CN214930629U - Unmanned aerial vehicle heat dissipation apron mounting structure - Google Patents
Unmanned aerial vehicle heat dissipation apron mounting structure Download PDFInfo
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- CN214930629U CN214930629U CN202121779989.2U CN202121779989U CN214930629U CN 214930629 U CN214930629 U CN 214930629U CN 202121779989 U CN202121779989 U CN 202121779989U CN 214930629 U CN214930629 U CN 214930629U
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Abstract
The utility model discloses an unmanned aerial vehicle heat dissipation apron mounting structure, including the unmanned aerial vehicle organism, open unmanned aerial vehicle organism upper end has built-in groove, unmanned aerial vehicle organism right-hand member is opened has the interlude groove of controlling the break-over, and interlude groove and built-in inslot portion communicate with each other, wear the other sliding connection of left part and right part in the slot and have a heating panel and No. two heating panels, the one end middle part that a heating panel and No. two heating panels are close to each other has all opened the groove of stirring, the radiating groove of break-over about a plurality of is all opened to a heating panel and No. two heating panels upper ends, a heating panel and No. two heating panel joints are in the same place, unmanned aerial vehicle organism upper end left part and upper end right part all are provided with fastening screw, a heating panel and No. two heating panels are all through fastening screw and unmanned aerial vehicle organism fixed mounting together. An unmanned aerial vehicle heat dissipation apron mounting structure, the installation is dismantled conveniently, is convenient for maintain.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, in particular to unmanned aerial vehicle heat dissipation apron mounting structure.
Background
Unmanned aerial vehicle belongs to automatic flight equipment, and in the use, unmanned aerial vehicle organism internal part operation can produce the heat, consequently all can install the heat dissipation apron in the unmanned aerial vehicle organism, has following drawback at least in current unmanned aerial vehicle heat dissipation apron mounting structure: 1. the conventional heat dissipation cover plate is usually fixedly mounted with the machine body through a plurality of bolts, so that a large amount of time is consumed in the mounting and dismounting processes of the heat dissipation cover plate; 2. conventional heat dissipation apron all is a monoblock direct coverage installation, and to the great little unmanned aerial vehicle of volume, the monoblock heat dissipation apron span is big, and is firm inadequately in difficult production and the use, and the installation is dismantled trouble during the maintenance, so, we release a new unmanned aerial vehicle heat dissipation apron mounting structure.
SUMMERY OF THE UTILITY MODEL
The utility model discloses a main aim at provides an unmanned aerial vehicle heat dissipation apron mounting structure can effectively solve the problem in the background art.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides an unmanned aerial vehicle heat dissipation apron mounting structure, includes the unmanned aerial vehicle organism, open unmanned aerial vehicle organism upper end has built-in groove, the unmanned aerial vehicle organism right-hand member is opened has the interlude groove of controlling the break-over, and interlude groove and built-in inslot portion communicate with each other, wear the other sliding connection of left part and right part has a heating panel and No. two heating panels in the slot, the one end middle part that a heating panel and No. two heating panels are close to each other has all opened stirring groove, the radiating groove of break-over about a plurality of is all opened to a heating panel and No. two heating panels upper ends, a heating panel and No. two heating panel joints are in the same place, unmanned aerial vehicle organism upper end left part and upper end right part all are provided with fastening screw, a heating panel and No. two heating panels all are in the same place through fastening screw and unmanned aerial vehicle organism fixed mounting.
Preferably, the equal fixedly connected with joint piece in the left end rear portion of a heating panel right-hand member front portion and No. two heating panels, the spread groove has all been opened to the left end front portion of a heating panel right-hand member rear portion and No. two heating panels, the joint groove of break-over about the joint piece upper end is opened, joint piece right-hand member is opened there is trapezoidal opening, joint groove and trapezoidal opening intercommunication, fixedly connected with joint post between upper wall and the lower wall in the spread groove.
Preferably, the size in joint post and joint groove coincide, contactless between joint post and the spread groove, the spread groove is the trapezium structure, the joint piece is located the spread groove and the joint post joint is in the joint inslot with heating panel and No. two heating panel joints together.
Preferably, the upper end and the two spacing strips that slide of the equal fixedly connected with of lower extreme of a heating panel and No. two heating panels, it has the slip spacing groove all to open on the upper and lower inner wall at anterior and rear portion of groove to alternate, the equal sliding connection of a heating panel and No. two heating panels is in wearing the slot and the spacing strip that slides is located the slip spacing inslot respectively.
Preferably, the screw groove has all been opened to unmanned aerial vehicle organism upper end left part and upper end right part, the screw groove runs through and wears the slot and extends to the lower cell wall of wearing the slot, the perforation has all been opened on a heating panel and No. two heating panels, the position of fenestrate position and screw groove is corresponding, fastening screw passes the screw groove and perforates with a heating panel and No. two heating panels and unmanned aerial vehicle organism fixed mounting together.
Preferably, the toggle groove is of a semicircular structure, the toggle groove is not communicated with the heat dissipation groove, and the toggle groove is not communicated with the connection groove.
Compared with the prior art, the utility model discloses following beneficial effect has:
1. in the utility model, the slot and the sliding limiting groove are arranged on the body of the unmanned aerial vehicle, the sliding limiting strip is fixedly connected on the first heat dissipation plate and the second heat dissipation plate, the first heat dissipation plate and the second heat dissipation plate are directly connected with the slot in a sliding way and are matched with the sliding limiting strip and the sliding limiting groove in a sliding way, and then the first heat dissipation plate and the second heat dissipation plate are fixed through two fastening screws, so that the first heat dissipation plate and the second heat dissipation plate are more convenient to mount and dismount, and the mounting and dismounting time is saved;
2. the utility model discloses in, the heat dissipation apron divide into two constitutions of heating panel and No. two heating panels to a heating panel and No. two heating panel joints are in the same place, can ensure the stability of heat dissipation apron after the installation, and the problem that large-scale unmanned aerial vehicle monoblock heating panel span is big has been solved to the form of two concatenations, and when needs maintenance, can only dismantle single heat dissipation apron, convenient operation.
Drawings
Fig. 1 is an overall installation schematic view of the installation structure of the radiating cover plate of the unmanned aerial vehicle of the present invention;
fig. 2 is a schematic view of the overall structure of a first heat dissipation plate and a second heat dissipation plate of the mounting structure of the heat dissipation cover plate of the unmanned aerial vehicle of the present invention;
fig. 3 is a cross-sectional view of an unmanned aerial vehicle body of the unmanned aerial vehicle heat dissipation cover plate mounting structure of the present invention;
fig. 4 is the utility model relates to a connection schematic diagram of a heating panel and No. two heating panels of unmanned aerial vehicle heat dissipation apron mounting structure.
In the figure: 1. an unmanned aerial vehicle body; 2. a built-in groove; 3. inserting the slot; 4. a first heat dissipation plate; 5. a second heat dissipation plate; 6. a heat sink; 7. fastening screws; 8. a poking groove; 9. sliding the limiting strip; 10. perforating; 11. a clamping block; 12. a clamping groove; 13. a trapezoidal opening; 14. connecting grooves; 15. a sliding limit groove; 16. a screw groove; 17. the clamping column.
Detailed Description
In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end" 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 to which the reference is made 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. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, and for example, "connected" may be either fixedly connected or detachably connected, or integrally connected; 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 in specific cases to those skilled in the art.
As shown in fig. 1-4, an unmanned aerial vehicle heat radiating cover plate mounting structure, including unmanned aerial vehicle organism 1, open at 1 upper end of unmanned aerial vehicle organism has built-in groove 2, open 1 right-hand member of unmanned aerial vehicle organism has the interlude groove 3 of controlling the break-over, and interlude groove 3 and built-in groove 2 are inside to communicate with each other, it has heating panel 4 and No. two heating panels 5 to alternate 3 interior left parts of inslot and the other sliding connection of right part, all open at the one end middle part that a heating panel 4 and No. two heating panels 5 are close to each other has a striking groove 8, the radiating groove 6 of break-over about a plurality of all opened at heating panel 4 and No. two heating panels 5 upper ends, heating panel 4 and No. two heating panels 5 joint together, 1 upper end left part of unmanned aerial vehicle organism and upper end right part all are provided with fastening screw 7, heating panel 4 and No. two heating panels 5 all are in the same place through fastening screw 7 and 1 fixed mounting of unmanned aerial vehicle organism.
The front part of the right end of the first heat dissipation plate 4 and the rear part of the left end of the second heat dissipation plate 5 are fixedly connected with clamping blocks 11, the rear part of the right end of the first heat dissipation plate 4 and the front part of the left end of the second heat dissipation plate 5 are respectively provided with a connecting groove 14, the upper end of each clamping block 11 is provided with a clamping groove 12 which penetrates up and down, the right end of each clamping block 11 is provided with a trapezoidal opening 13, each clamping groove 12 is communicated with the trapezoidal opening 13, and a clamping column 17 is fixedly connected between the upper wall and the lower wall in each connecting groove 14; the sizes of the clamping column 17 and the clamping groove 12 are matched, the clamping column 17 is not contacted with the connecting groove 14, the connecting groove 14 is of a trapezoidal structure, the clamping block 11 is positioned in the connecting groove 14, and the clamping column 17 is clamped in the clamping groove 12 to clamp the first heat dissipation plate 4 and the second heat dissipation plate 5 together; the clamping block 11 is made of plastic, when the clamping block 11 and the clamping column 17 are clamped, the trapezoidal opening 13 is extruded under the action of external force to enable the clamping column 17 to be clamped into the clamping groove 12, and the trapezoidal structure of the connecting groove 14 also provides a space for clamping the clamping block 11 and the clamping column 17; the upper ends and the lower ends of the first heat dissipation plate 4 and the second heat dissipation plate 5 are fixedly connected with two sliding limiting strips 9, the upper inner wall and the lower inner wall of the front part and the lower inner wall of the rear part of the inserting groove 3 are both provided with sliding limiting grooves 15, the first heat dissipation plate 4 and the second heat dissipation plate 5 are both connected in the inserting groove 3 in a sliding mode, the sliding limiting strips 9 are respectively located in the sliding limiting grooves 15, and the inserting groove 3 and the sliding limiting grooves 15 enable the connection between the first heat dissipation plate 4 and the second heat dissipation plate 5 and the unmanned aerial vehicle body 1 to be more stable; the left part and the right part of the upper end of the unmanned aerial vehicle body 1 are both provided with screw grooves 16, the screw grooves 16 penetrate through the slot 3 and extend to the lower slot wall penetrating through the slot 3, the upper ends of the first heat dissipation plate 4 and the second heat dissipation plate 5 are both provided with through holes 10, the positions of the through holes 10 correspond to the positions of the screw grooves 16, and fastening screws 7 penetrate through the screw grooves 16 and the through holes 10 to fixedly install the first heat dissipation plate 4 and the second heat dissipation plate 5 with the unmanned aerial vehicle body 1; the toggle groove 8 is of a semicircular structure, the toggle groove 8 is not communicated with the radiating groove 6, and the toggle groove 8 is not communicated with the connecting groove 14; the poking groove 8 can facilitate the pushing of the first heat dissipation plate 4 and the second heat dissipation plate 5 by an operator.
It should be noted that, the utility model relates to an unmanned aerial vehicle heat dissipation cover plate mounting structure, in the use process, firstly, a first heat dissipation plate 4 and a second heat dissipation plate 5 are respectively inserted into the sliding connection into the slot 3 from the left end and the right end of the unmanned aerial vehicle body 1, at the moment, the sliding limiting strip 9 is just positioned in the sliding limiting groove 15, the clamping block 11 is just butted into the connecting groove 14 through the thrust of the left side and the right side, under the action of external force, the clamping block 11 is extruded by the trapezoid opening 13 and the clamping column 17, so that the clamping column 17 is clamped into the clamping groove 12, thereby the first heat dissipation plate 4 and the second heat dissipation plate 5 are clamped together, at the moment, the positions of the first heat dissipation plate 4 and the second heat dissipation plate 5 are adjusted, the perforation 10 is just corresponding to the position of the screw groove 16, the first heat dissipation plate 4 and the second heat dissipation plate 5 are fixedly connected with the unmanned aerial vehicle body 1 through two fastening screws 7, the whole radiating cover plate is convenient to install and detach, the screws are few, the installing and detaching time is saved, the splicing mode is adopted, the problem that the span of the whole radiating plate of the large unmanned aerial vehicle is large is solved, and when the radiating cover plate needs to be maintained, only a single radiating cover plate can be detached, and the operation is convenient.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (6)
1. The utility model provides an unmanned aerial vehicle heat dissipation apron mounting structure, includes unmanned aerial vehicle organism (1), its characterized in that: the upper end of the unmanned aerial vehicle body (1) is provided with an internal groove (2), the right end of the unmanned aerial vehicle body (1) is provided with a penetrating groove (3) which penetrates through the unmanned aerial vehicle body from left to right, the penetrating slot (3) is communicated with the inner part of the built-in slot (2), the left part and the right part in the penetrating slot (3) are respectively connected with a first heat dissipation plate (4) and a second heat dissipation plate (5) in a sliding way, the middle parts of the ends of the first heat dissipation plate (4) and the second heat dissipation plate (5) which are close to each other are both provided with toggle grooves (8), the upper ends of the first heat dissipation plate (4) and the second heat dissipation plate (5) are respectively provided with a plurality of heat dissipation grooves (6) which are penetrated up and down, the first heat dissipation plate (4) and the second heat dissipation plate (5) are clamped together, the left part and the right part of the upper end of the unmanned aerial vehicle body (1) are both provided with fastening screws (7), a heating panel (4) and No. two heating panels (5) all pass through fastening screw (7) and unmanned aerial vehicle organism (1) fixed mounting together.
2. The unmanned aerial vehicle heat dissipation cover plate mounting structure of claim 1, characterized in that: the equal fixedly connected with joint piece (11) in left end rear portion of heating panel (4) right-hand member front portion and No. two heating panels (5), spread groove (14) have all been opened in the left end front portion of heating panel (4) right-hand member rear portion and No. two heating panels (5), joint groove (12) of break-over about joint piece (11) upper end is opened, joint piece (11) right-hand member is opened trapezoidal opening (13), joint groove (12) and trapezoidal opening (13) intercommunication, fixedly connected with joint post (17) between upper wall and the lower wall in spread groove (14).
3. The unmanned aerial vehicle heat dissipation cover plate mounting structure of claim 2, characterized in that: the size of joint post (17) and joint groove (12) coincide, contactless between joint post (17) and connecting groove (14), connecting groove (14) are the trapezium structure, joint piece (11) are located connecting groove (14) and joint post (17) joint in joint groove (12) with a heating panel (4) and No. two heating panels (5) joint together.
4. The unmanned aerial vehicle heat dissipation cover plate mounting structure of claim 1, characterized in that: the upper end and the equal fixedly connected with two slip spacing (9) of lower extreme of a heating panel (4) and No. two heating panels (5), it has slip spacing groove (15) all to open on the upper and lower inner wall at slot (3) front portion and rear portion to wear, heating panel (4) and No. two equal sliding connection of heating panel (5) are in wearing slot (3) and slip spacing (9) and are located slip spacing groove (15) respectively.
5. The unmanned aerial vehicle heat dissipation cover plate mounting structure of claim 1, characterized in that: unmanned aerial vehicle organism (1) upper end left part and upper end right part have all been opened screw groove (16), screw groove (16) run through and wear slot (3) and extend to the lower cell wall of wearing slot (3), a heating panel (4) and No. two heating panel (5) upper ends have all been opened perforation (10), the position of perforation (10) is corresponding with the position of screw groove (16), fastening screw (7) pass screw groove (16) and perforation (10) with heating panel (4) and No. two heating panel (5) and unmanned aerial vehicle organism (1) fixed mounting together.
6. The unmanned aerial vehicle heat dissipation cover plate mounting structure of claim 1, characterized in that: the toggle groove (8) is of a semicircular structure, the toggle groove (8) is not communicated with the heat dissipation groove (6), and the toggle groove (8) is not communicated with the connecting groove (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121779989.2U CN214930629U (en) | 2021-08-02 | 2021-08-02 | Unmanned aerial vehicle heat dissipation apron mounting structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121779989.2U CN214930629U (en) | 2021-08-02 | 2021-08-02 | Unmanned aerial vehicle heat dissipation apron mounting structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214930629U true CN214930629U (en) | 2021-11-30 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121779989.2U Active CN214930629U (en) | 2021-08-02 | 2021-08-02 | Unmanned aerial vehicle heat dissipation apron mounting structure |
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| Country | Link |
|---|---|
| CN (1) | CN214930629U (en) |
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2021
- 2021-08-02 CN CN202121779989.2U patent/CN214930629U/en active Active
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