CN219601626U - Shooting assembly for unmanned aerial vehicle - Google Patents
Shooting assembly for unmanned aerial vehicle Download PDFInfo
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- CN219601626U CN219601626U CN202320099515.6U CN202320099515U CN219601626U CN 219601626 U CN219601626 U CN 219601626U CN 202320099515 U CN202320099515 U CN 202320099515U CN 219601626 U CN219601626 U CN 219601626U
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- shooting
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- 238000009434 installation Methods 0.000 claims description 7
- 238000000034 method Methods 0.000 description 9
- 230000008569 process Effects 0.000 description 7
- 238000010521 absorption reaction Methods 0.000 description 4
- 238000006073 displacement reaction Methods 0.000 description 4
- 230000008030 elimination Effects 0.000 description 4
- 238000003379 elimination reaction Methods 0.000 description 4
- 230000035939 shock Effects 0.000 description 4
- 230000005484 gravity Effects 0.000 description 3
- 230000003139 buffering effect Effects 0.000 description 2
- 230000003993 interaction Effects 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004590 computer program Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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Abstract
The utility model discloses a shooting assembly for an unmanned aerial vehicle, which relates to the technical field of unmanned aerial vehicle shooting and comprises a supporting base arranged in the center of the inside of the unmanned aerial vehicle, wherein a first rotating shaft extending out of the unmanned aerial vehicle is arranged at the bottom of the supporting base, a rotatable first connecting structure is arranged at the bottom of the first rotating shaft, a connecting arm structure is fixed on the side surface of the first connecting structure, a rotatable second connecting structure is arranged at the end part of the connecting arm structure, a shooting head structure is fixed on the side surface of the second connecting structure, and a first rotating motor is connected with the shooting head structure; wherein, first swivel axis top is provided with the second rotation motor that is located unmanned aerial vehicle inside, and first connection structure is inside to be provided with first buffer, and second connection structure is inside to be provided with second buffer. The utility model has the advantages of high structural strength, safety and stability.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle shooting, in particular to a shooting assembly for an unmanned aerial vehicle.
Background
Unmanned aerial vehicle is unmanned aerial vehicle that controls through radio remote control equipment or airborne computer program control system, unmanned aerial vehicle simple structure, use cost is low, not only can accomplish the task that has the piloted aircraft to carry out, it is more applicable to the task that has the piloted aircraft to be unsuitable to carry out, emergent, the early warning in unexpected things has very big effect, in whole unmanned aerial vehicle's system, unmanned aerial vehicle shoots and is regard unmanned aircraft as air platform, with airborne remote sensing equipment, handle image information with the computer, and make into the image according to certain precision requirement, one of them is the structural reliability of high altitude shooting, among them, some shooting components that carry out high altitude shooting imbeds inside unmanned aerial vehicle, need unmanned aerial vehicle to carry out panorama shooting, the shooting process is complicated, security risk appears very easily, the reliability is low, but shooting range is little simultaneously, shooting quality has been reduced, still some shooting components extend outside unmanned aerial vehicle, but these shooting components focus outside, the structural strength is low, unmanned aerial vehicle is in steering, lifting and landing process, the part that shooting components stress is concentrated has the emergence risk, the reliability is reduced.
Disclosure of Invention
Aiming at the defects in the prior art, the utility model provides a shooting assembly for an unmanned aerial vehicle.
The shooting assembly for the unmanned aerial vehicle comprises a supporting base arranged in the center of the inside of the unmanned aerial vehicle, wherein a first rotating shaft extending out of the unmanned aerial vehicle is arranged at the bottom of the supporting base, a rotatable first connecting structure is arranged at the bottom of the first rotating shaft, a connecting arm structure is fixed on the side face of the first connecting structure, a rotatable second connecting structure is arranged at the end part of the connecting arm structure, a shooting head structure is fixed on the side face of the second connecting structure, and a first rotating motor is connected with the shooting head structure; the first rotary shaft top is provided with a second rotary motor positioned in the unmanned aerial vehicle, a first buffer part is arranged in the first connecting structure, and a second buffer part is arranged in the second connecting structure.
Preferably, the first connection structure comprises: the arc-shaped block is fixed on the bottom end face of the first rotary shaft; an arc groove arranged in the center of the arc block; the rotating block is arranged inside the arc-shaped groove; the connecting arm structure is fixed to the side face of the rotating block, a first limiting block is fixed to the inner wall of the arc-shaped groove, a second limiting block is fixed to the side face of the rotating block, a first buffer space is formed between the first limiting block and the second limiting block, and the first buffer portion is arranged in the first buffer space. The arc-shaped block and the first rotary shaft bottom surface form a step-shaped gap, so that the rotary block fixed with the connecting arm structure can rotate to a certain extent, and then if a setback occurs, the connecting arm structure drives the rotary block to rotate, or the arc-shaped block and the first rotary shaft in the first connecting structure rotate, the size of the first buffer space is changed, and the first buffer part in the buffer space can deform and generate elasticity to a certain extent to compensate and cope with the displacement, so that the shock absorption and the stress concentration elimination are realized.
Preferably, a connecting column is clamped at the center of the rotating block, and the top of the connecting column is fixed on the first rotating shaft. The connecting column can be connected with the upper rotating block in a clamping mode.
Preferably, the second connection structure comprises: the mounting body is arranged at the end part of the connecting arm structure; a sliding ring arranged on the end surface of the installation body; the sliding block is clamped in the sliding ring; and a connecting body fixed on the sliding block; the camera structure is fixed on the side face of the connecting body, a fixed block is fixed in the sliding ring, a second buffer space is formed between the fixed block and the sliding block, and the second buffer part is arranged in the second buffer space. The sliding ring on the installation body forms an annular gap, and the sliding block clamped in the sliding ring can slide in the annular gap, so that if the connection body and the installation body rotate relatively, the sliding block slides, the distance between the fixed block and the sliding block is changed, namely the size of the second buffer space is changed, and the second buffer part in the second buffer space can deform and elasticity to a certain extent to compensate and cope with the displacement, thereby realizing shock absorption and stress concentration elimination.
Preferably, the shooting head structure comprises a mounting frame fixed on the side face of the second connecting structure, a shooting head unit and a first rotating motor are arranged on the mounting frame in a erected mode, and the first rotating motor is used for driving the shooting head unit to rotate.
Preferably, the connecting arm structure comprises a horizontal section and a vertical section integrally connected, the horizontal section extending in a horizontal direction and being fixed to the first connecting structure side face, and the vertical section extending in a vertical direction and being fixed to the second connecting structure. The horizontal segment and the vertical segment can adjust the gravity center of the whole shooting assembly on a vertical connecting line between the shooting head structure and the first rotary shaft, so that the stability of the shooting head structure in the whole shooting operation process is improved.
Preferably, the shooting head structure is electrically connected with a storage module and a communication module which are arranged inside the unmanned aerial vehicle. The storage module is used for storing shooting information, and the communication module is used for remotely transmitting the shooting information to the cloud or man-machine interaction equipment.
The beneficial effects of the utility model are as follows:
according to the utility model, the supporting base is arranged inside the unmanned aerial vehicle and is partially exposed outside the bottom of the unmanned aerial vehicle, and meanwhile, the unmanned aerial vehicle extends out of the bottom of the first rotary shaft, so that the first connecting structure, the connecting arm structure, the second connecting structure and the shooting head structure are all located outside the unmanned aerial vehicle, the camera structure is enabled to carry out more comprehensive and clear panoramic shooting, the direction of the camera structure is regulated through the first rotary motor and the second rotary motor, frequent steering and other operations of the unmanned aerial vehicle are avoided, the shooting process is simple, the occurrence probability of safety risks is reduced, the reliability is high, more importantly, a rotatable first connecting structure and a rotatable second connecting structure are arranged between the supporting base and the shooting head structure, the directions and the installation positions of the first connecting structure and the second connecting structure are different, the gravity center of the whole shooting assembly can be reasonably regulated, the installation space of the first buffer part and the second buffer part can be provided, thereby reliable buffering is provided for the whole shooting assembly from a plurality of force points, the shooting assembly is reliably handled, and the structure strength and safety are greatly improved in the process of steering, lifting and landing and the like.
Drawings
In order to more clearly illustrate the embodiments of the present utility model or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below. Like elements or portions are generally identified by like reference numerals throughout the several figures. In the drawings, elements or portions thereof are not necessarily drawn to scale.
FIG. 1 is a schematic diagram of the structure of the present utility model;
FIG. 2 is a schematic structural view of a first connecting structure and a part of the structure of the present utility model;
fig. 3 is a schematic structural view of a first connecting structure and a part of the structure of the present utility model.
Reference numerals:
1-supporting base, 2-first revolving axle, 21-spliced pole, 3-first connection structure, 31-arc piece, 32-arc wall, 321-first stopper, 33-rotating block, 331-second stopper, 4-linking arm structure, 41-horizontal segment, 42-vertical segment, 5-second connection structure, 51-installation body, 52-sliding ring, 521-fixed block, 53-sliding block, 54-connector, 6-shooting head structure, 61-mounting bracket, 62-shooting head unit, 7-first rotating motor, 8-first buffer portion, 9-second buffer portion.
Detailed Description
For the purpose of making the objects, technical solutions and advantages of the embodiments of the present utility model more apparent, the technical solutions of the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model, and it is apparent that the described embodiments are some embodiments of the present utility model, but not all embodiments of the present utility model. The components of the embodiments of the present utility model generally described and illustrated in the figures herein may be arranged and designed in a wide variety of different configurations.
Thus, the following detailed description of the embodiments of the utility model, as presented in the figures, is not intended to limit the scope of the utility model, as claimed, but is merely representative of selected embodiments of the utility model. 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.
It should be noted that: like reference numerals and letters denote like items in the following figures, and thus once an item is defined in one figure, no further definition or explanation thereof is necessary in the following figures. Furthermore, the terms "first," "second," and the like, are used merely to distinguish between descriptions and should not be construed as indicating or implying relative importance.
In describing embodiments of the present utility model, it should be noted that the directions or positional relationships indicated by the terms "inner", "outer", "upper", etc. are directions or positional relationships based on those shown in the drawings, or those that are conventionally put in place when the inventive product is used, are merely for convenience of description and simplification of description, and are not indicative or implying that the apparatus or element in question must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be construed as limiting the present utility model.
As shown in fig. 1 to 3, a shooting assembly for an unmanned aerial vehicle comprises a supporting base 1 arranged in the center of the inside of the unmanned aerial vehicle, a first rotating shaft 2 extending out of the unmanned aerial vehicle is arranged at the bottom of the supporting base 1, a rotatable first connecting structure 3 is arranged at the bottom of the first rotating shaft 2, a connecting arm structure 4 is fixed on the side surface of the first connecting structure 3, a rotatable second connecting structure 5 is arranged at the end part of the connecting arm structure 4, a shooting head structure 6 is fixed on the side surface of the second connecting structure 5, and a first rotating motor 7 is connected with the shooting head structure 6; wherein, first swivel axis 2 top is provided with the inside second rotating electrical machines that is located unmanned aerial vehicle, and first connection structure 3 is inside to be provided with first buffer portion 8, and second connection structure 5 is inside to be provided with second buffer portion 9.
In this embodiment, it should be noted that, in the whole subassembly of shooing, support base 1 installs inside unmanned aerial vehicle and the part exposes outside the unmanned aerial vehicle bottom, unmanned aerial vehicle is extended to first revolving axle 2 bottom simultaneously, consequently, first connection structure 3, link arm structure 4, second connection structure 5 and shooting head structure 6 all are located the unmanned aerial vehicle outside, let the camera structure carry out more comprehensive and clear panorama shooting, and adjust the orientation of camera structure through first rotation motor 7 and second rotation motor, avoid unmanned aerial vehicle frequent steering etc. to operate, thereby let shooting process simple, the probability of occurrence of security risk is reduced, and reliability is strong, more importantly, there is rotatable first connection structure 3 and second connection structure 5 between support base 1 and the shooting head structure 6, simultaneously the orientation and the mounted position of first connection structure 3 and second connection structure 5 are different, can rationally adjust the focus of whole subassembly of shooing, can provide the focus of first buffer 8 and second buffer 9, thereby provide reliable buffering to whole subassembly of shooing through a plurality of force points, reliability corresponds, the in-process of occurrence of security landing and the big landing structure of the improvement, the safety landing structure of taking place, and the landing structure of security is greatly improved.
Specifically, the first connection structure 3 includes: an arc-shaped block 31 fixed on the bottom end surface of the first rotary shaft 2; an arc groove 32 formed in the center of the arc block 31; and a rotating block 33 disposed inside the arc-shaped groove 32; wherein, the fixed connection arm structure 4 in the side of the rotating block 33, the first stopper 321 is fixed on the inner wall of the arc-shaped groove 32, the second stopper 331 is fixed on the side of the rotating block 33, a first buffer space is formed between the first stopper 321 and the second stopper 331, and the first buffer portion 8 is arranged in the first buffer space.
In this embodiment, a stepped gap is formed between the arc-shaped block 31 and the bottom surface of the first rotating shaft 2, so that the rotating block 33 fixed with the connecting arm structure 4 can rotate to a certain extent, and thus, if a setback occurs, the connecting arm structure 4 drives the rotating block 33 to rotate, or the arc-shaped block 31 and the first rotating shaft 2 in the first connecting structure 3 rotate, the size of the first buffer space is changed, and the first buffer portion 8 therein deforms and has a certain degree of elasticity to compensate and cope with the displacement, thereby realizing shock absorption and stress concentration elimination.
Specifically, the center of the rotating block 33 is clamped with a connecting column 21, and the top of the connecting column 21 is fixed on the first rotating shaft 2.
In the present embodiment, the connection post 21 can be connected to the upper turning block 33 by a snap-fit method.
Specifically, the second connection structure 5 includes: a mounting body 51 provided at an end of the link arm structure 4; a slide ring 52 provided on an end surface of the mounting body 51; a slider 53 engaged with the inside of the slider 52; and a connecting body 54 fixed to the slider 53; the camera structure 6 is fixed on the side of the connector 54, the fixed block 521 is fixed in the sliding ring 52, a second buffer space is formed between the fixed block 521 and the sliding block 53, and the second buffer portion 9 is disposed in the second buffer space.
In this embodiment, the sliding ring 52 on the mounting body 51 forms an annular gap, and the sliding block 53 clamped in the sliding ring 52 can slide in the annular gap, so that if a setback occurs, the connecting body 54 and the mounting body 51 relatively rotate, the sliding block 53 slides, the distance between the fixed block 521 and the sliding block 53 changes, that is, the size of the second buffer space changes, and the second buffer portion 9 therein deforms and has a certain degree of elasticity to compensate and cope with the displacement, thereby realizing shock absorption and stress concentration elimination.
Specifically, the camera structure 6 includes a mounting frame 61 fixed on a side of the second connection structure 5, and a camera unit 62 and a first rotation motor 7 are mounted on the mounting frame 61, and the first rotation motor 7 is used for driving the camera unit 62 to rotate.
Specifically, the connecting arm structure 4 includes a horizontal section 41 and a vertical section 42 integrally connected, the horizontal section 41 extending in the horizontal direction and being fixed to the side of the first connecting structure 3, and the vertical section 42 extending in the vertical direction and being fixed to the second connecting structure 5.
In this embodiment, it should be noted that, the horizontal section 41 and the vertical section 42 can adjust the center of gravity of the entire shooting assembly on the vertical connecting line between the shooting head structure 6 and the first rotation shaft 2, so as to improve the stability of the shooting head structure 6 in the process of the entire shooting operation.
Specifically, the camera structure 6 is electrically connected with a storage module and a communication module that are disposed inside the unmanned aerial vehicle.
In this embodiment, it should be noted that the storage module is configured to store shooting information, and the communication module is configured to remotely transmit the shooting information to the cloud or the man-machine interaction device.
Finally, it should be noted that: the above embodiments are only for illustrating the technical solution of the present utility model, and not for limiting the same; although the utility model has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical scheme described in the foregoing embodiments can be modified or some or all of the technical features thereof can be replaced by equivalents; such modifications and substitutions do not depart from the spirit of the utility model, and are intended to be included within the scope of the appended claims and description.
Claims (7)
1. The shooting assembly for the unmanned aerial vehicle is characterized by comprising a supporting base arranged in the center of the inside of the unmanned aerial vehicle, wherein a first rotating shaft extending out of the unmanned aerial vehicle is arranged at the bottom of the supporting base, a first rotatable connecting structure is arranged at the bottom of the first rotating shaft, a connecting arm structure is fixed on the side face of the first connecting structure, a second rotatable connecting structure is arranged at the end part of the connecting arm structure, a shooting head structure is fixed on the side face of the second connecting structure, and a first rotating motor is connected with the shooting head structure; wherein,,
the first rotary shaft top is provided with and is located the inside second rotation motor of unmanned aerial vehicle, the inside first buffer portion that is provided with of first connection structure, the inside second buffer portion that is provided with of second connection structure.
2. The camera assembly for an unmanned aerial vehicle of claim 1, wherein the first connection structure comprises:
the arc-shaped block is fixed on the bottom end face of the first rotary shaft;
an arc groove arranged in the center of the arc block; and
the rotating block is arranged in the arc-shaped groove; wherein,,
the connecting arm structure is fixed to the side face of the rotating block, a first limiting block is fixed to the inner wall of the arc-shaped groove, a second limiting block is fixed to the side face of the rotating block, a first buffer space is formed between the first limiting block and the second limiting block, and the first buffer portion is arranged in the first buffer space.
3. The shooting assembly for the unmanned aerial vehicle according to claim 2, wherein a connecting column is arranged in the center of the rotating block in a clamping manner, and the top of the connecting column is fixed on the first rotating shaft.
4. The shooting assembly for an unmanned aerial vehicle of claim 1, wherein the second connection structure comprises:
the mounting body is arranged at the end part of the connecting arm structure;
a sliding ring arranged on the end surface of the installation body;
the sliding block is clamped in the sliding ring; and
a connector fixed on the sliding block; wherein,,
the camera structure is fixed to the connector side, the fixed block is fixed to the sliding ring, a second buffer space is formed between the fixed block and the sliding block, and the second buffer portion is arranged in the second buffer space.
5. The shooting assembly for the unmanned aerial vehicle according to claim 1, wherein the shooting head structure comprises a mounting frame fixed on the side face of the second connecting structure, a shooting head unit and the first rotating motor are arranged on the mounting frame in a erected mode, and the first rotating motor is used for driving the shooting head unit to rotate.
6. The camera assembly for an unmanned aerial vehicle of claim 1, wherein the connecting arm structure comprises a horizontal section and a vertical section integrally connected, the horizontal section extending in a horizontal direction and being fixed to the first connecting structure side, and the vertical section extending in a vertical direction and being fixed to the second connecting structure.
7. The shooting assembly for an unmanned aerial vehicle of claim 1, wherein the shooting head structure is electrically connected with a storage module and a communication module which are arranged inside the unmanned aerial vehicle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320099515.6U CN219601626U (en) | 2023-02-02 | 2023-02-02 | Shooting assembly for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320099515.6U CN219601626U (en) | 2023-02-02 | 2023-02-02 | Shooting assembly for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219601626U true CN219601626U (en) | 2023-08-29 |
Family
ID=87752156
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320099515.6U Active CN219601626U (en) | 2023-02-02 | 2023-02-02 | Shooting assembly for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219601626U (en) |
-
2023
- 2023-02-02 CN CN202320099515.6U patent/CN219601626U/en active Active
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