CN110937124A - Lighting unmanned aerial vehicle - Google Patents
Lighting unmanned aerial vehicle Download PDFInfo
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- CN110937124A CN110937124A CN201911108004.0A CN201911108004A CN110937124A CN 110937124 A CN110937124 A CN 110937124A CN 201911108004 A CN201911108004 A CN 201911108004A CN 110937124 A CN110937124 A CN 110937124A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/02—Arrangements or adaptations of signal or lighting devices
- B64D47/04—Arrangements or adaptations of signal or lighting devices the lighting devices being primarily intended to illuminate the way ahead
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F3/00—Ground installations specially adapted for captive aircraft
- B64F3/02—Ground installations specially adapted for captive aircraft with means for supplying electricity to aircraft during flight
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
- H01B7/00—Insulated conductors or cables characterised by their form
- H01B7/17—Protection against damage caused by external factors, e.g. sheaths or armouring
- H01B7/18—Protection against damage caused by wear, mechanical force or pressure; Sheaths; Armouring
- H01B7/1895—Internal space filling-up means
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
- H01B9/00—Power cables
- H01B9/005—Power cables including optical transmission elements
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
- H01B9/00—Power cables
- H01B9/02—Power cables with screens or conductive layers, e.g. for avoiding large potential gradients
- H01B9/024—Power cables with screens or conductive layers, e.g. for avoiding large potential gradients composed of braided metal wire
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Lighting Device Outwards From Vehicle And Optical Signal (AREA)
Abstract
The invention belongs to the technical field of aircrafts, and particularly relates to an illumination unmanned aerial vehicle which comprises an unmanned aerial vehicle main body, a mooring cable and a mooring unit, wherein a belly lamp is arranged at the bottom of the unmanned aerial vehicle main body, the mooring unit comprises a generator, a direct-current high-voltage power supply and a mooring cable winch, the generator is electrically connected with the direct-current high-voltage power supply, the mooring cable is wound on the mooring cable winch, and two ends of the mooring cable are respectively electrically connected with the direct-current high-voltage power supply and the unmanned aerial vehicle main body. In the lighting unmanned aerial vehicle, on one hand, the mooring cables are wound on the mooring cable winch, so that the mooring cable winch has enough large-range activity space, and the flying height and diameter of the lighting unmanned aerial vehicle are ensured; on the other hand, the direct-current high-voltage power supply generates electric quantity through the generator, so that the lighting unmanned aerial vehicle can be ensured to have enough electric quantity to realize enough lighting time, and the lighting unmanned aerial vehicle can be ensured to realize an emergency lighting task.
Description
Technical Field
The invention belongs to the technical field of aircrafts, and particularly relates to an illumination unmanned aerial vehicle.
Background
In weak light environments such as power line repair and night search, normal operation at night cannot be performed due to the influence of the environment, and personal safety of operating personnel cannot be guaranteed. For this reason, among the prior art, adopt the mode of unmanned aerial vehicle flight to provide the illumination to reduce the influence that environment or personnel's limitation caused providing the illumination. For example, chinese application No. 201811551849.2 discloses a technical solution of a matrix lighting lamp based on unmanned aerial vehicle signal control and a method of use. Among this technical scheme, through adopting fixing bandage to stabilize the load matrix lamp under the unmanned aerial vehicle horn, then unmanned aerial vehicle takes off the back and realizes the illumination. However, in this kind of technical scheme, its power is supplied by the unmanned aerial vehicle battery, but is subject to the restriction of unmanned aerial vehicle self structure volume, and it can not carry the battery of big electric capacity, but the illumination time is shorter, leads to it can only carry out the illumination work in limited time.
Disclosure of Invention
The invention aims to provide an illumination unmanned aerial vehicle, and aims to solve the technical problem that the illumination time is short when a battery carried by the unmanned aerial vehicle is used as an illumination power supply when the unmanned aerial vehicle in the prior art performs illumination work.
In order to achieve the above purpose, an illumination unmanned aerial vehicle provided by the embodiment of the invention comprises an unmanned aerial vehicle main body, a mooring cable and a mooring unit, wherein a belly lamp is arranged at the bottom of the unmanned aerial vehicle main body, the mooring unit comprises a generator, a direct-current high-voltage power supply and a mooring cable winch, the generator is electrically connected with the direct-current high-voltage power supply, the mooring cable is wound on the mooring cable winch, and two ends of the mooring cable are respectively electrically connected with the direct-current high-voltage power supply and the unmanned aerial vehicle main body.
Preferably, the mooring cable comprises a bearing cable, a direct current power line, a communication optical fiber, a high-voltage insulating layer, a ground wire mesh and an outer sleeve, the direct current power line and the communication optical fiber are arranged around the bearing cable, the high-voltage insulating layer is coated on the peripheries of the direct current power line and the communication optical fiber, the ground wire mesh is coated on the periphery of the high-voltage insulating layer, and the outer sleeve is coated on the periphery of the ground wire mesh.
Preferably, the captive cable further comprises a strength material layer, wherein the strength material layer is filled between the high-voltage insulating layer and the ground wire net.
Preferably, the ground wire net is a metal net.
Preferably, be provided with rechargeable battery in the unmanned aerial vehicle main part.
Preferably, the belly lamps and lanterns include coupling mechanism, lighting fixture and a plurality of light, each the light all install in on the lighting fixture, coupling mechanism includes protruding seat of joint, joint recess seat and at least one latch segment, the protruding seat of joint with one of them in the joint recess seat with unmanned aerial vehicle main part bottom is connected, the protruding seat of joint with another one in the joint recess seat with the lighting fixture is connected, the protruding seat of joint with joint recess seat sliding fit, at least one the latch segment install in the protruding seat of joint or the lateral part of joint recess seat is used for locking the complex the protruding seat of joint with joint recess seat.
Preferably, protruding seat of joint includes first connecting block and sets up in dovetail on the first connecting block, joint recess seat include the second connecting block with set up in dovetail on the second connecting block, one of them in first connecting block with in the second connecting block with unmanned aerial vehicle main part bottom is connected, another one in first connecting block and the second connecting block with the lighting fixture is connected, the dovetail with dovetail sliding fit, at least one the latch segment install in the lateral part of first connecting block or second connecting block is used for locking complex the dovetail with the dovetail.
Preferably, the middle part of the dovetail block is provided with a deformation groove which penetrates through two opposite ends of the dovetail block, and the extending direction of the deformation groove is consistent with the sliding fit direction of the dovetail block and the dovetail groove.
Preferably, the lighting fixture includes the lamp panel, each light equipartition is installed on the lamp panel, joint protruding seat with one of them with in the joint recess seat with the lamp panel is connected.
Preferably, the lamp holder comprises a lamp disc and a u-shaped frame, the u-shaped frame is arranged in an inverted manner, an opening of the u-shaped frame faces to the side, the lamp disc is mounted at the bottom of the u-shaped frame, the lighting lamps are uniformly mounted on the lamp disc, and one of the clamping protrusion seat and the clamping groove seat is connected with the top of the u-shaped frame.
One or more technical solutions in the illumination unmanned aerial vehicle provided by the embodiment of the present invention at least have one of the following technical effects: in the lighting unmanned aerial vehicle, the belly lamp arranged at the bottom of the unmanned aerial vehicle main body is used for high-altitude lighting, a power supply required by the belly lamp is electrically connected with a direct-current high-voltage power supply of the mooring unit through the mooring cable, and the belly lamp is supplied with power through the direct-current high-voltage power supply; on the other hand, the direct-current high-voltage power supply generates electric quantity through the generator, so that the lighting unmanned aerial vehicle can be ensured to have enough electric quantity to realize enough lighting time, and the lighting unmanned aerial vehicle can be ensured to realize an emergency lighting task.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the embodiments or the prior art descriptions will be briefly described 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 to obtain other drawings based on these drawings without inventive exercise.
Fig. 1 is a schematic structural view of a belly light fixture of an illumination unmanned aerial vehicle according to an embodiment of the present invention.
Fig. 2 is a schematic structural view of a belly light fixture of a lighting drone according to another embodiment of the present invention.
Fig. 3 is a schematic structural diagram of another view angle of the belly light fixture of the lighting drone provided in the embodiment of fig. 2.
Fig. 4 is a schematic structural diagram of a view angle of a connecting mechanism of an illumination unmanned aerial vehicle according to an embodiment of the present invention.
Fig. 5 is a schematic structural diagram of another view angle of the connecting mechanism of the lighting drone according to the embodiment of the present invention.
Fig. 6 is a schematic structural view of a clamping boss of a connecting mechanism of an illumination unmanned aerial vehicle according to an embodiment of the present invention.
Fig. 7 is a schematic structural diagram of a clamping groove seat of a connecting mechanism of an illumination unmanned aerial vehicle according to an embodiment of the present invention.
Fig. 8 is a schematic structural diagram of an unmanned aerial vehicle main body of the illumination unmanned aerial vehicle provided in the embodiment of the present invention.
Fig. 9 is a schematic structural diagram of an illumination drone provided in the embodiment of the present invention.
Fig. 10 is a structural cross-sectional view of a mooring cable of an illumination drone provided by an embodiment of the present invention.
Wherein, in the figures, the respective reference numerals:
10-unmanned aerial vehicle main body 20-ventral lamp 21-connecting mechanism
22-lamp bracket 23-lighting lamp 30-mooring cable
31-bearing cable 32-direct current power line 33-communication optical fiber
34-high voltage insulating layer 35-ground wire net 36-outer sleeve
37-strength material layer 40-mooring unit 41-generator
42-DC high-voltage power supply 43-mooring winch 211-clamping convex seat
212-clamping groove seat 213-locking block 221-lamp panel
222-U-shaped frame 2111-first connecting block 2112-dovetail block
2121-second connecting block 2122-dovetail groove 21121-deformation groove.
Detailed Description
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to fig. 1-10 are exemplary and intended to be used to illustrate embodiments of the invention, and should not be construed as limiting the invention.
In the description of the embodiments of the present invention, it should be understood that the terms "length", "width", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc. indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience in describing the embodiments of the present invention and simplifying the description, but do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the embodiments of the present invention, "a plurality" means two or more unless specifically limited otherwise.
In the embodiments of the present invention, unless otherwise explicitly specified or limited, the terms "mounted," "connected," "fixed," and the like are to be construed broadly, e.g., as being fixedly connected, detachably connected, or integrated; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. Specific meanings of the above terms in the embodiments of the present invention can be understood by those of ordinary skill in the art according to specific situations.
In an embodiment of the present invention, as shown in fig. 9 to 10, there is provided an illumination unmanned aerial vehicle, including an unmanned aerial vehicle main body 10, a mooring cable 30 and a mooring unit 40, wherein a belly light 20 is disposed at a bottom of the unmanned aerial vehicle main body 10, the mooring unit 40 includes a generator 41, a dc high voltage power supply 42 and a mooring winch 43, the generator 41 is electrically connected to the dc high voltage power supply 42, the mooring cable 30 is wound around the mooring winch 43, and two ends of the mooring cable 30 are electrically connected to the dc high voltage power supply 42 and the unmanned aerial vehicle main body 10, respectively.
In the lighting unmanned aerial vehicle, the belly lamp 20 arranged at the bottom of the unmanned aerial vehicle main body 10 is used for high-altitude lighting, a power supply required by the belly lamp 20 is electrically connected with the direct-current high-voltage power supply 42 of the mooring unit 40 through the mooring cable 30, and the belly lamp 20 is supplied with power through the direct-current high-voltage power supply 42, on one hand, the mooring cable 30 is wound on the mooring cable winch 43, so that the lighting unmanned aerial vehicle has a large enough range of activity space, and the flying height and diameter of the lighting unmanned aerial vehicle are ensured; on the other hand, the direct-current high-voltage power supply 42 generates electric quantity through the generator 41, so that the lighting unmanned aerial vehicle can be ensured to have enough electric quantity to realize enough lighting time, and the lighting unmanned aerial vehicle can be ensured to realize an emergency lighting task.
The illumination unmanned aerial vehicle provided by the embodiment of the invention at least has the following advantages:
firstly, the method is helpful for reducing unnecessary casualties in emergency rescue: the problems that the traditional mobile illuminating lamp 23 tower is flexible, poor in flexibility, difficult to adapt to severe environment sites, difficult to transport, difficult to rapidly deploy and the like are solved, and unnecessary casualties caused by untimely emergency illumination supply are reduced.
Secondly, the method helps to stabilize the mind of people in emergency rescue, improves the image of power supply enterprises, and embodies the social responsibility of the power enterprises: under the condition of sudden disasters, particularly at night, because the damage of a power grid causes electric paralysis in a disaster area, the disaster-stricken masses are easy to be highly panic in a dark environment, and power supply enterprises provide stable and reliable large-area illumination on the spot in the first time, can stabilize the mind to a greater extent, are convenient to maintain, and can greatly improve the image of the power supply enterprises and embody the social responsibility of the power grid enterprises at key moments.
Third, help reduce emergency lighting equipment investment: in the emergency work of the power emergency, the emergency lighting work is an indispensable important link in the whole emergency procedure, and the selection of the related emergency lighting equipment and the formulation of the emergency lighting scheme are of great importance to the whole emergency work. The 800W high-power LED lighting system is designed and carried on an emergency all-time airspace lighting system, and 8000-10000 m of illumination can be provided for an emergency rescue site2Effective illumination, simultaneously in illumination unmanned aerial vehicle's the belly bottom design carry on 200W strenghthened type illumination, can carry out illumination angle through remote control and freely adjust, carry out the illuminance to special or specified region and strengthen. The analysis from illumination area and lighting effect, be equivalent to several even tens of large-scale removal lighthouses's lighting effect, can reduce the input of lighting apparatus to a great extent.
Fourthly, help the scene rescue at night, reduce the rescue and put into, reduce the rescue cost, improve rescue efficiency: the emergency full-time airspace lighting system integrates a high-power lighting system and a wireless picture transmission system, can provide clear images for an emergency command center at night, helps the emergency command center to carry out reconnaissance on the site in advance, carries out integral assessment on the site condition, reasonably schedules superior resources, realizes optimal utilization of the resources through overall and overall measures, and finishes emergency rescue work in the shortest time.
Fifthly, the field personnel investment is reduced, and the personnel allocation efficiency is improved: the emergency full-time airspace lighting system combines the advantages of an illumination unmanned aerial vehicle, optimizes emergency lighting equipment from multiple aspects such as equipment transportation, weight, illumination power, mobility and rapid deployment, reduces personnel investment, and improves personnel allocation efficiency of emergency management departments.
In another embodiment of the present invention, as shown in fig. 10, the mooring cable 30 includes a messenger cable 31, a dc power line 32, a communication optical fiber 33, a high-voltage insulating layer 34, a ground wire mesh 35 and an outer sleeve 36, the dc power line 32 and the communication optical fiber 33 are surrounded on the outer periphery of the messenger cable 31, the high-voltage insulating layer 34 is coated on the outer peripheries of the dc power line 32 and the communication optical fiber 33, the ground wire mesh 35 is coated on the outer periphery of the high-voltage insulating layer 34, and the outer sleeve 36 is coated on the outer periphery of the ground wire mesh 35. The mooring cable 30 having such a structure can realize current transmission and transmission of an electric signal, and is good in durability, suitable for field or outdoor use, and not easy to damage due to high-strength work in severe environments.
In another embodiment of the present invention, as shown in fig. 10, the mooring cable 30 further comprises a layer of strength material 37, wherein the layer of strength material 37 is filled between the high voltage insulation layer 34 and the ground wire network 35. Specifically, intensity material layer 37 can strengthen the intensity of mooring cable 30, in the use, even receive powerful centrifugal force or striking etc. can effectively prevent the problem emergence of fracture etc. ensure to be the transport for illumination unmanned aerial vehicle power supply and signal.
Preferably, the ground wire net 35 is a metal net.
In another embodiment of the present invention, a rechargeable battery is disposed on the main body 10 of the drone. Rechargeable battery can regard as stand-by power supply, at the scope that mooring cable 30 can not touch, can use stand-by power supply through temporarily not using mooring cable 30, but unmanned aerial vehicle main part 10's flight is bigger like this, uses more in a flexible way.
In another embodiment of the invention, as shown in fig. 4 to 7, the belly light fixture 20 is installed on the belly (bottom of main body) of the main body 10 of the unmanned aerial vehicle, so that the horn light fixture different from the conventional lighting unmanned aerial vehicle is installed on the bottom of the wing wall of the lighting unmanned aerial vehicle, and further, the irradiated light can be more concentrated, and the lighting effect is better. Specifically, the belly light fixture 20 of the present embodiment includes a connecting mechanism 21, a lamp holder 22 and a plurality of illuminating lamps 23, and different numbers of illuminating lamps 23 can be selected according to actual requirements, such as the size of an applicable lighting drone. Each light 23 all install in on lighting fixture 22, realize being connected through lighting fixture 22 and illumination unmanned aerial vehicle's ventral.
Further, as shown in fig. 4 to 5, the connecting mechanism 21 includes a clamping protrusion seat 211, a clamping groove seat 212, and at least one locking block 213, one of the clamping protrusion seat 211 and the clamping groove seat 212 is connected to the bottom of the main body 10 of the unmanned aerial vehicle, and the other of the clamping protrusion seat 211 and the clamping groove seat 212 is connected to the lamp holder 22, that is, when the clamping protrusion seat 211 is connected to the bottom of the main body 10 of the unmanned aerial vehicle, the clamping groove seat 212 is connected to the frame; similarly, when the clamping groove seat 212 is connected with the bottom of the main body 10 of the unmanned aerial vehicle, the clamping convex seat 211 is connected with the frame. The clamping convex seat 211 is matched with the clamping groove seat 212 in a sliding mode, namely, the clamping convex seat 211 can be drawn into the clamping groove seat 212 relative to the clamping groove seat 212 and can be matched with the clamping groove seat 212. At least one locking block 213 is installed at the side of the clamping protrusion seat 211 or the clamping groove seat 212 and is used for locking the clamping protrusion seat 211 and the clamping groove seat 212. Specifically, the locking block 213 may be one or two, and may be installed at a side of the catching protrusion holder 211 or the catching groove holder 212 using one locking block 213, and the catching protrusion holder 211 may be locked with the catching groove holder 212 by rotating the locking block 213. Accordingly, the two locking blocks 213 can be used to clamp the sides of the two locking block 213 mounting seats 211 and the clamping groove seat 212, respectively, and also can lock the connection between the clamping protrusion seat 211 and the clamping groove seat 212.
The belly light fixture 20 of the embodiment of the invention can be applied to lighting the belly of the unmanned aerial vehicle, namely can be arranged at the bottom of the main body 10 of the unmanned aerial vehicle, since it includes the connection mechanism 21, and the connection mechanism 21 includes the catching convex seat 211, the catching concave seat 212 and at least one locking block 213, when installed, by mounting two of the snap boss 211 and the snap recess 212 on the bottom of the main body 10 of the drone and on the lamp holder 22 respectively, then the clamping convex seat 211 is slid into the clamping groove seat 212 to realize the matching connection with the clamping groove seat 212, and finally the clamping convex seat 211 and the clamping groove seat 212 which are matched and connected are locked and connected by the locking block 213, so that the belly lamp 20 is very convenient to be installed on the unmanned lighting vehicle, in addition, the clamping convex seat 211 and the clamping groove seat 212 are matched and then locked by the locking block 213, so that the stability of the belly light 20 after installation can be effectively guaranteed.
In another embodiment of the present invention, as shown in fig. 4 to 7, the clamping protrusion holder 211 includes a first connection block 2111 and a dovetail block 2112 disposed on the first connection block 2111, the clamping groove holder 212 includes a second connection block 2121 and a dovetail groove 2122 disposed on the second connection block 2121, one of the first connection block 2111 and the second connection block 2121 is connected to the bottom of the main body 10 of the drone, the other of the first connection block 2111 and the second connection block 2121 is connected to the lamp holder 22, the dovetail block 2112 is slidably fitted into the dovetail groove 2122, specifically, the first connection block 2111 and the second connection block 2121 have substantially the same or the same structure, such as a square or a circle, and may also have other irregular shapes, by protruding a dovetail block 2112 on the first connection block 2111 and digging a dovetail groove 2122 on the second connection block 2121, and ensures that the dovetail block is identical to and can fit within the cross-section of the dovetail slot 2122, creating a clearance fit so that when the dovetail block 2112 is slid into the dovetail slot 2122, an interlocking fit is achieved and the dovetail block 2112 and dovetail slot 2122, once mated, do not easily release due to the dovetail-shaped configuration. Further, at least one locking block 213 is installed at a side of the first connecting block 2111 or the second connecting block 2121 and serves to lock the dovetail block 2112 and the dovetail groove 2122 in cooperation. Namely, the dovetail block 2112 and the dovetail groove 2122 which are matched with each other can be locked and connected by rotating the locking block 213 by a certain angle, thereby realizing the installation and fixation of the belly light 20.
Preferably, the corners of the dovetail block 2112 are chamfered to facilitate assembly and reduce interference and collision between the dovetail block 2112 and the walls of the dovetail slot 2122.
It should be noted that the cross-section of both the dovetail block 2112 and the dovetail groove 2122 in the present embodiment has a dovetail shape or a substantially dovetail shape. I.e. with a trapezoidal cross-section.
In another embodiment of the invention, as shown in fig. 4 and 6 to 7, deformation grooves 21121 penetrating through opposite ends of the dovetail block 2112 are arranged in the middle of the dovetail block 2112, and the extending direction of the deformation grooves 21121 is consistent with the sliding fit direction of the dovetail block 2112 and the dovetail groove 2122, so that the design can avoid the deformation grooves 21121 from damaging the fit position of the dovetail block 2112 and the dovetail groove 2122, and ensure that the dovetail block 2112 can be normally in sliding fit with the dovetail groove 2122. Specifically, the deformation groove 21121 is set up as the space provided by the deformation of the dovetail block 2112, namely, when the dovetail block 2112 is slid into the dovetail groove 2122, the dovetail block 2112 receives a certain extrusion force and then can generate a small deformation, so that the dovetail block can be matched with the dovetail groove 2122 more quickly and easily, the structural design is ingenious, the connection of the connecting mechanism 21 is facilitated, the design is reasonable, and the practicability is high.
In another embodiment of the present invention, as shown in fig. 1 to 3, the lamp holder 22 includes a lamp panel 221, the lamps 23 are uniformly installed on the lamp panel 221, and one of the clamping protrusion seat 211 and the clamping groove seat 212 is connected to the lamp panel 221. Specifically, the lamp panel 221 can collectively install the respective illumination lamps 23 together, which is beneficial to the respective illumination lamps 23 to collectively illuminate the light together, thereby improving the illumination effect. Moreover, the lighting lamps 23 can be installed in a centralized manner through the lamp panel 221, and then the lamp panel 221 is connected with the bottom of the unmanned aerial vehicle main body 10 through the connecting mechanism 21, so that the lighting lamps 23 can be installed on the unmanned aerial vehicle.
In another embodiment of the present invention, as shown in fig. 1, the lamp holder 22 includes a lamp disc 221 and a u-shaped frame 222, the u-shaped frame 222 is inverted, the opening of the u-shaped frame 222 faces the side, the lamp disc 221 is mounted at the bottom of the u-shaped frame 222, the illuminating lamps 23 are uniformly mounted on the lamp disc 221, and one of the u-shaped frame 222 and the u-shaped frame 212 is connected to the top of the u-shaped frame 222. Specifically, the u-shaped frame 222 serves as a centering member between the lamp panel 221 and the main body 10 of the drone, so that the lamp panel 221 is vertically installed, and thus the illumination direction of the illumination lamp 23 is also located laterally, thereby forming illumination at different angles. Wherein, the connection between the lamp plate 221 and the U-shaped frame 222 can be realized by a detachable connection manner of a fastener.
In another embodiment of the present invention, an angle adjuster (not shown) for adjusting an illumination angle of the illumination lamp 23 is installed between the illumination lamp 23 and the lamp holder 22. Specifically, the angle adjuster can be arranged to adjust the angle of the illuminating lamp 23, so that the illumination in different directions can be realized by adjusting the angle of the illuminating lamp 23. Further, the angle adjuster may be a joint such as a universal joint or the like that can be positioned.
In another embodiment of the present invention, as shown in fig. 1-2, the illumination lamp 23 includes a lamp housing (not shown) and a lamp bead (not shown), the lamp housing is installed on the lamp holder 22, the lamp bead is disposed inside the lamp housing, and a heat sink (not shown) is further disposed inside the lamp housing. Specifically, set up the fin in the inside of lamp body, scatter and disappear when going on the heat that can produce the inside lamp pearl of lamp body, reduce the influence that high temperature caused the lamp pearl, improve light 23's life.
In another embodiment of the present invention, as shown in fig. 1-2, the lamp housing is made of an aircraft material. Specifically, the aircraft material may be, for example, a metal material (structural steel, stainless steel, high-temperature alloy, non-ferrous metal, alloy, etc.), an organic polymer material (rubber, plastic, transparent material, paint, etc.), and a composite material, which has advantages of light weight and long service life.
In another embodiment of the invention, as shown in fig. 1-2, the lamp bead is a high-flux three-dimensional lamp bead. The high-flux three-dimensional lamp bead is, for example, an 800W high-power LED lamp bead, and can be8000-1000 m of emergency rescue site is provided2The effective illumination of (1).
Because the lighting unmanned aerial vehicle of the embodiment uses the ventral lamp 20, the lamp on the lighting unmanned aerial vehicle is installed in a clamping and locking manner, which is different from the traditional installation manner of binding, so that the installation convenience is greatly improved, and the stability of the ventral lamp 20 after installation is greatly improved.
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 invention, 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 illumination unmanned aerial vehicle, its characterized in that: including unmanned aerial vehicle main part, mooring cable and mooring unit, the bottom of unmanned aerial vehicle main part is provided with the ventral lamps and lanterns, mooring unit includes generator, direct current high voltage power supply and mooring rope capstan winch, the generator with direct current high voltage power supply electricity is connected, mooring cable all around in on the mooring rope capstan winch, just mooring cable's both ends respectively with direct current high voltage power supply with unmanned aerial vehicle main part electricity is connected.
2. The unmanned aerial vehicle of claim 1, wherein: the mooring cable comprises a bearing cable, a direct current power line, a communication optical fiber, a high-voltage insulating layer, a ground wire net and an outer sleeve, wherein the direct current power line and the communication optical fiber are arranged around the periphery of the bearing cable, the high-voltage insulating layer is coated on the periphery of the direct current power line and the periphery of the communication optical fiber, the ground wire net is coated on the periphery of the high-voltage insulating layer, and the outer sleeve is coated on the periphery of the ground wire net.
3. The illuminated drone of claim 2, wherein: the mooring cable further comprises a strength material layer, and the strength material layer is filled between the high-voltage insulating layer and the ground wire net.
4. A belly light fixture according to claim 2, wherein: the ground wire net is a metal net.
5. The unmanned aerial vehicle of claim 1, wherein: be provided with rechargeable battery in the unmanned aerial vehicle main part.
6. An illuminating unmanned aerial vehicle according to any one of claims 1-5, wherein: the belly lamps and lanterns include coupling mechanism, lighting fixture and a plurality of light, each the light all install in on the lighting fixture, coupling mechanism includes joint protruding seat, joint recess seat and at least one latch segment, the joint protruding seat with one of them in the joint recess seat with unmanned aerial vehicle main part bottom is connected, the joint protruding seat with another one in the joint recess seat with the lighting fixture is connected, the joint protruding seat with joint recess seat sliding fit, at least one the latch segment install in the joint protruding seat or the lateral part of joint recess seat is used for locking the complex the joint protruding seat with joint recess seat.
7. A belly light fixture according to claim 6, wherein: protruding seat of joint includes first connecting block and sets up in dovetail on the first connecting block, joint recess seat include the second connecting block with set up in dovetail on the second connecting block, first connecting block with one of them in the second connecting block with unmanned aerial vehicle main part bottom is connected, another one in first connecting block and the second connecting block with the lighting fixture is connected, the dovetail with dovetail sliding fit, at least one the latch segment install in the lateral part of first connecting block or the second connecting block is used for locking the complex the dovetail with the dovetail.
8. A belly light fixture according to claim 7, wherein: the middle part of the dovetail block is provided with a deformation groove which penetrates through two opposite ends of the dovetail block, and the extending direction of the deformation groove is consistent with the sliding fit direction of the dovetail block and the dovetail groove.
9. A belly light fixture according to claim 6, wherein: the lighting fixture includes the lamp panel, each the light equipartition is installed on the lamp panel, joint protruding seat with one of them with in the joint recess seat with the lamp panel is connected.
10. A belly light fixture according to claim 6, wherein: the U-shaped frame is arranged in an inverted mode, the opening of the U-shaped frame faces the side, the lamp disc is installed at the bottom of the U-shaped frame, the illuminating lamps are evenly installed on the lamp disc, and one of the clamping protruding seat and the clamping groove seat is connected with the top of the U-shaped frame.
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| CN201911108004.0A CN110937124A (en) | 2019-11-13 | 2019-11-13 | Lighting unmanned aerial vehicle |
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| CN201911108004.0A CN110937124A (en) | 2019-11-13 | 2019-11-13 | Lighting unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111650949A (en) * | 2020-06-30 | 2020-09-11 | 深圳高度创新技术有限公司 | Mooring unmanned aerial vehicle control system and method |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2759716A1 (en) * | 2013-01-25 | 2014-07-30 | Adrianus Franciscus Maria Verbossen | Dovetail connection for releasably connecting two construction elements |
| CN204297104U (en) * | 2014-12-04 | 2015-04-29 | 马鞍山市靓马航空科技有限公司 | A kind of monitoring aircraft of leaving a blank that intense light source searchlighting is provided |
| KR101730496B1 (en) * | 2016-03-31 | 2017-05-11 | 삼우금속공업 주식회사 | Manufacturing method of strobe light housing |
| CN107046437A (en) * | 2016-12-15 | 2017-08-15 | 北京计算机技术及应用研究所 | A kind of vehicle-mounted unmanned aerial vehicle is tethered at signal reconnaissance system |
| US20170240277A1 (en) * | 2015-12-28 | 2017-08-24 | Dezso Molnar | Tethered Unmanned Aerial System |
| US20170305537A1 (en) * | 2016-04-20 | 2017-10-26 | Tenshi Technologies, LLC (A Utah, LLC) | Un-manned aerial vehicle |
| CN207697997U (en) * | 2018-01-03 | 2018-08-07 | 江苏和正特种装备有限公司 | A kind of more rotors of measurement type are tethered at unmanned vehicle system |
| WO2018147522A1 (en) * | 2017-02-08 | 2018-08-16 | (주)두영티앤에스 | Flying lighting device having heat dissipation part provided in gimbal |
| KR101949246B1 (en) * | 2018-03-14 | 2019-02-18 | 조한희 | Drones with searchlight function |
| CN209396060U (en) * | 2018-10-19 | 2019-09-17 | 桂林系留航空科技有限公司 | It is conveniently replaceable the police of headlamp and is tethered at UAV Intelligent lift-off platform |
| CN211442795U (en) * | 2019-11-13 | 2020-09-08 | 深圳市光明顶照明科技有限公司 | Lighting unmanned aerial vehicle |
-
2019
- 2019-11-13 CN CN201911108004.0A patent/CN110937124A/en active Pending
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2759716A1 (en) * | 2013-01-25 | 2014-07-30 | Adrianus Franciscus Maria Verbossen | Dovetail connection for releasably connecting two construction elements |
| CN204297104U (en) * | 2014-12-04 | 2015-04-29 | 马鞍山市靓马航空科技有限公司 | A kind of monitoring aircraft of leaving a blank that intense light source searchlighting is provided |
| US20170240277A1 (en) * | 2015-12-28 | 2017-08-24 | Dezso Molnar | Tethered Unmanned Aerial System |
| KR101730496B1 (en) * | 2016-03-31 | 2017-05-11 | 삼우금속공업 주식회사 | Manufacturing method of strobe light housing |
| US20170305537A1 (en) * | 2016-04-20 | 2017-10-26 | Tenshi Technologies, LLC (A Utah, LLC) | Un-manned aerial vehicle |
| CN107046437A (en) * | 2016-12-15 | 2017-08-15 | 北京计算机技术及应用研究所 | A kind of vehicle-mounted unmanned aerial vehicle is tethered at signal reconnaissance system |
| WO2018147522A1 (en) * | 2017-02-08 | 2018-08-16 | (주)두영티앤에스 | Flying lighting device having heat dissipation part provided in gimbal |
| CN207697997U (en) * | 2018-01-03 | 2018-08-07 | 江苏和正特种装备有限公司 | A kind of more rotors of measurement type are tethered at unmanned vehicle system |
| KR101949246B1 (en) * | 2018-03-14 | 2019-02-18 | 조한희 | Drones with searchlight function |
| CN209396060U (en) * | 2018-10-19 | 2019-09-17 | 桂林系留航空科技有限公司 | It is conveniently replaceable the police of headlamp and is tethered at UAV Intelligent lift-off platform |
| CN211442795U (en) * | 2019-11-13 | 2020-09-08 | 深圳市光明顶照明科技有限公司 | Lighting unmanned aerial vehicle |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111650949A (en) * | 2020-06-30 | 2020-09-11 | 深圳高度创新技术有限公司 | Mooring unmanned aerial vehicle control system and method |
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