CN221251762U - A test platform for unmanned aerial vehicle - Google Patents

Abstract

The utility model discloses a test platform for an unmanned aerial vehicle, which comprises a bottom plate, wherein two groups of support columns are fixedly connected to the upper surface of the bottom plate, top plates are fixedly connected to the top ends of the two groups of support columns together, bearings are fixedly inlaid on the upper surface of the top plates, and rotating rods are fixedly connected to the inner rings of the bearings. This device can blow to equipment inside through mounting panel and hair-dryer to the unmanned aerial vehicle carries out the anti-wind test to utilize the power that servo motor provided, can make bull stick, diaphragm and mounting panel rotate, make the blower can rotate to different positions, thereby carry out multi-angle anti-wind test to unmanned aerial vehicle, the wind-force that has solved being inconvenient for receiving each wind direction to unmanned aerial vehicle tests, lead to unmanned aerial vehicle in the inaccurate problem of in-process test data that carries out the test, can protect the staff through first foraminiferous protection shield and second foraminiferous protection shield, avoid unmanned aerial vehicle wind resistance performance relatively poor, cause the injury to the staff.

Description

A test platform for unmanned aerial vehicle

Technical Field

The utility model relates to the field of unmanned aerial vehicles, in particular to a test platform for an unmanned aerial vehicle.

Background

Along with development of unmanned aerial vehicle technology, more and more industries begin to adopt unmanned aerial vehicles to carry out related operations, so that testing of various parameters of the unmanned aerial vehicles becomes very important, such as parameters of vibration frequency, acceleration, flight frequency and the like of the unmanned aerial vehicles, and therefore, the unmanned aerial vehicles need to be tested by using a testing platform.

At present, after unmanned aerial vehicle production is accomplished, need use test platform to test unmanned aerial vehicle data, but the testing arrangement of present stage can test unmanned aerial vehicle when using, but still there are some shortages in the in-process of using, for example when testing, be inconvenient for to unmanned aerial vehicle under the wind-force of each wind direction test, lead to unmanned aerial vehicle in-process test data inaccurate that tests, for this reason, we propose a test platform for unmanned aerial vehicle to solve above-mentioned problem.

Disclosure of utility model

The utility model aims to provide a test platform for an unmanned aerial vehicle, so as to solve the problems in the background technology.

In order to achieve the above purpose, the present utility model provides the following technical solutions:

The utility model provides a test platform for unmanned aerial vehicle, includes the bottom plate, the last fixed surface of bottom plate is connected with two sets of support columns, two sets of the common fixedly connected with roof in top of support column, the last fixed surface of roof is inlayed and is had the bearing, the inner circle fixedly connected with bull stick of bearing, the last fixed surface of roof is connected with servo motor, servo motor's output and the top fixed connection of bull stick, the bottom surface fixedly connected with diaphragm of bull stick, the bottom surface fixedly connected with mounting panel of diaphragm, the fixed hair-dryer that inlays in the right flank of mounting panel, the last fixed surface of bottom plate is connected with unmanned aerial vehicle platform, the bottom surface fixedly connected with of roof two first foraminiferous protection shield and two second foraminiferous protection shield, two a side that the first foraminiferous protection shield is close to each other respectively with a side fixed connection that the mutual distance from of two sets of support columns, two sets of foraminiferous protection shield and the surface fixed connection that the second foraminiferous protection shield is close to each other.

In a further embodiment, a positioning ring is fixedly connected to the outer surface of the servo motor, and the bottom surface of the positioning ring is fixedly connected with the upper surface of the top plate.

In a further embodiment, an anti-slip pad is arranged above the bottom plate, and the bottom surface of the anti-slip pad is fixedly connected with the upper surface of the unmanned aerial vehicle platform.

In a further embodiment, the bottom surface of the cross plate is fixedly connected with a connecting block, and the left side surface of the connecting block is fixedly connected with the right side surface of the mounting plate.

In a further embodiment, an illuminating lamp is arranged above the bottom plate, and the upper surface of the illuminating lamp is fixedly connected with the bottom surface of the transverse plate.

In a further embodiment, an annular chute is formed in the bottom surface of the top plate, a sliding block is slidably connected to the inner wall of the annular chute, and the bottom surface of the sliding block is fixedly connected with the upper surface of the transverse plate.

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

This device can blow to equipment inside through being equipped with mounting panel and hair-dryer to the unmanned aerial vehicle carries out the wind-resistant test to utilize the power that servo motor provided, can make bull stick, diaphragm and mounting panel rotate, make the blower can rotate to different positions, thereby can carry out the multi-angle wind-resistant test to unmanned aerial vehicle, the wind-force that is inconvenient for receiving each wind direction to unmanned aerial vehicle is tested, lead to unmanned aerial vehicle in the inaccurate problem of in-process test data that carries out the test, can protect the staff through first foraminiferous protection shield and second foraminiferous protection shield, avoid unmanned aerial vehicle wind-resistant performance relatively poor, cause the injury to the staff.

Drawings

Fig. 1 is a schematic perspective view of a test platform for a drone.

Fig. 2 is a schematic perspective view of a side cross-sectional view of a test platform for an unmanned aerial vehicle.

Fig. 3 is a schematic perspective view of a side view of a test platform for a drone.

Fig. 4 is a schematic perspective view of a front cross-section of a test platform for an unmanned aerial vehicle.

In the figure: 1. a bottom plate; 2. a support column; 3. a control panel; 4. a first perforated protection plate; 5. a top plate; 6. a positioning ring; 7. a servo motor; 8. a second perforated protection plate; 9. an anti-slip pad; 10. an unmanned aerial vehicle platform; 11. a blower; 12. a mounting plate; 13. an annular chute; 14. a bearing; 15. a rotating rod; 16. a connecting block; 17. a slide block; 18. a cross plate; 19. an illuminating lamp.

Detailed Description

In the description of the present utility model, it should be understood that the terms "center", "longitudinal", "lateral", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are merely for convenience in describing the present utility model and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present utility model. Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first", "a second", etc. may explicitly or implicitly include one or more such feature. In the description of the present utility model, unless otherwise indicated, the meaning of "a plurality" is two or more.

In the description of the present utility model, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be either fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present utility model can be understood by those of ordinary skill in the art in a specific case.

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

Referring to fig. 1-4, in the utility model, a test platform for an unmanned aerial vehicle comprises a bottom plate 1, two groups of support columns 2 are fixedly connected to the upper surface of the bottom plate 1, top plates 5 are fixedly connected to the top ends of the two groups of support columns 2, bearings 14 are fixedly embedded on the upper surface of the top plates 5, a rotating rod 15 is fixedly connected to the inner ring of the bearings 14, a servo motor 7 is fixedly connected to the upper surface of the top plates 5, the output end of the servo motor 7 is fixedly connected to the top ends of the rotating rod 15, a transverse plate 18 is fixedly connected to the bottom surface of the rotating rod 15, a mounting plate 12 is fixedly connected to the bottom surface of the transverse plate 18, a blower 11 is fixedly embedded on the right side surface of the mounting plate 12, two first perforated protection plates 4 and two second perforated protection plates 8 are fixedly connected to the upper surface of the bottom plate 1, one side surfaces of the two first perforated protection plates 4 close to each other are fixedly connected to one side surfaces of the two groups of support columns 2, and one side surface of the two groups of second perforated protection plates 8 close to each other are fixedly connected to the outer surfaces of the two groups of support columns 2.

The outer surface fixedly connected with holding ring 6 of servo motor 7, the bottom surface of holding ring 6 and the last fixed surface of roof 5 are connected, can consolidate servo motor 7 through being equipped with holding ring 6, avoid servo motor 7 to appear not hard up, the top of bottom plate 1 is equipped with slipmat 9, the bottom surface of slipmat 9 and the last fixed surface of unmanned aerial vehicle platform 10 are connected, can increase unmanned aerial vehicle platform 10's frictional force through being equipped with slipmat 9, avoid unmanned aerial vehicle to appear sliding, the bottom surface fixedly connected with connecting block 16 of diaphragm 18, the left surface of connecting block 16 and the right side fixed connection of mounting panel 12, can consolidate mounting panel 12 through being equipped with connecting block 16, avoid mounting panel 12 to appear droing.

The top of bottom plate 1 is equipped with light 19, and the upper surface of light 19 and the bottom surface fixed connection of diaphragm 18 can throw light on the equipment inside through light 19 to observe the device inside, annular spout 13 has been seted up to the bottom surface of roof 5, and the inner wall sliding connection of annular spout 13 has slider 17, and the bottom surface of slider 17 and the upper surface fixed connection of diaphragm 18 can guide diaphragm 18 through being equipped with slider 17 and annular spout 13, increases the stability of diaphragm 18.

The working principle of the utility model is as follows:

Install the device in the assigned position when using to control the device through control panel 3, put unmanned aerial vehicle on the slipmat 9 on unmanned aerial vehicle board 10 when using, and start unmanned aerial vehicle and rise, make unmanned aerial vehicle and unmanned aerial vehicle board 10 separate, and remove to the right side of mounting panel 12, start blower 11, make blower 11 blow to unmanned aerial vehicle, wind-resistant test is carried out to unmanned aerial vehicle, and through starting servo motor 7, make servo motor 7 drive bull stick 15 rotatory, bull stick 15 drives mounting panel 12 through diaphragm 18 and rotates, adjust blower 11's position, thereby can carry out diversified wind-resistant test to unmanned aerial vehicle.

It will be evident to those skilled in the art that the utility model is not limited to the details of the foregoing illustrative embodiments, and that the present utility model may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are, therefore, to be considered in all respects as illustrative and not restrictive, the scope of the utility model being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

Furthermore, it should be understood that although the present disclosure describes embodiments, not every embodiment is provided with a separate embodiment, and that this description is provided for clarity only, and that the disclosure is not limited to the embodiments described in detail below, and that the embodiments described in the examples may be combined as appropriate to form other embodiments that will be apparent to those skilled in the art.

Claims (6)

1. A test platform for unmanned aerial vehicle, its characterized in that: including bottom plate (1), the last fixed surface of bottom plate (1) is connected with two sets of support columns (2), two sets of the common fixedly connected with roof (5) in top of support column (2), the last fixed surface of roof (5) is inlayed and is had bearing (14), the inner circle fixedly connected with bull stick (15) of bearing (14), the last fixed surface of roof (5) is connected with servo motor (7), the output of servo motor (7) and the top fixed connection of bull stick (15), the bottom surface fixedly connected with diaphragm (18) of bull stick (15), the bottom surface fixedly connected with mounting panel (12) of diaphragm (18), the right flank of mounting panel (12) is fixedly inlayed and is had hair-dryer (11), the last fixed surface of bottom plate (1) is connected with unmanned aerial vehicle platform (10), the bottom surface fixedly connected with two first foraminiferous protection shield (4) and two second foraminiferous protection shield (8), two the protection shield side that first foraminiferous protection shield (4) are close to each other is kept away from each other with two sets of protection shield side (2) of side fixedly connected with two sets of support column (2) are kept away from each other respectively.

2. A test platform for an unmanned aerial vehicle according to claim 1, wherein: the outer surface of the servo motor (7) is fixedly connected with a positioning ring (6), and the bottom surface of the positioning ring (6) is fixedly connected with the upper surface of the top plate (5).

3. A test platform for an unmanned aerial vehicle according to claim 1, wherein: an anti-slip pad (9) is arranged above the bottom plate (1), and the bottom surface of the anti-slip pad (9) is fixedly connected with the upper surface of the unmanned aerial vehicle platform (10).

4. A test platform for an unmanned aerial vehicle according to claim 1, wherein: the bottom surface of diaphragm (18) fixedly connected with connecting block (16), the left surface of connecting block (16) and the right side fixed connection of mounting panel (12).

5. A test platform for an unmanned aerial vehicle according to claim 1, wherein: an illuminating lamp (19) is arranged above the bottom plate (1), and the upper surface of the illuminating lamp (19) is fixedly connected with the bottom surface of the transverse plate (18).

6. A test platform for an unmanned aerial vehicle according to claim 1, wherein: an annular chute (13) is formed in the bottom surface of the top plate (5), a sliding block (17) is connected to the inner wall of the annular chute (13) in a sliding mode, and the bottom surface of the sliding block (17) is fixedly connected with the upper surface of the transverse plate (18).