CN116613522A - Satellite antenna forming method with power generation function - Google Patents
Satellite antenna forming method with power generation function Download PDFInfo
- Publication number
- CN116613522A CN116613522A CN202310496005.7A CN202310496005A CN116613522A CN 116613522 A CN116613522 A CN 116613522A CN 202310496005 A CN202310496005 A CN 202310496005A CN 116613522 A CN116613522 A CN 116613522A
- Authority
- CN
- China
- Prior art keywords
- power generation
- layer
- satellite antenna
- generation function
- forming
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000010248 power generation Methods 0.000 title claims abstract description 21
- 238000000034 method Methods 0.000 title claims abstract description 15
- 239000010410 layer Substances 0.000 claims abstract description 33
- 239000011241 protective layer Substances 0.000 claims abstract description 21
- 239000002184 metal Substances 0.000 claims abstract description 20
- 238000003466 welding Methods 0.000 claims description 3
- 238000000748 compression moulding Methods 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 abstract description 2
- 239000010409 thin film Substances 0.000 description 9
- 230000005611 electricity Effects 0.000 description 5
- 239000010408 film Substances 0.000 description 5
- 239000000047 product Substances 0.000 description 3
- 238000000465 moulding Methods 0.000 description 2
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000007723 die pressing method Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
- 239000011265 semifinished product Substances 0.000 description 1
Classifications
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/36—Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith
- H01Q1/38—Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith formed by a conductive layer on an insulating support
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
- H01Q1/288—Satellite antennas
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q15/00—Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
- H01Q15/14—Reflecting surfaces; Equivalent structures
- H01Q15/16—Reflecting surfaces; Equivalent structures curved in two dimensions, e.g. paraboloidal
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
- H02S20/00—Supporting structures for PV modules
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
- H02S20/00—Supporting structures for PV modules
- H02S20/20—Supporting structures directly fixed to an immovable object
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Astronomy & Astrophysics (AREA)
- General Physics & Mathematics (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Electromagnetism (AREA)
- Aerials With Secondary Devices (AREA)
Abstract
The invention belongs to the technical field of photoelectric correlation switches, and particularly relates to a satellite antenna forming method with a power generation function, wherein a satellite antenna structure sequentially comprises a bottom protective layer, a metal reflecting layer, a middle protective layer and a solar energy receiving layer from bottom to top; the invention provides a satellite antenna forming method with a power generation function, which integrates photovoltaic power generation and satellite reception onto the same pot body, has a simple and feasible structure, is convenient for production and forming, is stable and reliable in forming, can not interfere with the satellite reception, realizes solar energy reception through direct irradiation, has a large receiving area of a photovoltaic panel, does not need to calculate a complex transmitting angle, is stable in power generation, and ensures power generation.
Description
Technical Field
The invention belongs to the technical field of photoelectric correlation switches, and particularly relates to a satellite antenna forming method with a power generation function.
Background
The satellite receiving antenna, which is a so-called big pot, is a metal paraboloid and is responsible for reflecting satellite signals into a feed source and a tuner which are positioned at a focus.
Photovoltaic panels generally refer to photovoltaic panel assemblies. The photovoltaic panel assembly is a power generation device which generates direct current when exposed to sunlight;
at present, camping heat and travel heat occur, many young people can camp in the field, but some barren suburbs can not be electrified in the field, and mobile phone signals are not available, so that many people select to use a photovoltaic plate to generate electricity, and use a satellite antenna to receive satellite programs, and at present, the photovoltaic plate and the satellite antenna are independent products, and how to skillfully combine the photovoltaic plate and the satellite antenna together to form an integrated product is the research and development direction of people.
Patent CN207852893U discloses a portable satellite communication antenna, and it includes that the front surface fixed of parabolic reflection panel 4 is provided with the connecting rod and around the fixed surface of connecting rod being provided with solar film battery 9, the top of connecting rod is provided with feed source 10 jointly and feed source 10 electricity is connected the down converter, and solar film battery 9 electricity is connected the charge-discharge controller. The parabolic reflecting panel can reflect sunlight at the same time, and the solar thin film battery is arranged on the surface of the connecting rod, so that solar energy can be utilized to generate electricity, and energy sources are saved.
Through the device. The parabolic reflection panel reflects sunlight to the solar thin film battery, and the solar energy utilization rate is poor because the sunlight is not directly irradiated, so that stable power generation is difficult; in addition, because the solar thin film battery can shield part of the parabolic reflecting surface, and the angle of the sun changes at any time, the solar thin film battery can stably reflect sunlight to the solar thin film battery, the solar thin film battery is very difficult to realize, the requirement on the angle calculation is very high, the solar thin film battery is difficult to be used in practice, the solar thin film battery can stably generate electricity, and the solar thin film battery is arranged on the connecting rod, so that the problem of how to stabilize the film on the connecting rod is also very great exists.
Disclosure of Invention
The invention provides a satellite antenna forming method with a power generation function, which can solve the problems pointed out in the background technology.
The satellite antenna structure sequentially comprises a bottom protective layer, a metal reflecting layer, a middle protective layer and a solar energy receiving layer from bottom to top; the solar energy receiving layer is a solar energy film layer which is fixed on the surface of the middle protective layer through a fixing ring.
Preferably, the bottom protective layer and the middle protective layer are both plastic protective layers, and are molded integrally with the metal reflecting layer.
Preferably, the metal reflecting layer is a metal grid.
Preferably, the fixing ring is a plastic fixing ring which is fixedly connected through an ultrasonic welding process.
The beneficial effects are that: the invention provides a satellite antenna forming method with a power generation function, which integrates photovoltaic power generation and satellite reception on the same pot body, has the advantages of simple and feasible structure, convenient production and forming, stable and reliable forming, no mutual interference of the photovoltaic power generation and the satellite reception, realization of solar energy receiving through direct irradiation, large receiving area of a photovoltaic panel, no need of calculating a complex transmitting angle, stable power generation and guaranteed power generation.
Drawings
Figure 1 is a schematic view of the structure of the present invention,
reference numerals illustrate:
reference numerals in the drawings: a bottom protective layer 1; a metal reflective layer 2; an intermediate protective layer 3; a solar energy receiving layer 4; and a fixing ring 5.
Detailed Description
One embodiment of the present invention will be described in detail below with reference to the attached drawings, but it should be understood that the scope of the present invention is not limited by the embodiment.
Example 1:
as shown in fig. 1, in the method for forming a satellite antenna with a power generation function provided by the embodiment of the invention, the satellite antenna structure sequentially comprises a bottom protective layer 1, a metal reflecting layer 2, an intermediate protective layer 3 and a solar receiving layer 4 from bottom to top; the bottom protective layer 1, the metal reflecting layer 2 and the middle protective layer 3 are integrally formed through compression molding, and the solar receiving layer 4 is a solar film layer and is fixed on the surface of the middle protective layer 3 through a fixing ring 5.
The bottom protection layer 1 and the middle protection layer 3 are both plastic protection layers, the metal reflection layer 2 is a metal grid, the metal reflection layer and the metal reflection layer 2 are molded into a whole, the plastic material cost is low, the molding is convenient, and the metal grid design is combined, so that the metal reflection layer has the advantages of light weight, low cost and convenience in molding.
The fixing ring 5 is a plastic fixing ring, the plastic fixing ring is fixedly connected through an ultrasonic welding process, and the plastic fixing ring is welded on the semi-finished product formed by the die pressing and the integral forming, so that the solar energy receiving layer 4 is stabilized on the surface of the middle protective layer 3, the forming quality of the finished product is good, and the forming is stable.
The foregoing disclosure is merely illustrative of some embodiments of the invention, but the embodiments are not limited thereto and variations within the scope of the invention will be apparent to those skilled in the art.
Claims (4)
1. A forming method of a satellite antenna structure with a power generation function is characterized by comprising the following steps: the satellite antenna structure comprises a bottom protective layer (1), a metal reflecting layer (2), a middle protective layer (3) and a solar energy receiving layer (4) from bottom to top in sequence; the bottom protection layer (1), the metal reflection layer (2) and the middle protection layer (3) are integrally formed through compression molding, and the solar energy receiving layer (4) is a solar energy film layer which is laid on the surface of the middle protection layer (3) and is fixed through the fixing ring (5).
2. The method for forming a satellite antenna with power generation function according to claim 1, wherein: the bottom protective layer (1) and the middle protective layer (3) are plastic protective layers and are molded integrally with the metal reflecting layer (2).
3. The method for forming a satellite antenna with power generation function according to claim 2, wherein: the metal reflecting layer (2) is a metal grid.
4. The method for forming a satellite antenna with power generation function according to claim 2, wherein: the fixing ring (5) is a plastic fixing ring and is fixedly connected through an ultrasonic welding process.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310496005.7A CN116613522A (en) | 2023-05-05 | 2023-05-05 | Satellite antenna forming method with power generation function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310496005.7A CN116613522A (en) | 2023-05-05 | 2023-05-05 | Satellite antenna forming method with power generation function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN116613522A true CN116613522A (en) | 2023-08-18 |
Family
ID=87673884
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202310496005.7A Pending CN116613522A (en) | 2023-05-05 | 2023-05-05 | Satellite antenna forming method with power generation function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN116613522A (en) |
-
2023
- 2023-05-05 CN CN202310496005.7A patent/CN116613522A/en active Pending
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