CN217198697U

CN217198697U - A test platform for unmanned aerial vehicle

Info

Publication number: CN217198697U
Application number: CN202221281783.1U
Authority: CN
Inventors: 刘彩云; 任雪峰
Original assignee: Beijing Zhuoyi Intelligent Technology Co Ltd
Current assignee: Beijing Zhuoyi Intelligent Technology Co Ltd
Priority date: 2022-05-25
Filing date: 2022-05-25
Publication date: 2022-08-16
Anticipated expiration: 2032-05-25

Abstract

The utility model relates to a test platform for unmanned aerial vehicle, including universal pivot, bracing piece, fixed station and base, unmanned aerial vehicle sets up the upper surface at the fixed station, and universal pivot is fixed to be set up in the lower surface of fixed station, the first end and the universal pivot fixed connection of bracing piece, the second end and the base fixed connection of bracing piece. The utility model discloses can satisfy unmanned aerial vehicle's every single move, driftage and flight tests such as rotation, guarantee test safety simultaneously.

Description

A test platform for unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned air vehicle technique field especially relates to a test platform for unmanned aerial vehicle.

Background

In recent years, four-rotor unmanned aerial vehicles gradually develop towards high efficiency and multi-functionalization direction due to advantages such as simple structure, flexible operation and the like, and are widely applied to the fields such as plant protection, electric power, fire control and movie and television. Because stability is not good enough and flight environment is complicated for four rotor unmanned aerial vehicle itself, the explosive accident often can appear in the in-process of debugging four rotor unmanned aerial vehicle, and the tester is in order to reduce casualties and unmanned aerial vehicle's loss, often utilizes the rope to pull unmanned aerial vehicle and tests, and unmanned aerial vehicle's performance can't be tested in comprehensive to this kind of test method, has very big potential safety hazard simultaneously.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a test platform for unmanned aerial vehicle to satisfy unmanned aerial vehicle's every single move, driftage and flight tests such as rotation, guarantee test safety simultaneously.

The purpose of the utility model is realized by adopting the following technical scheme. The foundation the utility model provides a test platform for unmanned aerial vehicle, including universal pivot, bracing piece, fixed station and base, unmanned aerial vehicle sets up the upper surface of fixed station, universal pivot fixed set up in the lower surface of fixed station, the first end of bracing piece with universal pivot fixed connection, the second end of bracing piece with base fixed connection.

In some embodiments, the test platform further comprises a side bar, a first end of the side bar being connected to the support bar and a second end of the side bar being connected to the base.

In some embodiments, the test platform further includes a fixing member, the fixing member is sleeved on the arm of the unmanned aerial vehicle, and the fixing member is used for fixing the unmanned aerial vehicle on the upper surface of the fixing table.

In some embodiments, the fixing member includes a pipe clamp and a connecting member, the pipe clamp is sleeved on the arm of the unmanned aerial vehicle, the connecting member is disposed on a side surface of the pipe clamp, and the connecting member is fixedly connected with the fixing table.

In some embodiments, the test platform further includes a balance bar, a first end of the balance bar is provided with a locking port, the locking port is locked on the lower surface of the fixing table, and a second end of the balance bar is rotatably connected to the base.

In some embodiments, the test platform further comprises an elastic connector, a first end of the elastic connector is connected to the balance bar, and a second end of the elastic connector is connected to the base.

In some embodiments, the resilient connector is a rubber band.

In some embodiments, the test platform further includes a protection frame, the protection frame is integrally formed with the base, and the protection frame is used for surrounding the unmanned aerial vehicle, the fixed station, the supporting rod and the balancing rod in the protection frame.

In some embodiments, a protective mesh is disposed on the protective frame.

In some embodiments, the tube clamp is integrally formed with the connector.

The beneficial effects of the utility model include at least:

1. the utility model discloses a set up unmanned aerial vehicle setting at the upper surface of fixed station, the first pot head of the fixed station of fixed station, bracing piece is put in the inside of universal pivot and with universal pivot fixed connection, the second end and the base fixed connection of bracing piece can make the fixed station rotatory or slope under the effect of cardan shaft to satisfy flight tests such as unmanned aerial vehicle every single move, driftage and rotation. Furthermore, the utility model discloses owing to avoid utilizing the rope to pull unmanned aerial vehicle and test, promoted the security of test.

2. The utility model discloses a set up the balancing pole to make the block mouth block of balancing pole fit in the position of keeping away from the bracing piece incline direction of fixed station lower surface, thereby make unmanned aerial vehicle reach the horizontality through the combined action of bracing piece and balancing pole before taking off.

3. The utility model discloses a bearer bar surrounds unmanned aerial vehicle, fixed station, bracing piece and balancing pole etc. and sets up the protecting wire net in inside and on the bearer bar, when unmanned aerial vehicle takes place to penetrate accidents such as oar, bearer bar and protecting wire net can play the effect of further protection personnel safety, avoid taking place the incident.

The foregoing description is only an overview of the technical solutions of the present invention, and in order to make the technical means of the present invention more clearly understood, the present invention may be implemented according to the content of the description, and in order to make the above and other objects, features, and advantages of the present invention more obvious and understandable, the following preferred embodiments are described in detail with reference to the accompanying drawings.

Drawings

Fig. 1 is a schematic structural diagram of a test platform for an unmanned aerial vehicle according to an embodiment of the present invention;

fig. 2 is another schematic structural diagram of the test platform for the unmanned aerial vehicle according to an embodiment of the present invention;

fig. 3 is another schematic structural diagram of a test platform for an unmanned aerial vehicle according to an embodiment of the present invention.

Detailed Description

In order to further explain the technical means of the present invention, the following detailed description of the specific implementation of the test platform for an unmanned aerial vehicle according to the present invention is provided with the accompanying drawings and the preferred embodiments. The following examples are merely for illustrating the technical solutions of the present invention more clearly, and therefore are only examples, and the scope of protection of the present invention is not limited thereby.

Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this application belongs; the terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the application; the terms "including" and "having," and any variations thereof, in the description and claims of this application and the description of the above figures are intended to cover non-exclusive inclusions.

In the description of the embodiments of the present application, the technical terms "first", "second", and the like are used only for distinguishing different objects, and are not to be construed as indicating or implying relative importance or implicitly indicating the number, specific order, or primary-secondary relationship of the technical features indicated.

As shown in fig. 1, fig. 2 and fig. 3, a test platform for unmanned aerial vehicle include universal pivot 1, bracing piece 2, fixed station 3 and base 4, unmanned aerial vehicle 93 sets up the upper surface at

fixed station

3, 1 fixed settings in the lower surface of fixed station 3 of universal pivot, specifically, 1 fixed settings in the central authorities of the lower surface of fixed station 3 of universal pivot and with the lower surface contact of fixed station 3,

universal pivot

1 and 3 accessible screw thread spare fixed connection of fixed station. The first end setting of bracing piece 2 is in the inside of universal rotating shaft 1, the first end of

bracing piece

2 and 1 accessible buckle of universal rotating shaft or screw fixed connection, the second end and the 4 fixed connection of base of bracing piece 2. A test platform for unmanned aerial vehicle still including the side lever 5 that the slope set up, the first end joint support pole 2 of side lever 5, base 4 is connected to the second end of side lever 5, side lever 5 is used for keeping the stability between bracing piece 2 and the base 4.

A test platform for unmanned aerial vehicle still include mounting 9, mounting 9 sets on each horn of unmanned aerial vehicle 93, the mounting is used for fixing unmanned aerial vehicle 93 at the upper surface of fixed station 3. The fixing member 9 includes a pipe clamp 91 and a connector 92, the pipe clamp 91 is sleeved on each arm of the unmanned aerial vehicle 93, the connector 92 is disposed on a side surface of the pipe clamp 91, the pipe clamp 91 and the connector 92 can be integrally formed, the connector 92 is configured into a cylindrical shape, and the connector 92 is fixedly connected with the fixing table 3 through a screw.

The utility model discloses a set up unmanned aerial vehicle 93 at the upper surface of

fixed station

3, 1 fixed settings in the lower surface of fixed station 3 of universal pivot, the first pot head of bracing piece 2 put in 1 inside of universal pivot and with 1 fixed connection of universal pivot, the second end and the 4 fixed connection of base of bracing piece 2, can make fixed station 3 rotatory or slope under the effect of universal shaft 1, thereby satisfy unmanned aerial vehicle every single move, flight tests such as driftage and rotation, unmanned aerial vehicle's flight test demand has greatly been satisfied. Furthermore, the utility model discloses owing to avoid utilizing the rope to pull unmanned aerial vehicle and test, promoted the security of test.

A test platform for unmanned aerial vehicle still include balancing pole 6, the first end of balancing pole 6 is provided with block mouth 61, block mouth 61 blocks in the position of keeping away from the center of 3 lower surfaces of fixed station, the second end rotation of balancing pole 6 is connected in base 4. Illustratively, the second end of the spreader beam 6 may be hinged to the base 4. A test platform for unmanned aerial vehicle still include elastic connection spare 7, the slope of elastic connection spare 7 sets up, elastic connection spare 7's first end is connected in balancing pole 6, elastic connection spare 7's second end is connected in base 4. The elastic connection 7 is preferably a rubber band.

When unmanned aerial vehicle is in quiescent condition, can lead to fixed station 3 and bracing piece 2 to be in small amplitude tilt state because self gravity, thereby be unfavorable for the test before unmanned aerial vehicle takes off, the utility model discloses a set up balancing pole 6, and make the block mouth 61 block of balancing pole 6 in the position of keeping away from 2 incline directions of bracing piece of fixed station 3 lower surface, thereby make unmanned aerial vehicle reach the horizontality through bracing piece 2 and balancing pole 6 combined action before taking off, again because balancing pole 6 passes through the block mouth with the lower surface of fixed station 3 and is connected, after unmanned aerial vehicle takes off, unmanned aerial vehicle and fixed station 3 can slightly incline, make the block mouth 61 of balancing pole 6 and the lower surface of fixed station 3 break away from the block, balancing pole 6 emptys under elastic connection 7's tensile force, unmanned aerial vehicle then can normally fly the test.

A test platform for unmanned aerial vehicle still include bearer bar 8, but bearer bar 8 and base 4 integrated into one piece, bearer bar 8 is used for surrounding unmanned aerial vehicle, fixed station 3, bracing piece 2 and balancing pole 6 etc. in inside, sets up protecting wire netting 81 on the bearer bar 8, when unmanned aerial vehicle takes place to penetrate accidents such as oar, bearer bar 8 and protecting wire netting 81 can play the effect of further protection personnel safety, avoid taking place the incident.

The previous description of the disclosed aspects is provided to enable any person skilled in the art to practice the present invention. Various modifications to these aspects will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other aspects without departing from the scope of the invention. Thus, the present invention is not intended to be limited to the aspects shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.

Claims

1. The utility model provides a test platform for unmanned aerial vehicle, its characterized in that, includes universal pivot, bracing piece, fixed station and base, unmanned aerial vehicle sets up the upper surface of fixed station, universal pivot fixed set up in the lower surface of fixed station, the first end of bracing piece with universal pivot fixed connection, the second end of bracing piece with base fixed connection.

2. The test platform for unmanned aerial vehicle of claim 1, further comprising a side bar, a first end of the side bar being connected to the support bar and a second end of the side bar being connected to the base.

3. The test platform for unmanned aerial vehicle of claim 1, further comprising a fixing member, wherein the fixing member is sleeved on the arm of the unmanned aerial vehicle, and the fixing member is used for fixing the unmanned aerial vehicle on the upper surface of the fixing table.

4. The test platform for the unmanned aerial vehicle of claim 3, wherein the fixing member comprises a pipe clamp and a connecting member, the pipe clamp is sleeved on the arm of the unmanned aerial vehicle, the connecting member is arranged on a side surface of the pipe clamp, and the connecting member is fixedly connected with the fixing platform.

5. The test platform for the unmanned aerial vehicle of claim 1, further comprising a balance bar, wherein a first end of the balance bar is provided with a clamping opening, the clamping opening is clamped on a lower surface of the fixing table, and a second end of the balance bar is rotatably connected to the base.

6. The test platform for unmanned aerial vehicle of claim 5, further comprising an elastic connector, a first end of the elastic connector being connected to the balance bar, and a second end of the elastic connector being connected to the base.

7. The test platform for unmanned aerial vehicle of claim 6, wherein the elastic connector is a rubber band.

8. The test platform for unmanned aerial vehicle of claim 5, further comprising a protective frame integrally formed with the base, the protective frame being configured to enclose the unmanned aerial vehicle, the stationary platen, the support bar, and the balance bar inside the protective frame.

9. The test platform for unmanned aerial vehicles of claim 8, wherein a protective mesh is disposed on the protective frame.

10. The test platform for unmanned aerial vehicle of claim 4, wherein the tube clamp is integrally formed with the connector.