CN102456949A - Beam wave adjusting device for horn antenna - Google Patents
Beam wave adjusting device for horn antenna Download PDFInfo
- Publication number
- CN102456949A CN102456949A CN2010105095387A CN201010509538A CN102456949A CN 102456949 A CN102456949 A CN 102456949A CN 2010105095387 A CN2010105095387 A CN 2010105095387A CN 201010509538 A CN201010509538 A CN 201010509538A CN 102456949 A CN102456949 A CN 102456949A
- Authority
- CN
- China
- Prior art keywords
- horn antenna
- adjusting device
- antenna
- guiding element
- satellite
- 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.)
- Granted
Links
- 239000002184 metal Substances 0.000 claims abstract description 26
- 229910052751 metal Inorganic materials 0.000 claims abstract description 26
- 230000005855 radiation Effects 0.000 claims description 2
- 235000012489 doughnuts Nutrition 0.000 claims 1
- 238000013461 design Methods 0.000 abstract description 25
- 238000010586 diagram Methods 0.000 description 9
- 238000004891 communication Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 230000005684 electric field Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000010287 polarization Effects 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 239000012141 concentrate Substances 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000009713 electroplating Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000001746 injection moulding Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- -1 nickel-nickel metals Chemical class 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
Images
Landscapes
- Waveguide Aerials (AREA)
- Aerials With Secondary Devices (AREA)
Abstract
Description
技术领域 technical field
本发明涉及一种束波整调装置,尤指一种用来调整一喇叭天线所形成的束波宽度的束波调整装置。The invention relates to a beam adjustment device, especially a beam adjustment device for adjusting the width of a beam formed by a horn antenna.
背景技术 Background technique
卫星通信具有覆盖范围广大及不受地面环境干扰等优点,广泛用于军事、探测及商用通信服务,如卫星导航、卫星语音广播或卫星电视广播等。公知的卫星通信接收装置由一碟型反射面(Dish Reflector)及一集波器(Low Noise Block Down-converter with Feedhom,LNBF)组成,集波器设于碟型反射面的焦点位置,用来接收碟型反射面所反射的无线电波信号,将无线电波信号降频至中频,再传送至后端的一卫星信号处理器进行信号处理,使大众能够收看卫星电视节目。Satellite communication has the advantages of wide coverage and no interference from the ground environment. It is widely used in military, detection and commercial communication services, such as satellite navigation, satellite voice broadcast or satellite TV broadcast. The known satellite communication receiving device is composed of a dish reflector (Dish Reflector) and a wave collector (Low Noise Block Down-converter with Feedhom, LNBF). Receive the radio wave signal reflected by the dish-shaped reflector, down-convert the radio wave signal to an intermediate frequency, and then send it to a satellite signal processor at the back end for signal processing, so that the public can watch satellite TV programs.
集波器由一喇叭天线(Feedhom)、一导波管(Waveguide)以及一低噪声降频放大器(Low Noise Block Down-converter,LNB)所组成。其中,喇叭天线用来将卫星天线所反射的信号搜集导引入导波管,接着输出至低噪声降频放大器。喇叭天线的功能除了接收卫星信号外,在不同应用中也可发射信号(经碟型反射面反射)给卫星。The wave collector is composed of a horn antenna (Feedhom), a waveguide (Waveguide) and a low noise down-converter (LNB). Among them, the horn antenna is used to collect the signal reflected by the satellite antenna and guide it into the waveguide, and then output it to the low-noise down-frequency amplifier. In addition to receiving satellite signals, the function of the horn antenna can also transmit signals (reflected by the dish reflector) to satellites in different applications.
卫星天线的收讯质量优劣与喇叭天线的设置位置有相当重要的关系。举例来说,喇叭天线由焦点位置发出的电磁波经碟型反射面反射给卫星。当喇叭天线与焦点位置稍有偏离,卫星天线可接收的信号将会大大减小。实际上,焦点位置通常是根据碟面的焦距直径比(Focal Length to Diameter ratio,F/D)来表示。值得注意的是,碟面的焦距直径比(以下简称为F/D值)与喇叭天线所发射的束波宽度的搭配与否会影响卫星天线的接收效能。换句话说,不同的F/D设计需搭配不同的束波宽度,使卫星天线能有效接收喇叭天线的束波。举例来说,F/D=0.6的碟面设计相比较于F/D=0.4的碟面设计需搭配束波宽度较窄的束波,若束波的宽度不符合碟面设计(如过宽或过窄),则会影响卫星天线的收讯效能,并降低卫星信号的收讯质量。The receiving quality of the satellite antenna has a very important relationship with the setting position of the horn antenna. For example, the electromagnetic wave emitted by the horn antenna from the focal point is reflected to the satellite by the dish-shaped reflector. When the horn antenna deviates slightly from the focus position, the signal received by the satellite antenna will be greatly reduced. In fact, the focus position is usually expressed according to the focal length-diameter ratio (Focal Length to Diameter ratio, F/D) of the dish surface. It is worth noting that the combination of the focal length-to-diameter ratio of the dish surface (hereinafter referred to as F/D value) and the beam width emitted by the horn antenna will affect the receiving performance of the satellite antenna. In other words, different F/D designs need to be matched with different beam widths so that the satellite antenna can effectively receive the beam of the horn antenna. For example, compared to the dish design of F/D=0.4, the dish design of F/D=0.6 needs to match the beam with a narrower beam width. If the beam width does not meet the dish design (such as too wide or too narrow), it will affect the receiving performance of the satellite antenna and reduce the receiving quality of the satellite signal.
然而,目前市场上尚未有调整喇叭天线的束波宽度的相关装置,因此无法提升与不同碟面设计的搭配性。此外,为了因应小型化的趋势以及降低成本,在产品设计之初,制造厂商皆会竭尽所能的将产品设计到最小化。因此,如何在喇叭天线的张口尺寸缩小下,还能达到与碟面最适当搭配的束波宽度的设计亦为重要议题之一。However, currently there is no related device for adjusting the beam width of the horn antenna in the market, so it is impossible to improve the compatibility with different dish designs. In addition, in order to cope with the trend of miniaturization and reduce costs, manufacturers will try their best to minimize the product design at the beginning of product design. Therefore, how to design the beamwidth that best matches the dish surface while reducing the aperture size of the horn antenna is also one of the important issues.
发明内容Contents of the invention
因此,本发明的主要目的在于提供一种用于喇叭天线的束波调整装置,用来调整喇叭天线所发射的束波宽度,以达到与卫星天线的碟面更好的搭配效能。Therefore, the main purpose of the present invention is to provide a beam adjusting device for a horn antenna, which is used to adjust the width of the beam emitted by the horn antenna, so as to achieve better matching performance with the dish of the satellite antenna.
本发明公开一种用于喇叭天线的束波调整装置,该喇叭天线包含有一张口及围绕该张口的环体,该束波调整装置包含有:一金属导件,该金属导件用来根据该喇叭天线所对应的一卫星天线的碟面特征,调整该喇叭天线所形成的束波宽度;以及一固定件,该固定件用来固定该金属导件于该喇叭天线;其中,该卫星天线用来接收该喇叭天线所发射的信号。The invention discloses a beam adjustment device for a horn antenna. The horn antenna includes an opening and a ring surrounding the opening. The beam adjustment device includes: a metal guide, which is used to The dish surface characteristics of a satellite antenna corresponding to the horn antenna, adjust the beam width formed by the horn antenna; and a fixing piece, the fixing piece is used to fix the metal guide to the horn antenna; To receive the signal transmitted by the horn antenna.
本发明可针对不同碟面设计(如不同的F/D值),在不更改喇叭天线模具尺寸的条件下,得到所需的束波宽度,以提升收讯质量。进一步地,本发明的束波调整装置能够在喇叭天线的张口尺寸缩小的情况下,维持相同的束波宽度,以搭配碟面设计,并有效降低成本。According to different dish surface designs (eg different F/D values), the present invention can obtain the required beam width without changing the mold size of the horn antenna, so as to improve the receiving quality. Furthermore, the beam adjusting device of the present invention can maintain the same beam width when the aperture size of the horn antenna is reduced, so as to match the dish design and effectively reduce the cost.
附图说明 Description of drawings
图1为本发明实施例的一束波调整装置用于一喇叭天线的示意图。FIG. 1 is a schematic diagram of a beam adjusting device used in a horn antenna according to an embodiment of the present invention.
图2~图5为本发明多种实施例的束波调整装置的示意图。2 to 5 are schematic diagrams of beam adjusting devices according to various embodiments of the present invention.
图6为图1的束波调整装置用于一防水机制组件的示意图。FIG. 6 is a schematic diagram of the beam adjusting device of FIG. 1 being used in a waterproof mechanism assembly.
图7为本发明实施例的一喇叭天线未使用束波调整装置的束波示意图。FIG. 7 is a schematic diagram of a beam of a horn antenna without a beam adjusting device according to an embodiment of the present invention.
图8为图1的喇叭天线的束波示意图。FIG. 8 is a schematic diagram of the beam of the horn antenna in FIG. 1 .
图9为图3的喇叭天线的束波示意图。FIG. 9 is a schematic diagram of the beam of the horn antenna in FIG. 3 .
图10为图7~图9的束波宽度的比较表。FIG. 10 is a comparison table of beam widths in FIGS. 7 to 9 .
主要组件符号说明:Description of main component symbols:
10、20、30、40、50 束波调整装置10, 20, 30, 40, 50 beam adjustment device
100 喇叭天线100 Horn Antenna
102 张口102 open mouth
104 环体104 ring body
200 防水机制组件200 Waterproof mechanism components
具体实施方式 Detailed ways
请参考图1,图1为本发明实施例的一束波调整装置10的示意图。束波调整装置10用于一喇叭天线100,喇叭天线100包含有一张口102及围绕张口102的环体104。在图1中,束波调整装置10由一金属导件(conductor)所构成,用来根据喇叭天线100所对应的一卫星天线(未表示于图中)的碟面特征,调整喇叭天线100所形成的束波宽度。其中,碟面特征可为焦距直径比。值得注意的是,束波调整装置10的金属导件可为正交十字、同心圆环、点状偏心圆或辐射发散等对称的几何形状,以及可通过一固定件(未表示于图中)设置于喇叭天线100的张口102的上方、下方或同平面基准。固定件主要是用来将金属导件固定于喇叭天线100,只要是用来将金属导件组装在喇叭天线100的组件或方式,皆属本发明的范畴。举例来说,固定件可为一焊点,用来将金属导件焊接于喇叭天线100的张口外缘或环体104的内壁;或是可为从环体104延伸至张口102的一柱体,用于金属导件组装在柱体的顶端,藉以达到将金属导件固定于喇叭天线100的功能。简单来说,金属导件的尺寸、形状或设置在喇叭天线100的位置会改变束波宽度,因此,本发明实施例通过束波调整装置10的设计,可调整喇叭天线100所发射至卫星天线的束波宽度,以提升卫星天线的信号接收效能,并达到最佳的收讯质量。进一步地,本发明实施例能使喇叭天线100与不同卫星天线(如不同F/D值的碟面设计)达到最佳的搭配性。Please refer to FIG. 1 , which is a schematic diagram of a beam adjusting
在图1中,束波调整装置10为一正交极化设计,可反射延长电场回馈路径及集中电流,以加强束波的指向性,并达到束波集中的效果,藉以避免束波宽度过大而造成部分束波无法被接收的情况发生,进而提升卫星天线的接收效能。其中,正交极化设计可为对称或不对称的正交(如长度、宽度或高度)。此外,通过束波调整装置10集中束波的设计,还可用来缩小喇叭天线100的张口尺寸,而不影响与碟面设计的搭配性,并可降低制造成本。In Fig. 1, the
由上述可知,在喇叭天线100的张口尺寸固定的情况下,通过束波调整装置10可提升与碟面的搭配性,以提升收讯质量。另一方面,在喇叭天线100的张口尺寸缩小的情况下,通过本发明实施例的束波调整装置能维持或得到更好的束波宽度,因此,可有效地减小喇叭天线100的张口面积,以增加与多种卫星天线安装的可行性。It can be seen from the above that, in the case that the opening size of the
值得注意的是,本发明实施例的束波调整装置10可应用于任何形式的喇叭天线,如锥型(conical)、金字塔型(pyramidal)、波纹型(corrugated)、介质负载(dielectric-load)、镜头校准(lens-corrected)、介质(dielectric)或阵列(array)等形式的喇叭天线,亦或是应用在不同的张口形状,如方形、圆形、矩形、菱形或椭圆形等,而不限于此。It is worth noting that the
因此,藉由不同形态的束波调整装置,喇叭天线100在不同的工作频率可得到最佳的天线效益。举例来说,请参考图2~图5,其为本发明多种实施例的束波调整装置20~50的示意图。如图2所示,束波调整装置20的金属导件与张口102非共平面且为辐射圆环状;如图3所示,束波调整装置30的金属导件与张口102共平面且为同心圆环状;如图4所示,束波调整装置40的金属导件与张口102共平面且为不连续圆环状;以及如图5所示,束波调整装置50的金属导件与张口102非共平面且为偏心圆状。因此,在图3与图4所示的束波调整装置30、40的设计下,可使得高频在电场反射回馈上较不易失去匹配而导致束波形状变形。另一方面,在图2与图5所示的束波调整装置20、50的设计下,可针对低频、中频与高频来调整束波宽度,以达到符合碟面的束波宽度,进而降低天线损耗,得到天线增益的最佳值。此外,本发明实施例的束波调整装置10、20、30、40、50还可达到阻抗匹配的效用,以降低天线的反射损耗(Return Loss)。Therefore, with different forms of beam adjusting devices, the
根据上述,本发明实施例的束波调整装置除了可设置在喇叭天线100的张口102平面之外,亦可设置在张口102上方或下方。例如,在图6中,束波调整装置10改为设置在对应于喇叭天线100的一防水机制组件200,如防水盖(Feed Cap)。更进一步的,束波调整装置10可以电镀方式电镀在防水机制组件200上,或是在射出成型制作时即包含在防水机制组件200上,亦或是以氧白铜类的金属薄片设置于防水机制组件200上。值得注意的是,除了束波调整装置10之外,束波调整装置20、30、40、50亦可应用在防水机制组件200,而不限于此。According to the above, the beam adjustment device of the embodiment of the present invention can be arranged not only on the plane of the
请继续参考图7~图9,其分别为喇叭天线100在10.7GHz的工作频率下,未使用任何束波调整装置、使用束波调整装置10,以及使用束波调整装置30的束波示意图。由图7~图9可知,未装设束波调整装置时,喇叭天线100的束波宽度较宽;而比较图8、图9还可得知,在10dB处的束波宽度中,使用正十字型设计的束波调整装置10的束波宽度较为集中,而使用同心圆环设计的束波调整装置30的束波宽度则较宽。另请参考图10,其为图7~图9的束波宽度的比较表。由图10可知,相比较于未使用任何束波调整装置的喇叭天线100,使用束波调整装置10的束波宽度由原先的80.22度(由水平、垂直及45度方向所量测到的束波宽度的平均值)缩小至69.35度,更符合F/D=0.6的碟面设计;而使用束波调整装置30的束波宽度可放大至92.66度,更符合F/D=0.4的碟面设计。由此可知,通过束波调整装置的设计,可使喇叭天线100的束波宽度在10dB处作正负15度的调整。值得注意的是,本发明实施例在未更动喇叭天线张口尺寸或开模尺寸的状况下,即可调整束波宽度而更符合卫星天线特性。Please continue to refer to FIGS. 7 to 9 , which are schematic diagrams of the
综上所述,相比较于公知技术无法调整束波宽度,而无法达到与碟面的最佳搭配效果,造成收讯质量不佳。本发明的实施例可针对不同碟面设计(如不同的F/D值),在不更改喇叭天线模具尺寸的条件下,得到所需的束波宽度,以提升收讯质量。进一步地,本发明实施例的束波调整装置能够在喇叭天线的张口尺寸缩小的情况下,维持相同的束波宽度,以搭配碟面设计,并有效降低成本。To sum up, compared with the known technology, the beam width cannot be adjusted, and the optimal matching effect with the dish surface cannot be achieved, resulting in poor reception quality. The embodiment of the present invention can obtain the required beam width for different dish surface designs (such as different F/D values) without changing the mold size of the horn antenna, so as to improve the receiving quality. Furthermore, the beam adjusting device of the embodiment of the present invention can maintain the same beam width when the aperture size of the horn antenna is reduced, so as to match the dish design and effectively reduce the cost.
以上所述仅为本发明的较佳实施例,凡是根据本发明权利要求书的范围所作的均等变化与修饰,皆应属本发明的涵盖范围。The above descriptions are only preferred embodiments of the present invention, and all equivalent changes and modifications made according to the scope of the claims of the present invention shall fall within the scope of the present invention.
Claims (7)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201010509538.7A CN102456949B (en) | 2010-10-18 | 2010-10-18 | Beam wave adjusting device for horn antenna |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201010509538.7A CN102456949B (en) | 2010-10-18 | 2010-10-18 | Beam wave adjusting device for horn antenna |
Publications (2)
Publication Number | Publication Date |
---|---|
CN102456949A true CN102456949A (en) | 2012-05-16 |
CN102456949B CN102456949B (en) | 2014-10-08 |
Family
ID=46039797
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201010509538.7A Active CN102456949B (en) | 2010-10-18 | 2010-10-18 | Beam wave adjusting device for horn antenna |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN102456949B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114583437A (en) * | 2020-11-18 | 2022-06-03 | 稜研科技股份有限公司 | Ultra-Wideband Non-Metallic Horn Antenna |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4042935A (en) * | 1974-08-01 | 1977-08-16 | Hughes Aircraft Company | Wideband multiplexing antenna feed employing cavity backed wing dipoles |
US6943744B1 (en) * | 2003-07-09 | 2005-09-13 | Patriot Antenna Systems, Inc. | Waveguide diplexing and filtering device |
CN2896561Y (en) * | 2006-04-19 | 2007-05-02 | 启碁科技股份有限公司 | Antenna feed for dish antenna |
CN101656353A (en) * | 2008-08-21 | 2010-02-24 | 百一电子股份有限公司 | Linearly polarized antenna |
-
2010
- 2010-10-18 CN CN201010509538.7A patent/CN102456949B/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4042935A (en) * | 1974-08-01 | 1977-08-16 | Hughes Aircraft Company | Wideband multiplexing antenna feed employing cavity backed wing dipoles |
US6943744B1 (en) * | 2003-07-09 | 2005-09-13 | Patriot Antenna Systems, Inc. | Waveguide diplexing and filtering device |
CN2896561Y (en) * | 2006-04-19 | 2007-05-02 | 启碁科技股份有限公司 | Antenna feed for dish antenna |
CN101656353A (en) * | 2008-08-21 | 2010-02-24 | 百一电子股份有限公司 | Linearly polarized antenna |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114583437A (en) * | 2020-11-18 | 2022-06-03 | 稜研科技股份有限公司 | Ultra-Wideband Non-Metallic Horn Antenna |
CN114583437B (en) * | 2020-11-18 | 2024-02-06 | 稜研科技股份有限公司 | Ultra-wideband non-metallic horn antenna |
Also Published As
Publication number | Publication date |
---|---|
CN102456949B (en) | 2014-10-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US11652288B2 (en) | Antenna | |
US9270013B2 (en) | Reflector arrangement for attachment to a wireless communications terminal | |
US7075492B1 (en) | High performance reflector antenna system and feed structure | |
US8102324B2 (en) | Sub-reflector of a dual-reflector antenna | |
US6184840B1 (en) | Parabolic reflector antenna | |
CN1151590C (en) | Improved reflector antenna with a self-supported feed | |
US20090146899A1 (en) | Antenna assemblies with tapered loop antenna elements and reflectors | |
JP2012205104A (en) | Lens antenna | |
JP5722112B2 (en) | Double-reflector antenna feeder | |
EP2763235A1 (en) | Antenna assemblies with tapered loop antenna elements | |
US20190221945A1 (en) | Method for dish reflector illumination via sub-reflector assembly with dielectric radiator portion | |
JP2015231062A (en) | Antenna device | |
TWI449445B (en) | Beamwidth adjustment device | |
CN102456949B (en) | Beam wave adjusting device for horn antenna | |
JP5337621B2 (en) | Satellite / terrestrial digital broadcasting antenna | |
US20020008671A1 (en) | Integrated dual-directional feed horn | |
JP5266314B2 (en) | Offset parabolic antenna | |
CN110676569A (en) | Annular omnidirectional antenna | |
CN212182537U (en) | Antenna with a shield | |
JPH10163737A (en) | Primary radiator for satellite receiving antenna and converter for satellite receiving | |
CN208820052U (en) | A kind of comprehensive oscillator disk | |
KR102124016B1 (en) | Dual reflector antenna with a hybrid subreflector | |
KR101727961B1 (en) | Apparatus for communicating satellite signal | |
CN109193151A (en) | A kind of comprehensive oscillator disk | |
KR102023959B1 (en) | Parabolic 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 |