CN211738944U - Unmanned aerial vehicle carries automatic focusing lighting device - Google Patents
Unmanned aerial vehicle carries automatic focusing lighting device Download PDFInfo
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- CN211738944U CN211738944U CN202020897992.3U CN202020897992U CN211738944U CN 211738944 U CN211738944 U CN 211738944U CN 202020897992 U CN202020897992 U CN 202020897992U CN 211738944 U CN211738944 U CN 211738944U
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- ring
- electric locking
- shock attenuation
- focusing
- aerial vehicle
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Abstract
The utility model discloses an unmanned aerial vehicle carries automatic focusing lighting device, including focusing flashlight, the outer wall of the body is wrapped up with the first manual electric locking semi-ring and the second manual electric locking semi-ring; the first manual electric locking semi-ring is provided with a clamping protrusion, the clamping protrusion is clamped in a reserved clamping groove of the connecting seat, the top surface of the connecting seat is provided with a positioning jackscrew for fixing the clamping protrusion, two side walls of the connecting seat are rotatably connected with side brackets at two sides through a rotating shaft, one side bracket is provided with a first motor for driving the rotating shaft to rotate, and the top ends of the two side brackets are fixedly connected with the mounting plate; the second manual-electric locking semi-ring is provided with a focusing support, the focusing support is provided with a second motor, and a driving shaft of the second motor is provided with a gear meshed with the annular teeth. The utility model discloses the structure is ingenious, simple to operate, and the illumination is better stable to the regulation of every single move angle is carried out to light energy, has better illuminating effect.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle carries automatic focusing lighting device.
Background
Among the prior art, chinese utility model patent that application number is CN201921002529.1 discloses an unmanned aerial vehicle carries automatic focusing lighting device, and this lighting device's focusing flashlight passes through the universal stand and installs on the organism, but unmanned aerial vehicle lift off the back, and the every single move angle of this focusing flashlight can not automatically regulated, the use of unmanned aerial vehicle illumination of being not convenient for.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing an unmanned aerial vehicle carries automatic focusing lighting device, in the solution background art, the focusing flashlight passes through the universal stand and installs on the organism, but unmanned aerial vehicle rises to the air after, the problem that the every single move angle of this focusing flashlight can not control and adjust.
In order to solve the technical problem, the utility model adopts the following technical scheme:
the utility model relates to an unmanned aerial vehicle carries automatic focusing lighting device, including the focusing flashlight, the focusing flashlight includes barrel and skull, the skull suit is in the front side of barrel, be provided with lens in the front side of skull, and the outer wall of skull rear side is formed with annular tooth along length direction all around, wrap up on the outer wall of barrel and have first flashlight lock semi-ring and second flashlight lock semi-ring;
the first electro-manual locking semi-ring is provided with a clamping protrusion, the clamping protrusion is clamped in a reserved clamping groove of a connecting seat (4), a positioning jackscrew used for fixing the clamping protrusion is arranged on the top surface of the connecting seat, two side walls of the connecting seat are rotatably connected with side brackets on two sides through a rotating shaft, one of the side brackets is provided with a first motor used for driving the rotating shaft to rotate, and the top ends of the two side brackets are fixedly connected with a mounting plate;
the second manual-electric locking semi-ring is provided with a focusing support, the focusing support is provided with a second motor, and a driving shaft of the second motor is provided with a gear meshed with the annular teeth.
Furthermore, one end of the first manual electric locking semi-ring is provided with an arc-shaped shaft, the other end of the first manual electric locking semi-ring is provided with a first connecting plate, one end of the second manual electric locking semi-ring is provided with an arc-shaped groove, the other end of the second manual electric locking semi-ring is provided with a second connecting plate, the arc-shaped shaft is connected with the arc-shaped groove in a rotating fit mode, and the first connecting plate and the second connecting plate are connected through a hand-screwing bolt.
Furthermore, all be provided with the rubber layer on the inner wall of first portable electric lock semi-ring and the second portable electric lock semi-ring.
Further, the top of mounting panel is provided with four shock attenuation pieces, the shock attenuation piece includes the shock attenuation casing of being connected with the unmanned aerial vehicle belly, be provided with the shock attenuation cushion in the shock attenuation casing, the top of shock attenuation cushion is run through support behind the preformed hole on the shock attenuation casing on the top surface of mounting panel, be provided with the double-screw bolt in the shock attenuation cushion, the bottom fixedly connected with bottom plate of double-screw bolt, run through on the top of double-screw bolt behind the preformed hole on the mounting panel with nut threaded connection.
Compared with the prior art, the utility model discloses a beneficial technological effect:
the utility model discloses the structure is ingenious, simple to operate, and the illumination is better stable to the regulation of every single move angle is carried out to light energy, has better illuminating effect.
Drawings
The present invention will be further explained with reference to the following description of the drawings.
Fig. 1 is a schematic structural view of the unmanned aerial vehicle-mounted automatic focusing illumination device of the present invention;
FIG. 2 is an enlarged view of a portion of FIG. 1 at A;
fig. 3 is a cross-sectional view of the shock-absorbing rubber pad of the present invention.
Description of reference numerals: 1. focusing the flashlight; 101. a barrel body; 102. a head cover; 103. an annular tooth; 2. a first electro-manual locking half-ring; 201. clamping the bulges; 202. an arc-shaped shaft; 203. a first connecting plate; 3. a second manual electric locking semi-ring; 301. an arc-shaped slot; 302. an arc-shaped shaft; 4. a connecting seat; 5. positioning a jackscrew; 6. a rotating shaft; 7. a side bracket; 8. a first motor; 9. a focusing bracket; 10. a second motor; 1001. a gear; 11. mounting a plate; 12. a shock absorbing member; 1201. a shock-absorbing housing; 1202. a shock-absorbing rubber pad; 1203. a stud; 1204. a base plate.
Detailed Description
In order to make the technical solutions of the present invention better understood by those skilled in the art, the present invention will be further described in detail with reference to the accompanying drawings and the detailed description.
As shown in fig. 1, the embodiment discloses an unmanned aerial vehicle carries automatic focusing lighting device, including focusing flashlight 1, focusing flashlight 1 includes stack 101 and skull 102, and skull 102 suit is provided with lens in the front side of stack 101, and the outer wall of skull 102 rear side is formed with the ring gear 103 along length direction all around, and focusing flashlight 1's specific structure has carried out detailed disclosure in the chinese utility model patent that application number is CN201921002529.1, no longer redundantly here. The outer wall of barrel 101 is wrapped up and is had first portable electric lock semi-ring 2 and second portable electric lock semi-ring 3.
Be provided with joint arch 201 on first flashlight lock semi-ring 2, the protruding 201 joint of joint is in the reservation joint groove of connecting seat 4, and the top surface of connecting seat 4 is provided with the location jackscrew 5 that is used for fixed joint arch 201, and the quick assembly disassembly of focusing flashlight 1 has been realized with connecting seat 4 to joint arch 201.
In order to enable the focusing flashlight 1 to be adjusted in a pitching mode, two side walls of the connecting seat 4 are rotatably connected with the side supports 7 on two sides through the rotating shaft 6, a first motor 8 used for driving the rotating shaft 6 to rotate is arranged on one side support 7, and the top ends of the two side supports 7 are fixedly connected with the mounting plate 11. The pitching adjustment of the focusing flashlight 1 can be realized by controlling the first motor 8.
The second manual-electric locking semi-ring 3 is provided with a focusing support 9, the focusing support 9 is provided with a second motor 10, and a driving shaft of the second motor 10 is provided with a gear 1001 meshed with the annular gear 103. The focusing process is that the ring-shaped teeth 103 can be driven to move along the length direction of the cylinder body 101 according to the rotation of the gear 1001, so that the lens moves relative to the light source, the distance between the lens and the light source is adjusted, and the adjustment of the illumination focal length is realized.
As shown in fig. 2, one end of the first manual electric locking half ring 2 is provided with an arc-shaped shaft 202, the other end is provided with a first connecting plate 203, one end of the second manual electric locking half ring 3 is provided with an arc-shaped groove 301, the other end is provided with a second connecting plate 302, the arc-shaped shaft 202 is connected with the arc-shaped groove 301 in a rotating fit manner, and the first connecting plate 203 and the second connecting plate 302 are connected through a hand-screwed bolt. In the present embodiment, in order to allow the locking half rings to clamp the focusing torch 1, a rubber layer is provided on the inner walls of the first and second manual-electric locking half rings 2 and 3.
In order to reduce the influence of fuselage vibrations to the illumination among the unmanned aerial vehicle flight process, be provided with four shock attenuation 12 at the top of mounting panel 11, as shown in fig. 1 and 3, shock attenuation 12 includes the shock attenuation casing 1201 that passes through bolted connection with the unmanned aerial vehicle belly, be provided with shock attenuation cushion 1202 in the shock attenuation casing 1201, support on the top surface of mounting panel 11 after the preformed hole on shock attenuation casing 1201 is run through at the top of shock attenuation cushion 1202, be provided with double-screw bolt 1203 in the shock attenuation cushion 1202, the bottom fixedly connected with bottom plate 1204 of double-screw bolt 1203, after the preformed hole on mounting panel 11 is run through at the top of double-screw bolt 1203 with nut threaded connection
The above-mentioned embodiments are only intended to describe the preferred embodiments of the present invention, but not to limit the scope of the present invention, and those skilled in the art should also be able to make various modifications and improvements to the technical solution of the present invention without departing from the spirit of the present invention, and all such modifications and improvements are intended to fall within the scope of the present invention as defined in the appended claims.
Claims (4)
1. The utility model provides an unmanned aerial vehicle carries automatic focusing lighting device, includes focusing flashlight (1), focusing flashlight (1) includes stack shell (101) and skull (102), skull (102) suit in the front side of stack shell (101), be provided with lens in the front side of skull (102), just the outer wall of skull (102) rear side is formed with annular tooth (103), its characterized in that along length direction all around: the outer wall of the barrel body (101) is wrapped with a first manual electric locking half ring (2) and a second manual electric locking half ring (3);
the first electro-manual locking semi-ring (2) is provided with a clamping protrusion (201), the clamping protrusion (201) is clamped in a reserved clamping groove of the connecting seat (4), a positioning jackscrew (5) used for fixing the clamping protrusion (201) is arranged on the top surface of the connecting seat (4), two side walls of the connecting seat (4) are rotatably connected with side brackets (7) on two sides through a rotating shaft (6), one side bracket (7) is provided with a first motor (8) used for driving the rotating shaft (6) to rotate, and the top ends of the two side brackets (7) are fixedly connected with the mounting plate (11);
a focusing support (9) is arranged on the second manual-electric locking semi-ring (3), a second motor (10) is arranged on the focusing support (9), and a gear (1001) meshed with the annular teeth (103) is arranged on a driving shaft of the second motor (10).
2. The unmanned aerial vehicle-mounted autofocus lighting device of claim 1, wherein: one end of the first manual electric locking semi-ring (2) is provided with an arc-shaped shaft (202), the other end of the first manual electric locking semi-ring is provided with a first connecting plate (203), one end of the second manual electric locking semi-ring (3) is provided with an arc-shaped groove (301), the other end of the second manual electric locking semi-ring is provided with a second connecting plate (302), the arc-shaped shaft (202) is connected with the arc-shaped groove (301) in a rotating fit mode, and the first connecting plate (203) is connected with the second connecting plate (302) through a hand-.
3. The unmanned aerial vehicle-mounted autofocus lighting device of claim 1, wherein: and rubber layers are arranged on the inner walls of the first manual electric locking semi-ring (2) and the second manual electric locking semi-ring (3).
4. The unmanned aerial vehicle-mounted autofocus lighting device of claim 1, wherein: the top of mounting panel (11) is provided with four shock attenuation pieces (12), shock attenuation piece (12) include with the shock attenuation casing (1201) that the unmanned aerial vehicle belly is connected, be provided with shock attenuation cushion (1202) in shock attenuation casing (1201), the top of shock attenuation cushion (1202) is run through support behind the preformed hole on shock attenuation casing (1201) on the top surface of mounting panel (11), be provided with double-screw bolt (1203) in shock attenuation cushion (1202), the bottom fixedly connected with bottom plate (1204) of double-screw bolt (1203), run through on the top of double-screw bolt (1203) with nut threaded connection behind the preformed hole on mounting panel (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020897992.3U CN211738944U (en) | 2020-05-26 | 2020-05-26 | Unmanned aerial vehicle carries automatic focusing lighting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020897992.3U CN211738944U (en) | 2020-05-26 | 2020-05-26 | Unmanned aerial vehicle carries automatic focusing lighting device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211738944U true CN211738944U (en) | 2020-10-23 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020897992.3U Active CN211738944U (en) | 2020-05-26 | 2020-05-26 | Unmanned aerial vehicle carries automatic focusing lighting device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211738944U (en) |
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2020
- 2020-05-26 CN CN202020897992.3U patent/CN211738944U/en active Active
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