CN211607211U - Unmanned aerial vehicle pressure reduction means - Google Patents
Unmanned aerial vehicle pressure reduction means Download PDFInfo
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- CN211607211U CN211607211U CN202020548564.XU CN202020548564U CN211607211U CN 211607211 U CN211607211 U CN 211607211U CN 202020548564 U CN202020548564 U CN 202020548564U CN 211607211 U CN211607211 U CN 211607211U
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Abstract
The utility model relates to an unmanned air vehicle technique field discloses an unmanned aerial vehicle pressure reduction means, including the mounting panel, the top fixedly connected with connecting plate of mounting panel, the inside of connecting plate is provided with the pressure reduction module main part, one side of pressure reduction module main part is provided with first wire, the one end of first wire is provided with female head, the one end that first wire was kept away from to pressure reduction module main part is provided with the second wire. The utility model has the advantages of it is following and effect: set up heating panel and fin through the surface at the pressure reducing module main part, pressure reducing module main part transmits the heating panel through self casing at produced heat of during operation, the heating panel again with heat transfer for a plurality of fin, heat compensation and sharing between the effectual improvement fin of a plurality of fin avoid thermal local concentrated, and a plurality of fin can effectual improvement thermal exchange efficiency moreover to the effect that improves the device heat dispersion has been reached.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, in particular to unmanned aerial vehicle pressure reduction means.
Background
Unmanned aerial vehicle step-down device indicates the step-down module of unmanned aerial vehicle power promptly, and power step-down module is one kind and brushless electricity regulation separation's external power voltage regulator device, and it can obtain the direct current voltage who is fit for receiver and other equipment work from higher input voltage to continuously stably provide up to 3A's output current, applicable various fields (like the unmanned aerial vehicle field) that have harsh requirement to volume and weight.
Unmanned aerial vehicle pressure reduction means among the prior art, it is relatively poor to design on the heat dissipation measure, because pressure reduction module self volume is less, very easily leads to inside temperature sharply to rise at the during operation, and the heat scatters out in time and causes the internals impaired easily to lead to this module life to descend.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing an unmanned aerial vehicle step-down gear has the effect that heat dispersion is strong.
The above technical purpose of the present invention can be achieved by the following technical solutions: the utility model provides an unmanned aerial vehicle pressure reduction means, includes the mounting panel, the top fixedly connected with connecting plate of mounting panel, the inside of connecting plate is provided with the pressure reduction module main part, one side of pressure reduction module main part is provided with first wire, the one end of first wire is provided with female head, the one end that first wire was kept away from to the pressure reduction module main part is provided with the second wire, the one end of second wire is provided with public head, the external fixed surface of pressure reduction module main part is connected with the heating panel, the external fixed surface of heating panel is connected with the fin.
Through adopting above-mentioned technical scheme, through setting up heating panel and fin at the surface of step-down module main part, step-down module main part transmits the heating panel through self casing at the produced heat of during operation, the heating panel transmits heat for a plurality of fin again, the effectual heat compensation and the share that improves between the fin of a plurality of fin avoid thermal local concentrated, and a plurality of fin can the effectual thermal exchange efficiency of improvement moreover, thereby reached the effect that improves the device heat dispersion.
The utility model discloses a further set up to: and a pressure-sensitive sensor is arranged in the pressure-reducing module main body.
By adopting the technical scheme, the pressure-sensitive sensor is a device or a device which can sense pressure signals and can convert the pressure signals into usable output electric signals according to a certain rule, the pressure-sensitive sensor generally consists of a pressure-sensitive element and a signal processing unit, and the pressure-sensitive sensor is the most common sensor in industrial practice and is widely applied to various industrial automatic control environments, relating to various industries such as water conservancy and hydropower, railway traffic, intelligent buildings, production automatic control, aerospace, war industry, petrifaction, oil wells, electric power, ships, machine tools, pipelines and the like.
The utility model discloses a further set up to: the outer surface of the voltage reduction module main body is fixedly connected with four mounting lugs.
Through adopting above-mentioned technical scheme, the setting of installation ear makes things convenient for the connecting plate on step-down module main part and the mounting panel to install.
The utility model discloses a further set up to: the upper surface of connecting plate has seted up the spread groove, the inner wall fixedly connected with slipmat of spread groove.
Through adopting above-mentioned technical scheme, through setting up the slipmat, can strengthen the stability of being connected between connecting plate and the step-down module main part, prevent that the step-down module main part is not hard up.
The utility model discloses a further set up to: mounting grooves are formed in the upper surface of the connecting plate, the number of the mounting grooves is four, and screw holes are formed in the inner bottom wall of each mounting groove.
Through adopting above-mentioned technical scheme, the mounting groove matches with the installation ear, conveniently installs the butt joint.
The utility model discloses a further set up to: the mounting hole has been seted up to the upper surface of mounting panel, the quantity of mounting hole is four.
Through adopting above-mentioned technical scheme, through seting up the mounting hole on the mounting panel, make things convenient for the device to carry out fixed connection with unmanned aerial vehicle, the mounting hole also can be seted up according to actual demand by oneself.
The utility model has the advantages that: set up heating panel and fin through the surface at the pressure reducing module main part, pressure reducing module main part transmits the heating panel through self casing at produced heat of during operation, the heating panel again with heat transfer for a plurality of fin, heat compensation and sharing between the effectual improvement fin of a plurality of fin avoid thermal local concentrated, and a plurality of fin can effectual improvement thermal exchange efficiency moreover to the effect that improves the device heat dispersion has been reached.
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 description of the embodiments 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 without creative efforts.
Fig. 1 is a schematic structural view of the present invention;
fig. 2 is a schematic top view of the present invention;
FIG. 3 is a schematic structural view of a mounting lug of the present invention;
fig. 4 is a schematic top view of the middle connection plate of the present invention.
In the figure, 1, mounting plate; 2. a connecting plate; 3. a voltage reduction module main body; 4. a first conductive line; 5. a female head; 6. a second conductive line; 7. a male head; 8. a heat dissipation plate; 9. a heat sink; 10. mounting lugs; 11. a non-slip mat; 12. mounting grooves; 13. a screw hole; 14. And (7) installing holes.
Detailed Description
The technical solution of the present invention will be clearly and completely described below with reference to the specific embodiments. It is obvious that the described embodiments are only some of the embodiments of the present invention, and not all of them. Based on the embodiments of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.
Referring to fig. 1-4, an unmanned aerial vehicle pressure reduction device comprises a mounting plate 1, a connecting plate 2 is fixedly connected to the top of the mounting plate 1, a pressure reduction module main body 3 is arranged inside the connecting plate 2, a first lead 4 is arranged on one side of the pressure reduction module main body 3, a female head 5 is arranged at one end of the first lead 4, a second lead 6 is arranged at one end of the pressure reduction module main body 3 away from the first lead 4, a male head 7 is arranged at one end of the second lead 6, a heat dissipation plate 8 is fixedly connected to the outer surface of the pressure reduction module main body 3, a heat dissipation plate 9 is fixedly connected to the outer surface of the heat dissipation plate 8, a heat dissipation plate 8 and a heat dissipation plate 9 are arranged on the outer surface of the pressure reduction module main body 3, heat generated during working of the pressure reduction module main body 3 is transferred to the heat dissipation plate 8 through a shell of, the pressure-sensitive sensor is arranged in the pressure-reducing module main body 3, the pressure-sensitive sensor is a device or a device which can sense pressure signals and can convert the pressure signals into usable output electric signals according to a certain rule, the pressure-sensitive sensor generally comprises a pressure-sensitive element and a signal processing unit, the pressure-sensitive sensor is the most common sensor in industrial practice and is widely applied to various industrial automatic control environments and relates to various industries such as water conservancy and hydropower, railway traffic, intelligent buildings, production automatic control, aerospace, war industry, petrochemical industry, oil wells, electric power, ships, machine tools, pipelines and the like, the outer surface of the pressure-reducing module main body 3 is fixedly connected with the mounting lugs 10, and the number of the mounting lugs 10 is four, installation ear 10's setting, make things convenient for connecting plate 2 on depressurization module main part 3 and the mounting panel 1 to install, the spread groove has been seted up to the upper surface of connecting plate 2, the inner wall fixedly connected with slipmat 11 of spread groove, through setting up slipmat 11, can strengthen the stability of being connected between connecting plate 2 and the depressurization module main part 3, it is not hard up to prevent depressurization module main part 3, mounting groove 12 has been seted up to the upper surface of connecting plate 2, the quantity of mounting groove 12 is four, screw 13 has been seted up to the inner diapire of mounting groove 12, mounting groove 12 matches with installation ear 10, conveniently install the butt joint, mounting hole 14 has been seted up to the upper surface of mounting panel 1, the quantity of mounting hole 14 is four, through set up mounting hole 14 on mounting panel 1, make things convenient for the device to carry out fixed connection with unmanned.
The utility model discloses in, through setting up heating panel 8 and fin 9 at the surface of step-down module main part 3, step-down module main part 3 transmits the produced heat of during operation for heating panel 8 through self casing, heating panel 8 is again with heat transfer for a plurality of fin 9, heat compensation and sharing between the effectual improvement fin 9 of a plurality of fin 9 avoid thermal local concentrated, and a plurality of fin 9 can the effectual thermal exchange efficiency of improvement moreover, thereby reached the effect that improves the device heat dispersion.
Claims (6)
1. The utility model provides an unmanned aerial vehicle pressure reduction means, includes mounting panel (1), its characterized in that: the top fixedly connected with connecting plate (2) of mounting panel (1), the inside of connecting plate (2) is provided with step-down module main part (3), one side of step-down module main part (3) is provided with first wire (4), the one end of first wire (4) is provided with female head (5), the one end that first wire (4) were kept away from in step-down module main part (3) is provided with second wire (6), the one end of second wire (6) is provided with public head (7), the external fixed surface of step-down module main part (3) is connected with heating panel (8), the external fixed surface of heating panel (8) is connected with fin (9).
2. An unmanned aerial vehicle pressure reduction device according to claim 1, wherein: and a pressure-sensitive sensor is arranged in the pressure-reducing module main body (3).
3. An unmanned aerial vehicle pressure reduction device according to claim 1, wherein: the outer surface of the voltage reduction module main body (3) is fixedly connected with mounting ears (10), and the number of the mounting ears (10) is four.
4. An unmanned aerial vehicle pressure reduction device according to claim 1, wherein: the upper surface of connecting plate (2) has seted up the spread groove, the inner wall fixedly connected with slipmat (11) of spread groove.
5. An unmanned aerial vehicle pressure reduction device according to claim 1, wherein: mounting grooves (12) are formed in the upper surface of the connecting plate (2), the number of the mounting grooves (12) is four, and screw holes (13) are formed in the inner bottom wall of each mounting groove (12).
6. An unmanned aerial vehicle pressure reduction device according to claim 1, wherein: mounting holes (14) are formed in the upper surface of the mounting plate (1), and the number of the mounting holes (14) is four.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020548564.XU CN211607211U (en) | 2020-04-14 | 2020-04-14 | Unmanned aerial vehicle pressure reduction means |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020548564.XU CN211607211U (en) | 2020-04-14 | 2020-04-14 | Unmanned aerial vehicle pressure reduction means |
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| Publication Number | Publication Date |
|---|---|
| CN211607211U true CN211607211U (en) | 2020-09-29 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020548564.XU Active CN211607211U (en) | 2020-04-14 | 2020-04-14 | Unmanned aerial vehicle pressure reduction means |
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| Country | Link |
|---|---|
| CN (1) | CN211607211U (en) |
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2020
- 2020-04-14 CN CN202020548564.XU patent/CN211607211U/en active Active
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