An S-band satellite antenna
By designing a ring-mounted S-band satellite antenna, using the combination of multiple antenna units and transceiver and receive synthesis units, the problem of existing antennas being unable to track over-top satellites and large space occupation is solved, and effective satellite communication and space savings are achieved.
Patent Information
- Application Number
- CN202211186180.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2022-09-27
- Publication Date
- 2025-03-07
- Estimated Expiration
- 2042-09-27
AI Technical Summary
Existing S-band satellite antennas cannot effectively track over-top satellites and occupy a large space.
An S-band satellite antenna including a plurality of antenna units and a corresponding transceiver and receive synthesis unit is designed. The antenna unit is mounted in a ring shape on the support frame. Each transceiver and receive synthesis unit is arranged under each antenna unit, and a metal layer is insulated on the upper surface of the first mounting plate, and an interface is electrically connected to the interface to realize the adjustment of the synthetic direction diagram.
Effective tracking of over-top satellites is achieved, ensuring good communication between antennas and satellites, and taking up less space.
Smart Images

Figure CN115513637B_ABST
Abstract
Description
Technical Field
[0001] The invention belongs to the field of antennas, and in particular relates to an S-band satellite antenna. Background Art
[0002] The revolution period of low-orbit communication satellites is relatively short, usually 1.5 to 2 hours. The best communication period is when the satellite passes overhead. In order to make full use of this period and ensure a certain communication link margin, the S-band satellite antenna has an application requirement for the design of an antenna whose directional pattern can track the satellite trajectory. Summary of the invention
[0003] The main technical problem solved by the present invention is to provide an S-band satellite antenna, which solves the problem in the prior art that the antenna of this frequency band cannot effectively track overhead satellites and occupies a large space.
[0004] In order to solve the above technical problems, the technical solution adopted by the present invention is to provide an S-band satellite antenna, including multiple antenna units and multiple corresponding transceiver synthesis units, and a base. The multiple antenna units are mounted on a support frame and form a ring. Each transceiver synthesis unit is correspondingly arranged under each antenna unit, and the base is arranged under the transceiver synthesis unit; the antenna unit includes a first mounting plate and a metal layer, the metal layer is insulated and arranged on the upper surface of the first mounting plate, an interface is arranged on the top of the transceiver synthesis unit, and the metal layer is electrically connected to the interface.
[0005] Preferably, there is a gap between adjacent antenna units.
[0006] Preferably, a first metal plate is arranged below the first mounting plate.
[0007] Preferably, the first mounting plate includes a substrate of metal material, a first raised layer of insulating material and a second raised layer of insulating material arranged in sequence from bottom to top, the metal layer includes a first metal layer and a second metal layer, the first metal layer is covered and arranged on the upper surface of the first raised layer, and the second metal layer is a hollow structure and is arranged on the upper surface of the second raised layer around the periphery of the first raised layer.
[0008] Preferably, there are eight antenna units and eight transceiver combining units, the eight transceiver combining units are arranged in a ring shape, and one antenna unit corresponds to one transceiver combining unit above and below.
[0009] Preferably, the first metal layer and the second metal layer are respectively connected to the corresponding transceiver combining unit via a feeder line.
[0010] Preferably, the support frame includes multiple support plates, a support plate and multiple support beams. The support plate is arranged below the antenna unit. The multiple support beams are connected to the edges of the support plate and surround the support plate. The support beams are connected to the upper part of the support plate, and the lower part of the support plate is connected to the base.
[0011] Preferably, the support plate is provided with a plurality of second via holes in a ring shape, and the first metal plate is provided with a corresponding first through hole, and the feeder connecting the first metal layer and the second metal layer is insulated and passes through the first through hole and the second through hole to be connected to the corresponding transceiver combining unit.
[0012] Preferably, the transmitting and receiving combining unit is arranged vertically, and its vertical height is adapted to the height of the supporting plate.
[0013] Preferably, it also includes a shell, which is covered on the base and covers the antenna unit, the transceiver combining unit and the supporting frame.
[0014] The beneficial effects of the present invention are as follows: the present invention discloses an S-band satellite antenna, comprising a plurality of antenna units and a plurality of corresponding transceiver synthesis units, and a base, wherein the plurality of antenna units are mounted on a support frame in a ring-shaped manner, each transceiver synthesis unit is correspondingly arranged below each antenna unit, and the base is arranged below the transceiver synthesis unit; the antenna unit comprises a first mounting plate and a metal layer, the metal layer is insulated and arranged on the upper surface of the first mounting plate, an interface is arranged on the top of the transceiver synthesis unit, and the metal layer is electrically connected to the interface. The S-band satellite antenna can effectively track overhead satellites, ensure good communication between the antenna and the satellite, and the S-band satellite antenna occupies less space volume. BRIEF DESCRIPTION OF THE DRAWINGS
[0015] Figure 1 is a schematic diagram of an embodiment of an S-band satellite antenna of the present invention;
[0016] Figure 2 yes Figure 1 An exploded schematic diagram of the illustrated embodiment;
[0017] Figure 3 yes Figure 1 An exploded schematic diagram of the illustrated embodiment (with the housing removed);
[0018] Figure 4 This is a schematic diagram of a first mounting plate in another embodiment of an S-band satellite antenna of the present invention;
[0019] Figure 5 is a schematic diagram of a metal layer in another embodiment of an S-band satellite antenna of the present invention;
[0020] Figure 6 is a schematic diagram of a support frame in another embodiment of an S-band satellite antenna of the present invention;
[0021] Figure 7 is a schematic diagram of support legs in another embodiment of the S-band satellite antenna of the present invention;
[0022] Figure 8 is a schematic diagram of support legs in another embodiment of the S-band satellite antenna of the present invention;
[0023] Fig. 9 is a cross-sectional view of a support frame in another embodiment of an S-band satellite antenna of the present invention;
[0024] Fig.10 It is a schematic diagram of a support plate in another embodiment of the S-band satellite antenna of the present invention. DETAILED DESCRIPTION
[0025] In order to facilitate the understanding of the present invention, the present invention is described in more detail below in conjunction with the accompanying drawings and specific embodiments. Preferred embodiments of the present invention are provided in the accompanying drawings. However, the present invention can be implemented in many different forms and is not limited to the embodiments described in this specification. On the contrary, the purpose of providing these embodiments is to make the understanding of the disclosure of the present invention more thorough and comprehensive.
[0026] It should be noted that, unless otherwise defined, all technical and scientific terms used in this specification have the same meaning as those commonly understood by those skilled in the art of the present invention. The terms used in the specification of the present invention are only for the purpose of describing specific embodiments and are not intended to limit the present invention.
[0027] In the drawings, arrow X indicates the front direction, that is, the front-rear direction, arrow Y indicates the side direction, that is, the left-right direction, and arrow Z indicates the vertical direction, that is, the up-down direction.
[0028] Combination Figure 1 , Figure 2 and Figure 3The S-band satellite antenna includes a plurality of antenna units S1 and a plurality of corresponding transceiver synthesis units S2, and a base 1. The plurality of antenna units S1 are mounted on a support frame in a ring shape. Each transceiver synthesis unit S2 is correspondingly arranged below each antenna unit S1. The base 1 is arranged below the transceiver synthesis unit S2. The antenna unit S1 includes a first mounting plate S11 and a metal layer S12. The metal layer S12 is insulated and arranged on the upper surface of the first mounting plate S11 and is electrically insulated from the first mounting plate S11. An interface S21 is arranged on the top of the transceiver synthesis unit S2. The metal layer S12 is electrically connected to the interface S21. Specifically, there is a gap between adjacent antenna units S1. There are eight antenna units S1, eight transceiver synthesis units S2, and eight transceiver synthesis units S2. It is ring-shaped, and one antenna unit S1 corresponds to a transceiver synthesis unit S2 above and below. There is a gap between adjacent antenna units S1, that is, the multiple antenna units S1 enclosed in a ring are actually composed of eight independent small units, and the diameter of the ring formed by the eight antenna units S1 is 300mm. The significance of setting the gap is to divide the ring-shaped antenna unit S1 into multiple small units through the gap. The size of each small unit becomes smaller, which can reduce the influence of the entire ring-shaped antenna unit S1 on the radiation pattern and improve the low elevation angle gain. Therefore, multiple antenna units and corresponding transceiver synthesis units can be controlled separately, and then the synthetic radiation pattern of the antenna can be changed according to the spatial position of the satellite passing overhead, so that the direction of the antenna can change with the position of the satellite.
[0029] In actual applications, according to the spatial position of the satellite passing overhead, these transceiver synthesis units S2 and the corresponding antenna units S1 are powered on in a targeted manner, and not all of the transceiver synthesis units S2 and the corresponding antenna units S1 are kept working all the time. In this way, each transceiver synthesis unit S2 and the corresponding antenna unit S1 can be controlled separately, so that the required directional pattern can be synthesized, so that the spatial position of the satellite can be tracked more targetedly.
[0030] Further preferably, combined with Figure 4 and Figure 5The first mounting plate S11 includes a substrate S111 of metal material, a first raised layer S112 of insulating material, and a second raised layer S113 of insulating material, which are arranged in sequence from bottom to top. The first raised layer S112 and the second raised layer S113 are formed integrally from insulating material. The substrate S111 is a sector with sharp corners cut off. The first raised layer S112 is arranged on the substrate S111, and the second raised layer S113 is arranged on the first raised layer S112. The sizes of the substrate S111, the first raised layer S112, and the second raised layer S113 decrease in sequence. The first raised layer S112 is a raised plate-like structure, and fixed mounting holes are arranged at the four corners for connecting and fixing the first raised layer S112 to the first mounting plate S11. The second raised layer S113 is a rectangular parallelepiped.
[0031] Preferably, the metal layer S12 includes a first metal layer S121 and a second metal layer S122, the first metal layer S121 is covered on the upper surface of the first raised layer S112, and the second metal layer S122 is a hollow structure and is arranged on the upper surface of the second raised layer S113 around the first raised layer S112.
[0032] Preferably, the first metal layer S121 and the second metal layer S122 are respectively connected to the corresponding transceiver combining unit S2 via a feeder line.
[0033] Preferably, a first metal plate S13 is disposed below the first mounting plate S11.
[0034] Preferably, a feeder for electrically connecting the metal layer S12 is provided in the first mounting plate S11. Specifically, the feeder is vertically arranged, with the lower end of the feeder connected to the first mounting plate S11 and the upper end of the feeder connected to the metal layer S12.
[0035] Preferably, the first metal plate S13 is in the shape of a sector with sharp corners cut off, and the shape is adapted to the shape of the base plate S111 of the first mounting plate S11.
[0036] Further preferably, a first through hole S131 is formed on the first metal plate S13, and the first through hole S131 corresponds to the upper and lower positions of the feeder line, that is, the vertical projection of the feeder line falls into the first through hole S131.
[0037] Preferably, the first mounting board S11 is provided with a first wire D1 and a second wire D2 inside, the first metal layer S121 is connected to the first end of the first wire D1, and the second metal layer S122 is connected to the first end of the second wire D2. Specifically, there are two feeders, the first metal layer S121 is connected to the first end of the first wire D1 through one of the feeders, the second metal layer S122 is connected to the second wire D2 through another feeder, and the second end of the first wire D1 and the second end of the second wire D2 are connected to the interface S21 at the top of the transceiver synthesis unit S2. More specifically, each transceiver synthesis unit S2 has two interfaces S21 at the top, the second end of the first wire D1 is connected to one of the interfaces S21, and the second end of the second wire D2 is connected to the other interface S21.
[0038] Preferably, the transceiver combining unit S2 is vertically arranged, and its vertical height is adapted to the height of the support plate, and the transceiver combining unit S2 is a vertically arranged column.
[0039] Preferably, combined with Figure 6 , Fig. 9 and Fig.10 The support frame S3 includes multiple support plates S31, a support plate S32 and multiple support beams S33. The support plate S32 is arranged below the antenna unit S1. Multiple support beams S33 are connected to the edges of the support plate S32 and enclose the support plate S32. The support beams S33 are connected to the upper part of the support plate S31. The lower part of the support plate S31 is connected to the base 1. The support plate S32 is used to support the S-band satellite antenna to enhance the support stability of the antenna.
[0040] Preferably, the support frame S3 is made of nylon.
[0041] Specifically, the support plate S32 is horizontally arranged, and the support plate S32 is in close contact with and supports the first metal plate S13. The support plate S32 is disc-shaped, and the support plate S32 is adapted to the shape of the plurality of first metal plates S13 arranged in an annular manner.
[0042] Preferably, the support beam S33 and the support plate S31 are integrally formed to make the structure more solid, or the support beam S33 and the support plate S31 are in surface contact, that is, the edge where the support beam S33 contacts the support plate S31 is an inclined surface, which is convenient for fitting to the surface of the support plate S31.
[0043] Preferably, the side walls of the plurality of support beams S33 are connected to the edges of the support plate S32 and enclose the support plate S32. This arrangement enables the support beams S33 to be connected in a surrounding manner with the support plate S32, thereby enhancing the stability of the support plate S32 itself.
[0044] Preferably, the lower portion of the support plate S31 is inclined toward the central axis of the support disk S32, that is, the opening formed by the upper edges of the multiple support plates S31 is larger than the opening formed by the lower edges of the multiple support plates S31. In this way, on the one hand, the lower edge of the support plate S31 can stably support the S-band satellite antenna, and on the other hand, it can also reduce the space area occupied by the lower edge support of the support plate S31, thereby reducing the overall volume of the S-band satellite antenna.
[0045] Preferably, the acute angle formed by the central axis of the support plate S31 and the support disk S32 is in the range of 20°-70°.
[0046] Preferably, the acute angle formed by the central axis of the support plate S31 and the support disk S32 is 30°, which can well form a support angle and enhance the support stability. At the same time, the 30° angle can also balance the support stability and the support height of the support plate S31. When the angle of the above-mentioned acute angle gradually increases, the support height of the support plate S31 will decrease, and the overall height of the S-band satellite antenna will also decrease, reducing the overall volume of the antenna.
[0047] Preferably, there are four support plates S31 and four support beams S33 , and the four support beams S33 are enclosed to form a square, which is conducive to the uniform arrangement of the support beams S33 and also convenient for surrounding the support plate S32 .
[0048] Preferably, the width of the support plate S31 gradually increases from bottom to top, and the body of the support plate S31 gradually tilts leftward from bottom to top.
[0049] Preferably, a plurality of mutually cross-connected reinforcing ribs S311 are provided on the plate surface of the support plate S31 . The provision of the reinforcing ribs S311 enhances the structural firmness of the support plate S31 and enhances the supporting stability of the support plate S31 .
[0050] Preferably, four connecting parts S321 extend from the edge of the support plate S32, and the four connecting parts S321 are respectively connected to the middle positions of the four support beams S33. The setting of the connecting parts S321 enhances the connection stability between the support plate S32 and the support beams S33, making the support of the support plate S32 more stable. At the same time, the setting of the connecting parts S321 also enables the support plate S32 to be quickly disassembled and assembled from the support beams S33, specifically by connecting the support plate S32 and the support beams S33 through screws.
[0051] Further preferably, the connection portion S321 is square, and a screw hole is provided on the connection portion S321 to facilitate fixing with screws.
[0052] Preferably, the support plate S32 is provided with a plurality of second via holes S323 in a ring shape, and the first metal plate S13 is correspondingly provided with a first through hole S131, and the feeder insulation connecting the first metal layer S121 and the second metal layer S122 passes through the first through hole S131 and the second through hole S323 and is connected to the corresponding transceiver combining unit S2.
[0053] Further preferably, the plurality of second via holes S323 are evenly arranged in a ring around the center point of the support plate S32 , the second via holes S323 are oblong holes, and each second via hole S323 corresponds to the metal layer S12 above and below.
[0054] Preferably, the support plate S31 is a straight hexagonal structure as a whole, including a first horizontal side 101 and a second horizontal side 102 arranged horizontally and in parallel, the first horizontal side 101 is located at the upper part, the second horizontal side 102 is located at the lower part, and the length of the first horizontal side 101 is greater than the length of the second horizontal side 102; it also includes a first vertical side 103 and a second vertical side 104 arranged vertically and in parallel, the first vertical side 103 is located at the upper part, and its upper end is combined with the left end of the first horizontal side 101, and the second vertical side 104 is located at the lower part, and its lower end is combined with the right end of the second horizontal side 102; it also includes a first inclined side 105 and a second inclined side 106 arranged obliquely, the upper end of the first inclined side 105 is connected to the lower end of the first vertical side 103, the lower end of the first inclined side 105 is connected to the left end of the second horizontal side 102, the upper end of the second inclined side 106 is connected to the right end of the first horizontal side 101, and the lower end of the second inclined side 106 is connected to the upper end of the second vertical side 104.
[0055] Preferably, combined with Figure 7 and Figure 8 , and also includes a supporting foot S4, the supporting foot S4 has an inclined supporting surface S41, the supporting surface S41 is used to fit the supporting plate S31, and a screw hole S411 is provided on the supporting surface S41 for screw connection with the supporting plate S31 to enhance the connection stability between the supporting plate S31 and the supporting foot S4.
[0056] Preferably, a supporting foot fixing hole is opened on the lower edge of the supporting plate S31, and the supporting foot fixing hole includes a first supporting foot fixing hole 107 and a second supporting foot fixing hole 108. The first supporting foot fixing hole 107 is located on the lower left side of the supporting plate S31, and the second supporting foot fixing hole 108 is located on the lower right side of the supporting plate S31, that is, the supporting foot fixing hole and the screw hole S411 are fastened together by screws, so that the supporting foot S4 is closely connected to the supporting plate S31.
[0057] Preferably, the inclination angle of the support surface S41 is the same as the inclination angle of the support plate S31.
[0058] Further preferably, the supporting foot S4 has a vertically opened fixing groove S42 , and a screw hole S421 for fixing is opened on the bottom surface of the fixing groove S42 .
[0059] Preferably, it further comprises a shell S5, which is covered on the base 1 and covers the antenna unit S1, the transceiver combining unit S2 and the supporting frame.
[0060] Preferably, a navigation and positioning antenna S6 is provided on the base 1. Specifically, a navigation and positioning antenna S6 is provided at each diagonal position of the base 1 for positioning and navigation.
[0061] Preferably, the size of the base 1 is: 480 mm long*480 mm wide.
[0062] Preferably, the base 1 includes a base body 11 and a cover plate 12. A base body opening 111 that passes through the base body 11 from top to bottom is provided in the middle of the base body 11. The base body 11 has a cavity inside, which is connected to the outside downward and to the base body opening 111 upward. The cover plate 12 is arranged at the bottom of the base body 11, and covers the cavity.
[0063] Based on the above embodiments, the present invention discloses an S-band satellite antenna, including multiple antenna units and multiple corresponding transceiver synthesis units, and a base. The multiple antenna units are mounted on a support frame in an enclosed manner to form a ring, each transceiver synthesis unit is correspondingly arranged below each antenna unit, and the base is arranged below the transceiver synthesis unit; the antenna unit includes a first mounting plate and a metal layer, the metal layer is insulated and arranged on the upper surface of the first mounting plate, an interface is arranged on the top of the transceiver synthesis unit, and the metal layer is electrically connected to the interface. The S-band satellite antenna can effectively track overhead satellites to ensure good communication between the antenna and the satellite, and the S-band satellite antenna occupies less space volume.
[0064] The above are only embodiments of the present invention, and are not intended to limit the patent scope of the present invention. Any equivalent structural transformations made using the contents of the present invention's specification and drawings, or directly or indirectly applied in other related technical fields, are included in the patent protection scope of the present invention.
Claims
1. An S-band satellite antenna, characterized in that: The invention comprises a plurality of antenna units and a plurality of corresponding transceiver combining units, and a base, wherein the plurality of antenna units are mounted on a support frame in a ring shape, each transceiver combining unit is correspondingly arranged below each antenna unit, and the base is arranged below the transceiver combining unit; the antenna unit comprises a first mounting plate and a metal layer, the metal layer is insulated and arranged on the upper surface of the first mounting plate, an interface is arranged on the top of the transceiver combining unit, and the metal layer is electrically connected to the interface; There is a gap between adjacent antenna units. A first metal plate is arranged under the first mounting plate. The first mounting plate includes a substrate of metal material, a first raised layer of insulating material and a second raised layer of insulating material arranged in sequence from bottom to top. The metal layer includes a first metal layer and a second metal layer. The first metal layer is covered on the upper surface of the first raised layer, and the second metal layer is a hollow structure and is arranged on the upper surface of the second raised layer around the periphery of the first raised layer.
2. The S-band satellite antenna according to claim 1, characterized in that: There are eight antenna units and eight transceiver combining units. The eight transceiver combining units are arranged in a ring shape, and one antenna unit corresponds to one transceiver combining unit above and below.
3. The S-band satellite antenna according to claim 2, characterized in that: The first metal layer and the second metal layer are respectively connected to corresponding transceiver combining units through a feeder line.
4. The S-band satellite antenna according to any one of claims 1 to 3, characterized in that: The support frame includes multiple support plates, a support plate and multiple support beams. The support plate is arranged below the antenna unit. The multiple support beams are connected to the edges of the support plate and surround the support plate. The support beams are connected to the upper part of the support plate, and the lower part of the support plate is connected to the base.
5. The S-band satellite antenna according to claim 4, characterized in that: The support plate is provided with a plurality of second via holes in a ring shape, and the first metal plate is provided with a corresponding first through hole. The feeder connecting the first metal layer and the second metal layer is insulated and passes through the first through hole and the second through hole to be connected to the corresponding transceiver combining unit.
6. The S-band satellite antenna according to claim 5, characterized in that: The transmitting and receiving combining unit is arranged vertically, and its vertical height is adapted to the height of the supporting plate.
7. The S-band satellite antenna according to claim 6, characterized in that: It also includes a shell, which is covered on the base and covers the antenna unit, the transceiver combining unit and the supporting frame.
Citation Information
Patent Citations
LS dual-band high-precision antenna for Beidou satellite navigation system ground monitoring station
CN105896104A
Transmitting-receiving common-aperture wide-angular-domain scanning satellite communication antenna array and aircraft with same
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