Adjustable unmanned aerial vehicle

Abstract

The utility model discloses an adjustable unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles. The unmanned aerial vehicle comprises a bearing seat and an unmanned aerial vehicle body, a mounting assembly is arranged between the bearing seat and the unmanned aerial vehicle body, a groove is formed in the lower side of the bearing seat, a buffer plate is arranged in the groove in a sliding and elastic fit mode, and two first baffles are arranged on the upper side of the bearing seat in a sliding fit mode; two second baffles are arranged between the two first baffles in a sliding fit mode, and two cushion blocks are fixedly connected to the lower portion of the buffer plate. When the unmanned aerial vehicle body drives the bearing seat to fly upwards, the buffer plate drives the relative moving assembly to operate through elastic reset, so that the two first baffles move relatively, the two first baffles move relatively to extrude the moving assembly to drive the two second baffles to move relatively, and the two first baffles and the second baffles move relatively for adjustment; and the equipment on the bearing seat is clamped and mounted, so that the condition that the equipment is mounted by additional operation is reduced.

Description

TECHNICAL FIELD

[0001] The utility model belongs to the field of unmanned aerial vehicle, concretely relates to an adjustable unmanned aerial vehicle. BACKGROUND

[0002] Unmanned aircraft is called unmanned aerial vehicle, and is a kind of aircraft without pilot, which is controlled by radio remote control equipment and self-provided program control device.

[0003] The utility model discloses a kind of unmanned aerial vehicles with adjustable mounting rack, including unmanned aerial vehicle rack, the top hexagonal of unmanned aerial vehicle rack is equidistantly connected with multiple driving paddles, the bottom of unmanned aerial vehicle rack is provided with mounting seat, the bottom of mounting seat is provided with fixed plate, and fixed plate is below unmanned aerial vehicle rack, bearing seat is provided below fixed plate, two adjusting baffles are slidably installed on the both sides of fixed plate and bearing seat, adjusting assembly is arranged in fixed plate and bearing seat, although the unmanned aerial vehicle of above-mentioned is convenient for mounting rack to be applicable to equipment of different sizes, but the unmanned aerial vehicle of above-mentioned still needs to make positioning knob screw out corresponding thread limiting hole in actual use, the position of adjusting baffle is adjusted, after positioning knob is screwed into corresponding thread limiting hole in reverse and the position of adjusting baffle is fixed, equipment can be installed on bearing seat, and operation step is tedious, the efficiency of installing equipment on bearing seat is reduced.

[0004] Therefore, the utility model is provided. UTILITY MODEL CONTENT

[0005] The utility model solves the problems in the background art by overcoming the deficiencies of the prior art.

[0006] To solve the above technical problems, the basic idea of the technical scheme of the utility model is as follows:

[0007] An adjustable unmanned aerial vehicle includes a bearing seat and an unmanned aerial vehicle body, an installation assembly is arranged between the bearing seat and the unmanned aerial vehicle body, a groove is formed in the lower side of the bearing seat, a buffer plate is slidably and elastically fitted in the groove, two first baffles are slidably fitted on the upper side of the bearing seat, two second baffles are slidably fitted between the two first baffles, and two cushion blocks are fixedly connected below the buffer plate.

[0008] A relative movement assembly is arranged on the bearing seat and cooperates with the two first baffles, one side of each of the two first baffles is provided with an extrusion movement assembly that cooperates with one side of the two second baffles, and the relative movement assembly is in transmission cooperation with the buffer plate.

[0009] Optionally, the relative moving assembly comprises a groove formed on the bearing seat, a bidirectional threaded rod rotatably fitted in the groove, and two threaded blocks slidably fitted in the groove and threadedly fitted on the bidirectional threaded rod, the two threaded blocks being fixedly connected to the bottoms of the two first baffles respectively, and the bidirectional threaded rod being drivingly fitted with the buffer plate.

[0010] Optionally, the groove is in communication with the recess, and a plurality of first springs are arranged between the buffer plate and the recess.

[0011] Optionally, a gear is arranged on the periphery of the middle portion of the bidirectional threaded rod, and a toothed plate is arranged on the upper side of the buffer plate and engaged with the gear.

[0012] Optionally, the extrusion moving assembly comprises an inclined chute formed on one side of the first baffle, a connecting block arranged on one side of the second baffle, a chamfer arranged on one side of the connecting block and abutting against the inclined chute, and a second spring arranged between the connecting block and the inclined chute.

[0013] Optionally, the mounting assembly comprises a mounting frame fixedly connected to the bearing seat, a mounting block fixedly connected to the upper side of the mounting frame, two mounting plates fixedly connected to the lower side of the unmanned aerial vehicle body, through holes formed on the mounting block and the two mounting plates, and fastening bolts located in the through holes.

[0014] After the above technical scheme is adopted, the present application has the following advantages compared with the prior art, of course, any product implementing the present application does not necessarily need to achieve all the advantages described below:

[0015] When the unmanned aerial vehicle body drives the bearing seat to fly upward, the buffer plate arranged on the bottom of the bearing seat drives the relative moving assembly to move by elastic return, so that the two first baffles move relatively, the extrusion moving assembly is driven to move by the relative movement of the two first baffles, and the two second baffles move relatively, the two first baffles and the second baffles move relatively to adjust, the equipment on the bearing seat is clamped and mounted, the additional operation for mounting the equipment is reduced, and the efficiency of mounting the equipment on the bearing seat is improved.

[0016] The specific embodiments of the present application will be further described in detail below with reference to the accompanying drawings. BRIEF DESCRIPTION OF DRAWINGS

[0017] The drawings in the following description are only some embodiments, and other drawings can be obtained by those skilled in the art without creative labor on the basis of the drawings. In the drawings:

[0018] Figure 1 is a schematic view of the unmanned aerial vehicle structure;

[0019] Figure 2 It is an installation assembly structure schematic view;

[0020] Figure 3 It is a relative movement assembly structure schematic view;

[0021] Figure 4 It is a bearing seat structure schematic view;

[0022] Figure 5 It is a extrusion movement assembly structure schematic view.

[0023] In the drawings, the components represented by each reference numeral are listed as follows:

[0024] Bearing seat 1, buffer plate 2, first baffle 3, groove 4, pad 5, relative movement assembly 6, channel 601, bidirectional threaded rod 602, threaded block 603, first spring 7, gear 8, toothed plate 9, second baffle 10, extrusion movement assembly 11, inclined groove 1101, connecting block 1102, chamfer 1103, second spring 1104, unmanned aerial vehicle body 12, installation assembly 14, mounting bracket 1401, mounting block 1402, mounting plate 1403, fastening bolt 1404.

[0025] It should be noted that these drawings and written descriptions are not intended to limit the scope of the concept of the utility model in any way, but to illustrate the concept of the utility model to those skilled in the art by referring to specific embodiments. DETAILED DESCRIPTION

[0026] The utility model will be further described in detail in combination with the drawings.

[0027] Please refer to Figures 1-5 As shown in the drawings, in this embodiment, an adjustable unmanned aerial vehicle is provided, which comprises a bearing seat 1 and an unmanned aerial vehicle body 12, an installation assembly 14 is arranged between the bearing seat 1 and the unmanned aerial vehicle body 12, a groove 4 is formed in the lower side of the bearing seat 1, a buffer plate 2 is elastically fitted in the groove 4 and slides in the groove 4, two first baffles 3 are slidably fitted on the upper side of the bearing seat 1, two second baffles 10 are slidably fitted between the two first baffles 3, and two pads 5 are fixedly connected below the buffer plate 2.

[0028] The bearing seat 1 is provided with a relative movement assembly 6 matched with the two first baffles 3, one side of the two first baffles 3 is provided with an extrusion movement assembly 11 matched with one side of the two second baffles 10, and the relative movement assembly 6 is in transmission cooperation with the buffer plate 2.

[0029] When the unmanned aerial vehicle body 12 drives the bearing seat 1 to fly upward, the buffer plate 2 drives the relative movement assembly 6 to move through the elastic reset, so that the two first baffles 3 are relatively moved, the two first baffles 3 relatively move to extrude the moving assembly 11 to drive the two second baffles 10 to relatively move, the two first baffles 3 and the second baffles 10 relatively move to adjust, clamp and install the equipment on the bearing seat 1, reduce the additional operation of the equipment installation, and improve the efficiency of installing the equipment on the bearing seat.

[0030] As shown in Figures 3-4 The relative movement assembly 6 of the embodiment includes a groove 601 opened on the bearing seat 1, a bidirectional threaded rod 602 rotationally fitted in the groove 601, and two threaded blocks 603 slidably fitted in the groove 601 and threadedly fitted on the bidirectional threaded rod 602, the two threaded blocks 603 are respectively fixedly connected with the bottom of the two first baffles 3, and the bidirectional threaded rod 602 is drivingly fitted with the buffer plate 2; the groove 601 is in communication with the groove 4, and a plurality of first springs 7 are arranged between the buffer plate 2 and the groove 4; the middle part of the bidirectional threaded rod 602 is provided with a gear 8 on the side, and the upper side of the buffer plate 2 is provided with a toothed plate 9 engaged with the gear 8;

[0031] As shown in Figure 5 The extrusion moving assembly 11 of the embodiment includes an inclined groove 1101 opened on one side of the first baffle 3, a connecting block 1102 arranged on one side of the second baffle 10, a chamfer 1103 arranged on one side of the connecting block 1102 and abutting with the inclined groove 1101, and a second spring 1104 arranged between the connecting block 1102 and the inclined groove 1101.

[0032] When the unmanned aerial vehicle body 12 drives the bearing seat 1 to fly upward, the cushion block 5 leaves the ground, the buffer plate 2 resets and moves through the elastic force of the plurality of first springs 7, the buffer plate 2 drives the toothed plate 9 to move, the toothed plate 9 drives the gear 8 to rotate, the gear 8 drives the bidirectional threaded rod 602 to rotate, the bidirectional threaded rod 602 drives the two threaded blocks 603 to relatively move in the groove 601, the two threaded blocks 603 relatively move to drive the two first baffles 3 to relatively move, the two first baffles 3 relatively move to extrude the chamfer 1103 of the connecting block 1102 through the inclined groove 1101 to drive the two second baffles 10 to relatively move, the two first baffles 3 and the second baffles 10 relatively move to adjust, clamp and install the equipment on the bearing seat 1, reduce the additional operation of the equipment installation, and improve the efficiency of installing the equipment on the bearing seat.

[0033] As shown in Figure 2As shown, the mounting assembly 14 of the embodiment comprises a mounting frame 1401 fixedly connected to the bearing seat 1, a mounting block 1402 fixedly connected to the upper side of the mounting frame 1401, two mounting plates 1403 fixedly connected below the unmanned aerial vehicle body 12, through holes opened in the mounting block 1402 and the two mounting plates 1403, and fastening bolts 1404 located in the through holes.

[0034] The fastening bolts 1404 pass through the through holes, and the mounting block 1402 is fixed between the two mounting plates 1403 by screwing nuts on the fastening bolts 1404, so that the unmanned aerial vehicle body 12 can be connected and mounted to the bearing seat 1 through the mounting frame 1401, thereby facilitating mounting of equipment on the bearing seat 1.

[0035] The utility model is not limited to the above-mentioned embodiment, any person should know the structural change made under the inspiration of the utility model, any technical scheme with the same or similar utility model falls into the protection scope of the utility model. The utility model is not described in detail, and the technical, shape and structure parts are known technology.

Claims

1. An adjustable drone, characterized in that, The utility model relates to a bearing seat (1) and unmanned aerial vehicle body (12) are provided with installation assembly (14) between bearing seat (1) with unmanned aerial vehicle body (12), recess (4) is seted up in bearing seat (1) downside, the buffer board (2) is elastically matched in the recess (4) inside sliding, two first baffle (3) are matched in bearing seat (1) upside sliding, two second baffle (10) are matched in sliding between two first baffle (3), two pad (5) are fixedly connected below buffer board (2). Bearing seat (1) is provided with relative movement assembly (6) with two first baffle (3) cooperation, one side of two first baffle (3) is provided with extrusion movement assembly (11) with one side of two second baffle (10) cooperation, relative movement assembly (6) is transmission cooperation with buffer board (2). Relative movement assembly (6) includes the groove (601) being set up on bearing seat (1), the two-way threaded rod (602) being rotationally cooperated in groove (601), two threaded blocks (603) being slidably cooperated in groove (601) and being threadedly cooperated on two-way threaded rod (602), two threaded blocks (603) are fixedly connected with two first baffle (3) bottom respectively, two-way threaded rod (602) is transmission cooperation with buffer board (2).

2. The adjustable drone of claim 1, wherein, The groove (601) is communicated with the recess (4), and a plurality of first springs (7) are arranged between the buffer plate (2) and the recess (4).

3. The adjustable drone of claim 2, wherein, The two-way threaded rod (602) is provided with a gear (8) on the middle circumferential side, and the buffer plate (2) is provided with a toothed plate (9) engaged with the gear (8) on the upper side.

4. The adjustable drone of claim 2, wherein, The extrusion movement assembly (11) includes an inclined slot (1101) formed on one side of the first baffle (3), a connecting block (1102) arranged on one side of the second baffle (10), a chamfer (1103) arranged on one side of the connecting block (1102) and abutting against the inclined slot (1101), and a second spring (1104) arranged between the connecting block (1102) and the inclined slot (1101).

5. The adjustable drone of claim 1, wherein, The installation assembly (14) includes a mounting bracket (1401) fixedly connected to the bearing seat (1), an installation block (1402) fixedly connected to the upper side of the mounting bracket (1401), two mounting plates (1403) fixedly connected below the unmanned aerial vehicle body (12), through holes formed in the installation block (1402) and the two mounting plates (1403), and fastening bolts (1404) located in the through holes.

6. The adjustable drone of claim 1, wherein, ​

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