CN112187308B - Method for installing satellite communication transceiver - Google Patents
Method for installing satellite communication transceiver Download PDFInfo
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- CN112187308B CN112187308B CN202010880746.1A CN202010880746A CN112187308B CN 112187308 B CN112187308 B CN 112187308B CN 202010880746 A CN202010880746 A CN 202010880746A CN 112187308 B CN112187308 B CN 112187308B
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- 238000000034 method Methods 0.000 title claims abstract description 14
- 238000009434 installation Methods 0.000 claims abstract description 16
- 230000005540 biological transmission Effects 0.000 claims description 4
- 238000009958 sewing Methods 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 230000001174 ascending effect Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B1/00—Details of transmission systems, not covered by a single one of groups H04B3/00 - H04B13/00; Details of transmission systems not characterised by the medium used for transmission
- H04B1/38—Transceivers, i.e. devices in which transmitter and receiver form a structural unit and in which at least one part is used for functions of transmitting and receiving
- H04B1/3827—Portable transceivers
- H04B1/3877—Arrangements for enabling portable transceivers to be used in a fixed position, e.g. cradles or boosters
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B7/00—Radio transmission systems, i.e. using radiation field
- H04B7/14—Relay systems
- H04B7/15—Active relay systems
- H04B7/185—Space-based or airborne stations; Stations for satellite systems
- H04B7/1851—Systems using a satellite or space-based relay
- H04B7/18515—Transmission equipment in satellites or space-based relays
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Abstract
The invention discloses an installation method of a satellite communication transceiver, which comprises a base fixed with the installation ground through a bolt, a lifting mechanism arranged on the base, a rotating mechanism connected to the lifting mechanism and used for rotating forwards or reversely when the lifting mechanism is lifted, a satellite component movably connected to the top of the lifting mechanism and used for receiving signals, and a head swinging mechanism connecting the rotating mechanism and the satellite component. The power part drives the sliding part to move up and down, the rack and pinion is used for driving the bevel gear set to rotate, the bevel gear set drives the lead screw to rotate, the driving external member longitudinally moves under the action of threaded force, the threaded sleeve of the longitudinal movement drives the swinging part and the satellite assembly installed on the swinging part to swing, the satellite assembly can still swing at an angle while moving up and down, the inclination angle can be automatically adjusted, the characteristic of convenience in installation and adjustment is achieved, and labor is saved.
Description
Technical Field
This patent is the divisional application, and the information of former application is as follows, the name: a satellite communication transceiver with simple installation and an installation method thereof are disclosed in the application number: 2019113379432, filing date: 2019-12-23.
Background
The satellite television receiving system is composed of: the parabolic antenna, the feed source, the tuner and the satellite receiver form a complete satellite receiving station. Generally, the larger the antenna aperture, the stronger the signal of the program, and the higher the reception quality. However, in consideration of cost, installation and other factors, users demand that the antenna aperture be as small as possible.
When a parabolic antenna is installed, it is generally installed in a structure diagram provided by a manufacturer. The antenna structures of all manufacturers are basically the same in size. The structural reflecting plate of the antenna has two types of integral forming and splitting (the reflecting plate with more than 2M is split basically), the foot rest mainly comprises two types of upright foot rests and tripods (the upright foot rest is common), and the individual foot rest with less than one point and eight meters is a horizontal foot rest.
However, in the existing satellite installation, the foot rest is firstly installed on a prepared base, the level is corrected, then the iron wire of the foot rest is firmed and welded and fixed, then the upper positioning tray and the elevation angle adjusting screw rod are installed, the reinforcing support and the reflecting plate of the reflecting plate are sequentially installed on the reflecting plate tray, and finally the feed source support and the feed source fixing disc are installed, so that the installation is very complicated, and the time and the labor are consumed.
Disclosure of Invention
The present invention is directed to a method for installing a satellite communication transceiver to solve the above problems.
In order to achieve the purpose, the invention provides the following technical scheme:
a method for installing a satellite communication transceiver comprises a base fixed with an installation ground through a bolt, a lifting mechanism arranged on the base, a rotating mechanism connected to the lifting mechanism and used for rotating forwards or reversely when the lifting mechanism is lifted, a satellite assembly movably connected to the top of the lifting mechanism and used for receiving signals, and a head swinging mechanism connecting the rotating mechanism and the satellite assembly.
In a further embodiment, the lifting mechanism comprises a fixed part fixed on the base, a sliding part slidably sleeved on the upper part of the fixed part, and a power assembly for connecting the sliding part and the base.
In a further embodiment, the power assembly comprises a power member fixed on the side wall of the sliding member and a lifting member connecting the power member and the base, wherein the lower part of the lifting member is fixed on the base, and the upper part of the lifting member is slidably connected in the power member.
In a further embodiment, the rotating mechanism includes a rack plate fixed to a surface of the fixed member, a mounting member fixed to a lower portion of the sliding member, and a gear rotatably provided on the mounting member and engaged with the rack plate.
In a further embodiment, the satellite assembly is mounted on the swinging member, the swinging member is connected to a gear in the rotating mechanism through a swinging head mechanism, and the swinging head mechanism comprises a bevel gear set rotatably arranged on the sliding member, a lead screw connected with the bevel gear set and bearing-mounted on the sliding member, and an adjusting assembly for connecting the lead screw with the swinging member.
In a further embodiment, the bevel gear set comprises a first bevel gear rotatably arranged on the sliding part and a second bevel gear fixed at the end of the lead screw and engaged with the first bevel gear, wherein the gears are connected with the first bevel gear through a transmission part.
In a further embodiment, the swinging member is rotatably connected to the top of the sliding member, and the adjusting assembly includes a sleeve member screwed on the lead screw and a driving member for connecting the swinging member and the sleeve member, wherein one end of the driving member is hinged on the sleeve member, and the other end is hinged on the swinging member.
In a further embodiment, the satellite assembly comprises a receiving part fixedly arranged on the swinging part, a detachable part detachably connected to the swinging part, a satellite feed source arranged at the end head of the detachable part, and a high-frequency head connected with the feed source and fixed on the detachable part, wherein the high-frequency head is connected with a receiver arranged on the back surface of the receiving part in a signal connection mode.
In a further embodiment, a method for installing a satellite communication transceiver includes the steps of:
firstly, determining the direction, namely hanging a magnetic sewing needle by a thin thread to judge the general position of the south, and accurately determining the direction of the satellite by means of a compass;
step two, mounting and fixing, namely enabling the opening direction of the satellite component to face the south alignment direction, fixing the base on the ground by using bolts, and ensuring that the satellite component keeps the south alignment direction after fixing the base;
step three, mounting a satellite assembly, and mounting a detachable piece, a satellite feed source and a tuner on the swinging piece;
and step four, debugging, namely connecting the satellite assembly with a power supply, starting the power part to drive the satellite assembly to lift the height and adjust the inclination angle, observing the signal receiving condition while adjusting the inclination angle, and stopping lifting when the signal is well received.
Compared with the prior art, the invention has the beneficial effects that: the device drives the slider through the power spare and follows utilize rack and pinion drive bevel gear group to rotate when the mounting goes up and down, and bevel gear group drives the lead screw and rotates to the drive external member is longitudinal movement under the screw force effect, and longitudinal movement's swivel nut drives with the help of the driving piece swing piece with install satellite component swing on the swing piece reaches satellite component and still swings the angle when going up and down, and the automatically regulated inclination has the convenient characteristics of installation regulation, saves the labour.
Drawings
Fig. 1 is a schematic structural diagram of a satellite communication transceiver after installation.
Fig. 2 is a schematic structural view of a fixing member and a sliding member, and a rack plate and a mounting member in a method of mounting a satellite communication transceiver.
Fig. 3 is a schematic structural diagram of a method for installing a satellite communication transceiver before installation.
In the figure: 1-a base; 2-a fixing piece; 3-a slide; 4-a power element; 5-a lifting member; 6-rack plate; 7-a gear; 8-a mounting member; 9-a transmission member; 10-a first bevel gear; 11-a second bevel gear; 12-a lead screw; 13-a kit; 14-a drive member; 15-a swinging member; 16-a receiver; 17-a detachable piece; 18-a satellite feed source; 19-a tuner; 20-receiver.
Detailed Description
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on those shown in the drawings, and are used only for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the referenced devices or elements must have a particular orientation, be constructed and operated in a particular orientation, and thus, are not to be construed as limiting the present invention. Furthermore, the terms "first", "second", etc. are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first," "second," etc. may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless otherwise specified.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art through specific situations.
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.
In an embodiment of the present invention, please refer to fig. 1, a method for installing a satellite communication transceiver includes a base 1 fixed to an installation ground through a bolt, a lifting mechanism installed on the base 1, a rotating mechanism connected to the lifting mechanism for forward rotation or reverse rotation when the lifting mechanism is lifted, a satellite assembly movably connected to the top of the lifting mechanism for receiving signals, and a head swing mechanism connecting the rotating mechanism and the satellite assembly;
the lifting mechanism is used for driving the rotating mechanism and the satellite assembly to adjust the height in the vertical direction, and the swinging mechanism is driven to swing by the rotating mechanism while the height is adjusted, so that the satellite assembly is driven to swing, the inclination angle receiving signal is automatically adjusted, the inclination angle is automatically adjusted while the satellite assembly is lifted, and the lifting mechanism has the characteristics of simplicity and convenience in installation and easiness in operation.
In another embodiment of the present invention, referring to fig. 3, the lifting mechanism includes a fixed part 2 fixed on the base 1, a sliding part 3 slidably sleeved on an upper portion of the fixed part 2, and a power assembly for connecting the sliding part 3 and the base 1, and the power assembly drives the sliding part 3 to longitudinally slide along a surface of the fixed part 2, so as to adjust a height of the satellite assembly.
In another embodiment of the present invention, the power assembly comprises a power member 4 fixed on the side wall of the sliding member 3 and a lifting member 5 connecting the power member 4 and the base 1, wherein the lower part of the lifting member 5 is fixed on the base 1, and the upper part of the lifting member 5 is slidably connected in the power member 4;
preferably, the power member 4 is an air cylinder or a hydraulic cylinder, the lifting member 5 is a piston rod hermetically and slidably connected in the power member 4, and the lifting member 5 is driven to extend and retract in the power member 4 by changing air pressure or oil pressure in the power member 4, so as to drive the sliding member 3 to lift along the fixing member 2.
In another embodiment of the present invention, referring to fig. 2, the rotating mechanism includes a rack plate 6 fixed on the surface of the fixed member 2, a mounting member 8 fixed on the lower portion of the sliding member 3, and a gear 7 rotatably disposed on the mounting member 8 and engaged with the rack plate 6, wherein when the sliding member 3 slides up and down along the fixed member 2, the gear 7 is driven to rotate by the action of the gear 7 and the fixed rack plate 6.
In a further embodiment of the present invention, the satellite assembly is mounted on the swinging member 15, the swinging member 15 is connected to the gear 7 in the rotating mechanism through a swinging head mechanism, the swinging head mechanism comprises a bevel gear set rotatably arranged on the sliding member 3, a lead screw 12 connected with the bevel gear set and bearing-mounted on the sliding member 3, and an adjusting assembly for connecting the lead screw 12 with the swinging member 15;
specifically, when the gear 7 rotates, the bevel gear set is driven to rotate, and then the lead screw 12 is driven to rotate, and the lead screw 12 drives the adjusting assembly to operate by using a thread rotating force, so as to drive the swinging member 15 and the satellite assembly mounted on the swinging member 15 to swing by an angle.
In another embodiment of the present invention, the bevel gear set comprises a first bevel gear 10 rotatably disposed on the sliding member 3 and a second bevel gear 11 fixed at an end of the lead screw 12 and engaged with the first bevel gear 10, wherein the gear 7 is connected to the first bevel gear 10 through a transmission member 9, and the rotating gear 7 drives the bevel gear set to rotate while ascending and descending, and further drives the lead screw 12 to rotate.
In another embodiment of the present invention, the swinging member 15 is rotatably connected to the top of the sliding member 3, and the adjusting assembly includes a sleeve member 13 screwed on the lead screw 12 and a driving member 14 for connecting the swinging member 15 and the sleeve member 13, wherein one end of the driving member 14 is hinged on the sleeve member 13, and the other end is hinged on the swinging member 15, and the lead screw 12 rotates while driving the sleeve member 13 to ascend and descend, in particular, the first bevel gear 10 rotates clockwise, and drives the sleeve member to move upward.
In another embodiment of the present invention, the satellite assembly comprises a receiving element 16 fixedly mounted on the swinging element 15, a detachable element 17 detachably connected to the swinging element 15, a satellite feed 18 mounted at the end of the detachable element 17, and a tuner 19 connected to the feed 18 and fixed on the detachable element 17, wherein the tuner 19 is in signal connection with a receiver 20 mounted on the back of the receiving element 16;
the device drives slider 3 through power spare 4 and follows utilize rack and pinion drive bevel gear group to rotate when 2 lifts of mounting, bevel gear group drives lead screw 12 and rotates to drive external member 13 longitudinal movement under the screw thread effect, longitudinal movement's swivel nut 13 drives with the help of driving piece 14 swing piece 15 with install satellite assembly swing on the swing piece 15 reaches satellite assembly and still swings the angle when going up and down, and the automatically regulated inclination has the convenient characteristics of installation regulation, saves the labour.
In another embodiment of the present invention, a method for installing a satellite communication transceiver includes the steps of:
firstly, determining the direction, namely hanging a magnetic sewing needle by a thin thread to judge the general position of the south, and accurately determining the direction of the satellite by means of a compass;
step two, mounting and fixing, namely enabling the opening direction of the satellite component to face the south alignment direction, fixing the base on the ground by using bolts, and ensuring that the satellite component keeps the south alignment direction after fixing the base;
mounting a satellite assembly, mounting a detachable piece, a satellite feed source and a tuner on the swinging piece, and keeping the centers of the satellite feed source and the receiving piece on the same axis;
and step four, debugging, namely connecting the satellite assembly with a power supply, starting the power part to drive the satellite assembly to lift the height and adjust the inclination angle, observing the signal receiving condition while adjusting the inclination angle, and stopping lifting when the signal is well received.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (1)
1. A method for installing a satellite communication transceiver is characterized in that the satellite communication transceiver is based on the following satellite communication initial transmitting device, and comprises the following steps:
the satellite positioning system comprises a base (1) fixed with the installation ground through bolts, a lifting mechanism arranged on the base (1), a rotating mechanism connected to the lifting mechanism and used for rotating forwards or reversely when the lifting mechanism is lifted, a satellite assembly movably connected to the top of the lifting mechanism and used for receiving signals, and a head swinging mechanism connected with the rotating mechanism and the satellite assembly;
the lifting mechanism comprises a fixed part (2) fixed on the base (1), a sliding part (3) sleeved on the upper part of the fixed part (2) in a sliding manner, and a power assembly used for connecting the sliding part (3) with the base (1);
the power assembly comprises a power part (4) fixed on the side wall of the sliding part (3) and a lifting part (5) for connecting the power part (4) with the base (1), wherein the lower part of the lifting part (5) is fixed on the base (1), and the upper part of the lifting part (5) is connected in the power part (4) in a sliding manner;
the rotating mechanism comprises a rack plate (6) fixed on the surface of the fixed part (2), a mounting part (8) fixed at the lower part of the sliding part (3), and a gear (7) which is rotatably arranged on the mounting part (8) and is meshed with the rack plate (6);
the satellite assembly is installed on a swinging piece (15), the swinging piece (15) is connected with a gear (7) in the rotating mechanism through a swinging head mechanism, and the swinging head mechanism comprises a bevel gear set which is rotatably arranged on the sliding piece (3), a lead screw (12) which is connected with the bevel gear set and is installed on the sliding piece (3) in a bearing mode, and an adjusting assembly which is used for connecting the lead screw (12) with the swinging piece (15);
the bevel gear set comprises a first bevel gear (10) rotatably arranged on the sliding part (3) and a second bevel gear (11) which is fixed at the end part of the lead screw (12) and is engaged with the first bevel gear (10), wherein the gear (7) is connected with the first bevel gear (10) through a transmission part (9);
the swinging piece (15) is rotatably connected to the top of the sliding piece (3), the adjusting assembly comprises a sleeve piece (13) which is in threaded connection with the lead screw (12) and a driving piece (14) which is used for connecting the swinging piece (15) and the sleeve piece (13), wherein one end of the driving piece (14) is hinged on the sleeve piece (13), and the other end of the driving piece (14) is hinged on the swinging piece (15);
the satellite assembly comprises a receiving part (16) fixedly arranged on the swinging part (15), a detachable part (17) detachably connected on the swinging part (15), a satellite feed source (18) arranged at the end of the detachable part (17), and a high-frequency head (19) connected with the feed source (18) and fixed on the detachable part (17), wherein the high-frequency head (19) is in signal connection with a receiver (20) arranged on the back surface of the receiving part (16);
the method comprises the following steps:
the method comprises the following steps:
firstly, determining the direction, namely hanging a magnetic sewing needle by a thin thread to judge the general position of the south, and accurately determining the direction of the satellite by means of a compass;
step two, mounting and fixing, namely enabling the opening direction of the satellite component to face the south and fixing the base (1) on the ground by utilizing bolts;
mounting a satellite assembly, mounting a detachable piece (17), a satellite feed source (18) and a tuner (19) on the swinging piece (15), and keeping the centers of the satellite feed source (18) and the receiving piece (16) on the same axis;
and step four, debugging, namely switching on the satellite assembly, starting the power part (4) to drive the satellite assembly to lift and adjust the inclination angle, observing the signal receiving condition while adjusting the inclination angle, and stopping lifting when the signal is well received.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202010880746.1A CN112187308B (en) | 2019-12-23 | 2019-12-23 | Method for installing satellite communication transceiver |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010880746.1A CN112187308B (en) | 2019-12-23 | 2019-12-23 | Method for installing satellite communication transceiver |
| CN201911337943.2A CN111082820B (en) | 2019-12-23 | 2019-12-23 | Satellite communication transceiver with simple installation and installation method thereof |
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| CN201911337943.2A Division CN111082820B (en) | 2019-12-23 | 2019-12-23 | Satellite communication transceiver with simple installation and installation method thereof |
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| CN112187308A CN112187308A (en) | 2021-01-05 |
| CN112187308B true CN112187308B (en) | 2022-02-18 |
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| CN202010880746.1A Active CN112187308B (en) | 2019-12-23 | 2019-12-23 | Method for installing satellite communication transceiver |
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| CN112332875B (en) * | 2020-11-13 | 2022-03-11 | 深圳铭薪房车科技有限公司 | Mobile signal receiving system for motor home |
| CN113960379B (en) * | 2021-12-21 | 2022-03-08 | 中国人民解放军军事科学院战争研究院 | 5G communication antenna test jig |
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|---|---|
| CN111082820B (en) | 2020-09-08 |
| CN112187308A (en) | 2021-01-05 |
| CN111082820A (en) | 2020-04-28 |
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Effective date of registration: 20240607 Address after: No. 586 Runhu Avenue, Hushu Street, Jiangning District, Nanjing City, Jiangsu Province, 210000 Patentee after: Jiangsu Liutou Technology Co.,Ltd. Country or region after: China Address before: 14 / F, building 4, 266 Chuangyan Road, Qilin hi tech Industrial Development Zone, Nanjing, Jiangsu 210000 Patentee before: JIANGSU JIUGAO ELECTRONIC TECHNOLOGY Co.,Ltd. Country or region before: China |