CN220492893U - Satellite telemetry terminal device - Google Patents
Satellite telemetry terminal device Download PDFInfo
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- CN220492893U CN220492893U CN202322110559.7U CN202322110559U CN220492893U CN 220492893 U CN220492893 U CN 220492893U CN 202322110559 U CN202322110559 U CN 202322110559U CN 220492893 U CN220492893 U CN 220492893U
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- cone
- satellite telemetry
- telemetry terminal
- solar panel
- shell
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- 239000000084 colloidal system Substances 0.000 claims abstract description 7
- 238000009434 installation Methods 0.000 abstract description 12
- 238000010248 power generation Methods 0.000 abstract description 4
- 230000001678 irradiating effect Effects 0.000 abstract 1
- 230000002035 prolonged effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 230000008707 rearrangement Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
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- Photovoltaic Devices (AREA)
Abstract
The utility model belongs to the technical field of satellite telemetry, and discloses a satellite telemetry terminal device. The satellite telemetry terminal device comprises a mounting seat, a shell and a solar panel, wherein the shell comprises an upper shell and a lower shell which are connected with each other, the lower shell is connected with the mounting seat, the center of the upper shell is provided with a circular arc-shaped bulge, the upper shell is also provided with a conical groove, and the conical groove is arranged on the periphery of the circular arc-shaped bulge in a surrounding manner; the solar panel is in a cone-shaped structure and is fixed in the cone-shaped groove through colloid. According to the satellite telemetry terminal device provided by the utility model, the solar panel is in a cone-shaped structure and is matched with the cone-shaped groove, the solar panel is fixed in the cone-shaped groove, and the solar panel with the cone-shaped structure can receive sunlight irradiation in a large area, so that the power generation is maximized; the solar panel is fixed on the upper shell, so that sunlight is effectively prevented from directly irradiating the upper shell, the upper shell is prevented from being too high in temperature, and electronic components in the shell are protected; the solar panel is fixed in the conical groove through the colloid, so that the installation is convenient and fast, and the installation cost is low.
Description
Technical Field
The utility model relates to the technical field of satellite telemetry, in particular to a satellite telemetry terminal device.
Background
The remote measuring terminal integrates data acquisition, transmission and storage functions, adopts a low-power consumption design, is particularly suitable for a solar power supply monitoring site, can greatly reduce the solar power supply cost and the construction difficulty, and is widely applied to industries such as weather, hydrology, geology and the like.
At present, a solar panel used for a domestic satellite telemetry terminal generally needs to be independently configured in a later period, is complex in installation, high in installation cost, complex in structure and limited in application scene. Therefore, a satellite telemetry terminal device is needed to solve the above technical problems.
Disclosure of Invention
The utility model aims to provide a satellite telemetry terminal device, which aims to solve the problems of complicated installation, high installation cost, complex structure and limited applicable scene of a solar panel in the prior art, optimize the structure of the solar panel, simplify the installation and enlarge the application range.
To achieve the purpose, the utility model adopts the following technical scheme:
a satellite telemetry terminal device, comprising:
a mounting base;
the shell comprises an upper shell and a lower shell which are connected with each other, the lower shell is connected with the mounting seat, the center of the upper shell is provided with a circular arc-shaped bulge, the upper shell is also provided with a conical groove, and the conical groove is arranged on the periphery of the circular arc-shaped bulge in a surrounding manner;
the solar panel is in a cone-shaped structure and is fixed in the cone-shaped groove through colloid.
Optionally, the lower shell comprises a cone and a dish-shaped body, the small end of the cone is connected with the mounting seat, the large end of the cone is connected with the dish-shaped body, and the upper shell is connected with one end of the dish-shaped body away from the cone.
Optionally, the mounting base comprises a base and a cylinder body arranged on the base, and the small end of the cone is connected with the base.
Optionally, the small end of the cone is convexly provided with a guide ring, and the guide ring stretches into the cylinder and is connected with the base.
Optionally, the guide ring is detachably connected with the base.
Optionally, the upper shell is a conical structure, the large end of the conical structure is detachably connected with the dish-shaped body, and the circular arc-shaped protrusion is arranged at the center of the small end of the conical structure.
Optionally, the upper shell is connected with the dish-shaped body through a first screw.
Optionally, the satellite telemetry terminal device further comprises a circuit board, wherein the circuit board is arranged in a containing cavity formed by surrounding the upper shell and the lower shell.
Optionally, the satellite telemetry terminal device further comprises a storage battery arranged in the accommodating cavity, and the storage battery is electrically connected with the solar panel.
Optionally, the satellite telemetry terminal device further comprises an antenna, wherein the antenna is arranged in the accommodating cavity.
The utility model has the beneficial effects that: the satellite telemetry terminal device provided by the utility model has the advantages that the conical groove is formed in the upper shell, the conical groove is arranged on the peripheral side of the circular arc-shaped bulge in a surrounding manner, the solar panel is in a conical structure and matched with the conical groove, the solar panel is fixed in the conical groove, the solar panel with the conical structure can receive sunlight irradiation in a large area, generate electricity in 360 degrees without dead angles, so that the power generation is maximized, the conical structure can play a role in quick drainage or foreign matter, and the satellite telemetry terminal device can be applied to the environments such as oceans, polar regions, deserts, island, glaciers, highland and the like; the solar panel is fixed on the upper shell, so that the upper shell is effectively prevented from being directly irradiated by sunlight, the overhigh temperature of the upper shell is avoided, electronic components in the shell are protected, meanwhile, the solar panel can resist the irradiation of sunlight ultraviolet rays, and the service life of the upper shell is prolonged; the solar panel is fixed in the conical groove through the colloid to form an independent power supply system, so that the working hours and the cost for independently installing the solar panel are omitted, the installation is convenient, and the cost is saved.
Drawings
Fig. 1 is a front view of a satellite telemetry terminal apparatus provided in an embodiment of the present utility model;
FIG. 2 is a cross-sectional view of a satellite telemetry terminal apparatus provided by an embodiment of the present utility model;
fig. 3 is a schematic view of wind direction provided by an embodiment of the present utility model.
In the figure:
100. a mounting base; 110. a base; 120. a cylinder;
210. an upper case; 211. arc-shaped protrusions; 212. a conical groove; 220. a lower case; 221. a cone; 2211. a guide ring; 222. a dish-shaped body;
300. a solar panel;
400. a first screw;
500. and a second screw.
Detailed Description
The utility model is described in further detail below with reference to the drawings and examples. It is to be understood that the specific embodiments described herein are merely illustrative of the utility model and are not limiting thereof. It should be further noted that, for convenience of description, only some, but not all of the structures related to the present utility model are shown in the drawings.
In the description of the present utility model, unless explicitly stated and limited otherwise, the terms "connected," "connected," and "fixed" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communicated with the inside of two elements or the interaction relationship of the two elements. The specific meaning of the above terms in the present utility model will be understood in specific cases by those of ordinary skill in the art.
In the present utility model, unless expressly stated or limited otherwise, a first feature "above" or "below" a second feature may include both the first and second features being in direct contact, as well as the first and second features not being in direct contact but being in contact with each other through additional features therebetween. Moreover, a first feature being "above," "over" and "on" a second feature includes the first feature being directly above and obliquely above the second feature, or simply indicating that the first feature is higher in level than the second feature. The first feature being "under", "below" and "beneath" the second feature includes the first feature being directly under and obliquely below the second feature, or simply means that the first feature is less level than the second feature.
In the description of the present embodiment, the terms "upper", "lower", "right", etc. orientation or positional relationship are based on the orientation or positional relationship shown in the drawings, and are merely for convenience of description and simplicity of operation, and do not indicate or imply that the apparatus or elements referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as limiting the utility model. Furthermore, the terms "first," "second," and the like, are used merely for distinguishing between descriptions and not for distinguishing between them.
The embodiment provides a satellite telemetry terminal device, and aims to solve the problems of complicated installation, high installation cost, complex structure and limited applicable scene of a solar panel in the prior art, optimize the structure of the solar panel, simplify the installation and enlarge the application range.
As shown in fig. 1-3, the satellite telemetry terminal device comprises a mounting base 100, a shell and a solar panel 300, wherein the shell comprises an upper shell 210 and a lower shell 220 which are connected with each other, the lower shell 220 is connected with the mounting base 100, a circular arc-shaped protrusion 211 is arranged at the center of the upper shell 210, a conical groove 212 is also arranged on the upper shell 210, and the conical groove 212 is surrounded on the periphery of the circular arc-shaped protrusion 211; the solar panel 300 has a conical structure, and the solar panel 300 is fixed in the conical groove 212 through colloid.
In the satellite telemetry terminal device provided by the embodiment, the upper shell 210 is provided with the conical groove 212, the conical groove 212 is surrounded on the periphery of the circular arc-shaped protrusion 211, the solar panel 300 is in a conical structure and matched with the conical groove 212, the solar panel 300 is fixed in the conical groove 212, the solar panel 300 with the conical structure can receive sunlight irradiation in a large area, 360-degree dead angle-free power generation is realized, the power generation is maximized, the conical structure can play a role in rapid drainage or foreign matter, and the satellite telemetry terminal device can be applied to the environments such as oceans, polar regions, deserts, island islands, glaciers, highland the like; the solar panel 300 is fixed on the upper shell 210, so that the upper shell 210 is effectively prevented from being directly irradiated by sunlight, the overhigh temperature of the upper shell 210 is avoided, electronic components in the shell are protected, meanwhile, the solar panel 300 can resist the irradiation of sunlight ultraviolet rays, and the service life of the upper shell 210 is prolonged; the solar panel 300 is fixed in the conical groove 212 through colloid to form an independent power supply system, so that the working hours and the cost for independently installing the solar panel 300 are omitted, the installation is convenient, and the cost is saved.
Optionally, the lower shell 220 includes a cone 221 and a dish 222, the small end of the cone 221 is connected to the mount 100, the large end of the cone 221 is connected to the dish 222, and the upper shell 210 is connected to the dish 222 at the end remote from the cone 221. The cone 221 plays a role in connection transition, and the cone 221 can support the dish-shaped body 222, so that the whole structure is stable and reliable; when wind blows to the satellite telemetry terminal device along one side, the structure of the dish-shaped body 222 generates tangential force to wind, so that wind resistance is reduced, and the satellite telemetry terminal device is stable and reliable in use.
In this embodiment, the mounting base 100 includes a base 110 and a cylinder 120 disposed on the base 110, the small end of the cone 221 is connected with the base 110, the base 110 increases the contact area between the whole mounting base 100 and other components, and ensures the stability of connection.
Preferably, the small end of the cone 221 is convexly provided with a guide ring 2211, the guide ring 2211 extends into the cylinder 120 and is connected with the base 110, and the arrangement of the guide ring 2211 prevents the cone 221 from shaking on the mounting seat 100, so that the connection stability between the lower shell 220 and the mounting seat 100 is improved.
Optionally, the upper shell 210 has a conical structure, a large end of the conical structure is detachably connected with the disc-shaped body 222, and the circular arc-shaped protrusion 211 is disposed at the center of a small end of the conical structure. When wind blows to the satellite telemetry terminal device along one side, the conical structure generates tangential force to wind, reduces wind resistance, ensures smooth air flow and improves the use stability of the satellite telemetry terminal device.
Preferably, the upper case 210 is connected with the dish 222 by a first screw 400; the guide ring 2211 is detachably connected with the base 110, so that the disassembly and the assembly are convenient. For example, the guide ring 2211 may be threadably coupled to the base 110 by a second threaded member.
The satellite telemetry terminal device further comprises a circuit board, a storage battery and an antenna, wherein the circuit board, the storage battery and the antenna are arranged in a containing cavity formed by surrounding the upper shell 210 and the lower shell 220, the storage battery is electrically connected with the solar panel 300, the upper shell 210 and the lower shell 220 prevent the circuit board, the storage battery and the antenna from being influenced by external environments, and the use reliability of the satellite telemetry terminal device is improved.
It is to be understood that the above examples of the present utility model are provided for clarity of illustration only and are not limiting of the embodiments of the present utility model. Various obvious changes, rearrangements and substitutions can be made by those skilled in the art without departing from the scope of the utility model. It is not necessary here nor is it exhaustive of all embodiments. Any modification, equivalent replacement, improvement, etc. which come within the spirit and principles of the utility model are desired to be protected by the following claims.
Claims (10)
1. A satellite telemetry terminal apparatus, comprising:
a mounting base (100);
the shell comprises an upper shell (210) and a lower shell (220) which are connected with each other, wherein the lower shell (220) is connected with the mounting seat (100), a circular arc-shaped protrusion (211) is arranged at the center of the upper shell (210), a conical groove (212) is further formed in the upper shell (210), and the conical groove (212) is arranged on the periphery of the circular arc-shaped protrusion (211) in a surrounding mode;
the solar panel (300) is in a cone-shaped structure, and the solar panel (300) is fixed in the cone-shaped groove (212) through colloid.
2. The satellite telemetry terminal assembly of claim 1 wherein the lower housing (220) comprises a cone (221) and a dish (222), the small end of the cone (221) being connected to the mount (100), the large end of the cone (221) being connected to the dish (222), the upper housing (210) being connected to the end of the dish (222) remote from the cone (221).
3. The satellite telemetry terminal assembly of claim 2 wherein said mounting block (100) comprises a base (110) and a barrel (120) disposed on said base (110), a small end of said cone (221) being connected to said base (110).
4. A satellite telemetry terminal device according to claim 3, characterized in that the small end of the cone (221) is provided with a protruding guide ring (2211), the guide ring (2211) extending into the barrel (120) and being connected to the base (110).
5. The satellite telemetry terminal assembly of claim 4 wherein said guide ring (2211) is removably connected to said base (110).
6. The satellite telemetry terminal assembly of claim 2 wherein the upper housing (210) is of a tapered configuration, a large end of the tapered configuration being detachably connected to the dish (222), and the arcuate projection (211) being centrally located at a small end of the tapered configuration.
7. The satellite telemetry terminal assembly of claim 6 wherein said upper housing (210) is connected to said dish (222) by a first screw (400).
8. The satellite telemetry terminal device of claim 1, further comprising a circuit board disposed within a receiving cavity formed by the upper shell (210) and the lower shell (220).
9. The satellite telemetry terminal assembly of claim 8, further comprising a battery disposed within the receiving cavity, the battery being electrically connected to the solar panel (300).
10. The satellite telemetry terminal apparatus of claim 8, further comprising an antenna disposed within the receiving cavity.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322110559.7U CN220492893U (en) | 2023-08-07 | 2023-08-07 | Satellite telemetry terminal device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322110559.7U CN220492893U (en) | 2023-08-07 | 2023-08-07 | Satellite telemetry terminal device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220492893U true CN220492893U (en) | 2024-02-13 |
Family
ID=89839103
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322110559.7U Active CN220492893U (en) | 2023-08-07 | 2023-08-07 | Satellite telemetry terminal device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220492893U (en) |
-
2023
- 2023-08-07 CN CN202322110559.7U patent/CN220492893U/en active Active
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