CN212829114U - Novel unmanned aerial vehicle illumination device - Google Patents
Novel unmanned aerial vehicle illumination device Download PDFInfo
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- CN212829114U CN212829114U CN202021305677.3U CN202021305677U CN212829114U CN 212829114 U CN212829114 U CN 212829114U CN 202021305677 U CN202021305677 U CN 202021305677U CN 212829114 U CN212829114 U CN 212829114U
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- 238000005286 illumination Methods 0.000 title abstract description 15
- 230000000694 effects Effects 0.000 claims abstract description 3
- 229910000639 Spring steel Inorganic materials 0.000 claims description 3
- 230000000149 penetrating effect Effects 0.000 claims 2
- 230000002093 peripheral effect Effects 0.000 claims 1
- 238000000034 method Methods 0.000 abstract description 10
- 230000008901 benefit Effects 0.000 abstract description 3
- 238000009434 installation Methods 0.000 description 7
- 238000005457 optimization Methods 0.000 description 5
- 230000008569 process Effects 0.000 description 5
- 230000009471 action Effects 0.000 description 4
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 2
- 229910052744 lithium Inorganic materials 0.000 description 2
- 230000006378 damage Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
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Abstract
The utility model relates to an unmanned air vehicle technique field, concretely relates to novel unmanned aerial vehicle lighting device, including fixed plate, mounting panel, pivot, grip ring, erection column, connecting plate, adjustment structure, the adjustment structure is including fixed free bearing, activity free bearing, drive element, adjustable shelf, swing arm. The utility model has the advantages that: through the removal of drive element drive adjustable shelf, make the swing arm drive the pivot and rotate, and then make the connecting plate rotate certain angle, because outside lighting apparatus installs on the connecting plate, consequently lighting apparatus's illumination angle can be adjusted, relative prior art, when adjusting lighting apparatus's illumination angle, it is more convenient to operate, in addition can be when unmanned aerial vehicle rises to the air the operation, carry out illumination angle and adjust, and the practicality has been better, set up taut structure, make the grip ring produce elastic shrinkage deformation through taut structure, and then press from both sides the erection column tightly, thereby make lighting apparatus can install on unmanned aerial vehicle fast, the efficiency of operation is improved.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, concretely relates to novel unmanned aerial vehicle illumination device.
Background
Unmanned aerial vehicle is the unmanned aircraft that utilizes radio remote control equipment and the program control device of self-contained to control, the wide application is military and civilian field, many rotor unmanned aerial vehicle have control simply, the reliability is high, and do not need the runway alright in order to take off and land perpendicularly, can hover advantage such as in the air after taking off, by the wide application in fields such as movie & TV aerial photograph, safety monitoring, agricultural plant protection and electric power patrol line, especially various natural disasters, for example earthquake, flood and massif landslide etc. can make water, electricity, infrastructure such as traffic receive destruction often, and to these comparatively abominable circumstances of rescue environment, take a photo by plane through unmanned aerial vehicle, know the latest developments of calamity, the trend that the calamity probably spreads is forecasted and appraised, be favorable to rescue decision-making.
Chinese patent No. CN201822137599.X discloses an airborne lighting device for an unmanned aerial vehicle, which comprises the unmanned aerial vehicle and a lighting device, wherein the unmanned aerial vehicle is provided with a case, a bracket is fixed on the case, and the lighting device is arranged on the bracket; the lighting device comprises a waterproof battery box and a main lighting lamp arranged on the front face of the waterproof battery box; the waterproof battery box is internally provided with a lithium battery, the top surface of the waterproof battery box is provided with two USB interfaces and a third switch, the two USB interfaces are respectively a first USB interface and a second USB interface, the three switches are respectively a first switch, a second switch and a third switch, the first switch, the second switch and the third switch are respectively electrically connected with the lithium battery, and the third switch is electrically connected with a main illuminating lamp; the utility model discloses the installation is simple, and convenient to use can selectivity be simultaneously to the place ahead illumination and both sides illumination, and easy operation has promoted the lighting efficiency when unmanned aerial vehicle takes photo by plane.
Above-mentioned unmanned aerial vehicle lighting device among the prior art, when using, need screw up the nut in advance, make lighting apparatus's illumination angle adjust, but when the in-service use, need constantly adjust lighting apparatus's illumination angle, it is obvious that prior art can't satisfy the illumination angle regulation in the operation process.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to overcome the problem that exists among the prior art, provide a novel unmanned aerial vehicle lighting device, it can realize solving prior art's problem to a certain extent at least.
In order to realize the technical purpose, the technical effect is achieved, the utility model discloses a realize through following technical scheme:
a novel unmanned aerial vehicle lighting device comprises a fixed plate arranged on an external unmanned aerial vehicle, a descending mounting plate is arranged on the fixed plate, a rotating shaft which is rotatably connected with the lower end part of the mounting plate is horizontally penetrated and arranged at the lower end part of the mounting plate, one end of the rotating shaft is fixedly provided with a clamping ring which is axially vertical to the rotating shaft, an installation column is inserted in the annular hole of the clamping ring, a connecting plate for installing external lighting equipment is arranged at one end of the installation column, which penetrates out of the clamping ring, the rotating shaft is driven to rotate by an adjusting structure, so as to adjust the lighting angle of the lighting device, the adjusting structure comprises a fixed hinged support arranged on a fixed plate, a movable hinged support is hinged on the fixed hinged support, a driving element is arranged on the movable hinged support, a movable frame is connected on the driving element in a driving way, the other end of the rotating shaft is provided with a swinging arm, and one end, far away from the rotating shaft, of the swinging arm is hinged to the movable frame.
As a further optimization of the above technical solution, the driving element is a telescopic cylinder.
As a further optimization of the above technical solution, the mounting plate is provided with a weight-reducing slot in the form of a through hole.
As a further optimization of the above technical solution, the clamping ring is of a split ring structure and is driven by a tensioning structure to elastically contract so as to clamp the mounting column.
As a further optimization of the solution described above, the clamping ring is made of spring steel material.
As a further optimization of the above technical solution, the tensioning structure includes two extending portions which are disposed on the circumferential surface of the clamping ring and respectively correspond to the opposite sides of the upper opening of the clamping ring, the two extending portions are respectively defined as a first extending portion and a second extending portion, the second extending portion is hinged with a movable ring, the circumferential surface of the movable ring is provided with a threaded post which extends to the radial outer side of the movable ring, the second extending portion is provided with a clamping groove through which the threaded post is far away from one end of the first extending portion and can freely pass through when rotating, one end of the threaded post, which penetrates through the clamping groove, is sleeved with a butterfly nut, and the end surface of the butterfly nut abuts against the surface of.
The utility model has the advantages that: through the removal of drive element drive adjustable shelf, make the swing arm drive the pivot and rotate, and then make the connecting plate rotate certain angle, because outside lighting apparatus installs on the connecting plate, consequently lighting apparatus's illumination angle can be adjusted, relative prior art, when adjusting lighting apparatus's illumination angle, it is more convenient to operate, in addition can be when unmanned aerial vehicle rises to the air the operation, carry out illumination angle and adjust, and the practicality has been better, set up taut structure, make the grip ring produce elastic shrinkage deformation through taut structure, and then press from both sides the erection column tightly, thereby make lighting apparatus can install on unmanned aerial vehicle fast, the efficiency of operation is improved.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art that other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a schematic perspective view of the present invention;
FIG. 2 is an enlarged view of a portion of the three-dimensional structure of FIG. 1 at A;
FIG. 3 is a schematic side view of the three-dimensional structure of FIG. 1;
FIG. 4 is a schematic side view of the three-dimensional structure of FIG. 1;
the reference numerals are explained below:
1-fixed plate, 2-fixed hinged support, 3-movable hinged support, 4-telescopic cylinder, 5-movable frame, 6-mounting column, 7-rotating shaft, 8-mounting plate, 9-clamping ring, 10-connecting plate, 11-movable ring, 12-threaded column, 13-butterfly nut, 14-second extension part, 15-clamping groove, 16-first extension part and 17-swinging arm.
Detailed Description
In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the drawings in the embodiments of the present invention are combined below to clearly and completely describe the technical solutions in the embodiments of the present invention, and obviously, the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.
Referring to fig. 1-4, fig. 1-4 show a novel lighting device for an unmanned aerial vehicle, which includes a fixing plate 1 installed on an external unmanned aerial vehicle, a mounting plate 8 extending downward is installed on the fixing plate 1, a weight reduction groove in the form of a through hole is installed on the mounting plate 8, a rotating shaft 7 rotatably connected to the mounting plate 8 is horizontally inserted through the lower end of the mounting plate 8, a clamping ring 9 axially perpendicular to the rotating shaft 7 is fixedly installed at one end of the rotating shaft 7, an installation column 6 is inserted into a ring hole of the clamping ring 9, a connecting plate 10 for installing an external lighting device is installed at one end of the installation column 6, which penetrates through the clamping ring 9, the rotating shaft 7 is driven to rotate by an adjusting structure to adjust a lighting angle of the lighting device, the adjusting structure includes a fixed hinge base 2 installed on the fixing plate 1, a movable hinge base 3 is hinged to the fixed hinge base 2, the telescopic cylinder 4 is connected with a movable frame 5 in a driving manner, the other end of the rotating shaft 7 is provided with a swing arm 17, one end of the swing arm 17, which is far away from the rotating shaft 7, is hinged with the movable frame 5, the clamping ring 9 is of a split ring structure and is driven by a tensioning structure to elastically contract so as to clamp the mounting column 6, the clamping ring 9 is made of spring steel, the tensioning structure comprises two extending parts which are arranged on the circumferential surface of the clamping ring 9 and respectively correspond to opposite sides of an opening on the clamping ring 9, the two extending parts are respectively defined as a first extending part 16 and a second extending part 14, the second extending part is hinged with a movable ring 11, the circumferential surface of the movable ring 11 is provided with a threaded column 12 which extends to the radial outer side of the movable ring 11, the second extending part 14 is provided with a clamping groove 15 through which one end of the threaded column 12, which is far away from the first extending part 16, the end surface of the wing nut 13 is abutted against the surface of the second extension part 14.
The utility model discloses when using: when the lighting equipment is installed, the lighting equipment (such as an LED searchlight) is installed on the connecting plate, the installation column is inserted into the annular hole of the clamping ring, then the threaded column is rotated to be clamped into the clamping groove of the second extending portion, the butterfly nut is rotated to be screwed on the threaded column, the end face of the butterfly nut is driven to abut against the second extending portion, in the abutting process, the threaded column has tension on the first extending portion, the first extending portion and the second extending portion are relatively closed, the clamping ring is elastically contracted and deformed, and the annular hole in the clamping ring clamps the installation column;
when unmanned aerial vehicle rises to the air, through the control cabinet on ground, control telescopic cylinder action, telescopic cylinder's cylinder pole extension \ shrink, and then make the adjustable shelf pulling swing arm rotate, make the pivot drive lighting apparatus rotate to lighting apparatus's illumination angle modulation has been realized.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
The preferred embodiments of the present invention disclosed above are intended only to help illustrate the present invention. The preferred embodiments are not intended to be exhaustive or to limit the invention to the precise embodiments disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the invention and its practical applications, to thereby enable others skilled in the art to best understand the invention for and utilize the invention. The present invention is limited only by the claims and their full scope and equivalents.
Claims (6)
1. The novel unmanned aerial vehicle lighting device is characterized by comprising a fixing plate (1) arranged on an external unmanned aerial vehicle, wherein a descending mounting plate (8) is arranged on the fixing plate (1), a rotating shaft (7) rotatably connected to the lower end of the mounting plate (8) is horizontally arranged in a penetrating manner, one end of the rotating shaft (7) is fixedly provided with a clamping ring (9) which is axially vertical to the axial direction of the rotating shaft, a mounting column (6) is inserted into a ring hole of the clamping ring (9), one end, penetrating out of the clamping ring (9), of the mounting column (6) is provided with a connecting plate (10) used for installing external lighting equipment, the rotating shaft (7) is driven to rotate by an adjusting structure to adjust the lighting angle of the lighting equipment, the adjusting structure comprises a fixed hinged support (2) arranged on the fixing plate (1), and a movable hinged support (3) is hinged on the fixed, install drive element on activity free bearing (3), the drive is connected with adjustable shelf (5) on the drive element, pivot (7) other end is equipped with swing arm (17), swing arm (17) are kept away from pivot (7) one end and are articulated with adjustable shelf (5).
2. A new unmanned aerial vehicle lighting device according to claim 1, characterized in that the driving element is a telescopic cylinder (4).
3. A novel lighting device for unmanned aerial vehicle according to claim 1, wherein the mounting plate (8) is provided with a lightening slot in the form of a through hole.
4. A novel lighting device for unmanned aerial vehicle according to claim 1, wherein the clamping ring (9) is a split ring structure and driven by a tension structure to elastically contract so as to clamp the mounting post (6).
5. A novel unmanned aerial vehicle lighting device according to claim 4, characterized in that the retaining ring (9) is made of spring steel.
6. A new unmanned aerial vehicle lighting device according to claim 4, characterized in that the tensioning structure comprises two extensions which are arranged on the circumference of the clamping ring (9) and correspond to the opposite sides of the opening on the clamping ring (9), the two extensions are respectively defined as a first extension (16) and a second extension (14), the second extending part is hinged with a movable ring (11), the peripheral surface of the movable ring (11) is provided with a threaded column (12) extending to the radial outer side of the movable ring, a clamping groove (15) through which one end of the threaded column (12) far away from the first extension part (16) can freely pass when rotating is formed on the second extension part (14), a butterfly nut (13) is sleeved on one end of the threaded column (12) which penetrates through the clamping groove (15) in a threaded manner, the end surface of the butterfly nut (13) is abutted against the surface of the second extension part (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021305677.3U CN212829114U (en) | 2020-07-06 | 2020-07-06 | Novel unmanned aerial vehicle illumination device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021305677.3U CN212829114U (en) | 2020-07-06 | 2020-07-06 | Novel unmanned aerial vehicle illumination device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212829114U true CN212829114U (en) | 2021-03-30 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021305677.3U Active CN212829114U (en) | 2020-07-06 | 2020-07-06 | Novel unmanned aerial vehicle illumination device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212829114U (en) |
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2020
- 2020-07-06 CN CN202021305677.3U patent/CN212829114U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A new lighting device for UAV Effective date of registration: 20210603 Granted publication date: 20210330 Pledgee: Bank of China Limited Dongshan Branch of Guangzhou Pledgor: GUANGZHOU AI AVIATION TECHNOLOGY Co.,Ltd. Registration number: Y2021440000194 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| CP02 | Change in the address of a patent holder |
Address after: 510700 Room 301, building C3, No. 11, Kaiyuan Avenue, Huangpu District, Guangzhou, Guangdong Patentee after: GUANGZHOU AI AVIATION TECHNOLOGY Co.,Ltd. Address before: 510335 room 706, 81 xuanyue East Street, Haizhu District, Guangzhou City, Guangdong Province (office only) Patentee before: GUANGZHOU AI AVIATION TECHNOLOGY Co.,Ltd. |
|
| CP02 | Change in the address of a patent holder | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 510700 Room 301, building C3, No. 11, Kaiyuan Avenue, Huangpu District, Guangzhou, Guangdong Patentee after: Guangzhou Aiwei Aviation Technology Co.,Ltd. Address before: 510700 Room 301, building C3, No. 11, Kaiyuan Avenue, Huangpu District, Guangzhou, Guangdong Patentee before: GUANGZHOU AI AVIATION TECHNOLOGY Co.,Ltd. |
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| CP01 | Change in the name or title of a patent holder | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20231023 Granted publication date: 20210330 Pledgee: Bank of China Limited Dongshan Branch of Guangzhou Pledgor: GUANGZHOU AI AVIATION TECHNOLOGY Co.,Ltd. Registration number: Y2021440000194 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A New Type of Unmanned Aerial Vehicle Lighting Device Effective date of registration: 20231030 Granted publication date: 20210330 Pledgee: Bank of China Limited Dongshan Branch of Guangzhou Pledgor: Guangzhou Aiwei Aviation Technology Co.,Ltd. Registration number: Y2023440000076 |
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| PE01 | Entry into force of the registration of the contract for pledge of patent right |