CN219857637U - Unmanned aerial vehicle is with heat abstractor - Google Patents

Unmanned aerial vehicle is with heat abstractor Download PDF

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Publication number
CN219857637U
CN219857637U CN202321000963.2U CN202321000963U CN219857637U CN 219857637 U CN219857637 U CN 219857637U CN 202321000963 U CN202321000963 U CN 202321000963U CN 219857637 U CN219857637 U CN 219857637U
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China
Prior art keywords
aerial vehicle
unmanned aerial
mounting
heat dissipation
plate
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CN202321000963.2U
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Chinese (zh)
Inventor
刘义
廖远辉
李华桥
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Huizhou Chitongda Technology Co ltd
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Huizhou Chitongda Technology Co ltd
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Abstract

The utility model discloses a heat dissipation device for an unmanned aerial vehicle, which comprises a heat dissipation assembly arranged on the unmanned aerial vehicle assembly, wherein the heat dissipation assembly comprises an unmanned aerial vehicle body, a wing arranged on the unmanned aerial vehicle body and a base arranged at the lower end of the wing, an opening is formed in the middle of the lower end of the unmanned aerial vehicle body, the heat dissipation assembly comprises two mounting plates arranged in the opening, a slot formed in the inner sides of the two mounting plates, a micro motor arranged at the upper end of one mounting plate, and a screw rod fixed at the output end of the micro motor. This heat abstractor for unmanned aerial vehicle, through the fluting internal motion of the miniature motor drive picture peg to one side mounting panel that sets up, opening and external intercommunication for the inside hot air of unmanned aerial vehicle can circulate with outside cold air, reaches the purpose of carrying out the heat dissipation to unmanned aerial vehicle, and the dust screen of fixing simultaneously in picture peg one side plays dirt-proof effect to unmanned aerial vehicle in the heat dissipation process, prevents that external dust from entering into the inside spare part of damaging of unmanned aerial vehicle.

Description

Unmanned aerial vehicle is with heat abstractor
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle heat dissipation, in particular to a heat dissipation device for an unmanned aerial vehicle.
Background
Unmanned aircraft, abbreviated "drone", english abbreviation "UAV", is an unmanned aircraft that is maneuvered using a radio remote control device and a self-contained programmed control device, or is operated autonomously, either entirely or intermittently, by an onboard computer. The unmanned plane generates heat during the flying process, so that heat dissipation is required.
The utility model discloses a heat abstractor for unmanned aerial vehicle is disclosed to authorization bulletin number CN211893650U, which comprises a fuselage, the inside fixedly connected with mounting panel of fuselage, the top fixedly connected with micro motor of mounting panel, micro motor's stiff end fixedly connected with hob once has been said, the surface activity of hob has cup jointed the cover board, the bottom fixedly connected with movable plate of cover board, the bottom fixedly connected with picture peg of movable plate. This heat abstractor for unmanned aerial vehicle, through setting up micro motor and hob in the fuselage inside, set up the cover board on the surface of hob, be provided with the movable plate in the bottom of cover board, spout and recess have been seted up at the interior bottom wall of fuselage, micro motor drives the hob and rotates, drives the cover board and remove, drives the movable plate and removes for the picture peg removes, and a mouth has been opened to the fuselage bottom, and at unmanned aerial vehicle flight in-process, the inside hot air of fuselage can circulate with the outside cold air of fuselage, reaches the purpose of dispelling the heat to the fuselage.
In the above patent, the miniature motor is utilized to open the opening at the bottom of the machine body for heat dissipation, but when in actual use, external dust easily enters the machine body from the opening, and the damage of parts in the machine body is easily caused, therefore, we propose a heat dissipation device for the unmanned aerial vehicle.
Disclosure of Invention
This section is intended to outline some aspects of embodiments of the utility model and to briefly introduce some preferred embodiments. Some simplifications or omissions may be made in this section as well as in the description of the utility model and in the title of the utility model, which may not be used to limit the scope of the utility model.
The present utility model has been made in view of the above and/or problems occurring in the prior art unmanned aerial vehicle heat sink.
Therefore, the utility model aims to provide the heat dissipating device for the unmanned aerial vehicle, the screw rod is driven to rotate through the arranged micro motor, the rotating screw rod drives the movable plate to move, and the inserting plate is driven to move into the groove of the mounting plate at one side, so that the opening is communicated with the outside, hot air in the unmanned aerial vehicle and cold air outside the unmanned aerial vehicle can circulate, the purpose of dissipating heat of the unmanned aerial vehicle is achieved, and meanwhile, the dust screen fixed at one side of the inserting plate plays a role in preventing dust from entering the unmanned aerial vehicle in the heat dissipating process, and the outside dust is prevented from damaging parts inside the unmanned aerial vehicle.
In order to solve the technical problems, according to one aspect of the present utility model, the following technical solutions are provided:
a heat abstractor for unmanned aerial vehicle, comprising:
the heat dissipation assembly is arranged on the unmanned aerial vehicle assembly and comprises an unmanned aerial vehicle body, a wing arranged on the unmanned aerial vehicle body and a base arranged at the lower end of the wing, wherein an opening is formed in the middle of the lower end of the unmanned aerial vehicle body;
the heat dissipation assembly comprises two mounting plates arranged in the opening, a slot formed in the inner side of each mounting plate, a micro motor arranged at the upper end of one mounting plate, a screw rod fixed at the output end of the micro motor, a movable plate arranged outside the screw rod in a threaded manner, a plugboard vertically fixed at the lower end of the movable plate and a dust screen fixed at one side of the plugboard, wherein the outer wall of the plugboard far away from the dust screen end is attached to the slot of one mounting plate, and the outer wall of the dust screen far away from the plugboard end is attached to the slot of the other mounting plate;
preferably, a bottom plate is fixed at the lower end of the base, and the diameter of the bottom plate is larger than that of the base. The bottom plate that sets up has increased unmanned aerial vehicle and the area of contact on ground, ensures unmanned aerial vehicle's stability.
Preferably, a protection pad is fixed at the lower end of the bottom plate, and the protection pad is a rubber pad. The protection pad that sets up plays the effect of protection to the bottom plate, has prolonged the life of protection pad.
Preferably, a first mounting bolt is arranged at the lower end of the mounting plate, and penetrates through the mounting plate into the unmanned aerial vehicle body. The mounting plate fixed through the first mounting bolt later stage is convenient for the operator to take off the mounting plate to clear up the dust screen on the mounting plate.
Preferably, the lower end of the miniature motor is fixed with a mounting seat, the upper end of the mounting seat is provided with a second mounting bolt, and the second mounting bolt penetrates through the mounting seat to the mounting plate. Later-stage operator can take off the second bolt and take off micro motor from the mounting panel, is convenient for carry out dismouting maintenance to micro motor.
Preferably, the first and second mounting bolts are wing bolts. The operator can directly and manually screw the first mounting bolt and the second mounting bolt which are the butterfly bolts, so that the trouble of using tools is saved, the disassembly and assembly are convenient and rapid, and the time is saved.
Compared with the prior art, the utility model has the following beneficial effects:
(1) Through the micro motor drive lead screw that sets up rotation, pivoted lead screw drives fly leaf motion to drive the fluting internal motion of picture peg to one side mounting panel, make opening and external intercommunication, make the inside hot air of unmanned aerial vehicle and outside cold air can circulate, reach the purpose that dispels the heat to unmanned aerial vehicle, fix the dust screen in picture peg one side simultaneously and play dirt-proof effect to unmanned aerial vehicle in the heat dissipation process, prevent that external dust from entering into the inside spare part of damaging of unmanned aerial vehicle.
(2) The first mounting bolt and the second mounting bolt are arranged, so that an operator can conveniently take down the mounting plate and the miniature motor, and the dust screen can be cleaned and the miniature motor can be disassembled and overhauled in the later stage.
In conclusion, the utility model has the advantages of heat dissipation, dust prevention, convenient cleaning and maintenance.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present utility model, the following detailed description of the embodiments of the present utility model will be given with reference to the accompanying drawings, which are to be understood as merely some embodiments of the present utility model, and from which other drawings can be obtained by those skilled in the art without inventive faculty. Wherein:
FIG. 1 is a schematic perspective view of the present utility model;
FIG. 2 is a schematic perspective view of a heat dissipating assembly according to the present utility model;
FIG. 3 is a schematic view of the structure of the present utility model shown in FIG. 2 at a partially enlarged scale;
in the figure: 100. an unmanned aerial vehicle assembly; 110. an unmanned aerial vehicle body; 111. an opening; 120. a wing; 130. a base; 131. a bottom plate; 132. a protective pad; 200. a heat dissipation assembly; 210. a mounting plate; 211. a first mounting bolt; 220. slotting; 230. a micro motor; 231. a mounting base; 232. a second mounting bolt; 240. a screw rod; 250. a movable plate; 260. inserting plate; 270. a dust-proof net.
Detailed Description
In order that the above objects, features and advantages of the utility model will be readily understood, a more particular description of the utility model will be rendered by reference to the appended drawings.
Next, the present utility model will be described in detail with reference to the drawings, wherein the sectional view of the device structure is not partially enlarged to general scale for the convenience of description, and the drawings are only examples, which should not limit the scope of the present utility model. In addition, the three-dimensional dimensions of length, width and depth should be included in actual fabrication.
For the purpose of making the objects, technical solutions and advantages of the present utility model more apparent, embodiments of the present utility model will be described in further detail below with reference to the accompanying drawings.
The utility model provides a heat dissipating device for an unmanned aerial vehicle, which is characterized in that a screw rod is driven to rotate by a miniature motor, and the rotating screw rod drives a movable plate to move, so that a plugboard is driven to move into a slot of a mounting plate on one side, an opening is communicated with the outside, hot air in the unmanned aerial vehicle and cold air outside the unmanned aerial vehicle can circulate, the purpose of dissipating heat of the unmanned aerial vehicle is achieved, and meanwhile, a dust screen fixed on one side of the plugboard plays a role in preventing dust from entering the unmanned aerial vehicle from the outside in the heat dissipating process, so that parts inside the unmanned aerial vehicle are prevented from being damaged.
Fig. 1 to 3 are schematic structural diagrams of an embodiment of a heat dissipating device for an unmanned aerial vehicle of the present utility model, referring to fig. 1 to 3, a main body of the heat dissipating device for an unmanned aerial vehicle of the present embodiment includes a heat dissipating component 200 mounted on an unmanned aerial vehicle component 100.
The heat dissipation assembly 200 mounted on the unmanned aerial vehicle assembly 100 comprises an unmanned aerial vehicle body 110, a wing 120 arranged on the unmanned aerial vehicle body 110 and a base 130 arranged at the lower end of the wing 120, wherein an opening 111 is formed in the middle of the lower end of the unmanned aerial vehicle body 110. Preferably, in this embodiment, the bottom plate 131 is fixed at the lower end of the base 130, the diameter of the bottom plate 131 is larger than that of the base 130, the contact area between the base 130 and the ground is increased by the bottom plate 131 fixed at the lower end of the base 130, the whole unmanned aerial vehicle assembly 100 is ensured to be stably placed on the ground, the protection pad 132 is fixed at the lower end of the bottom plate 131, the protection pad 132 is a rubber pad, the protection pad 132 fixed at the lower end of the bottom plate 131 can prevent the bottom plate 131 from directly contacting the ground, the bottom plate 131 and the ground are prevented from being worn, and the service life of the bottom plate 131 is prolonged.
The heat dissipation assembly 200 comprises two mounting plates 210 arranged in the opening 111, a slot 220 formed in the inner side of the two mounting plates 210, a micro motor 230 arranged at the upper end of one mounting plate 210, a screw rod 240 fixed at the output end of the micro motor 230, a movable plate 250 arranged outside the screw rod 240 in a threaded manner, a plugboard 260 vertically fixed at the lower end of the movable plate 250 and a dust screen 270 fixed at one side of the plugboard 260, wherein the outer wall of the plugboard 260, far away from the dust screen 270, is attached to the slot 220 of one mounting plate 210, and the outer wall of the dust screen 270, far away from the plugboard 260, is attached to the slot 220 of the other mounting plate 210. As a preference, in this embodiment, the lower end of the mounting plate 210 is provided with the first mounting bolt 211, the first mounting bolt 211 penetrates the mounting plate 210 into the unmanned aerial vehicle body 110, the mounting plate 210 is mounted in the opening 111 of the unmanned aerial vehicle body 110 under the action of the first mounting bolt 211, the first mounting bolt 211 is removed by a later operator, the mounting plate 210 is taken out from the opening 111 so as to clean the dust screen 270, the mounting seat 231 is fixed at the lower end of the micro motor 230, the second mounting bolt 232 is arranged at the upper end of the mounting seat 231, the second mounting bolt 232 penetrates the mounting seat 231 into the mounting plate 210, the micro motor 230 is mounted on the mounting plate 210 through the second mounting bolt 232 under the action of the mounting seat 231, the mounting seat 231 is removed from the mounting plate 210 together with the micro motor 230 by the later operator, so that the micro motor 230 is convenient to disassemble and overhaul, the first mounting bolt 211 and the second mounting bolt 232 are butterfly bolts, the operator can directly and manually screw the first mounting bolt 211 and the second mounting bolt 232 which are butterfly bolts, the trouble is omitted, and the time is saved by means of rapid screwing.
Referring to fig. 1 to 3, a heat dissipating device for an unmanned aerial vehicle according to the present embodiment is specifically as follows: the micro motor 230 is started, the micro motor 230 drives the screw rod 240 to rotate, the rotating screw rod 240 controls the movable plate 250 to move in the groove 220 of the mounting plate 210 on one side, and then the inserting plate 260 is driven to move to one side, so that the inserting plate 260 completely enters the groove 220, the opening 111 is communicated with the outside, hot air inside the unmanned aerial vehicle and cold air outside the unmanned aerial vehicle can circulate, thereby the purpose of heat dissipation of the unmanned aerial vehicle is achieved, at the moment, the dust screen 270 fixed on one side of the inserting plate 260 moves to the opening 111, the unmanned aerial vehicle in the heat dissipation process plays a dustproof role, and external dust can be prevented from entering the inside parts of damage of the unmanned aerial vehicle.
Although the utility model has been described hereinabove with reference to embodiments, various modifications thereof may be made and equivalents may be substituted for elements thereof without departing from the scope of the utility model. In particular, the features of the disclosed embodiments may be combined with each other in any manner as long as there is no structural conflict, and the exhaustive description of these combinations is not given in this specification merely for the sake of omitting the descriptions and saving resources. Therefore, it is intended that the utility model not be limited to the particular embodiment disclosed, but that the utility model will include all embodiments falling within the scope of the appended claims.

Claims (6)

1. The utility model provides a heat abstractor for unmanned aerial vehicle which characterized in that includes:
the heat dissipation assembly (200) is arranged on the unmanned aerial vehicle assembly (100) and comprises an unmanned aerial vehicle body (110), a wing (120) arranged on the unmanned aerial vehicle body (110) and a base (130) arranged at the lower end of the wing (120), wherein an opening (111) is formed in the middle of the lower end of the unmanned aerial vehicle body (110);
the heat dissipation assembly (200) comprises two mounting plates (210) arranged in the opening (111), grooves (220) formed in the inner sides of the two mounting plates (210), a micro motor (230) arranged at the upper end of one mounting plate (210), a screw rod (240) fixed at the output end of the micro motor (230), a movable plate (250) arranged outside the screw rod (240) in a threaded mode, an inserting plate (260) vertically fixed at the lower end of the movable plate (250) and a dust screen (270) fixed on one side of the inserting plate (260), wherein the outer wall of the end of the inserting plate (260) far away from the dust screen (270) is attached in the groove (220) of one mounting plate (210), and the outer wall of the end of the dust screen (270) far away from the inserting plate (260) is attached in the groove (220) of the other mounting plate (210).
2. The heat dissipating device for an unmanned aerial vehicle according to claim 1, wherein a bottom plate (131) is fixed to a lower end of the base (130), and a diameter of the bottom plate (131) is larger than a diameter of the base (130).
3. The heat dissipating device for an unmanned aerial vehicle according to claim 2, wherein a protection pad (132) is fixed to the lower end of the bottom plate (131), and the protection pad (132) is a rubber pad.
4. The heat dissipating device for an unmanned aerial vehicle according to claim 1, wherein a first mounting bolt (211) is provided at the lower end of the mounting plate (210), and the first mounting bolt (211) penetrates through the mounting plate (210) into the unmanned aerial vehicle body (110).
5. The heat dissipating device for an unmanned aerial vehicle according to claim 1, wherein a mounting seat (231) is fixed at the lower end of the micro motor (230), a second mounting bolt (232) is provided at the upper end of the mounting seat (231), and the second mounting bolt (232) penetrates through the mounting seat (231) into the mounting plate (210).
6. The heat dissipating device for an unmanned aerial vehicle according to claim 1, wherein the first mounting bolt (211) and the second mounting bolt (232) are butterfly bolts.
CN202321000963.2U 2023-04-28 2023-04-28 Unmanned aerial vehicle is with heat abstractor Active CN219857637U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202321000963.2U CN219857637U (en) 2023-04-28 2023-04-28 Unmanned aerial vehicle is with heat abstractor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202321000963.2U CN219857637U (en) 2023-04-28 2023-04-28 Unmanned aerial vehicle is with heat abstractor

Publications (1)

Publication Number Publication Date
CN219857637U true CN219857637U (en) 2023-10-20

Family

ID=88341592

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202321000963.2U Active CN219857637U (en) 2023-04-28 2023-04-28 Unmanned aerial vehicle is with heat abstractor

Country Status (1)

Country Link
CN (1) CN219857637U (en)

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