CN220010104U - Tethered unmanned aerial vehicle lighting system - Google Patents

Tethered unmanned aerial vehicle lighting system Download PDF

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Publication number
CN220010104U
CN220010104U CN202320993765.4U CN202320993765U CN220010104U CN 220010104 U CN220010104 U CN 220010104U CN 202320993765 U CN202320993765 U CN 202320993765U CN 220010104 U CN220010104 U CN 220010104U
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aerial vehicle
unmanned aerial
tethered
light source
source module
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CN202320993765.4U
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Chinese (zh)
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黄国军
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Shenzhen Lehui Emergency Technology Co ltd
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Shenzhen Lehui Emergency Technology Co ltd
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Abstract

The utility model discloses a tethered unmanned aerial vehicle lighting system, which comprises a tethered box, an unmanned aerial vehicle body, a rotary driving piece and a light source module, wherein the unmanned aerial vehicle body is connected with the tethered box through a tethered line; the outside of unmanned aerial vehicle body is equipped with a plurality of installation poles, the light source module cover is located on the installation pole, rotary driving spare is fixed in on the installation pole and drive connection light source module. The unmanned aerial vehicle of this tethered unmanned aerial vehicle lighting system is equipped with rotary drive spare on the unmanned aerial vehicle body, can drive the cover through rotary drive spare and locate the light source module on the installation pole and rotate to change light source module's irradiation angle and irradiation range in real time, satisfy the illumination demand in real time, need not the angle at subaerial debugging light source module.

Description

Tethered unmanned aerial vehicle lighting system
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a tethered unmanned aerial vehicle lighting system.
Background
Along with the development of civilian and miniaturized equipment of unmanned aerial vehicle technique, unmanned aerial vehicle has obtained effective application in fields such as energy, survey and drawing, security protection, agriculture, rescue, control, in rescue or control field, unmanned aerial vehicle can carry on communication base station and carry out long-time aerial communication relay guarantee and static detection, cooperates matrix lamp on the unmanned aerial vehicle to carry out long-time, large tracts of land emergency lighting demand, satisfies the actual combat scene such as control, rescue and uses. In the existing unmanned aerial vehicle lighting system, a light source module is usually fixedly installed on an unmanned aerial vehicle body, and the irradiation angle and irradiation range of the light source module on the unmanned aerial vehicle cannot be adjusted according to real-time use requirements.
Disclosure of Invention
The technical problems to be solved by the utility model are as follows: the tethered unmanned aerial vehicle lighting system can adjust the irradiation angle of the light source module on the unmanned aerial vehicle body in real time.
In order to solve the technical problems, the utility model adopts the following technical scheme: the tethered unmanned aerial vehicle lighting system comprises a tethered box, an unmanned aerial vehicle body, a rotary driving piece and a light source module, wherein the unmanned aerial vehicle body is connected with the tethered box through a tethered line; the outside of unmanned aerial vehicle body is equipped with a plurality of installation poles, the light source module cover is located on the installation pole, rotary driving spare is fixed in on the installation pole and drive connection light source module.
Further, the unmanned aerial vehicle body includes control main part and a plurality of rotor arm, and is a plurality of the rotor arm encircles control main part arranges, and two adjacent rotor arms are connected respectively one the both ends of installation pole.
Further, the unmanned aerial vehicle body further comprises mounting pieces, the mounting pieces are sleeved on the rotor wing arms, and two ends of the mounting rod are connected with the two mounting pieces respectively.
Further, the unmanned aerial vehicle body further comprises a fastening piece, an external thread part is arranged on the fastening piece, a threaded through hole matched with the fastening piece is formed in the mounting piece, and the fastening piece penetrates through the threaded through hole to abut against the rotor arm.
Further, the number of the rotor arms and the number of the mounting rods are four respectively.
Further, the control main body is integrated with a remote control module, and the remote control module can receive signals of ground remote control equipment to control the light source module, the rotary driving piece and the rotor arm.
Further, the light source module comprises a back shell and a light-emitting main body, wherein the back shell is fixedly connected with the light-emitting main body, and grooves matched with the mounting rods are respectively formed in one surface, close to the light-emitting main body, of the back shell.
Further, the back shell is in screw connection, snap connection or adhesive connection with the luminous main body.
Further, a plurality of heat dissipation fins are arranged on one surface of the back shell, which is far away from the luminous main body.
The utility model has the beneficial effects that: the unmanned aerial vehicle of this tethered unmanned aerial vehicle lighting system is equipped with rotary drive spare on the unmanned aerial vehicle body, can drive the cover through rotary drive spare and locate the light source module on the installation pole and rotate to change light source module's irradiation angle and irradiation range in real time, satisfy the illumination demand in real time, need not the angle at subaerial debugging light source module.
Drawings
Fig. 1 is a schematic diagram of the overall structure of a unmanned aerial vehicle in a tethered unmanned aerial vehicle lighting system according to a first embodiment of the present utility model;
FIG. 2 is an enlarged detail view of portion A of FIG. 1;
fig. 3 is a schematic diagram of the overall structure of a unmanned aerial vehicle in the tethered unmanned aerial vehicle lighting system according to the first embodiment of the present utility model;
fig. 4 is an exploded view of a light source module in a tethered unmanned aerial vehicle illumination system according to a first embodiment of the utility model.
Description of the reference numerals:
1. an unmanned body; 11. a mounting rod; 12. a control main body; 13. a rotor arm; 131. a clamping groove; 14. a mounting member; 15. a fastener;
2. a rotary driving member;
3. a light source module; 31. a back shell; 311. a heat radiation fin; 32. a light emitting body; 321. a groove; 322. a reflective trough.
Detailed Description
In order to describe the technical contents, the achieved objects and effects of the present utility model in detail, the following description will be made with reference to the embodiments in conjunction with the accompanying drawings.
Referring to fig. 1 to 4, a tethered unmanned aerial vehicle lighting system comprises a tethered case, an unmanned aerial vehicle body 1, a rotary driving piece 2 and a light source module 3, wherein the unmanned aerial vehicle body 1 is connected with the tethered case through a tethered line; the outside of unmanned aerial vehicle body 1 is equipped with a plurality of installation poles 11, light source module 3 cover is located on the installation pole 11, rotary driving piece 2 is fixed in on the installation pole 11 and drive connection light source module 3.
From the above description, the beneficial effects of the utility model are as follows: the unmanned aerial vehicle illuminating system is characterized in that the unmanned aerial vehicle body 1 is provided with the rotary driving piece 2, and the light source module 3 sleeved on the mounting rod 11 can be driven to rotate by the rotary driving piece 2, so that the illumination angle and the illumination range of the light source module 3 are changed in real time, the illuminating requirement is met in real time, and the angle of the light source module 3 is not required to be debugged on the ground.
Further, the unmanned aerial vehicle body 1 includes a control main body 12 and a plurality of rotor arms 13, the plurality of rotor arms 13 are arranged around the control main body 12, and two adjacent rotor arms 13 are respectively connected with two ends of one mounting rod 11.
As is clear from the above description, the mounting bar 11 is provided between the rotor arms 13 outside the control body 12, which is advantageous in expanding the irradiation range of the light source module 3.
Further, the rotor arm assembly further comprises an installation piece 14, the installation piece 14 is sleeved on the rotor arm 13, and two ends of the installation rod 11 are respectively connected with the two installation pieces 14.
As is apparent from the above description, the mounting member 14 is slid along the rotor arm 13, so that the mounting bars 11 with different lengths can be mounted on the unmanned aerial vehicle 1 to meet the assembly requirements of the light source modules 3 with different models and sizes, and the relative positions of the light source modules 3 and the control body 12 can be changed.
Further, the rotor arm assembly further comprises a fastener 15, an external thread part is arranged on the fastener 15, a threaded through hole matched with the fastener 15 is arranged on the mounting piece 14, and the fastener 15 passes through the threaded through hole to abut against the rotor arm 13.
From the above description, the mounting 14 is able to lock itself in relative position with the rotor arm 13 by means of friction between the fastener 15 and the rotor arm 13.
Further, the number of the rotor arms 13 and the mounting bars 11 is four, respectively.
Further, the control main body 12 has a remote control module integrated therein, and the remote control module is capable of receiving signals of a ground remote control device to control the light source module 3, the rotary driving member 2, and the rotor arm 13.
As can be seen from the above description, the worker can control the flight, lighting or not and the lighting angle of the unmanned aerial vehicle 1 on the ground through the remote control device.
Further, the light source module 3 includes a back shell 31 and a light-emitting body 32, the back shell 31 is fixedly connected with the light-emitting body 32, and grooves 321 matched with the mounting rod 11 are respectively provided on a surface of the back shell 31 close to the light-emitting body 32.
As can be seen from the above description, the light source module 3 and the mounting rod 11 are connected in a simple manner, which is beneficial to improving the assembly efficiency.
Further, the back shell 31 is screwed, snapped or glued to the light-emitting body 32.
Further, a plurality of heat dissipation fins 311 are disposed on a surface of the back shell 31 away from the light-emitting body 32.
As can be seen from the above description, the heat dissipation fins 311 can quickly conduct the heat generated by the light-emitting body 32 to the air, so that the light-emitting body 32 maintains a good working temperature, which is beneficial to improving the working life of the light-emitting body 32.
Example 1
Referring to fig. 1 to 4, a first embodiment of the present utility model is as follows: the tethered unmanned aerial vehicle lighting system is applied to the rescue or monitoring field and meets the requirement of large-area emergency lighting.
The tethered unmanned aerial vehicle lighting system comprises a tethered box, an unmanned aerial vehicle body 1, a rotary driving piece 2 and a light source module 3, wherein the unmanned aerial vehicle body 1 is connected with the tethered box through a tethered line; the outside of unmanned aerial vehicle body 1 is equipped with a plurality of installation poles 11, and light source module 3 cover is located on the installation pole 11, and rotary driving piece 2 is fixed in on the installation pole 11 and drive connection light source module 3. Specifically, the length of the mooring line is 50m. The mounting bar 11 is a cylindrical bar. As shown in fig. 1 and 3, the drone body 1 includes a control body 12 and four rotor arms 13, the four rotor arms 13 being arranged around the control body 12. The rotor arms 13, the rotary driving members 2 and the light source modules 3 are arranged in one-to-one correspondence, and two adjacent rotor arms 13 are respectively connected with two ends of one mounting rod 11. The longitudinal direction of the light source module 3 is parallel to the longitudinal direction of the mounting bar 11. The rotary driving member 2 is preferably a motor, and the rotary driving member 2 is fixedly mounted to one end of the mounting rod 11. The four light source modules 3 and the four rotary drivers 2 are symmetrically disposed at both sides of the control body 12, respectively, or the four light source modules 3 and the four rotary drivers 2 are symmetrically disposed with respect to the center of the control body 12, respectively. As a preferred embodiment, the light source module 3 is mounted on the mounting bar 11 by means of bearings.
Preferably, as shown in fig. 1 and 2, the unmanned aerial vehicle 1 further includes a mounting member 14, the mounting member 14 is sleeved on the rotor arm 13, and two ends of the mounting rod 11 are respectively in plug-in fit with the two mounting members 14. Specifically, the rotor arm 13 includes an arm portion and a rotor driving unit provided at one end of the arm portion, and the other end of the arm portion is connected to the control body 12. The mounting member 14 comprises a cylindrical barrel, a first connecting part and a second connecting part, wherein the first connecting part and the second connecting part are respectively arranged on two sides of the barrel, the barrel is sleeved on the arm part, the first connecting part is in plug-in fit with one end of one mounting rod 11, and the second connecting part is provided with the rotary driving member 2.
Preferably, as shown in fig. 2, the unmanned aerial vehicle 1 further includes a fastener 15, an external thread portion is provided on the fastener 15, a threaded through hole matched with the fastener 15 is provided on the mounting member 14, and the fastener 15 passes through the threaded through hole to abut against the rotor arm 13. In particular, threaded through holes are provided in the barrel of the mounting member 14, and the fasteners 15 are preferably fastening screws. As a preferred embodiment, the arm portion of the rotor arm 13 is provided with a plurality of engaging grooves 131 for engaging with the fastener 15, and the engaging grooves 131 are arranged at intervals along the length direction of the arm portion. It is easy to understand that the fastener 15 is snapped into the catch groove 131 to better prevent the mounting member 14 from sliding relative to the rotor arm 13, and to more conveniently keep the relative positions of the plurality of mounting bars 11 and the rotor arm 13 consistent, so as to avoid unstable flying posture caused by the offset of the center of gravity of the unmanned aerial vehicle body 1 to one side.
Preferably, the control body 12 has integrated therein a remote control module capable of receiving signals from a ground remote control device to control the light source module 3, the rotary drive 2 and the rotor arm 13. It is easy to understand that a worker can control the flying of the unmanned aerial vehicle 1 in the air, whether to emit light, and the irradiation angle of the light source module 3 on the ground through the remote control device.
Preferably, as shown in fig. 3 and 4, the light source module 3 includes a back shell 31 and a light emitting body 32, the back shell 31 is fixedly connected with the light emitting body 32, and grooves 321 matched with the mounting rods 11 are respectively arranged on one surface of the back shell 31, which is close to the light emitting body 32. In this embodiment, the back shell 31 is screwed to the light emitting body 32, and in other embodiments, the back shell 31 and the light emitting body 32 may be connected by a snap connection or an adhesive connection. Specifically, six light reflecting grooves 322 are disposed on a surface of the light emitting body 32 far away from the back shell 31, the six light reflecting grooves 322 are arranged at intervals along the length direction of the light emitting body 32, and each light reflecting groove 322 is provided with a lamp bead. The surface of the back shell 31 far away from the light-emitting main body 32 is rectangular, the four corners of the surface of the back shell 31 far away from the light-emitting main body 32 are respectively provided with countersunk holes, and the light-emitting main body 32 is provided with threaded holes corresponding to the countersunk holes, so that the back shell 31 is fixedly connected with the light-emitting main body 32 through screws. The cross section of the groove 321 is semicircular, and the bearing is arranged in the groove 321.
Preferably, as shown in fig. 4, a plurality of heat dissipation fins 311 are disposed on a surface of the back shell 31 away from the light emitting body 32.
In summary, the unmanned aerial vehicle body of the tethered unmanned aerial vehicle lighting system provided by the utility model is provided with the rotary driving piece, and the light source module sleeved on the mounting rod can be driven to rotate by the rotary driving piece, so that the irradiation angle and the irradiation range of the light source module are changed in real time, the lighting requirement is met in real time, and the angle of the light source module is not required to be debugged on the ground.
The foregoing description is only illustrative of the present utility model and is not intended to limit the scope of the utility model, and all equivalent changes made by the specification and drawings of the present utility model, or direct or indirect application in the relevant art, are included in the scope of the present utility model.

Claims (9)

1. The tethered unmanned aerial vehicle lighting system comprises a tethered box and an unmanned aerial vehicle body, wherein the unmanned aerial vehicle body is connected with the tethered box through a tethered line; the method is characterized in that: the unmanned aerial vehicle is characterized by further comprising a rotary driving piece and a light source module, wherein a plurality of mounting rods are arranged on the outer side of the unmanned aerial vehicle body, the light source module is sleeved on the mounting rods, and the rotary driving piece is fixed on the mounting rods and is in driving connection with the light source module.
2. The tethered unmanned lighting system of claim 1, wherein: the unmanned aerial vehicle body comprises a control main body and a plurality of rotor arms, wherein the rotor arms encircle the control main body, and two adjacent rotor arms are respectively connected with two ends of the mounting rod.
3. The tethered unmanned aerial vehicle lighting system of claim 2, wherein: the unmanned aerial vehicle body further comprises mounting pieces, the mounting pieces are sleeved on the rotor wing arms, and two ends of the mounting rod are connected with the two mounting pieces respectively.
4. A tethered unmanned lighting system according to claim 3, wherein: the unmanned aerial vehicle body further comprises a fastener, an external thread part is arranged on the fastener, a threaded through hole matched with the fastener is formed in the mounting piece, and the fastener penetrates through the threaded through hole to abut against the rotor arm.
5. The tethered unmanned aerial vehicle lighting system of claim 2, wherein: the number of the rotor arms and the number of the mounting rods are four respectively.
6. The tethered unmanned aerial vehicle lighting system of claim 2, wherein: the control main body is integrated with a remote control module, and the remote control module can receive signals of ground remote control equipment to control the light source module, the rotary driving piece and the rotor arm.
7. The tethered unmanned lighting system of claim 1, wherein: the light source module comprises a back shell and a light-emitting main body, wherein the back shell is fixedly connected with the light-emitting main body, and grooves matched with the mounting rods are respectively formed in one surface, close to the light-emitting main body, of the back shell.
8. The tethered unmanned aerial vehicle lighting system of claim 7, wherein: the back shell is connected with the luminous main body through screws, buckles or glue.
9. The tethered unmanned aerial vehicle lighting system of claim 7, wherein: and a plurality of radiating fins are arranged on one surface of the back shell, which is far away from the luminous main body.
CN202320993765.4U 2023-04-25 2023-04-25 Tethered unmanned aerial vehicle lighting system Active CN220010104U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202320993765.4U CN220010104U (en) 2023-04-25 2023-04-25 Tethered unmanned aerial vehicle lighting system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202320993765.4U CN220010104U (en) 2023-04-25 2023-04-25 Tethered unmanned aerial vehicle lighting system

Publications (1)

Publication Number Publication Date
CN220010104U true CN220010104U (en) 2023-11-14

Family

ID=88672209

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202320993765.4U Active CN220010104U (en) 2023-04-25 2023-04-25 Tethered unmanned aerial vehicle lighting system

Country Status (1)

Country Link
CN (1) CN220010104U (en)

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