CN220465814U - Unmanned aerial vehicle oblique photography cloud platform and unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle oblique photography cloud platform and unmanned aerial vehicle Download PDFInfo
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- CN220465814U CN220465814U CN202320987619.0U CN202320987619U CN220465814U CN 220465814 U CN220465814 U CN 220465814U CN 202320987619 U CN202320987619 U CN 202320987619U CN 220465814 U CN220465814 U CN 220465814U
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- 238000013016 damping Methods 0.000 claims description 43
- 230000007246 mechanism Effects 0.000 claims description 15
- 230000035939 shock Effects 0.000 claims description 5
- 238000010521 absorption reaction Methods 0.000 claims 2
- 230000000694 effects Effects 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 230000009471 action Effects 0.000 description 2
- 230000003139 buffering effect Effects 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle oblique photography holder and an unmanned aerial vehicle, and relates to the field of unmanned aerial vehicles. This unmanned aerial vehicle oblique photography cloud platform and unmanned aerial vehicle, oblique cloud platform main part is including horizontal rotation linking arm and control swivelling joint seat, the horizontal rotation linking arm rotates the bottom of connecting assembly, control swivelling joint seat and rotate the bottom surface of connecting arm at the horizontal rotation, control the other end of swivelling joint seat and be provided with the photographic camera that can overturn from beginning to end, folding rotor support's terminal top is provided with motor drive's rotor main part, folding rotor support's terminal bottom is provided with rotatable folding lift damper, lift damper's both sides all are provided with the torsional spring. This unmanned aerial vehicle oblique photography cloud platform and unmanned aerial vehicle, when carrying and overhauling, the dismantlement and the folding of lift damper of the slope cloud platform main part of being convenient for accomodate.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle oblique photography holder and an unmanned aerial vehicle.
Background
Unmanned aerial vehicle is as a mature remote control flight equipment now, wide application in topography survey, investigation and picture shooting, and the current more and more civilian unmanned aerial vehicle enters into people's field of vision, can carry out the shooting of whole picture in the air through unmanned aerial vehicle.
In order to ensure that a camera can accurately face a position to be photographed in real time along with the change of various angles and heights in the flight process of the unmanned aerial vehicle, a camera is generally installed through an inclined cradle head, and in the movement process of the unmanned aerial vehicle, the angle of the camera is kept to be fixed through the angle change of a three-dimensional shaft;
the existing tilt cradle head is assembled in a fixed mode and is installed at the bottom of the unmanned aerial vehicle, a certain fault rate exists in the tilt cradle head in the long-time use process, the existing assembly mode is inconvenient to overhaul, and after the use is finished, the existing tilt cradle head occupies more space, meanwhile, most of the existing unmanned aerial vehicle is provided with a lifting shock-absorbing bracket, the same shock-absorbing bracket also basically belongs to a fixed structure and is inconvenient to fold and store and carry, and therefore the unmanned aerial vehicle tilt photography cradle head and the unmanned aerial vehicle are needed to be provided to solve the problems.
Disclosure of Invention
(one) solving the technical problems
Aiming at the defects of the prior art, the utility model discloses an unmanned aerial vehicle oblique photographing cradle head and an unmanned aerial vehicle, and aims to solve the problems that the existing photographing unmanned aerial vehicle oblique cradle head and a damping bracket which are proposed in the background art are fixedly assembled and are inconvenient to overhaul, store and carry.
(II) technical scheme
In order to achieve the above purpose, the utility model is realized by the following technical scheme: an unmanned aerial vehicle oblique photography tripod head and an unmanned aerial vehicle comprise an oblique tripod head main body and a connecting component arranged at the top of the oblique tripod head main body;
the tilting cradle head main body comprises a horizontal connecting arm and a left-right rotary connecting seat, wherein the horizontal connecting arm is rotationally connected to the bottom of the connecting assembly, the left-right rotary connecting seat is rotationally connected to the outer surface of the bottom end of the horizontal connecting arm, and a photographic camera capable of overturning forwards and backwards is arranged at the other end of the left-right rotary connecting seat;
the horizontal connecting arm, the left-right rotary connecting seat and the photographic camera are driven by three groups of servo motors respectively.
An unmanned aerial vehicle comprises an unmanned aerial vehicle main body and a folding rotor wing bracket arranged on the side surface of the unmanned aerial vehicle main body;
the folding rotor support comprises a folding rotor support body, wherein a motor-driven rotor body is arranged at the top of the tail end of the folding rotor support body, a rotatable folding lifting damping mechanism is arranged at the bottom of the tail end of the folding rotor support body, and torsion springs are arranged on two sides of the lifting damping mechanism.
Preferably, the front end lower surface of unmanned aerial vehicle main part has seted up the mounting groove, coupling assembling installs the inside at the mounting groove.
Preferably, the connecting assembly comprises a connecting seat, a U-shaped movable block and locking springs, wherein the U-shaped movable block is movably inserted into two sides of the connecting seat, the locking springs are arranged on two sides of the inside of the connecting seat, and the locking springs are propped against the U-shaped movable block.
Preferably, the inside of mounting groove has seted up the draw-in groove, the top activity of U-shaped movable block is pegged graft in the inside of draw-in groove.
Preferably, the lifting damping mechanism comprises a rotating sleeve, a sliding damping rod and a damping spring, wherein the damping spring is arranged in the rotating sleeve, and the end part of the sliding damping rod is movably inserted into the rotating sleeve.
Preferably, the lower surface of folding rotor support has been seted up and has been accomodate the groove, it is inside accomodating the one end of groove to rotate the sleeve and rotate the connection, accomodate the other end of groove and seted up the constant head tank, the tip activity of slip shock attenuation pole is pegged graft in the inside of constant head tank, the middle part surface fixedly connected with shifting block of slip shock attenuation pole.
The utility model discloses an unmanned aerial vehicle oblique photography holder and an unmanned aerial vehicle, which have the following beneficial effects:
1. this unmanned aerial vehicle oblique photography cloud platform and unmanned aerial vehicle, in the use, along with the removal of unmanned aerial vehicle main part, horizontal connection arm is at the bottom horizontal rotation of unmanned aerial vehicle main part, the rotation is controlled to the rotation connecting seat, photographic camera upset around, with this three-dimensional orientation adjustment of shooting angle to photographic camera carries out the adaptation, make photographic camera can remain all the time just to the direction of taking, and when carrying or being overhauld, through pressing the bottom to the middle part of two sets of U-shaped movable blocks, make locking spring compressed, make the top of U-shaped movable block shift out from the draw-in groove inside simultaneously, take out the connecting seat from the mounting groove is inside this moment, make oblique cloud platform main part convenient dismantlement get off.
2. This unmanned aerial vehicle oblique photography cloud platform and unmanned aerial vehicle is through being close to the inside extrusion of rotating telescopic with the shifting block for damping spring is compressed, then will rotate the sleeve to accomodate the inside rotation of groove, rotates the torsional spring of sleeve tip both sides this moment and is rotated the compression, then loosens the shifting block, and at this moment under damping spring's effect, the tip of slip shock attenuation pole inserts inside the constant head tank voluntarily, sends out at this moment and conveniently accomodates lifting damping mechanism, reduces the space occupation when carrying.
Drawings
FIG. 1 is a schematic view of the overall upper surface structure of the present utility model;
FIG. 2 is a schematic view of the overall lower surface structure of the present utility model;
FIG. 3 is a cross-sectional view of a bottom portion of the main body of the unmanned aerial vehicle of the present utility model;
figure 4 is a schematic view of the exterior surface configuration of the folding rotor support of the present utility model.
In the figure: 1. an unmanned aerial vehicle main body; 2. folding the rotor support; 3. a rotor body; 4. a photographic camera; 5. a connection assembly; 51. a connecting seat; 52. a U-shaped movable block; 53. a locking spring; 6. a lifting damping mechanism; 61. rotating the sleeve; 62. a sliding shock-absorbing rod; 63. a damping spring; 7. tilting the pan-tilt main body; 71. a horizontal connecting arm; 72. a connecting seat is rotated left and right; 8. a mounting groove; 9. a clamping groove; 10. a shifting block; 11. a storage groove; 12. and a positioning groove.
Detailed Description
The embodiment of the utility model discloses an unmanned aerial vehicle oblique photography holder and an unmanned aerial vehicle, as shown in figures 1-4, comprising an oblique holder main body 7 and a connecting component 5 arranged at the top of the oblique holder main body 7;
the tilting pan-tilt main body 7 comprises a horizontal connecting arm 71 and a left-right rotary connecting seat 72, wherein the horizontal connecting arm 71 is rotationally connected to the bottom of the connecting assembly 5, the left-right rotary connecting seat 72 is rotationally connected to the outer surface of the bottom end of the horizontal connecting arm 71, and the other end of the left-right rotary connecting seat 72 is provided with a photographic camera 4 capable of being turned back and forth;
the horizontal connection arm 71, the left-right rotation connection base 72, and the photographic camera 4 are driven by three sets of servo motors, respectively.
An unmanned aerial vehicle comprises an unmanned aerial vehicle main body 1 and a folding rotor bracket 2 arranged on the side surface of the unmanned aerial vehicle main body 1;
the end top of folding rotor support 2 is provided with motor drive's rotor main part 3, and folding rotor support 2's end bottom is provided with rotatable folding lift damper 6, and lift damper 6's both sides all are provided with the torsional spring, and the device when using, lift damper 6 outwards overturns under the effect of torsional spring, keeps being vertical state with folding rotor support 2.
Referring to fig. 3, the front end lower surface of the unmanned aerial vehicle main body 1 is provided with a mounting groove 8, the connecting component 5 is mounted in the mounting groove 8, the connecting component 5 comprises a connecting seat 51, a U-shaped movable block 52 and locking springs 53, the U-shaped movable block 52 is movably inserted in two sides of the connecting seat 51, the locking springs 53 are arranged in two sides of the inner portion of the connecting seat 51, the locking springs 53 are abutted against the U-shaped movable block 52, a clamping groove 9,U is formed in the inner portion of the mounting groove 8, the top ends of the clamping groove 9 are movably inserted in the inner portion of the clamping groove, the bottom ends of the two groups of U-shaped movable blocks 52 are pressed towards the middle, the locking springs 53 are compressed, meanwhile, the top ends of the U-shaped movable blocks 52 are moved out from the inner portion of the clamping groove 9, and at the moment, the connecting seat 51 is drawn out from the inner portion of the mounting groove 8, so that the tilt cradle main body 7 is convenient to detach.
Referring to fig. 4, the lifting damping mechanism 6 includes a rotating sleeve 61, a sliding damping rod 62 and a damping spring 63, the damping spring 63 is disposed in the rotating sleeve 61, the end portion of the sliding damping rod 62 is movably inserted into the rotating sleeve 61, a receiving groove 11 is formed in the lower surface of the folding rotor bracket 2, the rotating sleeve 61 is rotatably connected in one end of the receiving groove 11, a positioning groove 12 is formed in the other end of the receiving groove 11, the end portion of the sliding damping rod 62 is movably inserted into the positioning groove 12, a shifting block 10 is fixedly connected to the outer surface of the middle portion of the sliding damping rod 62, when the lifting damping mechanism is lowered, the sliding damping rod 62 is in contact with the ground, the damping spring 63 is compressed at the moment, so that the damping and buffering effects are achieved, when the lifting damping mechanism is recovered and carried, the shifting block 10 is released by extruding the shifting block 10 into the interior close to the rotating sleeve 61 into the receiving groove 11, the end portion of the sliding damping rod 62 is automatically inserted into the positioning groove 12, and at the moment, the lifting damping mechanism 6 is conveniently received, and the space occupation is reduced when the lifting damping mechanism is carried.
Working principle: the device is in control connection with the unmanned aerial vehicle main body 1 through remote control equipment when in use, so as to control the lifting and flying of the unmanned aerial vehicle main body 1, and meanwhile, in the use process, along with the movement of the unmanned aerial vehicle main body 1, a horizontal connecting arm 71 in the inclined cradle head main body 7 horizontally rotates at the bottom of the unmanned aerial vehicle main body 1, a left-right rotation connecting seat 72 horizontally rotates at the tail end of the horizontal connecting arm 71, and meanwhile, a photographic camera 4 overturns back and forth at the front end of the horizontal connecting arm 72, so that the shooting angle of the photographic camera 4 is adaptively adjusted in three-dimensional directions, and the photographic camera 4 can always keep right to the direction to be shot;
meanwhile, when the device is used, the lifting damping mechanism 6 turns outwards under the action of the torsion spring, keeps a vertical state with the folding rotor bracket 2, when the device falls, the sliding damping rod 62 is in contact with the ground, the damping spring 63 is compressed at the moment, so that the damping and buffering effects are achieved, when the device is recovered and carried, the damping spring 63 is compressed by extruding the shifting block 10 towards the inside close to the rotating sleeve 61, then the rotating sleeve 61 is rotated towards the inside of the containing groove 11, the torsion springs at the two sides of the end part of the rotating sleeve 61 are rotationally compressed at the moment, then the shifting block 10 is loosened, at the moment, under the action of the damping spring 63, the end part of the sliding damping rod 62 is automatically inserted into the positioning groove 12, at the moment, the lifting damping mechanism 6 is conveniently contained, and the space occupation is reduced when the device is carried;
and when carrying or overhauling, the bottom ends of the two groups of U-shaped movable blocks 52 are pressed towards the middle part, so that the locking springs 53 are compressed, meanwhile, the top ends of the U-shaped movable blocks 52 are moved out of the clamping grooves 9, and at the moment, the connecting seat 51 is pulled out of the mounting groove 8, so that the tilting head main body 7 is convenient to detach.
The foregoing has shown and described the basic principles and main features of the present utility model and the advantages of the present utility model. It will be understood by those skilled in the art that the present utility model is not limited to the embodiments described above, and that the above embodiments and descriptions are merely illustrative of the principles of the present utility model, and various changes and modifications may be made without departing from the spirit and scope of the utility model, which is defined in the appended claims. The scope of the utility model is defined by the appended claims and equivalents thereof.
Claims (4)
1. An unmanned aerial vehicle oblique photography cloud platform, its characterized in that: comprises an inclined cradle head main body (7) and a connecting component (5) arranged at the top of the inclined cradle head main body (7);
the tilting cradle head body (7) comprises a horizontal connecting arm (71) and a left-right rotating connecting seat (72), wherein the horizontal connecting arm (71) is connected to the bottom of the connecting assembly (5), the left-right rotating connecting seat (72) is connected to the outer surface of the bottom end of the horizontal connecting arm (71), and a photographic camera (4) capable of overturning forwards and backwards is arranged at the other end of the left-right rotating connecting seat (72);
the horizontal connecting arm (71), the left-right rotary connecting seat (72) and the photographic camera (4) are driven by three groups of servo motors respectively;
the connecting assembly (5) comprises a connecting seat (51), a U-shaped movable block (52) and locking springs (53), wherein the U-shaped movable block (52) is arranged on two sides of the connecting seat (51), the locking springs (53) are arranged on two sides of the connecting seat (51), and the locking springs (53) are propped against the U-shaped movable block (52).
2. An unmanned aerial vehicle assembled by using the oblique photography tripod head of claim 1, wherein; comprises an unmanned aerial vehicle main body (1) and a folding rotor wing bracket (2) arranged on the side surface of the unmanned aerial vehicle main body (1);
the foldable rotor wing comprises a foldable rotor wing support (2), wherein a motor-driven rotor wing main body (3) is arranged at the top of the tail end of the foldable rotor wing support (2), a rotatable and foldable lifting damping mechanism (6) is arranged at the bottom of the tail end of the foldable rotor wing support (2), and torsion springs are arranged on two sides of the lifting damping mechanism (6);
the lower surface of the front end of the unmanned aerial vehicle main body (1) is provided with a mounting groove (8), and the connecting component (5) is mounted in the mounting groove (8);
the mounting groove (8) is internally provided with a clamping groove (9), and the top end of the U-shaped movable block (52) is arranged in the clamping groove (9).
3. A drone as claimed in claim 2, wherein: the lifting damping mechanism (6) comprises a rotating sleeve (61), a sliding damping rod (62) and a damping spring (63), wherein the damping spring (63) is arranged in the rotating sleeve (61), and the end part of the sliding damping rod (62) is arranged in the rotating sleeve (61).
4. A drone according to claim 3, wherein: the folding rotor support (2) is provided with a storage groove (11), the rotating sleeve (61) is connected to one end of the storage groove (11), the other end of the storage groove (11) is provided with a positioning groove (12), the end part of the sliding shock absorption rod (62) is arranged in the positioning groove (12), and the middle outer surface of the sliding shock absorption rod (62) is provided with a shifting block (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320987619.0U CN220465814U (en) | 2023-04-27 | 2023-04-27 | Unmanned aerial vehicle oblique photography cloud platform and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320987619.0U CN220465814U (en) | 2023-04-27 | 2023-04-27 | Unmanned aerial vehicle oblique photography cloud platform and unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220465814U true CN220465814U (en) | 2024-02-09 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320987619.0U Active CN220465814U (en) | 2023-04-27 | 2023-04-27 | Unmanned aerial vehicle oblique photography cloud platform and unmanned aerial vehicle |
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| Country | Link |
|---|---|
| CN (1) | CN220465814U (en) |
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2023
- 2023-04-27 CN CN202320987619.0U patent/CN220465814U/en active Active
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