has linked firmly expanding spring, expanding spring's bottom has linked firmly the support, be equipped with the guiding mechanism that leads to the moving direction of support between support and the spliced pole.

When placing the support, put it in waiting the launch area, support it through a supporting angle and support, according to the installation topography of reality, drive the support through guiding mechanism and remove, change the relative position between spliced pole and the support to support the spliced pole through expanding spring, improve the stability of placing of support, place unmanned aerial vehicle on the roof at last, do benefit to fixed launch support, easily launch unmanned aerial vehicle, stability is high.

Further, the top of roof is equipped with the support bar that two symmetries set up, these two it is connected with the pivot to rotate between the support bar, the pivot level sets up, the launch pad has been linked firmly in the pivot, the transmission mouth has been seted up at the top of launch pad, and the bottom surface level of this transmission mouth sets up, the focus of launch pad is located the pivot axle center under.

Put unmanned aerial vehicle in the bottom surface of this launching port, because the focus of launching pad is located the pivot axle center under, can ensure this bottom surface and be in the level setting always, be convenient for make unmanned aerial vehicle level put.

Furthermore, the bottom end of the launching platform is provided with a balancing weight which is positioned under the rotating shaft. The weight of launching pad is improved through the balancing weight that sets up, is convenient for ensure that the center of launching pad maintains under the pivot.

Further, guiding mechanism is including coaxial setting in the guide post of spliced pole bottom and the gib block that links firmly in the support top, set up the guide way of the axial extension along the spliced pole on the guide post, the both ends of guide way link up, gib block sliding fit is in the guide way.

When the support is placed, one end of the support is supported through the support, when the support abuts against the installation bottom surface, the guide strip is driven to slide in the guide groove, the relative position of the support and the connecting column is changed through self-adaption of the guide strip and the guide groove, the connecting column is supported through the telescopic spring, and the placing stability of the support is improved.

Furthermore, a placing head is arranged at the bottom end of the support, the cross section of the placing head is in an inverted round table shape, and the placing head is made of rubber; the support is convenient to support.

The utility model has the advantages that:

1. when placing the support, put it in waiting the launch area, support it through a supporting angle and support, according to the installation topography of reality, drive the support through guiding mechanism and remove, change the relative position between spliced pole and the support to support the spliced pole through expanding spring, improve the stability of placing of support, place unmanned aerial vehicle on the roof at last, do benefit to fixed launch support, easily launch unmanned aerial vehicle, stability is high.

2. Put unmanned aerial vehicle in the bottom surface of this launching port, because the focus of launching pad is located the pivot axle center under, can ensure this bottom surface and be in the level setting always, be convenient for make unmanned aerial vehicle level put.

3. Due to the fact that the guide post and the guide strip are arranged, when the support is placed, one end of the support is supported through the support, when the support abuts against the installation bottom surface, the guide strip is driven to slide in the guide groove, the relative position of the support and the connecting post is changed in a self-adaptive mode through the guide strip and the guide groove, the connecting post is supported through the telescopic spring, and the placing stability of the support is improved.

Drawings

Fig. 1 is a schematic structural view of the field launching cradle of the unmanned aerial vehicle;

FIG. 2 is a schematic diagram of a transmitting station;

FIG. 3 is a structural cross-sectional view of the field launch cradle of the present unmanned aerial vehicle;

description of reference numerals:

1. a stent body; 2. a top plate; 3. a supporting corner; 4. connecting columns; 5. a tension spring; 6. a support; 7. a supporting strip; 8. a rotating shaft; 9. a launch pad; 10. an emission port; 11. a balancing weight; 12. a guide post; 13. a guide strip; 14. a guide groove; 15. the head is placed.

Detailed Description

In order to facilitate understanding of those skilled in the art, the present invention will be further described with reference to the following examples and drawings, which are not intended to limit the present invention.

As shown in fig. 1, an open-air transmission support of unmanned aerial vehicle, including support body 1, be equipped with roof 2 on the support body 1, the one end of 1 bottom of support body articulates there is a journal angle 3, the other end of 1 bottom of support body is equipped with spliced pole 4, the bottom of spliced pole 4 has linked firmly expanding spring 5, expanding spring 5's bottom has linked firmly support 6, is equipped with the guiding mechanism that leads to the moving direction of support 6 between support 6 and the spliced pole 4.

As shown in fig. 1, in this embodiment, when placing the support, put it in waiting to launch the region, support it through journal angle 3 and support 6, according to actual installation topography, drive support 6 through guiding mechanism and remove, change the relative position between spliced pole 4 and the support 6, and support spliced pole 4 through expanding spring 5, improve the stability of placing of support, place unmanned aerial vehicle on roof 2 at last, do benefit to fixed launch support, easily launch unmanned aerial vehicle, stability is high.

As shown in fig. 1 and 3, in this embodiment, the top end of the top plate 2 is provided with two symmetrical support bars 7, the two support bars 7 are connected with a rotating shaft 8 in a rotating manner, the rotating shaft 8 is horizontally arranged, as shown in fig. 2, the rotating shaft 8 is fixedly connected with a transmitting table 9, the top of the transmitting table 9 is provided with a transmitting port 10, the bottom surface of the transmitting port 10 is horizontally arranged, and the center of gravity of the transmitting table 9 is located under the axis of the rotating shaft 8.

As shown in figures 1 and 3, the unmanned aerial vehicle is placed on the bottom surface of the launching port 10, and the center of gravity of the launching platform 9 is located under the axis of the rotating shaft 8, so that the bottom surface can be ensured to be always horizontally arranged, and the unmanned aerial vehicle can be conveniently horizontally placed.

As shown in fig. 1 and 3, in the present embodiment, a weight block 11 is disposed at the bottom end of the launching platform 9, and the weight block 11 is located right below the rotating shaft 8. The weight of the launching platform 9 is improved through the arranged balancing weight 11, and the center of the launching platform 9 is maintained under the rotating shaft 8 conveniently.

As shown in fig. 3, in this embodiment, the guiding mechanism includes a guiding post 12 coaxially disposed at the bottom of the connecting post 4 and a guiding strip 13 fixedly connected to the top of the support 6, a guiding groove 14 extending along the axial direction of the connecting post 4 is formed on the guiding post 12, two ends of the guiding groove 14 are through, and the guiding strip 13 is in sliding fit in the guiding groove 14.

As shown in fig. 1 and 3, when the bracket is placed, one end of the bracket is supported by the support 6, when the support 6 abuts against the installation bottom surface, the guide strip 13 is driven to slide in the guide groove 14, the relative position of the support 6 and the connecting column 4 is changed in a self-adaptive manner through the guide strip 13 and the guide groove 14, the connecting column 4 is supported by the telescopic spring 5, and the placing stability of the bracket is improved.

As shown in fig. 1 and 3, in this embodiment, a placing head 15 is disposed at the bottom end of the support 6, the cross section of the placing head 15 is in an inverted circular truncated cone shape, and the placing head 15 is made of rubber; the support is convenient to support.

All the technical features in the embodiment can be freely combined according to actual needs.

The above embodiments are preferred implementations of the present invention, and in addition, the present invention includes other implementations, and any obvious replacement is within the protection scope of the present invention without departing from the concept of the present invention.

Claims (5)

1. The utility model provides an unmanned aerial vehicle field launch support, includes support body (1), its characterized in that, be equipped with roof (2) on support body (1), the one end of support body (1) bottom articulates there is journal angle (3), the other end of support body (1) bottom is equipped with spliced pole (4), the bottom of spliced pole (4) has linked firmly expanding spring (5), the bottom of expanding spring (5) has linked firmly support (6), be equipped with the guiding mechanism that leads to the moving direction of support (6) between support (6) and spliced pole (4).

2. The field launch support of unmanned aerial vehicle as claimed in claim 1, characterized in that, the top of roof (2) is equipped with two support bars (7) of symmetrical setting, and these two are connected with pivot (8) between the support bar (7) are rotated, pivot (8) level setting, launch pad (9) has been linked firmly on pivot (8), launch port (10) have been seted up at the top of launch pad (9), and the bottom surface level setting of this launch port (10), the focus of launch pad (9) is located the pivot of pivot (8) under.

3. The unmanned aerial vehicle field launch stand of claim 2, characterized in that the bottom end of the launch pad (9) is provided with a counterweight (11), the counterweight (11) being located directly below the rotating shaft (8).

4. The unmanned aerial vehicle field emission support of claim 3, characterized in that, the guiding mechanism includes the guide post (12) of coaxial setting in spliced pole (4) bottom and the gib block (13) of linking firmly in support (6) top, seted up on the guide post (12) along the axially extended guide way (14) of spliced pole (4), the both ends of guide way (14) are link up, gib block (13) sliding fit is in guide way (14).

5. The unmanned aerial vehicle field emission support of claim 4, characterized in that, the bottom of support (6) is equipped with places head (15), place head (15) cross-section is the form of the frustum of a cone, place head (15) the material of material for rubber.

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