CN101673862B - Satellite antenna equipment, transceiver module and filtering unit thereof - Google Patents
Satellite antenna equipment, transceiver module and filtering unit thereof Download PDFInfo
- Publication number
- CN101673862B CN101673862B CN 200810215570 CN200810215570A CN101673862B CN 101673862 B CN101673862 B CN 101673862B CN 200810215570 CN200810215570 CN 200810215570 CN 200810215570 A CN200810215570 A CN 200810215570A CN 101673862 B CN101673862 B CN 101673862B
- Authority
- CN
- China
- Prior art keywords
- filter
- zinc
- filtering
- satellite antenna
- transceiver module
- 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.)
- Expired - Fee Related
Links
- 238000001914 filtration Methods 0.000 title claims description 36
- 229910000611 Zinc aluminium Inorganic materials 0.000 claims abstract description 19
- HXFVOUUOTHJFPX-UHFFFAOYSA-N alumane;zinc Chemical compound [AlH3].[Zn] HXFVOUUOTHJFPX-UHFFFAOYSA-N 0.000 claims abstract description 19
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 17
- 229910052725 zinc Inorganic materials 0.000 claims description 17
- 239000011701 zinc Substances 0.000 claims description 17
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 15
- 229910052782 aluminium Inorganic materials 0.000 claims description 15
- 239000000463 material Substances 0.000 claims description 6
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims 14
- 239000004411 aluminium Substances 0.000 claims 6
- 229910045601 alloy Inorganic materials 0.000 abstract description 9
- 239000000956 alloy Substances 0.000 abstract description 9
- 238000006243 chemical reaction Methods 0.000 description 7
- 230000005540 biological transmission Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 229910001297 Zn alloy Inorganic materials 0.000 description 1
- FJMNNXLGOUYVHO-UHFFFAOYSA-N aluminum zinc Chemical compound [Al].[Zn] FJMNNXLGOUYVHO-UHFFFAOYSA-N 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
Images
Landscapes
- Control Of Motors That Do Not Use Commutators (AREA)
- Aerials With Secondary Devices (AREA)
- Radio Relay Systems (AREA)
Abstract
一种滤波单元,包括滤波基座以及盖体。滤波基座具有多个间隔排列的第一滤波槽;盖体与滤波基座接合而形成滤波空间,并具有与该第一滤波槽对应设置的多个间隔排列的第二滤波槽。其中,滤波基座与盖体的材料包括锌铝合金。本发明还公开了一种应用滤波单元的卫星天线设备及其收发模块。
A filter unit includes a filter base and a cover. The filter base has a plurality of first filter slots arranged at intervals; the cover is joined to the filter base to form a filter space, and has a plurality of second filter slots arranged at intervals corresponding to the first filter slots. The filter base and the cover are made of zinc-aluminum alloy. The present invention also discloses a satellite antenna device and a transceiver module thereof using the filter unit.
Description
技术领域 technical field
本发明涉及一种卫星天线设备、收发模块及其滤波单元。The invention relates to a satellite antenna device, a transceiver module and a filtering unit thereof.
背景技术 Background technique
随着太空科技的发展,卫星传输技术也逐渐地进入一般人的日常生活中。例如,导航用的全球定位系统(Global Positioning System,GPS),或是电视台用以现场直播的卫星新闻采集(Satellite NewsGathering,SNG)系统等。其中,例如在SNG系统中,会利用卫星天线设备来进行信号的传输与接收,而为使卫星天线设备传输与接收的信号清晰,多会利用滤波器来过滤干扰信号。With the development of space technology, satellite transmission technology has gradually entered the daily life of ordinary people. For example, the Global Positioning System (Global Positioning System, GPS) used for navigation, or the Satellite News Gathering (SNG) system used by TV stations for live broadcasting. Among them, for example, in the SNG system, satellite antenna equipment is used to transmit and receive signals, and in order to make the signals transmitted and received by satellite antenna equipment clear, filters are often used to filter out interference signals.
请参照图1所示,其为一种现有卫星天线设备的滤波器1的剖面图。滤波器1包括滤波基座11以及多个调整组件12,该调整组件12连接于滤波基座11上下两侧。滤波基座11具有滤波空间111以及多个间隔排列的滤波槽112,通过移动调整组件12的位置,可调整滤波槽112的深度,以对应不同的滤波范围。Please refer to FIG. 1 , which is a cross-sectional view of a filter 1 of a conventional satellite antenna device. The filter 1 includes a
因此,当例如Ka或Ku波段的传输信号进入滤波器1后,对应于该滤波槽112的间隔距离的波长,即可直接穿过滤波空间111。但是,其它波长则会落入滤波槽112中,进而产生共振并抵销。Therefore, when the Ka or Ku band transmission signal enters the filter 1 , the wavelength corresponding to the distance between the
然而,由于滤波槽112的深度为可调的,因此对应不同滤波范围作调整时,可能因人为调整误差或因材料或制程造成的机械误差等,使得滤波器1的滤波效果不佳。此外,可能因不断地移动调整组件12的位置,而造成调整组件12的损耗,也造成滤波器1的损坏。另外,现有滤波器1多利用铝成分比例较高的铝锌合金制成,在制造过程中,于滤波器1脱模后,经常造成滤波槽112表面平整度不够,从而影响滤波效果。However, since the depth of the
因此,如何设计一种具有良好滤波效果的滤波器,而可应用于卫星天线设备及收发模块,已成为重要课题之一。Therefore, how to design a filter with good filtering effect, which can be applied to satellite antenna equipment and transceiver modules, has become one of the important issues.
发明内容 Contents of the invention
有鉴于上述课题,本发明的目的为提供一种具有良好滤波效果的与滤波单元、及其应用的卫星天线设备与收发模块。In view of the above problems, the object of the present invention is to provide a filter unit with good filtering effect, and a satellite antenna device and a transceiver module for its application.
为达到上述目的,依据本发明的一种滤波单元包括滤波基座以及盖体。滤波基座具有多个间隔排列的第一滤波槽;盖体与滤波基座接合而形成滤波空间,并具有与该第一滤波槽对应设置的多个间隔排列的第二滤波槽。其中,滤波基座与盖体的材料包括锌铝合金,其锌铝含量比例为锌含量大于铝含量。To achieve the above object, a filter unit according to the present invention includes a filter base and a cover. The filter base has a plurality of first filter slots arranged at intervals; the cover is joined with the filter base to form a filter space, and has a plurality of second filter slots arranged at intervals corresponding to the first filter slots. Wherein, the material of the filter base and the cover body includes zinc-aluminum alloy, and its zinc-aluminum content ratio is such that the zinc content is greater than the aluminum content.
为达到上述目的,依据本发明的一种收发模块包括转换单元、导波单元以及滤波单元。导波单元及滤波单元皆与转换单元连接,滤波单元具有滤波基座及盖体。滤波基座具有多个间隔排列的第一滤波槽,盖体与滤波基座接合而形成滤波空间,并具有与该第一滤波槽对应设置的多个间隔排列的第二滤波槽。其中,滤波基座与盖体的材料包括锌铝合金,其锌铝含量的比例为锌含量大于铝含量。To achieve the above object, a transceiver module according to the present invention includes a conversion unit, a wave guiding unit and a filtering unit. Both the waveguide unit and the filter unit are connected with the conversion unit, and the filter unit has a filter base and a cover. The filter base has a plurality of first filter slots arranged at intervals, the cover body is joined with the filter base to form a filter space, and has a plurality of second filter slots arranged at intervals corresponding to the first filter slots. Wherein, the material of the filter base and the cover body includes zinc-aluminum alloy, and the ratio of the zinc-aluminum content is such that the zinc content is greater than the aluminum content.
为达到上述目的,依据本发明的一种卫星天线设备包括碟形反射模块、馈源模块以及收发模块。馈源模块邻设于碟形反射模块,收发模块与馈源模块连接,收发模块包括转换单元、导波单元及滤波单元。导波单元及滤波单元皆与转换单元连接,滤波单元具有滤波基座及盖体。滤波基座具有多间隔排列的第一滤波槽,盖体与滤波基座接合而形成滤波空间,并具有与该第一滤波槽对应设置的多间隔排列的第二滤波槽。其中,滤波基座与盖体的材料包括锌铝合金,其锌铝含量比例为锌含量大于铝含量。To achieve the above object, a satellite antenna device according to the present invention includes a dish reflection module, a feed source module and a transceiver module. The feed source module is adjacent to the dish reflection module, and the transceiver module is connected to the feed source module. The transceiver module includes a conversion unit, a wave guiding unit and a filter unit. Both the waveguide unit and the filter unit are connected with the conversion unit, and the filter unit has a filter base and a cover. The filter base has first filter slots arranged at multiple intervals, the cover body is joined with the filter base to form a filter space, and has second filter slots arranged at multiple intervals corresponding to the first filter slots. Wherein, the material of the filter base and the cover body includes zinc-aluminum alloy, and its zinc-aluminum content ratio is such that the zinc content is greater than the aluminum content.
承上所述,依据本发明的滤波单元通过滤波基座与盖体共同形成滤波空间,其中滤波基座具有多个第一滤波槽,而盖体则具有多个与该第一滤波槽对应的第二滤波槽。因此,当滤波基座与盖体接合,该第一滤波槽与该第二滤波槽即彼此对称,并间隔排列于滤波空间中,且该滤波槽的深度都为固定的。这样,即可避免滤波槽对应不同滤波范围作调整时,可能产生的调整误差或机械误差,以提升滤波单元对于预设滤波范围的滤波效果,而能够应用于卫星天线设备及收发模块。Based on the above, the filter unit according to the present invention forms a filter space through the filter base and the cover, wherein the filter base has a plurality of first filter slots, and the cover has a plurality of filter slots corresponding to the first filter slots. Second filter slot. Therefore, when the filter base is engaged with the cover body, the first filter groove and the second filter groove are symmetrical to each other and arranged at intervals in the filter space, and the depths of the filter grooves are fixed. In this way, adjustment errors or mechanical errors that may occur when the filter tank is adjusted corresponding to different filter ranges can be avoided, so as to improve the filter effect of the filter unit for the preset filter range, and can be applied to satellite antenna equipment and transceiver modules.
另外,本发明的滤波单元还利用锌成分比例较高的锌铝合金,用来提升滤波单元脱模后的表面平整度,以进一步地提升滤波单元的滤波效果。In addition, the filter unit of the present invention also uses zinc-aluminum alloy with a high proportion of zinc to improve the surface smoothness of the filter unit after demoulding, so as to further improve the filtering effect of the filter unit.
附图说明 Description of drawings
图1是一种现有卫星天线设备的滤波器的剖面图;Fig. 1 is the sectional view of the filter of a kind of existing satellite antenna equipment;
图2是本发明优选实施例的一种卫星天线设备的示意图;Fig. 2 is the schematic diagram of a kind of satellite antenna equipment of preferred embodiment of the present invention;
图3是本发明优选实施例的一种滤波单元的分解图;Fig. 3 is an exploded view of a filter unit of a preferred embodiment of the present invention;
图4A是图3的滤波单元的结合图;以及FIG. 4A is a combination diagram of the filtering unit of FIG. 3; and
图4B是滤波单元沿图4A中A-A直线的剖面图。FIG. 4B is a cross-sectional view of the filter unit along the line A-A in FIG. 4A.
主要组件符号说明Explanation of main component symbols
1:滤波器1: filter
11:滤波基座11: Filter base
111:滤波空间111: Filter space
112:滤波槽112: filter slot
12:调整组件12: Adjust components
2:滤波单元2: Filter unit
21:滤波基座21: Filter base
211:第一滤波槽211: The first filter slot
212:馈入部212: Feed-in Department
213:馈出部213: Outgoing Department
22:盖体22: Cover body
221:第二滤波槽221: Second filter slot
3:转换单元3: Conversion unit
4:导波单元4: waveguide unit
5:收发模块5: transceiver module
6:馈源模块6: Feed source module
7:碟形反射模块7: Dish reflector module
8:卫星天线设备8: Satellite dish equipment
D1、D2:延伸方向D1, D2: Extension direction
L1:第一长边L1: first long side
L2:第二长边L2: second long side
S:滤波空间S: filter space
具体实施方式 Detailed ways
以下将参照相关附图,说明依据本发明优选实施例的卫星天线设备、收发模块及其滤波单元。The satellite antenna device, transceiver module and filtering unit thereof according to preferred embodiments of the present invention will be described below with reference to related drawings.
请参照图2所示,本发明优选实施例的一种卫星天线设备8包括碟形反射模块7、馈源模块6以及收发模块5。碟形反射模块7例如为碟形天线;馈源模块6例如为馈电器(feed horn),其邻设于碟形反射模块7,收发模块5与馈源模块6连接。Referring to FIG. 2 , a
收发模块5包括转换单元3、导波单元4及滤波单元2。转换单元3例如为正交模式转换器(Orthogonal Mode Transducer,OMT),导波单元4例如为导波管(waveguide)。导波单元4及滤波单元2皆与转换单元3连接。The transceiver module 5 includes a converting unit 3 , a wave guiding unit 4 and a
接着,请参照图3所示,以说明本发明优选实施例的滤波单元2。Next, please refer to FIG. 3 to illustrate the
滤波单元2具有滤波基座21及盖体22。其中,滤波基座21与盖体22的材料为锌铝合金,其锌铝含量的比例为锌含量大于铝含量。锌铝合金的锌铝重量百分比优选为锌占90%~99%,铝占1%~10%。更优地,锌铝重量百分比为锌占95%~96%,铝占3.9%~4.3%。The
滤波基座21具有多个间隔排列的第一滤波槽211,盖体22具有与该第一滤波槽211对应设置的多个间隔排列的第二滤波槽221。另外,在本实施例中,以该第一滤波槽211和该第二滤波槽221以等间隔排列,而该第一滤波槽211至少其中两个的长、宽、高实质上彼此相等,该第二滤波槽221至少其中两个的长、宽、高实质上彼此相等为例作说明,然而这不是用来限制本发明,换言之,该第一滤波槽211可完全相同,该第二滤波槽221也可完全相同。The
另外,滤波基座21还具有馈入部212及馈出部213,馈入部212与馈出部213分别位于滤波基座21两侧。另外,在本实施例中,第一滤波槽211具有第一底面(图中未示),第一底面的至少其中之一具有第一长边L1,馈入部212或馈出部213具有第二长边L2,第一长边L1的延伸方向D1与第二长边L2的延伸方向D2相同,然而这不是限制性的。In addition, the
请参照图4A及图4B所示,其中图4A为本实施例的滤波单元2的结合图,图4B为滤波单元2沿图4A中A-A直线的剖面图。滤波基座21与盖体22接合后会形成滤波空间S,其位于馈入部212与馈出部213之间。其中,滤波基座21与盖体22例如可通过锁合、卡合或嵌合等方式接合;在本实施例中,滤波基座21与盖体22通过锁合方式接合,但这不是限制性。Please refer to FIG. 4A and FIG. 4B , wherein FIG. 4A is a combined view of the
因此,当滤波基座21与盖体22接合后,该第一滤波槽211与该第二滤波槽221即彼此对称并间隔排列于滤波空间S中,且该滤波槽211、221的深度皆为固定。当例如Ka或Ku波段的传输信号进入滤波单元2后,对应于该滤波槽211、221的间隔距离的波长,即可直接穿过滤波空间S,其它波长则会落入滤波槽211、221中,进而产生共振并抵销。Therefore, when the
由此,即可避免滤波槽211、221对应不同滤波范围作调整时,可能产生的调整误差或机械误差,以提升滤波单元2对于预设滤波范围的滤波效果。另外,本实施例的滤波单元2还利用锌成分比例较高的锌铝合金,由此提升滤波单元2脱模后的表面平整度,以进一步地提升滤波单元2的滤波效果。Thus, adjustment errors or mechanical errors that may occur when the
综上所述,依据本发明的滤波单元通过滤波基座与盖体共同形成滤波空间,其中滤波基座具有多个第一滤波槽,而盖体则具有多个与第一滤波槽对应的第二滤波槽。因此,当滤波基座与盖体接合,第一滤波槽与第二滤波槽即彼此对称,并间隔排列于滤波空间中,且滤波槽的深度皆为固定的。由此,即可避免滤波槽对应不同滤波范围作调整时,可能产生的调整误差或机械误差,以提升滤波单元对于预设滤波范围的滤波效果,而能够应用于卫星天线设备及收发模块。In summary, according to the filter unit of the present invention, the filter base and the cover jointly form a filter space, wherein the filter base has a plurality of first filter slots, and the cover has a plurality of first filter slots corresponding to the first filter slots. Two filter slots. Therefore, when the filter base is engaged with the cover body, the first filter groove and the second filter groove are symmetrical to each other and arranged at intervals in the filter space, and the depths of the filter grooves are fixed. In this way, adjustment errors or mechanical errors that may occur when the filter slots are adjusted corresponding to different filter ranges can be avoided, so as to improve the filter effect of the filter unit for the preset filter range, and can be applied to satellite antenna equipment and transceiver modules.
另外,本发明的滤波单元还利用锌成分比例较高的锌铝合金,由此提升滤波单元脱模后的表面平整度,以进一步地提升滤波单元的滤波效果。In addition, the filter unit of the present invention also uses zinc-aluminum alloy with a high proportion of zinc, thereby improving the surface smoothness of the filter unit after demoulding, so as to further enhance the filtering effect of the filter unit.
以上所述仅为举例性,而不是限制性。任何未脱离本发明的精神与范畴,而对其进行的等效修改或变更,均应包括于后附的权利要求中。The above description is only illustrative, not restrictive. Any equivalent modifications or changes made without departing from the spirit and scope of the present invention shall be included in the appended claims.
Claims (16)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 200810215570 CN101673862B (en) | 2008-09-09 | 2008-09-09 | Satellite antenna equipment, transceiver module and filtering unit thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 200810215570 CN101673862B (en) | 2008-09-09 | 2008-09-09 | Satellite antenna equipment, transceiver module and filtering unit thereof |
Publications (2)
Publication Number | Publication Date |
---|---|
CN101673862A CN101673862A (en) | 2010-03-17 |
CN101673862B true CN101673862B (en) | 2013-01-02 |
Family
ID=42020939
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 200810215570 Expired - Fee Related CN101673862B (en) | 2008-09-09 | 2008-09-09 | Satellite antenna equipment, transceiver module and filtering unit thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN101673862B (en) |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3777286A (en) * | 1972-08-07 | 1973-12-04 | Hughes Aircraft Co | Die cast waveguide low pass filter |
CN1339850A (en) * | 2000-08-18 | 2002-03-13 | 启碁科技股份有限公司 | Rotation device for dish antenna |
US6809696B1 (en) * | 1999-10-18 | 2004-10-26 | Polymer Kompositer I Goteborg Ab | Microwave components |
CN2899141Y (en) * | 2006-03-28 | 2007-05-09 | 柯玉荣 | planar antenna |
-
2008
- 2008-09-09 CN CN 200810215570 patent/CN101673862B/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3777286A (en) * | 1972-08-07 | 1973-12-04 | Hughes Aircraft Co | Die cast waveguide low pass filter |
US6809696B1 (en) * | 1999-10-18 | 2004-10-26 | Polymer Kompositer I Goteborg Ab | Microwave components |
CN1339850A (en) * | 2000-08-18 | 2002-03-13 | 启碁科技股份有限公司 | Rotation device for dish antenna |
CN2899141Y (en) * | 2006-03-28 | 2007-05-09 | 柯玉荣 | planar antenna |
Also Published As
Publication number | Publication date |
---|---|
CN101673862A (en) | 2010-03-17 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US10158165B2 (en) | Baffle board for base station antenna and base station antenna array structure | |
CN1151590C (en) | Improved reflector antenna with a self-supported feed | |
US7642982B2 (en) | Multi-band circular polarity elliptical horn antenna | |
US7907097B2 (en) | Self-supporting unitary feed assembly | |
US20140203995A1 (en) | Creating low cost multi-band and multi-feed passive array feed antennas and low-noise block feeds | |
WO2018228415A1 (en) | Base station antenna | |
US20090184886A1 (en) | Sub-reflector of a dual-reflector antenna | |
CN102195141B (en) | Bipolarized reflector antenna assembly | |
US20050259026A1 (en) | Circular polarity elliptical horn antenna | |
WO2018209600A1 (en) | Radiation element, as well as antenna unit and antenna array thereof | |
US20050062663A1 (en) | Tuned perturbation cone feed for reflector antenna | |
US9478864B2 (en) | Waveguide horn arrays, methods for forming the same and antenna systems | |
CN104025383A (en) | Reflector antenna including dual band splashplate support | |
CN109633824A (en) | A kind of optical fiber connector and preparation method thereof | |
CN101673862B (en) | Satellite antenna equipment, transceiver module and filtering unit thereof | |
KR20140031360A (en) | High efficient antenna with air-strip radiator and feed structure | |
CN203406422U (en) | Dual-polarization microstrip antenna | |
CN102326384A (en) | Reception apparatus | |
EP2750244A1 (en) | Diplexer and waveguide | |
US20120112977A1 (en) | Antenna simply manufactured according to frequency characteristic | |
US11955703B2 (en) | Antenna and unmanned aerial vehicle | |
US8350640B2 (en) | Transceiver module for satellite antenna | |
CN104201479A (en) | Ku waveband low-profile planar antenna | |
KR101216010B1 (en) | Satellite vsat antenna for transmitting/receiving co and cross polarization | |
KR101477911B1 (en) | Circularly Polarized Antenna |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130102 Termination date: 20170909 |