CN213443124U - Waterproof unmanned aerial vehicle remote sensing measurement and control device - Google Patents
Waterproof unmanned aerial vehicle remote sensing measurement and control device Download PDFInfo
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- CN213443124U CN213443124U CN202022590985.1U CN202022590985U CN213443124U CN 213443124 U CN213443124 U CN 213443124U CN 202022590985 U CN202022590985 U CN 202022590985U CN 213443124 U CN213443124 U CN 213443124U
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Abstract
The utility model discloses a waterproof unmanned aerial vehicle remote sensing measurement and control device, including outer protective housing, the shell of making an uproar, cooling tube and interior protective housing fall, the cushion chamber has been seted up to the inboard of outer protective housing, the installation shell is installed to the upper end of outer protective housing, the sealing washer is installed to the lower extreme of outer protective housing, the inboard of outer closing cap is provided with down the cooling chamber, the shell of making an uproar falls is installed to the upside of blotter, interior closing cap is installed to the upside of interior protective housing, and the upside of interior closing cap is provided with damping spring, damping spring's the outside is provided with vertical rib plate, and vertical rib plate's inboard is provided with horizontal. This waterproof unmanned aerial vehicle remote sensing measurement and control device can be waterproof for unmanned aerial vehicle can avoid the rainwater to get into in the measurement and control device and lead to the electronic component short circuit at the during operation under the special environment of rainy day, and can dispel the heat to measurement and control device, makes electronic component can work under suitable environment, thereby increases its operating mass with rated load.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is a waterproof unmanned aerial vehicle remote sensing measurement and control device.
Background
Unmanned aerial vehicle need not the driver and gets into and drives in the unmanned aerial vehicle, and can carry out those too "fool, dirty or dangerous" tasks, and civil unmanned aerial vehicle can be used for observing and controling, fields such as taking photo by plane, mostly adopts remote sensing control, but most unmanned aerial vehicle remote sensing measurement and control device still has some problems on the market, for example:
waterproof is not convenient for carry on, leads to unmanned aerial vehicle when special circumstances operations such as rainy day, probably makes in the rainwater gets into measurement and control device and leads to the electronic component short circuit, and is not convenient for dispel the heat to measurement and control device for electronic component probably works under unsuitable environment, thereby influences its operating mass with rated load, consequently, the utility model provides a waterproof unmanned aerial vehicle remote sensing measurement and control device to solve the above-mentioned problem of proposing.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a waterproof unmanned aerial vehicle remote sensing measurement and control device to solve most unmanned aerial vehicle remote sensing measurement and control devices on the market that provide in the above-mentioned background art and be not convenient for waterproof, lead to unmanned aerial vehicle when special circumstances operations such as rainy day, probably make the rainwater get into in the measurement and control device and lead to the electronic component short circuit, and be not convenient for dispel the heat to measurement and control device, make electronic component probably work under unsuitable environment, thereby influence its operating mass's problem.
In order to achieve the above object, the utility model provides a following technical scheme: a waterproof unmanned aerial vehicle remote sensing measurement and control device comprises an outer protective shell, a noise reduction shell, a cooling pipe and an inner protective shell, wherein a buffer cavity is formed in the inner side of the outer protective shell, and the inner side of the buffer cavity is provided with a side cooling cavity, the upper end of the outer protective shell is provided with an installation shell, the inner side of the installation shell is provided with a cooling box, and the lower side of the cooling box is provided with a cooling pipe, the lower end of the outer protective shell is provided with a sealing ring, and the outer side of the sealing ring is provided with an outer sealing cover, the inner side of the outer sealing cover is provided with a lower cooling cavity, the upper side of the outer sealing cover is provided with a buffer pad, the upper side of the buffer pad is provided with a noise reduction shell, an inner protective shell is arranged at the inner side of the noise reduction shell, an inner sealing cover is arranged at the upper side of the inner protective shell, and the upper side of the inner sealing cover is provided with a damping spring, the outer side of the damping spring is provided with a longitudinal rib plate, and the inner side of the longitudinal rib plate is provided with a transverse rib plate.
Preferably, the outer side and the inner side of the noise reduction shell are both uniformly provided with trapezoidal protruding structures, the noise reduction shell is connected with the inner protective shell in a nested manner, and the opening direction of the inner protective shell and the opening direction of the outer protective shell are opposite.
Preferably, the cooling pipes are arranged in the outer protective shell at equal intervals, the inner side of the outer protective shell is uniformly provided with protruding structures, and the damping springs are arranged in one-to-one correspondence with the protruding structures.
Preferably, the longitudinal ribs are arranged at equal intervals on the inner side of the outer protective shell, and the longitudinal sections of the longitudinal ribs are triangular.
Preferably, the cross section of the transverse rib plate is triangular, and the transverse rib plate is arranged at an equal angle relative to the center of the outer protective shell.
Preferably, the sealing ring and the outer protective shell are arranged in a fitting mode, the sealing ring and the outer sealing cover are connected in a clamping mode, and the outer sealing cover and the outer protective shell are connected in a clamping mode.
Compared with the prior art, the beneficial effects of the utility model are that: the waterproof unmanned aerial vehicle remote sensing measurement and control device can be waterproof, so that when the unmanned aerial vehicle works in a special environment in rainy days, rainwater is prevented from entering the measurement and control device to cause short circuit of electronic elements, the measurement and control device can be cooled, and the electronic elements can work in a proper environment, so that the working quality of the unmanned aerial vehicle is improved;
1. the opening of the outer protective shell and the opening of the inner protective shell are arranged oppositely, so that the amount of entering rainwater can be reduced, and the joint arrangement of the sealing ring and the outer protective shell can compensate for a gap between the outer protective shell and the outer sealing cover, so that the sealing performance is improved, and the unmanned aerial vehicle can be waterproof, so that when the unmanned aerial vehicle works in a special environment in rainy days, the phenomenon that rainwater enters the measurement and control device to cause short circuit of an electronic element is avoided;
2. the cooling pipes are arranged in the outer protective shell at equal intervals, so that the cooling pipes can absorb heat and radiate the measurement and control device, and the electronic element can work in a proper environment, so that the working quality of the electronic element is improved;
3. through the trapezoidal protruding structure that falls the shell outside of making an uproar and evenly set up, can carry out certain noise elimination and fall and make an uproar for the inboard measuring and control device of inner protective housing can carry out work under the condition of no external disturbance, and can improve the structural stability of outer protective housing through the indulge rib plate of the inboard equidistant setting of outer protective housing.
Drawings
Fig. 1 is a schematic view of the front cross-sectional structure of the present invention;
FIG. 2 is a schematic side view of the cross-sectional structure of the present invention;
FIG. 3 is a schematic top view of the cross-sectional structure of the present invention;
fig. 4 is an enlarged schematic structural view of a portion a in fig. 1 according to the present invention.
In the figure: 1. an outer protective shell; 2. a buffer chamber; 3. a noise reducing housing; 4. a side cooling cavity; 5. an outer cover; 6. a lower cooling chamber; 7. a cushion pad; 8. installing a shell; 9. a cooling tube; 10. a cooling tank; 11. a damping spring; 12. longitudinal rib plates; 13. an inner sealing cover; 14. an inner protective shell; 15. a transverse rib plate; 16. and (5) sealing rings.
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.
Referring to fig. 1-4, the present invention provides a technical solution: a waterproof unmanned aerial vehicle remote sensing measurement and control device comprises an outer protective shell 1, a buffer cavity 2, a noise reduction shell 3, a side cooling cavity 4, an outer sealing cover 5, a lower cooling cavity 6, a buffer cushion 7, an installation shell 8, a cooling pipe 9, a cooling box 10, a damping spring 11, a longitudinal rib plate 12, an inner sealing cover 13, an inner protective shell 14, a transverse rib plate 15 and a sealing ring 16, wherein the buffer cavity 2 is arranged on the inner side of the outer protective shell 1, the side cooling cavity 4 is arranged on the inner side of the buffer cavity 2, the installation shell 8 is arranged at the upper end of the outer protective shell 1, the cooling box 10 is arranged on the inner side of the installation shell 8, the cooling pipe 9 is arranged on the lower side of the cooling box 10, the sealing ring 16 is arranged at the lower end of the outer protective shell 1, the outer sealing cover 5 is arranged on the outer side of the sealing ring 16, the lower cooling cavity 6 is arranged on the inner, an inner protective shell 14 is arranged on the inner side of the noise reduction shell 3, an inner sealing cover 13 is mounted on the upper side of the inner protective shell 14, a damping spring 11 is arranged on the upper side of the inner sealing cover 13, a longitudinal rib plate 12 is arranged on the outer side of the damping spring 11, and a transverse rib plate 15 is arranged on the inner side of the longitudinal rib plate 12;
as shown in fig. 1 and 2, trapezoidal protruding structures are uniformly arranged on the outer side and the inner side of the noise reduction shell 3, the noise reduction shell 3 and the inner protective shell 14 are in nested connection, the opening direction of the inner protective shell 14 and the opening direction of the outer protective shell 1 are opposite to each other, the quantity of rainwater entering can be reduced, certain noise elimination and noise reduction can be performed, so that a measurement and control device on the inner side of the inner protective shell 14 can work without external interference, the cooling pipes 9 are arranged in the outer protective shell 1 at equal intervals, the protruding structures are uniformly arranged on the inner side of the outer protective shell 1, the damping springs 11 and the protruding structures are arranged in a one-to-one correspondence manner, certain damping and buffering can be performed on the inner protective shell 14, and the stability of the device is improved;
as shown in fig. 1, 2 and 3, the longitudinal ribs 12 are disposed at equal intervals on the inner side of the outer protective shell 1, and the longitudinal cross section of the longitudinal ribs 12 is triangular, which can improve the structural stability of the outer protective shell 1, as shown in fig. 3, the cross section of the transverse rib 15 is triangular, and the transverse rib 15 is disposed at equal angles with respect to the center of the outer protective shell 1, which improves the stability of the outer protective shell 1, as shown in fig. 4, the sealing ring 16 is disposed in a manner of being attached to the outer protective shell 1, the sealing ring 16 is connected to the outer sealing cover 5 in a manner of being clamped, and the outer sealing cover 5 is connected to the outer protective shell 1 in a manner of being clamped, which can compensate for the gap between the outer protective shell 1 and.
The working principle is as follows: when the waterproof unmanned aerial vehicle remote sensing measurement and control device is used, firstly, as shown in fig. 1 and fig. 2, the anti-collision capacity of the outer protective shell 1 can be improved through the buffer cavity 2 formed in the outer protective shell 1, the whole weight of the outer protective shell 1 is reduced, meanwhile, the temperature in the outer protective shell 1 is cooled through the side cooling cavity 4 and the lower cooling cavity 6, the cooling pipes 9 are arranged in the outer protective shell 1 at equal intervals, so that the cooling box 10 arranged in the installation shell 8 circulates cooling liquid in the cooling pipes 9, the cooling efficiency of the cooling pipes 9 is increased, certain noise elimination and reduction can be carried out through the trapezoidal convex structures uniformly arranged on the outer side of the noise reduction shell 3, the measurement and control device on the inner side of the inner protective shell 14 can work under the condition of no external interference, as shown in fig. 1 and fig. 3, the damping springs 11 correspond to the convex structures on the inner side of the outer protective shell 1, the inner protective shell 14 can be subjected to certain shock absorption and buffering, and the structural stability of the outer protective shell 1 can be improved through the triangular cross sections of the longitudinal rib plates 12 and the transverse rib plates 15 which are arranged at equal intervals on the inner side of the outer protective shell 1;
as in fig. 1 and 4, the opening through outer protective housing 1 and the opening of inner protective housing 14 are opposite each other and set up, can reduce the quantity that the rainwater got into, and set up through the laminating of sealing washer 16 with outer protective housing 1, can compensate the gap between outer protective housing 1 and the outer closing cap 5, increase the leakproofness to it is waterproof, this is this waterproof unmanned aerial vehicle remote sensing measurement and control device's application method.
The utility model discloses the standard part that uses all can purchase from the market, and dysmorphism piece all can be customized according to the description with the record of drawing of description, and the concrete connected mode of each part all adopts conventional means such as ripe bolt, rivet, welding among the prior art, and machinery, part and equipment all adopt among the prior art, and conventional model, including the conventional connected mode among the circuit connection adoption prior art, and the details are not repeated here, and the content that does not make detailed description in this description belongs to the prior art that skilled person in the art knows.
Although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments or portions thereof without departing from the spirit and scope of the invention.
Claims (6)
1. The utility model provides a waterproof unmanned aerial vehicle remote sensing measurement and control device, includes outer protective housing (1), falls shell (3), cooling tube (9) and inner protective housing (14) of making an uproar, its characterized in that: the inner side of the outer protective shell (1) is provided with a buffer cavity (2), the inner side of the buffer cavity (2) is provided with a side cooling cavity (4), the upper end of the outer protective shell (1) is provided with an installation shell (8), the inner side of the installation shell (8) is provided with a cooling box (10), the lower side of the cooling box (10) is provided with a cooling pipe (9), the lower end of the outer protective shell (1) is provided with a sealing ring (16), the outer side of the sealing ring (16) is provided with an outer sealing cover (5), the inner side of the outer sealing cover (5) is provided with a lower cooling cavity (6), the upper side of the outer sealing cover (5) is provided with a cushion pad (7), the upper side of the cushion pad (7) is provided with a noise reduction shell (3), the inner side of the noise reduction shell (3) is provided with an inner protective shell (, and the upper side of the inner sealing cover (13) is provided with a damping spring (11), the outer side of the damping spring (11) is provided with a longitudinal rib plate (12), and the inner side of the longitudinal rib plate (12) is provided with a transverse rib plate (15).
2. The waterproof unmanned aerial vehicle remote sensing measurement and control device of claim 1, characterized in that: the outer side and the inner side of the noise reduction shell (3) are uniformly provided with trapezoidal protruding structures, the noise reduction shell (3) is connected with the inner protection shell (14) in a nested mode, and the opening direction of the inner protection shell (14) is opposite to that of the outer protection shell (1).
3. The waterproof unmanned aerial vehicle remote sensing measurement and control device of claim 1, characterized in that: the cooling pipes (9) are arranged in the outer protective shell (1) at equal intervals, protruding structures are evenly arranged on the inner side of the outer protective shell (1), and the damping springs (11) are arranged in a one-to-one correspondence mode with the protruding structures.
4. The waterproof unmanned aerial vehicle remote sensing measurement and control device of claim 1, characterized in that: the longitudinal rib plates (12) are arranged on the inner side of the outer protective shell (1) at equal intervals, and the longitudinal sections of the longitudinal rib plates (12) are triangular.
5. The waterproof unmanned aerial vehicle remote sensing measurement and control device of claim 1, characterized in that: the cross section of the transverse rib plate (15) is triangular, and the transverse rib plate (15) is arranged at an equal angle relative to the center of the outer protective shell (1).
6. The waterproof unmanned aerial vehicle remote sensing measurement and control device of claim 1, characterized in that: sealing washer (16) and outer protective housing (1) are the laminating setting, and sealing washer (16) and outer closing cap (5) are the block connection to outer closing cap (5) are the block connection with outer protective housing (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022590985.1U CN213443124U (en) | 2020-11-11 | 2020-11-11 | Waterproof unmanned aerial vehicle remote sensing measurement and control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022590985.1U CN213443124U (en) | 2020-11-11 | 2020-11-11 | Waterproof unmanned aerial vehicle remote sensing measurement and control device |
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| CN213443124U true CN213443124U (en) | 2021-06-15 |
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| CN202022590985.1U Active CN213443124U (en) | 2020-11-11 | 2020-11-11 | Waterproof unmanned aerial vehicle remote sensing measurement and control device |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113329601A (en) * | 2021-07-07 | 2021-08-31 | 辽宁工程技术大学 | Unmanned aerial vehicle remote sensing device for surveying and mapping engineering measurement |
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2020
- 2020-11-11 CN CN202022590985.1U patent/CN213443124U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113329601A (en) * | 2021-07-07 | 2021-08-31 | 辽宁工程技术大学 | Unmanned aerial vehicle remote sensing device for surveying and mapping engineering measurement |
| CN113329601B (en) * | 2021-07-07 | 2023-12-01 | 郑道仓 | Unmanned aerial vehicle remote sensing device for surveying and mapping engineering measurement |
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