CN106887715B - Self-powered satellite pot - Google Patents
Self-powered satellite pot Download PDFInfo
- Publication number
- CN106887715B CN106887715B CN201710065125.6A CN201710065125A CN106887715B CN 106887715 B CN106887715 B CN 106887715B CN 201710065125 A CN201710065125 A CN 201710065125A CN 106887715 B CN106887715 B CN 106887715B
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- CN
- China
- Prior art keywords
- storage battery
- solar cell
- self
- cell panel
- deformable
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q19/00—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
- H01Q19/10—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces
- H01Q19/12—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces wherein the surfaces are concave
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
- H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
- Y02E10/56—Power conversion systems, e.g. maximum power point trackers
Abstract
The invention discloses a self-powered satellite pan, which comprises a circular shell and a deformable solar panel, wherein a fixed support is fixedly arranged in the middle of the circular shell, a high-frequency head is fixedly arranged on the front surface of the fixed support, the lower end of the high-frequency head penetrates through the inlet of the deformable solar panel and is connected with a storage battery pack arranged at the lower end of the deformable solar panel, a photovoltaic inverter is fixedly connected with the lower end of the storage battery pack, a photomultiplier is arranged on the surface of the photovoltaic inverter, the bottom end of the photomultiplier is connected with a locking amplifier through a rotating shaft, the lower end of the deformable solar panel is also connected with a focusing plate through a lens antenna, electric energy can be stored for the whole system, electric energy can be saved, and partial electric energy can be stored in the storage battery pack to prevent the solar energy from being used when the power supply is insufficient, and the whole device has simple structure and strong practicability.
Description
Technical Field
The invention relates to the technical field of satellite pots, in particular to a self-powered satellite pot.
Background
The satellite pan is an antenna which is commonly called by people, is a metal paraboloid and is responsible for reflecting satellite signals to a feed source and a high-frequency head which are positioned at the focus of the satellite antenna, the satellite pan is used for collecting weak signals transmitted by the satellite and removing noise as much as possible, most of the satellite pans are generally in a paraboloid shape, some multi-focus satellite pans are formed by combining a spherical surface and a paraboloid, the satellite signals are concentrated to the focus of the satellite pan after being reflected by the paraboloid satellite pan, a solar panel (Solarpanel) is a device for directly or indirectly converting solar radiation energy into electric energy through a photoelectric effect or a photochemical effect by absorbing sunlight, most of the solar panel is made of silicon, but the manufacturing cost is high, so that the solar panel cannot be widely and generally used in a large quantity.
Disclosure of Invention
In order to solve the problems, the invention provides a self-powered satellite pan which is provided with a deformable solar cell panel, can store electric energy for the whole system to use, not only can save the electric energy, but also can store partial electric energy in a storage battery pack to prevent the electric energy from being used when the solar energy is insufficient, and uses a focusing plate to focus a tuner, so that the electric energy is completely utilized, and the problems in the background art can be effectively solved.
In order to achieve the purpose, the invention provides the following technical scheme: a self-powered satellite pan comprises a circular shell and a deformable solar panel, wherein a waterproof coating layer is fixedly coated on the inner surface of the circular shell, a fixed bracket is fixedly arranged in the middle of the circular shell, a high-frequency head is fixedly arranged on the front surface of the fixed support, the lower end of the high-frequency head passes through the inlet of the deformable solar cell panel and is connected with a storage battery set arranged at the lower end of the deformable solar cell panel, the lower end of the storage battery set is also fixedly connected with a photovoltaic inverter, the surface of the photovoltaic inverter is provided with a photomultiplier, the bottom end of the photomultiplier is connected with a lock-in amplifier through a rotating shaft, the left end of the locking amplifier is also fixedly connected with a radio receiving card, two ends of the deformable solar cell panel are fixedly provided with radiation plates, and the lower end of the deformable solar cell panel is also connected with the focusing plate through a lens antenna.
In a preferred embodiment of the present invention, the focusing plate is connected to the main reflecting surface through a rotating block installed inside the focusing plate, and the sub-reflecting surface is fixedly installed on the front surface of the main reflecting surface.
As a preferable technical scheme, a plurality of shock insulation layers are fixedly arranged on the periphery of the circular shell, and the shock insulation layers are symmetrically distributed on the upper surface of the circular shell.
As a preferred technical solution of the present invention, the number of the battery packs is four, and the four battery packs are respectively and fixedly mounted on two sides of the inner wall of the fixing bracket.
Compared with the prior art, the invention has the beneficial effects that: the self-powered satellite pot is provided with the deformable solar cell panel, can store electric energy for the whole system to use, can save the electric energy, can store part of the electric energy in the storage battery pack to prevent the electric energy from being used when the solar energy is insufficient, and uses the focusing plate to focus on the tuner, so that the electric energy is completely utilized, and due to the focusing effect, the focus of the solar energy collection is also at the focus of the satellite pot, and the deformable solar cell panel can be covered around the tuner. Through photovoltaic inverter, store received light energy in the battery, prepare for the power supply when having a power failure, when the battery is full of, also can be directly for the power supply of TV receiving system to unnecessary electric energy, and whole device simple structure, the practicality is strong.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic cross-sectional view of the present invention.
In the figure: 1-a circular housing; 2-a shock insulation layer; 3-waterproof coating layer; 4-a solar panel; 5-a tuner; 6-fixing a bracket; 7-a battery pack; 8-a photovoltaic inverter; 9-a rotating shaft; 10-a photomultiplier tube; 11-a lock-in amplifier; 12-a radio receiving card; 13-a radiation plate; 14-a lens antenna; 15-a focusing plate; 16-a main reflective surface; 17-sub-reflecting surface.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Example (b):
referring to fig. 1 and fig. 2, the present invention provides a technical solution: a self-powered satellite pan comprises a circular shell 1 and a deformable solar cell panel 4, wherein a waterproof coating layer 3 is fixedly coated on the inner surface of the circular shell 1, a plurality of shock insulation layers 2 are fixedly arranged on the periphery of the circular shell 1, the shock insulation layers 2 are symmetrically distributed on the upper surface of the circular shell 1, the shock insulation layers 2 are used for effectively reducing the influence of external resistance on the whole circular shell 1, the service life of the device is prolonged, a fixing support 6 is fixedly arranged in the middle of the circular shell 1, a tuner 5 is fixedly arranged on the front surface of the fixing support 6, the lower end of the tuner 5 penetrates through an inlet of the deformable solar cell panel 4 and is connected with storage battery packs 7 arranged at the lower end of the deformable solar cell panel 4, the number of the storage battery packs 7 is four, and the four storage battery packs 7 are respectively and fixedly arranged on two sides of the inner wall of the fixing support 6, the lower end of the storage battery pack 7 is also fixedly connected with a photovoltaic inverter 8, a photomultiplier tube 10 is arranged on the surface of the photovoltaic inverter 8, the bottom end of the photomultiplier tube 10 is connected with a lock-in amplifier 11 through a rotating shaft 9, the left end of the lock-in amplifier 11 is also fixedly connected with a radio receiving card 12, the radio receiving card 12 is used for receiving wireless signals, so that the system can receive not only television signals but also other types of communication signals, radiation plates 13 are fixedly arranged at the two ends of the deformable solar cell panel 4, the lower end of the deformable solar cell panel 4 is also connected with a focusing plate 15 through a lens antenna 14, the focusing plate 15 is connected with a main reflecting surface 16 through a rotating block arranged on the inner side of the focusing plate, an auxiliary reflecting surface 17 is fixedly arranged on the front surface of the main reflecting surface 16, and the main reflecting surface 16 and the auxiliary reflecting surface 17 are used for realizing the omnibearing reflection of light rays, the utilization rate of the light source is improved.
The working principle of the invention is as follows: the self-powered satellite pot is provided with the deformable solar cell panel, can store electric energy for the whole system to use, can save the electric energy, can store part of the electric energy in the storage battery pack to prevent the electric energy from being used when the solar energy is insufficient, and uses the focusing plate to focus on the tuner, so that the electric energy is completely utilized, and due to the focusing effect, the focus of the solar energy collection is also at the focus of the satellite pot, and the deformable solar cell panel can be covered around the tuner. The received light energy is stored in the storage battery through the photovoltaic inverter, and preparation is made for power supply during power failure. When the storage battery is full, redundant electric energy can be directly supplied to the television receiving system, and the whole device is simple in structure and high in practicability.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents and improvements made within the spirit and principle of the present invention are intended to be included within the scope of the present invention.
Claims (4)
1. The utility model provides a self-power satellite pan, includes circular shell (1) and deformable solar cell panel (4), the internal fixed surface of circular shell (1) scribbles waterproof coating layer (3), its characterized in that: the solar energy conversion device is characterized in that a fixing support (6) is fixedly mounted in the middle of the circular shell (1), a high-frequency head (5) is fixedly mounted on the front face of the fixing support (6), the lower end of the high-frequency head (5) penetrates through an inlet of the deformable solar cell panel (4) and is connected with a storage battery (7) arranged at the lower end of the deformable solar cell panel (4), a photovoltaic inverter (8) is fixedly connected with the lower end of the storage battery (7), a photomultiplier (10) is arranged on the surface of the photovoltaic inverter (8), the bottom end of the photomultiplier (10) is connected with a locking amplifier (11) through a rotating shaft (9), a radio receiving card (12) is fixedly connected with the left end of the locking amplifier (11), radiation plates (13) are fixedly mounted at two ends of the deformable solar cell panel (4), and the lower end of the deformable solar cell panel (4) is connected with a focusing plate (15) through a lens antenna (14) And (6) connecting.
2. A self-powered satellite dish as claimed in claim 1, wherein: the focusing plate (15) is connected with the main reflecting surface (16) through a rotating block arranged on the inner side of the focusing plate, and an auxiliary reflecting surface (17) is fixedly arranged on the front surface of the main reflecting surface (16).
3. A self-powered satellite dish as claimed in claim 1, wherein: a plurality of shock insulation layers (2) are fixedly mounted on the periphery of the round shell (1), and the shock insulation layers (2) are symmetrically distributed on the upper surface of the round shell (1).
4. A self-powered satellite dish as claimed in claim 1, wherein: the number of the storage battery packs (7) is four, and the four storage battery packs (7) are respectively and fixedly installed on two sides of the inner wall of the fixing support (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710065125.6A CN106887715B (en) | 2017-02-06 | 2017-02-06 | Self-powered satellite pot |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710065125.6A CN106887715B (en) | 2017-02-06 | 2017-02-06 | Self-powered satellite pot |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106887715A CN106887715A (en) | 2017-06-23 |
| CN106887715B true CN106887715B (en) | 2020-08-07 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710065125.6A Active CN106887715B (en) | 2017-02-06 | 2017-02-06 | Self-powered satellite pot |
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| Country | Link |
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| CN (1) | CN106887715B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108322717A (en) * | 2018-02-07 | 2018-07-24 | 马海刚 | A kind of household automatic adjustment satellite pot |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201315344Y (en) * | 2008-11-17 | 2009-09-23 | 海尔集团公司 | Satellite antenna and satellite TV receiving system installing same |
| JP2009231315A (en) * | 2008-03-19 | 2009-10-08 | Noritsugu Miyamoto | Solar power generator |
| CN201657150U (en) * | 2010-05-21 | 2010-11-24 | 昆明学院 | Portable solar satellite television |
| CN103490142A (en) * | 2013-08-30 | 2014-01-01 | 常州亚邦天线有限公司 | Solar television antenna |
| CN103812431A (en) * | 2014-01-28 | 2014-05-21 | 山东华宇空间技术公司北京分部 | Comprehensive integrated system for solar panel and antenna |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9995507B2 (en) * | 2009-04-15 | 2018-06-12 | Richard Norman | Systems for cost-effective concentration and utilization of solar energy |
| US9167228B2 (en) * | 2012-01-03 | 2015-10-20 | Lawrence Maxwell Monari | Instrumented sports paraphernalia system |
-
2017
- 2017-02-06 CN CN201710065125.6A patent/CN106887715B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009231315A (en) * | 2008-03-19 | 2009-10-08 | Noritsugu Miyamoto | Solar power generator |
| CN201315344Y (en) * | 2008-11-17 | 2009-09-23 | 海尔集团公司 | Satellite antenna and satellite TV receiving system installing same |
| CN201657150U (en) * | 2010-05-21 | 2010-11-24 | 昆明学院 | Portable solar satellite television |
| CN103490142A (en) * | 2013-08-30 | 2014-01-01 | 常州亚邦天线有限公司 | Solar television antenna |
| CN103812431A (en) * | 2014-01-28 | 2014-05-21 | 山东华宇空间技术公司北京分部 | Comprehensive integrated system for solar panel and antenna |
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| Publication number | Publication date |
|---|---|
| CN106887715A (en) | 2017-06-23 |
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