CN219172668U - Quick detach formula lighting device based on many rotor unmanned aerial vehicle crash bars - Google Patents
Quick detach formula lighting device based on many rotor unmanned aerial vehicle crash bars Download PDFInfo
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- CN219172668U CN219172668U CN202223534450.8U CN202223534450U CN219172668U CN 219172668 U CN219172668 U CN 219172668U CN 202223534450 U CN202223534450 U CN 202223534450U CN 219172668 U CN219172668 U CN 219172668U
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Abstract
The utility model provides a quick-dismantling type lighting device based on a multi-rotor unmanned aerial vehicle crash bar, which comprises a tubular clamping assembly and a lighting assembly, wherein the tubular clamping assembly can be fixedly connected to an unmanned aerial vehicle horn, the lighting assembly is integrated at the bottom of the clamping assembly, the clamping assembly comprises a quick-dismantling arm clamp lower part and a quick-dismantling arm clamp upper part, the cross section of the quick-dismantling arm clamp lower part is arc-shaped, one end of the quick-dismantling arm clamp lower part is hinged to one end of the quick-dismantling arm clamp upper part, the movable end of the quick-dismantling arm clamp lower part is connected with a locking rod with external threads, the movable end of the quick-dismantling arm clamp upper part is provided with a slot for accommodating the locking rod, and the movable end of the locking rod is in threaded fit connection with a movable knob for fixing the movable end of the quick-dismantling arm clamp upper part on the movable end of the quick-dismantling arm clamp lower part. The utility model has the effect of enhancing the night illumination capability of the unmanned aerial vehicle.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle illumination, in particular to a quick-dismantling type illumination device based on a multi-rotor unmanned aerial vehicle crash bar.
Background
Unmanned aerial vehicle lighting system is not configured in general in unmanned aerial vehicle market at present, but because unmanned aerial vehicle service environment, place are more and more extensive, ordinary unmanned aerial vehicle can't satisfy night or dim environment operation requirement, usually needs the manual work to carry out auxiliary illumination to satisfy unmanned aerial vehicle shooting, demand such as monitor. The common lamplight device has large volume and weight, cannot be easily installed on an unmanned plane platform, has small lamplight irradiation range and single direction, and is easy to form halation of bright and dark connection of an irradiated object, thereby influencing the quality of a photographed image.
Disclosure of Invention
Aiming at the defects in the prior art, the utility model provides a quick-dismantling type lighting device based on a multi-rotor unmanned aerial vehicle crash bar, which solves the problems that the integrated lamplight irradiation capability of an unmanned aerial vehicle is insufficient and the quality of a shot image is affected in the prior art.
According to the embodiment of the utility model, the quick-dismantling type lighting device based on the multi-rotor unmanned aerial vehicle crash bar comprises a tubular clamping component which can be fixedly connected to an unmanned aerial vehicle horn and a lighting component which is integrated at the bottom of the clamping component, wherein the clamping component comprises a quick-dismantling horn clamp lower part and a quick-dismantling horn clamp upper part, the cross section of the quick-dismantling horn clamp lower part is arc-shaped, one end of the quick-dismantling horn clamp lower part is hinged to one end of the quick-dismantling horn clamp upper part, the movable end of the quick-dismantling horn clamp lower part is connected with a locking rod with external threads, the movable end of the quick-dismantling horn clamp upper part is provided with a slot for accommodating the locking rod, and the movable end of the locking rod is connected with a movable knob which fixes the movable end of the quick-dismantling horn clamp upper part on the movable end of the quick-dismantling horn clamp lower part in a threaded fit manner.
Preferably, the lighting assembly comprises a lamp core base connected to the lower part of the quick-release arm clamp and a lamp core arranged on the lamp core base, a shell fixing base used for connecting a shell is arranged on the lamp core, the shell is arranged on the lamp core through a shell fixing base cover, a convex lens used for guiding light and a light reflecting cup are arranged between the shell and the lamp core, the light reflecting cup is hollow in a round table shape, and a light emitting part of the lamp core is positioned on the inner side of the light reflecting cup.
Preferably, a radiating fin is connected to one side of the lamp wick base away from the lamp wick.
Preferably, an anti-collision rod is arranged at the lower part of the quick-release arm clamp along the illumination direction of the lamp wick, and the anti-collision rod is positioned right above the lamp wick.
Preferably, the anti-collision rod is a hollow pipe, and the movable end of the anti-collision rod is connected with a shock pad.
Compared with the prior art, the utility model has the following beneficial effects:
1. the illumination assembly is integrated on the clamping assembly, the clamping assembly is fixedly clamped on the horn of the multi-rotor unmanned aerial vehicle, and the illumination capability of the unmanned aerial vehicle is enhanced by additionally installing the illumination assembly on the unmanned aerial vehicle so as to obtain a sufficiently clear image and a sufficiently clear view.
2. The clamping assembly is matched with the movable knob through the lock rod, so that the fixed connection between the lower part of the quick-release arm clamp and the movable end of the upper part of the quick-release arm clamp is realized, and the quick-installation and the quick-release of the lighting assembly can be realized.
Drawings
Fig. 1 is an exploded view of an embodiment of the present utility model.
In the above figures: 1. a shock pad; 2. an anti-collision rod; 3. a housing; 4. a convex lens; 5. a reflective cup; 6. a wick; 7. a housing fixing base; 8. a wick base; 9. a heat sink; 10. the lower part of the quick-release arm clamp; 11. the upper part of the quick-release arm clamp; 12. a movable knob; 13. a rotating shaft; 14. a lock rod.
Detailed Description
The technical scheme of the utility model is further described below with reference to the accompanying drawings and examples.
As shown in fig. 1, to enhance the illumination capability of the drone. The utility model provides a quick-dismantling type lighting device based on a multi-rotor unmanned aerial vehicle crash bar, which comprises a tubular clamping assembly and a lighting assembly, wherein the tubular clamping assembly can be fixedly connected to an unmanned aerial vehicle horn, the lighting assembly is integrated at the bottom of the clamping assembly, the clamping assembly comprises a quick-dismantling horn clamp lower part 10 and a quick-dismantling horn clamp upper part 11, the cross section of the quick-dismantling horn clamp lower part 10 is arc-shaped, one end of the quick-dismantling horn clamp lower part 10 is hinged to one end of the quick-dismantling horn clamp upper part 11, the movable end of the quick-dismantling horn clamp lower part 10 is connected with a locking rod 14 with external threads, the movable end of the quick-dismantling horn clamp upper part 11 is provided with a slot for accommodating the locking rod 14, and the movable end of the locking rod 14 is connected with a movable knob 12 which fixes the movable end of the quick-dismantling horn clamp upper part 11 on the movable end of the quick-dismantling horn clamp lower part 10 in a threaded fit manner.
The hinge ends of the quick-release arm clamp lower part 10 and the quick-release arm clamp upper part 11 are hinged through a rotating shaft 13, the bottom end of a lock rod 14 is hinged to the fixed end of the quick-release arm clamp lower part 10 through the rotating shaft 13, when the quick-release arm clamp lower part 10 and the quick-release arm clamp upper part 11 are fixedly connected, the quick-release arm clamp upper part 11 is rotated, an unmanned aerial vehicle arm is positioned between the quick-release arm clamp upper part 11 and the quick-release arm clamp lower part 10, the movable end of the quick-release arm clamp upper part 11 is abutted to the movable end of the quick-release arm clamp lower part 10, the lock rod 14 is rotated, the top of the lock rod 14 enters a groove of the movable end of the quick-release arm clamp upper part 11, and the bottom of the movable knob 12 is extruded to the movable end of the quick-release arm clamp upper part 11 through screwing down the movable knob 12, so that the fixed connection between the quick-release arm clamp upper part 11 and the quick-release arm clamp lower part 10 is realized. The illumination assembly is integrated on the bottom of the quick release arm clamp lower part 10 for illumination.
As shown in fig. 1, to provide sufficient illumination intensity. The lighting assembly comprises a lamp core base 8 connected to the lower portion 10 of the quick-release arm clamp and a lamp core 6 arranged on the lamp core base 8, wherein a shell fixing base 7 used for connecting the shell 3 is arranged on the lamp core 6, the shell 3 is covered on the lamp core 6 through the shell fixing base 7, a convex lens 4 used for guiding light and a reflecting cup 5 are arranged between the shell 3 and the lamp core 6, the reflecting cup 5 is in a hollow round table shape, and a light-emitting part of the lamp core 6 is positioned on the inner side of the reflecting cup 5. The illumination component is integrated at the bottom of the lower part 10 of the quick-release arm clamp, so that the installation is convenient; the light emitted by the lamp core 6 is reflected by the reflecting cup 5, the light is collected, and the light is refracted by the convex lens 4 to be changed into parallel light. The lampwick 6 is powered by an independent power supply, so that charging and replacement are convenient, grooves are formed in two sides of the contact end of the reflecting cup 5 and the lampwick 6, and a power line of the lampwick 6 is led out from the grooves between the lampwick 6 and the reflecting cup 5 and is connected with a power supply through a quick plug.
As shown in fig. 1, heat dissipation from the wick 6 is performed. And a radiating fin 9 is connected to one side of the lamp wick base 8 away from the lamp wick 6. The heat sink 9 is a conventional fan-type heat sink.
As shown in fig. 1, to achieve protection of the drone at night. The anti-collision rod 2 is arranged at the lower part 10 of the quick-release arm clamp along the illumination direction of the lamp wick 6, and the anti-collision rod 2 is positioned right above the lamp wick 6. In unmanned aerial vehicle flight, unmanned aerial vehicle flies along lighting assembly's light irradiation direction, in order to avoid the unmanned aerial vehicle collision damage that causes because of the operating personnel reaction is untimely, sets up crashproof pole 2 along lighting assembly's light irradiation direction.
As shown in fig. 1, in order to reduce the weight of the impact beam 2 and to extend the service life of the impact beam, the impact is damped. The anti-collision rod 2 is a hollow pipe, and the movable end of the anti-collision rod 2 is connected with a shock pad 1.
Claims (5)
1. Quick detach formula lighting device based on many rotor unmanned aerial vehicle crash bars, its characterized in that: including but fixed connection in the tubular clamping assembly on the unmanned aerial vehicle horn and the lighting assembly of integration in clamping assembly bottom, clamping assembly includes that the cross section becomes curved quick detach horn clamp lower part (10) and quick detach horn clamp upper portion (11), the one end of quick detach horn clamp lower part (10) articulates in the one end of quick detach horn clamp upper portion (11), the expansion end of quick detach horn clamp lower part (10) is connected with locking lever (14) of external screw thread, the expansion end of quick detach horn clamp upper portion (11) is provided with the fluting that is used for holding locking lever (14), screw-fit connection has on the expansion end of locking lever (14) with the activity knob (12) of the expansion end of quick detach horn clamp upper portion (11) fixed on the expansion end of quick detach horn clamp lower part (10).
2. The multi-rotor unmanned aerial vehicle bumper-based quick release lighting device of claim 1, wherein: the illuminating assembly comprises a lamp core base (8) connected to the lower portion (10) of the quick-release arm clamp and a lamp core (6) arranged on the lamp core base (8), wherein a shell fixing base (7) used for connecting the shell (3) is arranged on the lamp core (6), the shell (3) is covered on the lamp core (6) through the shell fixing base (7), a convex lens (4) used for guiding light and a reflecting cup (5) are arranged between the shell (3) and the lamp core (6), the reflecting cup (5) is in a hollow round table shape, and a light-emitting part of the lamp core (6) is located on the inner side of the reflecting cup (5).
3. The multi-rotor unmanned aerial vehicle bumper-based quick release lighting device of claim 2, wherein: one side of the lamp wick base (8) far away from the lamp wick (6) is connected with a radiating fin (9).
4. The multi-rotor unmanned aerial vehicle bumper-based quick release lighting device of claim 2, wherein: an anti-collision rod (2) is arranged at the lower part (10) of the quick-release arm clamp along the illumination direction of the lampwick (6), and the anti-collision rod (2) is positioned right above the lampwick (6).
5. The multi-rotor unmanned aerial vehicle bumper-based quick release lighting device of claim 4, wherein: the anti-collision rod (2) is a hollow pipe, and the movable end of the anti-collision rod (2) is connected with a shock pad (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223534450.8U CN219172668U (en) | 2022-12-29 | 2022-12-29 | Quick detach formula lighting device based on many rotor unmanned aerial vehicle crash bars |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223534450.8U CN219172668U (en) | 2022-12-29 | 2022-12-29 | Quick detach formula lighting device based on many rotor unmanned aerial vehicle crash bars |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219172668U true CN219172668U (en) | 2023-06-13 |
Family
ID=86671111
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223534450.8U Active CN219172668U (en) | 2022-12-29 | 2022-12-29 | Quick detach formula lighting device based on many rotor unmanned aerial vehicle crash bars |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219172668U (en) |
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2022
- 2022-12-29 CN CN202223534450.8U patent/CN219172668U/en active Active
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