CN109088167A - A kind of satellite aerial rotary seat - Google Patents

A kind of satellite aerial rotary seat Download PDF

Info

Publication number
CN109088167A
CN109088167A CN201810864008.0A CN201810864008A CN109088167A CN 109088167 A CN109088167 A CN 109088167A CN 201810864008 A CN201810864008 A CN 201810864008A CN 109088167 A CN109088167 A CN 109088167A
Authority
CN
China
Prior art keywords
fixedly connected
satellite
under casing
electric machine
gearcase
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
Application number
CN201810864008.0A
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Chinese (zh)
Inventor
董如迅
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Suzhou Yu Frequency Pml Precision Mechanism Ltd
Original Assignee
Suzhou Yu Frequency Pml Precision Mechanism Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Suzhou Yu Frequency Pml Precision Mechanism Ltd filed Critical Suzhou Yu Frequency Pml Precision Mechanism Ltd
Priority to CN201810864008.0A priority Critical patent/CN109088167A/en
Publication of CN109088167A publication Critical patent/CN109088167A/en
Pending legal-status Critical Current

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Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/02Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
    • H01Q3/08Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying two co-ordinates of the orientation
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/12Supports; Mounting means
    • H01Q1/1235Collapsible supports; Means for erecting a rigid antenna

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

The invention discloses a kind of satellite aerial rotary seats, including under casing, the bottom of the under casing inner wall is fixedly connected with rotary electric machine case, the bottom of the rotary electric machine chamber interior wall is fixedly connected with rotation motor by motor cabinet, one end of the rotation motor output shaft runs through rotary electric machine case and extends to the top of rotary electric machine case, connecting shaft is fixedly connected on the output shaft of the rotation motor, the surface of the connecting shaft is arranged with transmission gear, the side of the transmission gear is engaged with connection gear, the two sides of the under casing inner wall pass through support plate and are fixedly connected with support return pulley, the present invention relates to satellite antenna technical fields.The satellite aerial rotary seat, solve the problems, such as that rotary antenna pedestal does not often have speed control device, the ability that satellite antenna captures satellite-signal when rotated is effectively raised, the failure rate for capturing satellite-signal greatly reduces, improves the ability that satellite antenna receives signal.

Description

A kind of satellite aerial rotary seat
Technical field
The present invention relates to satellite antenna technical field, specially a kind of satellite aerial rotary seat.
Background technique
Satellite antenna is exactly the cauldron often said, is a metal paraboloid, is responsible for for satellite-signal being reflected into positioned at focus In the feed and tuner at place.The effect of satellite antenna is to collect the small-signal transmitted by satellite, and be eliminated as much as noise. Most of antennas are usually parabolic, there are also multifocal antenna are composed of spherical surface and paraboloid.Satellite letter Number by focusing on its focal point after the reflection of parabola antenna.Satellite antenna can be divided into positive feedback and two kinds of offset-fed.Positive coke day Line finds satellite, usually only it is to be understood that elevation angle device, is placed in antenna centre and is adjusted and faced upward by the reception elevation angle of satellite locality Degree, then compass of arranging in pairs or groups with satellite-signal test equipment are easy for that the satellite that you want can be found.Satellite television receiving system By: parabola antenna, feed, tuner, satellite receiver form the Satellite Receiving Station of complete set.
Traditional satellite antenna pedestal is satellite day fixed, that Partial Height excitement satellite needs can rotate in time Line rotating seat drives satellite antenna rotary that can keep continuing to receive satellite-signal, and some advanced units use rotary antenna base Seat, but often without speed control device, so that pedestal rotation speed is too fast, it is unfavorable for signal capture, and work as satellite antenna pair It after satelloid, needs pedestal long-time stable motionless, lacks necessary fixed device.
Summary of the invention
In view of the deficiencies of the prior art, the present invention provides a kind of satellite aerial rotary seats, solve rotary antenna base Seat is often without speed control device, and satellite antenna is to the necessary the problem of fixing device of shortage after satelloid.
In order to achieve the above object, the present invention is achieved by the following technical programs: a kind of satellite aerial rotary seat, including Under casing, the bottom of the under casing inner wall are fixedly connected with rotary electric machine case, and the bottom of the rotary electric machine chamber interior wall passes through motor Seat is fixedly connected with rotation motor, and one end of the rotation motor output shaft through rotary electric machine case and extends to rotation The top of motor housing, it is described rotation motor output shaft on be fixedly connected with connecting shaft, the surface of the connecting shaft is arranged with Transmission gear, the side of the transmission gear are engaged with connection gear, and the two sides of the under casing inner wall are fixed by support plate It is connected with support return pulley, the top movable of the support return pulley is connected with gearcase, the side of the connection gear and gearcase The side of inner wall is engaged, and one end of the connecting shaft runs through gearcase and extends to the inside of gearcase, the gearcase Top is fixedly connected with transmission shaft, and the top of the transmission shaft runs through under casing and extends to the top of under casing, the gearcase Bottom offer card slot, one end that the transmission shaft is located at the top of under casing is fixedly connected with support baseboard, the support baseboard Link block is fixedly connected on the left of top, the surface pivots of the link block are connected with satellite antenna.
Preferably, the right side at the top of the support baseboard is fixedly connected with electric expansion column, the top of the electric expansion column End is fixedly connected with the bottom of satellite antenna.
Preferably, the two sides of the support baseboard bottom are fixedly connected to fixed pulley, the bottom end of the fixed pulley It is connect with the top slide of under casing.
Preferably, the two sides of under casing inner wall bottom are fixedly connected to fixed bin, the bottom of the fixed bin inner wall It is fixedly connected with garter spring.
Preferably, the top of the garter spring is fixedly connected with sliding panel, is fixedly connected at the top of the sliding panel Extension bar.
Preferably, the side of the movable plate is fixedly connected with handlebar stem, one end of the handlebar stem through fixed bin and Extend to the outside of fixed bin.
Beneficial effect
The present invention provides a kind of satellite aerial rotary seats.Have it is following the utility model has the advantages that
(1), it is electronic by motor cabinet to be fixedly connected with rotation by the bottom of rotary electric machine chamber interior wall for the satellite aerial rotary seat Machine rotates one end of motor output shaft through rotary electric machine case and extends to the top of rotary electric machine case, rotates motor Output shaft on be fixedly connected with connecting shaft, the surface of connecting shaft is arranged with transmission gear, and the side of transmission gear is engaged with company Gear is connect, the two sides of under casing inner wall pass through support plate and are fixedly connected with support return pulley, and the top movable of return pulley is supported to be connected with The side of gearcase, connection gear is engaged with the side of gearcase inner wall, and one end of connecting shaft through gearcase and extends to The inside of gearcase is fixedly connected with transmission shaft, rotation motor, connecting shaft, transmission gear and tooth connection at the top of gearcase The joint of wheel is arranged, and solves the problems, such as that rotary antenna pedestal does not often have speed control device, effectively raises satellite antenna The ability for capturing satellite-signal when rotated, greatly reduces the failure rate for capturing satellite-signal, improves satellite antenna and connect The ability of the collection of letters number.
(2), the satellite aerial rotary seat is fixedly connected with electric expansion column by the right side at the top of bottom plate, described electronic The top of telescopic mast is fixedly connected with the bottom of satellite antenna, and the joint setting of electric expansion column and bottom plate solves satellite day The problem of line is to necessary fixed device is lacked after satelloid, avoiding in default of the fixed device of satellite antenna leads to satellite day The shaking of line effectively raises the fixed method of antenna, ensure that the degree of reliability of satellite antenna.
Detailed description of the invention
Fig. 1 is the structural schematic diagram inside the present invention;
Fig. 2 is the top view of transmission gear structure of the present invention.
In figure: 1- under casing, 2- rotary electric machine case, 3- rotation motor, 4- connecting shaft, 5- transmission gear, 6- connection gear, 7- supports return pulley, 8- gearcase, 9- transmission shaft, 10- card slot, 11- support baseboard, 12- link block, 13- satellite antenna, 14- electricity Dynamic telescopic mast, 15- fixed pulley, 16- fixed bin, 17- garter spring, 18- sliding panel, 19- extension bar, 20- handlebar stem.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other Embodiment shall fall within the protection scope of the present invention.
The present invention provides a kind of technical solution referring to FIG. 1-2: a kind of satellite aerial rotary seat, including under casing 1, under casing 1 The bottom of inner wall is fixedly connected with rotary electric machine case 2, and the bottom of 2 inner wall of rotary electric machine case is fixedly connected with rotation by motor cabinet Motor 3, rotation motor 3 drive satellite antenna unitary rotation, and rotary electric machine case is run through in one end of rotation 3 output shaft of motor 2 and the top of rotary electric machine case 2 is extended to, rotates and be fixedly connected with connecting shaft 4 on the output shaft of motor 3, connecting shaft 4 Surface is arranged with transmission gear 5, and the side of transmission gear 5 is engaged with connection gear 6, and the two sides of 1 inner wall of under casing pass through support Plate is fixedly connected with support return pulley 7, and support return pulley 7 has supporting role, the top movable connection of support return pulley 7 to gearcase 8 Have gearcase 8, the side of connection gear 6 is engaged with the side of 8 inner wall of gearcase, one end of connecting shaft 4 through gearcase 8 and Extend to the inside of gearcase 8, the top of gearcase 8 is fixedly connected with transmission shaft 9, the top of transmission shaft 9 through under casing 1 and The top of under casing 1 is extended to, the bottom of gearcase 8 offers card slot 10, and card slot 10 is distributed in 8 bottom of gearcase, quantity setting Several, one end that transmission shaft 9 is located at 1 top of under casing is fixedly connected with support baseboard 11, and the left side at 11 top of support baseboard is fixed It is connected with link block 12, the surface pivots of link block 12 are connected with satellite antenna 13, and the right side at 11 top of support baseboard is fixed to be connected It is connected to electric expansion column 14, the top of electric expansion column 14 is fixedly connected with the bottom of satellite antenna 13,11 bottom of support baseboard Two sides be fixedly connected to fixed pulley 15, the fixed sliding of pulley 15 reduces friction, the bottom end of fixed pulley 15 and under casing 1 Top slide connection, the two sides of 1 inner wall bottom of under casing are fixedly connected to fixed bin 16, and the bottom of 16 inner wall of fixed bin is fixed to be connected It is connected to garter spring 17, the top of garter spring 17 is fixedly connected with sliding panel 18, and the top of sliding panel 18, which is fixedly connected with, stretches Rod 19, the side of sliding panel 18 are fixedly connected with handlebar stem 20, and one end of handlebar stem 20 through fixed bin 16 and extends to The outside of fixed bin 16.
When work, handlebar stem 20 is pulled down, drives extension bar 19 to move down by the sliding panel 18 in fixed bin 16 and squeezes Garter spring 17 when satellite antenna needs free movement, opens 3 turns of rotation motor rotated inside motor housing 2 under casing 1 It is dynamic, it is rotated by connecting shaft 4 with nutating gear 5, so that connection gear 6 drives gearcase 8 to turn along the surface of support return pulley 7 Dynamic, so that transmission shaft 9 be driven to rotate, then support baseboard 11 drives link block 12 and satellite antenna 13 to rotate, and defends when needing to adjust When star aerial angle, electric expansion column 14, which is raised and lowered, makes satellite antenna 13 reach predeterminated level, when satellite antenna needs admittedly When determining facing one direction, opens rotation motor 3 and rotate, after satellite antenna 13 reaches predetermined position, unclamp handlebar stem 20, stretch Rod 19 and 10 clamping of card slot, are fixed.
It should be noted that, in this document, relational terms such as first and second and the like are used merely to a reality Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those Element, but also including other elements that are not explicitly listed, or further include for this process, method, article or equipment Intrinsic element.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding And modification, the scope of the present invention is defined by the appended.

Claims (6)

1. a kind of satellite aerial rotary seat, including under casing (1), it is characterised in that: the bottom of under casing (1) inner wall is fixedly connected Having rotary electric machine case (2), the bottom of rotary electric machine case (2) inner wall is fixedly connected with rotation motor (3) by motor cabinet, One end of described rotation motor (3) output shaft runs through rotary electric machine case (2) and extends to the top of rotary electric machine case (2), It is fixedly connected with connecting shaft (4) on the output shaft of rotation motor (3), the surface of the connecting shaft (4) is arranged with transmission The side of gear (5), the transmission gear (5) is engaged with connection gear (6), and the two sides of under casing (1) inner wall pass through branch Fagging is fixedly connected with support return pulley (7), and the top movable of support return pulley (7) is connected with gearcase (8), the tooth connection The side of wheel (6) is engaged with the side of gearcase (8) inner wall, and one end of the connecting shaft (4) through gearcase (8) and extends It to the inside of gearcase (8), is fixedly connected with transmission shaft (9) at the top of the gearcase (8), the top of the transmission shaft (9) Through under casing (1) and the top of under casing (1) is extended to, the bottom of the gearcase (8) offers card slot (10), the transmission One end that axis (9) is located at the top of under casing (1) is fixedly connected with support baseboard (11), and the left side at the top of the support baseboard (11) is solid Surely it is connected with link block (12), the surface pivots of the link block (12) are connected with satellite antenna (13).
2. a kind of satellite aerial rotary seat according to claim 1, it is characterised in that: at the top of the support baseboard (11) Right side is fixedly connected with electric expansion column (14), and the top of the electric expansion column (14) and the bottom of satellite antenna (13) are fixed Connection.
3. a kind of satellite aerial rotary seat according to claim 1, it is characterised in that: support baseboard (11) bottom Two sides are fixedly connected to fixed pulley (15), and the bottom end of the fixed pulley (15) is connect with the top slide of under casing (1).
4. a kind of satellite aerial rotary seat according to claim 1, it is characterised in that: under casing (1) the inner wall bottom Two sides are fixedly connected to fixed bin (16), and the bottom of fixed bin (16) inner wall is fixedly connected with garter spring (17).
5. a kind of satellite aerial rotary seat according to claim 4, it is characterised in that: the top of the garter spring (17) It is fixedly connected with sliding panel (18), is fixedly connected with extension bar (19) at the top of the sliding panel (18).
6. a kind of satellite aerial rotary seat according to claim 5, it is characterised in that: the side of the sliding panel (18) is solid Surely it is connected with handlebar stem (20), one end of the handlebar stem (20) through fixed bin (16) and extends to the outer of fixed bin (16) Portion.
CN201810864008.0A 2018-08-01 2018-08-01 A kind of satellite aerial rotary seat Pending CN109088167A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810864008.0A CN109088167A (en) 2018-08-01 2018-08-01 A kind of satellite aerial rotary seat

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810864008.0A CN109088167A (en) 2018-08-01 2018-08-01 A kind of satellite aerial rotary seat

Publications (1)

Publication Number Publication Date
CN109088167A true CN109088167A (en) 2018-12-25

Family

ID=64831181

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810864008.0A Pending CN109088167A (en) 2018-08-01 2018-08-01 A kind of satellite aerial rotary seat

Country Status (1)

Country Link
CN (1) CN109088167A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110120578A (en) * 2019-05-24 2019-08-13 彭伶铭 A kind of 5G signal receiving antenna
CN111063979A (en) * 2019-12-22 2020-04-24 嘉兴勤慎智能技术有限公司 Angle-adjustable antenna based on 5G signal transmission
CN112310594A (en) * 2020-11-11 2021-02-02 郑能成 Vehicular radar antenna flip structure
CN112532302A (en) * 2020-11-25 2021-03-19 湖南涉外经济学院 Signal receiving device for signal processing
CN113421389A (en) * 2021-06-23 2021-09-21 深圳市中天迅通信技术股份有限公司 Antenna device for POS machine
CN114278513A (en) * 2021-12-27 2022-04-05 安徽驭风能源科技有限公司 Satellite signal transmitter and satellite signal transmission system for wind power blade operation data

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4467726A (en) * 1980-10-28 1984-08-28 British Telecommunications Stabilizing apparatus
CN101814654A (en) * 2010-05-11 2010-08-25 四川省视频电子有限责任公司 Satellite television ground receiving indoor antenna for automatically searching satellites
CN205911418U (en) * 2016-07-19 2017-01-25 深圳奥视通电子有限公司 Mobile satellite television receiving antenna device
CN206322838U (en) * 2017-01-11 2017-07-11 广州壹盟电子有限公司 One kind can extract antenna antenna fixing seat
CN207474647U (en) * 2017-09-25 2018-06-08 深圳市东信通电子科技有限公司 A kind of efficient television antenna

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4467726A (en) * 1980-10-28 1984-08-28 British Telecommunications Stabilizing apparatus
CN101814654A (en) * 2010-05-11 2010-08-25 四川省视频电子有限责任公司 Satellite television ground receiving indoor antenna for automatically searching satellites
CN205911418U (en) * 2016-07-19 2017-01-25 深圳奥视通电子有限公司 Mobile satellite television receiving antenna device
CN206322838U (en) * 2017-01-11 2017-07-11 广州壹盟电子有限公司 One kind can extract antenna antenna fixing seat
CN207474647U (en) * 2017-09-25 2018-06-08 深圳市东信通电子科技有限公司 A kind of efficient television antenna

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110120578A (en) * 2019-05-24 2019-08-13 彭伶铭 A kind of 5G signal receiving antenna
CN110120578B (en) * 2019-05-24 2020-11-24 江苏三晟信息科技有限公司 5G signal receiving antenna
CN111063979A (en) * 2019-12-22 2020-04-24 嘉兴勤慎智能技术有限公司 Angle-adjustable antenna based on 5G signal transmission
CN112310594A (en) * 2020-11-11 2021-02-02 郑能成 Vehicular radar antenna flip structure
CN112310594B (en) * 2020-11-11 2022-06-14 郑能成 Vehicular radar antenna flip structure
CN112532302A (en) * 2020-11-25 2021-03-19 湖南涉外经济学院 Signal receiving device for signal processing
CN112532302B (en) * 2020-11-25 2022-04-08 湖南涉外经济学院 Signal receiving device for signal processing
CN113421389A (en) * 2021-06-23 2021-09-21 深圳市中天迅通信技术股份有限公司 Antenna device for POS machine
CN114278513A (en) * 2021-12-27 2022-04-05 安徽驭风能源科技有限公司 Satellite signal transmitter and satellite signal transmission system for wind power blade operation data

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PB01 Publication
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SE01 Entry into force of request for substantive examination
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WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20181225

WD01 Invention patent application deemed withdrawn after publication