CN216952960U - But angle regulation's lighting device and illumination unmanned aerial vehicle - Google Patents
But angle regulation's lighting device and illumination unmanned aerial vehicle Download PDFInfo
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- CN216952960U CN216952960U CN202220531086.0U CN202220531086U CN216952960U CN 216952960 U CN216952960 U CN 216952960U CN 202220531086 U CN202220531086 U CN 202220531086U CN 216952960 U CN216952960 U CN 216952960U
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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
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B20/00—Energy efficient lighting technologies, e.g. halogen lamps or gas discharge lamps
- Y02B20/40—Control techniques providing energy savings, e.g. smart controller or presence detection
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Abstract
The utility model relates to the technical field of illumination of unmanned aerial vehicles, in particular to an angle-adjustable illumination device and an illumination unmanned aerial vehicle. The lighting device comprises a supporting plate, a first lamp group, a second lamp group, a quick assembling and disassembling mechanism, a lamp controller and an angle adjusting mechanism capable of adjusting the irradiation angle of the lamp groups; the first lamp group is connected with one end of the supporting plate through the angle adjusting mechanism, and the other end of the supporting plate is connected with the second lamp group; the backup pad set up in lamp controller's top or around, lamp controller passes through quick assembly disassembly mechanism is fixed in on the horn of aircraft and the screw base that has the lockhole or the support foot rest of aircraft. Therefore, the angle of the lamp set can be adjusted by the angle adjusting mechanism, so that the lamp set is enabled to generate angular displacement, the irradiation range of the lamp set is improved, the brightness of an irradiation light source is improved, the applicability is improved and the like.
Description
Technical Field
The utility model relates to the technical field of illumination of unmanned aerial vehicles, in particular to an angle-adjustable illumination device and an illumination unmanned aerial vehicle.
Background
The existing unmanned aerial vehicle is mostly carried with a high-power lighting lamp group, and high-altitude large-area lighting can be realized at night, so that the unmanned aerial vehicle can carry out night shooting or night rescue. However, because unmanned aerial vehicle's lighting apparatus is fixed setting, so there is certain blind area can't be shone when searchlighting, and lighting apparatus does not possess adjustable irradiation angle function, illumination angle scope is not enough and the suitability is not strong scheduling problem when leading to shining the building.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide an illumination unmanned aerial vehicle and an illumination device thereof, and aims to solve the problems that illumination angle range is insufficient and applicability is poor when a building is illuminated due to the fact that illumination equipment of the existing unmanned aerial vehicle does not have the function of adjusting the illumination angle.
In order to solve the technical problems, the utility model adopts the following technical scheme:
the utility model provides an angle-adjustable lighting device, which comprises a supporting plate, a first lamp set, a second lamp set, a quick assembly and disassembly mechanism, a lamp controller and an angle adjusting mechanism capable of adjusting the irradiation angle of the lamp sets, wherein the supporting plate is arranged on the lamp set; the first lamp group is connected with one end of the supporting plate through the angle adjusting mechanism, and the other end of the supporting plate is connected with the second lamp group; or the angle adjusting mechanisms are arranged at two ends of the supporting plate, and the first lamp group and the second lamp group are respectively connected with the supporting plate through the angle adjusting mechanisms; the backup pad set up in lamp controller's top or around, lamp controller passes through quick assembly disassembly mechanism is fixed in on the horn of aircraft and the screw base that has the lockhole or the support foot rest of aircraft.
The angle adjusting mechanism comprises a base, an angle rotation adjusting sleeve, a locking piece, a limiting baffle and an elastic piece, wherein the limiting baffle and the elastic piece are arranged in the angle rotation adjusting sleeve; the upper end of the base is provided with a cylindrical boss with an internal thread through hole, and the outer surface of the cylindrical boss is provided with a limiting convex groove; one end of the angle rotation adjusting sleeve is provided with a plurality of axial limiting grooves matched with the limiting convex grooves; the limiting baffle is arranged in the angle rotation adjusting sleeve to form a first chamber and a second chamber, the cylindrical boss is located in the first chamber, the elastic piece is located in the second chamber, and the baffle is provided with a through hole for the locking piece to pass through; the one end of retaining member has the external screw thread, the one end that the retaining member has the external screw thread is inserted in the angular rotation adjusting sleeve the elastic component with the through-hole of baffle with the internal thread through-hole locking of cylinder boss.
The first lamp group and the second lamp group respectively comprise at least one floodlight, at least two spotlights, a fixing plate and a connecting plate, and each floodlight and each spotlight are fixed on the connecting plate through the fixing plate.
Wherein, quick dismouting mechanism includes quick locking fastener, prevents that rotation fixed plate and fixed connection plate, quick locking fastener set up in prevent rotation fixed plate's bottom, the bottom of lamps and lanterns controller is fixed in prevent rotation fixed plate's top.
One end of the fixed connection plate is fixedly connected with one end of the anti-rotation fixing plate through a bolt, and the other end of the fixed connection plate is fixedly connected with the propeller base through a bolt.
The floodlight and the spotlight are respectively electrically connected with the lamp controller through wires.
The floodlights are positioned between every two adjacent spotlights, and a space is reserved between each floodlight and each spotlight; the number of the floodlights is 1-4, and the number of the spotlights is 2-4.
The lamp controller comprises a shell with a waterproof heat dissipation structure, and a PCB power supply board and a control circuit board which are arranged in the shell, wherein the control circuit board is electrically connected with the PCB power supply board, and the floodlight and the spotlight are respectively electrically connected with the control circuit board through leads.
The base is connected with the supporting plate, and the base and the supporting plate are of an integrally formed structure; one side of the angle rotation adjusting sleeve is provided with a connecting piece, and the connecting piece is connected with the connecting plate.
The utility model also provides an illumination unmanned aerial vehicle, which comprises a ground power supply and pay-off and take-up integrated machine, an aircraft with a plurality of groups of arms and a rotor wing assembly arranged on the arms of the aircraft, wherein the rotor wing assembly comprises a propeller base with a lock hole, a propeller motor and a propeller driven by the propeller motor, the propeller base is arranged at the end part of the arms, and the propeller is arranged on the propeller base; illumination unmanned aerial vehicle is still including the installation be fixed in on horn and the screw base or on the supporting leg of aircraft as above but angle regulation's lighting device, lighting device passes through the cable and is connected with receive and release line all-in-one with ground power.
In the angle-adjustable lighting device, the lamp group adjusts the angle of the lamp group through the angle adjusting mechanism, specifically, the lamp group is pulled or pushed by external force, the compressed elastic part is utilized to enable the limiting groove of the current angle rotation adjusting sleeve to leave the limiting convex groove of the base cylindrical boss, then the angle rotation adjusting sleeve is rotated to determine the angle required by the lamp group and then releases the external force, and then the other limiting groove of the angle rotation adjusting sleeve is clamped on the limiting convex groove on the cylindrical boss, so that the lamp group generates angular displacement and is detected on an object, and the lamp group illuminates the ground and the building (high building). The lamp group is formed by mutually matching a floodlight and a spotlight to form a lighting three-dimensional layout, so that the lighting can be concentrated to illuminate the operation area and can be dispersed to illuminate the operation area, and the brightness of the whole operation area is greatly improved; the irradiation angle range reaches 0-160 degrees, and the irradiation range of the lamp group is improved. Therefore, the angle of the lamp set can be adjusted by the angle adjusting mechanism, so that the lamp set is enabled to generate angular displacement, the irradiation range of the lamp set is improved, the brightness of an irradiation light source is improved, the applicability is improved and the like.
Drawings
Fig. 1 is a schematic structural diagram of a lighting device according to a first embodiment of the present invention.
Fig. 2 is a schematic structural diagram of an angle adjustment mechanism according to an embodiment of the present invention.
Fig. 3 is a schematic cross-sectional view of an angle adjustment mechanism according to an embodiment of the present invention.
Fig. 4 is a schematic view illustrating that the base and the supporting plate of the lighting device according to the first embodiment of the present invention are integrally formed.
Fig. 5 is a schematic structural diagram of a quick-mounting and-dismounting mechanism of a lighting device according to an embodiment of the present invention.
Fig. 6 is an overall schematic view of a lighting device according to an embodiment of the present invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more clearly apparent, the present invention is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the utility model and are not intended to limit the utility model.
In order to explain the technical means of the present invention, the following description will be given by way of specific examples.
Referring to fig. 1 and fig. 6, an angle-adjustable lighting device 100 according to an embodiment of the present invention includes a supporting plate 1, a first lamp set 2, a second lamp set 3, a quick-assembly/disassembly mechanism 20, a lamp controller 30, and an angle-adjusting mechanism 10 capable of adjusting an illumination angle of the lamp sets; the first lamp group 2 is connected with one end of the supporting plate 1 through the angle adjusting mechanism 10, the other end of the supporting plate 1 is fixedly connected with the second lamp group 3 through a bolt mode, so that the angle adjusting mechanism 10 can adjust the angle of one lamp group, and the other lamp group is fixed on the supporting plate; or the two ends of the supporting plate 1 are both provided with the angle adjusting mechanisms 10, the first lamp group 2 and the second lamp group 3 are respectively connected with the supporting plate 1 through the angle adjusting mechanisms 10, and the first lamp group 2 and the second lamp group 3 can adjust the angles of the respective lamp groups through the angle adjusting mechanisms 10 which are respectively connected; the supporting plate 1 is arranged on the top or the periphery of the lamp controller 30, and the lamp controller 30 is fixed on a machine arm of an aircraft and a propeller base with a lock hole or a supporting foot stand of the aircraft through the quick assembly and disassembly mechanism 20. The lamp group is adjusted through the angle adjusting mechanism 10 to shine the angle displacement to let the lamp group produce angular displacement, make the lamp group searchly on the object, realize the lamp group to ground illumination and searchly to the building (high building).
Referring to fig. 2 to 4, in the first embodiment of the present invention, the angle adjustment mechanism 10 includes a base 11, an angle rotation adjustment sleeve 12, a locking member 13, and a limiting baffle 14 and an elastic member 15 disposed inside the angle rotation adjustment sleeve 12; a cylindrical boss 16 with an internal thread through hole 161 is arranged at the upper end of the base 11, and a limiting convex groove 17 is arranged on the outer surface of the cylindrical boss 16; one end of the angle rotation adjusting sleeve 12 is provided with a plurality of axial limiting grooves 18 matched with the limiting convex grooves 17, and the angle presented by the lamp group is different due to the matching of each limiting groove 18 on the angle rotation adjusting sleeve 12 and the limiting convex groove 17 of the cylindrical boss 16, so that the angle presented can be set according to the angle (such as 0 degree, 30 degree, 60 degree or 90 degree) required by the lamp group before the angle rotation adjusting sleeve 12 is produced and the distance between every two adjacent limiting grooves 18 is set and then matched with the limiting convex grooves 17. The limit baffle 14 is arranged in the angular rotation adjusting sleeve 12 to form a first chamber 121 and a second chamber 122, the cylindrical boss 16 is positioned in the first chamber 121, the elastic member is positioned in the second chamber 122, and the baffle 14 has a through hole 141 for the locking member 13 to pass through; one end of the locker 13 has an external thread 131, and the through hole 141 of the elastic member 15 and the shutter, which are inserted into the angular rotation adjusting sleeve 12 at one end of the locker 13 having the external thread, are locked with the internal thread through hole 161 of the cylindrical boss. The banks adjusts the angle of banks through angle adjustment mechanism 10, specifically with the banks through external force pulling or promote down, utilize compression elastic component 15 in the angle of rotation adjusting sleeve 12, make current angle of rotation adjusting sleeve's spacing recess 18 leave the spacing tongue 17 of base cylinder boss, rotation angle of rotation adjusting sleeve 12 is confirmed to release external force after the angle that the banks needs afterwards, let another spacing recess 18 of angle of rotation adjusting sleeve block to the spacing tongue 17 on the cylinder boss again, thereby let whole banks produce angular displacement, make whole banks searchlighted on the object, realize the banks to ground illumination and to building (high building) searchlighting.
In the first embodiment of the present invention, each of the first lamp set 2 and the second lamp set 3 includes at least one floodlight 4, at least two spotlights 5, a fixing plate 6 and a connecting plate 7, each of the floodlights 4 and the spotlights 5 is fixed to the connecting plate 7 through the fixing plate 6, the floodlights 4 are located between each adjacent spotlights 5, and a space is left between each floodlight 4 and each spotlight 5; the number of the floodlights 4 is 1-4, the number of the spotlights 5 is 2-4, in this embodiment, the number of the floodlights 4 is 1, and the number of the spotlights 5 is 2; the floodlights 4 and the spotlights 5 are mutually matched and distributed on the connecting plate 7, and a space is reserved between the floodlights 4 and the spotlights 5; the floodlight 4 and the spotlight 5 are matched with each other to form a group to form a lighting three-dimensional layout, so that the lighting can be concentrated to irradiate the operation area and can be dispersed to irradiate the operation area, and the brightness of the whole operation area is greatly improved.
Referring to fig. 5, in the first embodiment of the present invention, the quick-assembly/disassembly mechanism 20 includes a quick-locking fastener 21, an anti-rotation fixing plate 22 and a fixed connection plate 23, the quick-locking fastener 21 is disposed at the bottom of the anti-rotation fixing plate 22, the quick-locking fastener 21 is used for being fastened to the arm of the aircraft in a quick-disassembly manner, and the bottom of the lamp controller 30 is fixed to the top of the anti-rotation fixing plate 22 by bolts; one end of the fixed connection plate 23 is fixedly connected with one end of the anti-rotation fixing plate 22 through a bolt, and the other end of the fixed connection plate 23 is fixedly connected with the propeller base through a bolt, so that the effect of preventing the lamp bank from rotating and deviating caused by the vibration of the horn when the aircraft operates is achieved.
In the first embodiment of the present invention, the lamp controller 30 includes a housing (not shown) having a waterproof heat dissipation structure, a PCB power board (not shown), and a control circuit board (not shown), the housing having the waterproof heat dissipation structure is assembled by an upper cover having a groove and a lower cover having a groove in a snap-fit manner, the PCB power board and the control circuit board are disposed in the housing, the control circuit board is electrically connected to the PCB power board, and the floodlight 4 and the spotlight 5 are electrically connected to the control circuit board through wires, respectively, so as to control the floodlight 4 or the spotlight 5 to be turned on or turned off.
Referring to fig. 4, in the first embodiment of the present invention, the base 11 is connected to the supporting plate 1, and the base 11 and the supporting plate 1 are an integrally formed structure; one side of the angle rotation adjusting sleeve 12 is provided with a connecting piece 19, the angle rotation adjusting sleeve 12 and the connecting piece 19 are of an integrally formed structure, and the connecting piece 19 is connected with the connecting plate 7.
The second embodiment of the utility model also provides an illumination unmanned aerial vehicle, which comprises a ground power supply and pay-off and take-up integrated machine (not shown), an aircraft (not shown) with a plurality of groups of arms and a rotor assembly (not shown) arranged on the arms (not shown) of the aircraft; the rotor wing assembly comprises a propeller base (not shown) with a lock hole, a propeller motor (not shown) and a propeller (not shown) driven by the propeller motor, wherein the propeller base is arranged at the end part of the machine arm, and the propeller is arranged on the propeller base; the illumination unmanned aerial vehicle further comprises an illumination device 100 which is arranged and fixed on a horn and a propeller base or a support foot stand of the aircraft and can adjust the angle as in the first embodiment, and the illumination device 100 is electrically connected with the ground power supply and the take-up and pay-off all-in-one machine through a cable.
The angle-adjustable lighting device provided by the utility model adjusts the angle of the lamp set through the angle adjusting mechanism, so that the lamp set generates angular displacement, the irradiation range of the lamp set is improved, the brightness of an irradiation light source is improved, the applicability is improved and the like.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the utility model, and any modifications, equivalents and improvements made within the spirit and principle of the present invention are intended to be included within the scope of the present invention.
Claims (10)
1. An angle-adjustable lighting device, characterized in that: the lighting device comprises a supporting plate, a first lamp group, a second lamp group, a quick assembling and disassembling mechanism, a lamp controller and an angle adjusting mechanism capable of adjusting the irradiation angle of the lamp groups; the first lamp group is connected with one end of the supporting plate through the angle adjusting mechanism, and the other end of the supporting plate is connected with the second lamp group; or the angle adjusting mechanisms are arranged at two ends of the supporting plate, and the first lamp group and the second lamp group are respectively connected with the supporting plate through the angle adjusting mechanisms; the backup pad set up in lamp controller's top or around, lamp controller passes through quick assembly disassembly mechanism is fixed in on the horn of aircraft and the screw base that has the lockhole or the support foot rest of aircraft.
2. The adjustable angle lighting device according to claim 1, wherein the angle adjusting mechanism comprises a base, an angle rotation adjusting sleeve, a locking member, and a restricting flap and an elastic member built in the angle rotation adjusting sleeve; the upper end of the base is provided with a cylindrical boss with an internal thread through hole, and the outer surface of the cylindrical boss is provided with a limiting convex groove; one end of the angle rotation adjusting sleeve is provided with a plurality of axial limiting grooves matched with the limiting convex grooves; the limiting baffle is arranged in the angle rotation adjusting sleeve to form a first chamber and a second chamber, the cylindrical boss is located in the first chamber, the elastic piece is located in the second chamber, and the baffle is provided with a through hole for the locking piece to pass through; the one end of retaining member has the external screw thread, the one end that the retaining member has the external screw thread is inserted in the angular rotation adjusting sleeve the elastic component with the through-hole of baffle with the internal thread through-hole locking of cylinder boss.
3. The adjustable angle lighting fixture of claim 2, wherein the first light bank and the second light bank each comprise at least one floodlight, at least two spotlights, a mounting plate, and a connecting plate, each of the floodlights and the spotlights being secured to the connecting plate by the mounting plate.
4. The adjustable angle lighting device according to claim 1, wherein the quick-release mechanism comprises a quick-lock fastener, an anti-rotation fixing plate and a fixed connection plate, the quick-lock fastener is disposed at the bottom of the anti-rotation fixing plate, and the bottom of the lamp controller is fixed at the top of the anti-rotation fixing plate.
5. The adjustable angle lighting device according to claim 4, wherein one end of the fixed connection plate is fixedly connected to one end of the rotation-preventing fixing plate by a bolt, and the other end of the fixed connection plate is fixedly connected to the propeller base by a bolt.
6. The adjustable angle lighting device according to claim 3, wherein the floodlight and the spotlight are electrically connected to the lamp controller through wires, respectively.
7. The adjustable angle lighting device of claim 6, wherein the floodlights are positioned between each adjacent spot light, leaving a space between the floodlights and the spot lights; the number of the floodlights is 1-4, and the number of the spotlights is 2-4.
8. The adjustable angle lighting device according to claim 6, wherein the lamp controller comprises a housing having a waterproof heat dissipation structure, and a PCB power board and a control circuit board disposed in the housing, the control circuit board is electrically connected to the PCB power board, and the floodlight and the spotlight are electrically connected to the control circuit board through wires, respectively.
9. The adjustable angle lighting device of claim 3, wherein the base is connected to the support plate, the base and the support plate being of an integrally formed structure; one side of the outer surface of the angle rotation adjusting sleeve is provided with a connecting piece, and the connecting piece is connected with the connecting plate.
10. An illumination unmanned aerial vehicle comprises a ground power supply and pay-off and take-up integrated machine, an aircraft with a plurality of sets of arms and a rotor assembly arranged on the arms of the aircraft, wherein the rotor assembly comprises a propeller base with a lock hole, a propeller motor and a propeller driven by the propeller motor, the propeller base is arranged at the end part of the arms, and the propeller is arranged on the propeller base; the method is characterized in that: the illumination unmanned aerial vehicle further comprises an angle-adjustable illumination device according to any one of claims 1 to 9, which is fixedly installed on a horn and a propeller base or a support foot stool of an aircraft, and the illumination device is connected with a ground power supply and a take-up and pay-off all-in-one machine through a cable.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220531086.0U CN216952960U (en) | 2022-03-10 | 2022-03-10 | But angle regulation's lighting device and illumination unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220531086.0U CN216952960U (en) | 2022-03-10 | 2022-03-10 | But angle regulation's lighting device and illumination unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN216952960U true CN216952960U (en) | 2022-07-12 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220531086.0U Active CN216952960U (en) | 2022-03-10 | 2022-03-10 | But angle regulation's lighting device and illumination unmanned aerial vehicle |
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| Country | Link |
|---|---|
| CN (1) | CN216952960U (en) |
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- 2022-03-10 CN CN202220531086.0U patent/CN216952960U/en active Active
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