CN211139647U

CN211139647U - Heat radiator for carbon fiber unmanned aerial vehicle casing is used

Info

Publication number: CN211139647U
Application number: CN201921733714.8U
Authority: CN
Inventors: 蓝东延
Original assignee: XIAMEN ORACE COMPOSITE TECHNOLOGY CO LTD
Current assignee: Xiamen Oushi Composite Technology Co ltd
Priority date: 2019-10-16
Filing date: 2019-10-16
Publication date: 2020-07-31
Anticipated expiration: 2029-10-16

Abstract

The utility model belongs to the technical field of unmanned aerial vehicle equipment, specifically disclose a heat abstractor that carbon fiber unmanned aerial vehicle casing used, including unmanned aerial vehicle top shell, unmanned aerial vehicle drain pan, wing mounting bracket, first heat abstractor and second heat abstractor, unmanned aerial vehicle top shell middle part is provided with first heat abstractor, the unmanned aerial vehicle drain pan passes through fixing bolt and installs in unmanned aerial vehicle top shell below, unmanned aerial vehicle drain pan bilateral symmetry is provided with the second heat abstractor, wing mounting bracket symmetry sets up four sides at the unmanned aerial vehicle drain pan. The utility model discloses an unmanned aerial vehicle can be opened to the first heat abstractor and the second heat abstractor that set up for unmanned aerial vehicle is inside can realize ventilation cooling, accelerates the radiating efficiency, guarantees unmanned aerial vehicle's normal work, the utility model discloses simple structure, convenient operation, the practicality is strong.

Description

Heat radiator for carbon fiber unmanned aerial vehicle casing is used

Technical Field

The utility model relates to a heat abstractor that carbon fiber unmanned aerial vehicle casing used belongs to unmanned aerial vehicle equipment technical field.

Background

Unmanned aircraft, also known as "drones," are unmanned aircraft that are operated by radio remote control devices and self-contained program control devices, or are operated autonomously, either completely or intermittently, by an onboard computer, and are often more suited to tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil according to application fields, and unmanned aerial vehicles can be classified into reconnaissance planes and target planes; in the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.

The shell of the existing unmanned aerial vehicle is generally closed, so that the heat dissipation performance of the unmanned aerial vehicle is poor, the unmanned aerial vehicle is difficult to normally work stably for a long time, and the problem is solved by the heat dissipation device for the shell of the carbon fiber unmanned aerial vehicle.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a heat abstractor that carbon fiber unmanned aerial vehicle casing was used to solve the problem that proposes among the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a heat abstractor that carbon fiber unmanned aerial vehicle casing was used, includes unmanned aerial vehicle top shell, unmanned aerial vehicle drain pan, wing mounting bracket, first heat abstractor and second heat abstractor, unmanned aerial vehicle top shell middle part is provided with first heat abstractor, the unmanned aerial vehicle drain pan passes through fixing bolt and installs in unmanned aerial vehicle top shell below, unmanned aerial vehicle drain pan bilateral symmetry is provided with second heat abstractor, wing mounting bracket symmetry sets up four sides at the unmanned aerial vehicle drain pan.

Preferably, first heat abstractor includes heating panel, connecting axle, driven gear, mounting bracket, driving motor and drive gear, the heating panel passes through the connecting axle symmetry and sets up at unmanned aerial vehicle top shell middle part, be provided with driven gear on the connecting axle, driving motor passes through the mounting bracket and installs in unmanned aerial vehicle top shell bottom, the last drive gear that is provided with of driving motor, drive gear and driven gear intermeshing.

Preferably, the second heat abstractor includes baffle, mounting groove, spout, elevator motor and lifter, unmanned aerial vehicle drain pan bilateral symmetry is provided with the mounting groove, be provided with the baffle in the mounting groove, the mounting groove bilateral symmetry is provided with the spout, the spout top is provided with elevator motor, the last lifter that is provided with of elevator motor, lifter bottom end connection baffle bottom.

Preferably, the heat dissipation plate is provided with sealing gaskets on four sides.

Preferably, the bottom end of the baffle is provided with a sealing gasket, and the bottom end of the mounting groove is provided with a dust screen.

Compared with the prior art, the beneficial effects of the utility model are that:

the utility model belongs to the technical field of unmanned aerial vehicle equipment, specifically disclose a heat abstractor that carbon fiber unmanned aerial vehicle casing used can open the unmanned aerial vehicle shell through the first heat abstractor and the second heat abstractor who sets up for unmanned aerial vehicle can realize ventilation cooling, strengthens unmanned aerial vehicle's radiating effect, guarantees that unmanned aerial vehicle can stabilize normal work for a long time, the utility model discloses simple structure, convenient operation, the practicality is strong.

Drawings

Fig. 1 is a schematic structural view of the present invention;

fig. 2 is a schematic view of a first heat dissipation device of the present invention;

fig. 3 is a schematic view of a second heat dissipation device of the present invention;

fig. 4 is a side view of a second heat dissipation device of the present invention;

in the figure: 1. an unmanned aerial vehicle top shell; 2. a bottom shell of the unmanned aerial vehicle; 3. a wing mount; 4. a first heat sink; 5. a second heat sink; 6. fixing the bolt; 7. a heat dissipation plate; 8. a connecting shaft; 9. a driven gear; 10. a mounting frame; 11. a drive motor; 12. a drive gear; 13. a baffle plate; 14. mounting grooves; 15. a chute; 16. a lifting motor; 17. a lifting rod; 18. connecting blocks; 19. a gasket; 20. a dust screen.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

In the description of the present invention, it should be noted that the terms "vertical", "upper", "lower", "horizontal", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed in a specific orientation, and be operated, and thus should not be construed as limiting the present invention.

In the description of the present invention, it should also be noted that, unless otherwise explicitly specified or limited, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.

Referring to fig. 1-4, the present invention provides a technical solution: the utility model provides a heat abstractor that carbon fiber unmanned aerial vehicle casing was used, includes unmanned aerial vehicle top shell 1, unmanned aerial vehicle drain pan 2, wing mounting bracket 3, first heat abstractor 4 and second heat abstractor 5, unmanned aerial vehicle top shell 1 middle part is provided with first heat abstractor 4, unmanned aerial vehicle drain pan 2 is installed in unmanned aerial vehicle top shell 1 below through

fixing bolt

6, 2 bilateral symmetry of unmanned aerial vehicle drain pan are provided with

second heat abstractor

5, 3 symmetries of wing mounting bracket set up in four sides of unmanned aerial vehicle drain pan 2.

Further, first heat abstractor 4 includes heating panel 7, connecting axle 8, driven gear 9, mounting bracket 10, driving motor 11 and drive gear 12, heating panel 7 sets up at unmanned aerial vehicle top shell 1 middle part through 8 symmetries of connecting axle, be provided with driven gear 9 on the connecting axle 8, driving motor 11 passes through mounting bracket 10 and installs in unmanned aerial vehicle top shell 1 bottom, be provided with drive gear 12 on the driving motor 11, drive gear 12 and driven gear 9 intermeshing.

Further, second heat abstractor 5 includes baffle 13, mounting groove 14, spout 15, elevator motor 16 and

lifter

17, 2 bilateral symmetry of unmanned aerial vehicle drain pan is provided with mounting groove 14, be provided with baffle 13 in the

mounting groove

14, 14 bilateral symmetry of mounting groove is provided with spout 15, spout 15 top is provided with elevator motor 16, be provided with lifter 17 on the elevator motor 16, connecting block 18 linking stop 13 bottom is passed through to lifter 17 bottom.

Further, the heat dissipation plate 7 is provided with gaskets 19 on four sides.

Further, the bottom end of the baffle 13 is provided with a sealing gasket 19, and the bottom end of the mounting groove 14 is provided with a dust screen 20.

The working principle is as follows: the utility model relates to a heat abstractor that carbon fiber unmanned aerial vehicle casing was used, during the use, drive gear 12 is driven through 11 work of driving motor in the first heat abstractor 4 and rotates, drive gear 12 acts on and drives connecting axle 8 rotation on driven gear 9, thereby it rotates and opens unmanned aerial vehicle top shell 1 to drive

heating panel

7, 16 work of elevator motor in the second heat abstractor 5 simultaneously drive lifter 17 and rise, lifter 17 rises and drives baffle 13 and open unmanned aerial vehicle drain pan 2 both sides in removing mounting groove 14, realize unmanned aerial vehicle top shell 1 ventilation cooling, improve the radiating efficiency, guarantee the long-time steady operation of unmanned aerial vehicle, the utility model discloses simple structure, convenient operation, the practicality is strong.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides a heat abstractor that carbon fiber unmanned aerial vehicle casing used which characterized in that: including unmanned aerial vehicle top shell (1), unmanned aerial vehicle drain pan (2), wing mounting bracket (3), first heat abstractor (4) and second heat abstractor (5), unmanned aerial vehicle top shell (1) middle part is provided with first heat abstractor (4), unmanned aerial vehicle drain pan (2) are installed in unmanned aerial vehicle top shell (1) below through fixing bolt (6), unmanned aerial vehicle drain pan (2) bilateral symmetry is provided with second heat abstractor (5), wing mounting bracket (3) symmetry sets up four sides in unmanned aerial vehicle drain pan (2).

2. The heat dissipating device for the carbon fiber unmanned aerial vehicle body as claimed in claim 1, wherein: first heat abstractor (4) include heating panel (7), connecting axle (8), driven gear (9), mounting bracket (10), driving motor (11) and drive gear (12), heating panel (7) set up at unmanned aerial vehicle top shell (1) middle part through connecting axle (8) symmetry, be provided with driven gear (9) on connecting axle (8), driving motor (11) are installed in unmanned aerial vehicle top shell (1) bottom through mounting bracket (10), be provided with drive gear (12) on driving motor (11), drive gear (12) and driven gear (9) intermeshing.

3. The heat dissipating device for the carbon fiber unmanned aerial vehicle body as claimed in claim 1, wherein: second heat abstractor (5) are including baffle (13), mounting groove (14), spout (15), elevator motor (16) and lifter (17), unmanned aerial vehicle drain pan (2) bilateral symmetry is provided with mounting groove (14), be provided with baffle (13) in mounting groove (14), mounting groove (14) bilateral symmetry is provided with spout (15), spout (15) top is provided with elevator motor (16), be provided with lifter (17) on elevator motor (16), connecting block (18) linking stop (13) bottom is passed through to lifter (17) bottom.

4. The heat dissipating device for the carbon fiber unmanned aerial vehicle body as claimed in claim 2, wherein: sealing gaskets (19) are arranged on four sides of the heat dissipation plate (7).

5. The heat dissipating device for the carbon fiber unmanned aerial vehicle body as claimed in claim 3, wherein: the bottom end of the baffle (13) is provided with a sealing gasket (19), and the bottom end of the mounting groove (14) is provided with a dust screen (20).