CN115360550A - Satellite antenna feed source wiring conversion cover - Google Patents
Satellite antenna feed source wiring conversion cover Download PDFInfo
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- CN115360550A CN115360550A CN202211104560.2A CN202211104560A CN115360550A CN 115360550 A CN115360550 A CN 115360550A CN 202211104560 A CN202211104560 A CN 202211104560A CN 115360550 A CN115360550 A CN 115360550A
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- satellite antenna
- feed source
- wiring
- antenna feed
- cylindrical
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- 238000006243 chemical reaction Methods 0.000 title claims abstract description 17
- 230000001681 protective effect Effects 0.000 claims abstract description 17
- 229920003023 plastic Polymers 0.000 claims description 3
- 229910000838 Al alloy Inorganic materials 0.000 claims 1
- 239000000956 alloy Substances 0.000 claims 1
- 230000001012 protector Effects 0.000 description 4
- 238000012423 maintenance Methods 0.000 description 2
- 230000001419 dependent effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 238000009434 installation Methods 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
- 238000007789 sealing Methods 0.000 description 1
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Classifications
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
- H01R13/46—Bases; Cases
- H01R13/52—Dustproof, splashproof, drip-proof, waterproof, or flameproof cases
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/02—Arrangements for de-icing; Arrangements for drying-out ; Arrangements for cooling; Arrangements for preventing corrosion
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/12—Supports; Mounting means
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/42—Housings not intimately mechanically associated with radiating elements, e.g. radome
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/50—Structural association of antennas with earthing switches, lead-in devices or lightning protectors
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- Details Of Aerials (AREA)
Abstract
Description
技术领域technical field
本发明属于卫星天线馈源防护技术领域。The invention belongs to the technical field of satellite antenna feed source protection.
背景技术Background technique
一般卫星天线馈源的接线端口暴露在外面,在正常的使用环境中,由于定期维护,故障消除及时,可以正常运行。但是卫星天线安装在野外,长期处于风吹日晒及雨水侵蚀等恶劣工况下,且维护不及时,馈源的接线端口处的故障率非常高。Generally, the wiring port of the satellite antenna feed is exposed outside. In a normal use environment, due to regular maintenance, the fault is eliminated in time, and it can operate normally. However, the satellite antenna is installed in the wild, and has been exposed to harsh working conditions such as wind, sun, rain and erosion for a long time, and the maintenance is not timely, so the failure rate at the wiring port of the feed source is very high.
发明内容Contents of the invention
本发明目的是为了解决现有卫星天线馈源的接线端口暴露在外面导致馈源的接线端口处故障率高的问题,提出了一种卫星天线馈源接线转换罩。The purpose of the present invention is to solve the problem that the wiring port of the existing satellite antenna feed source is exposed to the outside, resulting in a high failure rate at the wiring port of the feed source, and proposes a satellite antenna feed source wiring conversion cover.
本发明所述的一种卫星天线馈源接线转换罩,包括筒形防护罩、固定支架和接线保护件;A satellite antenna feed wiring conversion cover according to the present invention includes a cylindrical protective cover, a fixing bracket and a wiring protection piece;
筒形防护罩包括上下开口的筒形和半球形结构,所述的半球形结构扣设在所述筒形结构的上端;筒形结构的侧面等间隔固定有三个固定支架,且位于筒形防护罩的下部;The cylindrical protective cover includes a cylindrical and hemispherical structure with upper and lower openings. The hemispherical structure is buckled on the upper end of the cylindrical structure; three fixing brackets are fixed at equal intervals on the side of the cylindrical structure, and are located the lower part of the hood;
所述三个固定支架的下表面开有沿长度方向的凹槽,所述凹槽用于卡接在卫星天线馈源的支架上;The lower surfaces of the three fixing brackets are provided with grooves along the length direction, and the grooves are used for clamping on the bracket of the satellite antenna feed source;
筒形防护罩的侧面还固定有接线保护件,筒形防护罩的侧壁还开有条形口,所述条形口位于所述接线保护件的下侧,且临近接线保护件设置,所述接线保护件为沿长度方向开口的筒形结构,所述卫星天线馈源输出线经所述条形口后卡设在接线保护件内。The side of the cylindrical protective cover is also fixed with a wiring protector, and the side wall of the cylindrical protective cover is also provided with a bar-shaped opening. The wiring protector is a cylindrical structure with openings along the length direction, and the satellite antenna feed output line passes through the strip-shaped opening and is clamped in the wiring protector.
进一步地,本发明中,还包括F头接口,所述F头接口的一端与天线馈源信号输出线连接,所述F头接口设置在在接线保护件内。Furthermore, in the present invention, an F-head interface is also included, one end of the F-head interface is connected to the antenna feed signal output line, and the F-head interface is arranged in the wiring protection member.
进一步地,本发明中,还包括卡夹,所述卡夹卡接在接线保护件上,用于对天线馈源信号输出线进行固定。Further, in the present invention, a clamp is also included, and the clamp is clamped on the wire protection member, and is used for fixing the output wire of the antenna feed signal.
进一步地,本发明中,三个固定支架通过螺丝与馈源支架固定。Further, in the present invention, the three fixing brackets are fixed to the feed source bracket by screws.
进一步地,本发明中,筒形防护罩为透明塑料制成。Further, in the present invention, the cylindrical protective cover is made of transparent plastic.
本发明所述结构有效的保护了卫星天线馈源的接线端口,克服了野外的恶劣环境对卫星天线馈源的影响,将天线馈源的接线端口及连接电缆的接头全部保护起来,并且具备防水密封功能,使接线端口及接头长期处于干燥环境,有利于运行,采用三个固定支架将防护罩固定到馈源支架上,方便现场安装及拆卸。馈源的连接电缆可以沿着馈源支架固定并引出,使电缆固定更牢固且引出线的方式更合理。The structure of the invention effectively protects the connection port of the satellite antenna feed source, overcomes the influence of the harsh environment in the field on the satellite antenna feed source, protects all the connection ports of the antenna feed source and the joints connecting the cables, and has waterproof The sealing function keeps the wiring ports and joints in a dry environment for a long time, which is conducive to operation. Three fixing brackets are used to fix the protective cover to the feed source bracket, which is convenient for on-site installation and disassembly. The connecting cable of the feed source can be fixed and led out along the feed source bracket, so that the cable is fixed more firmly and the way of leading out the wire is more reasonable.
附图说明Description of drawings
图1是本发明所述卫星天线馈源接线转换罩的立体结构示意图;Fig. 1 is the schematic diagram of the three-dimensional structure of the satellite antenna feed wiring conversion cover of the present invention;
图2是卫星天线馈源接线转换罩的主视图;Fig. 2 is the front view of the satellite antenna feed wiring conversion cover;
图3是卫星天线馈源接线转换罩的侧视图;Fig. 3 is a side view of the satellite antenna feed wiring conversion cover;
图4是卫星天线馈源接线转换罩的俯视图。Fig. 4 is a top view of the satellite antenna feed wire conversion cover.
具体实施方式Detailed ways
下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有作出创造性劳动的前提下所获得的所有其他实施例,都属于本发明保护的范围。The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.
需要说明的是,在不冲突的情况下,本发明中的实施例及实施例中的特征可以相互组合。It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other.
具体实施方式一:下面结合图1至图4说明本实施方式,本实施方式所述一种卫星天线馈源接线转换罩,包括筒形防护罩1、固定支架2和接线保护件3;Specific Embodiment 1: The present embodiment will be described below in conjunction with FIG. 1 to FIG. 4 . A satellite antenna feed wiring conversion cover described in this embodiment includes a cylindrical
筒形防护罩1包括上下开口的筒形和半球形结构,所述透明的半球形结构扣设在所述筒形结构的上端;筒形结构的侧面等间隔固定有三个固定支架2,且位于筒形防护罩1的下部;The cylindrical
所述三个固定支架2的下表面开有沿长度方向的凹槽,所述凹槽用于卡接在卫星天线馈源的支架上;The lower surfaces of the three fixed
筒形防护罩1的侧面还固定有接线保护件3,筒形防护罩1的侧壁还开有条形口,所述条形口位于所述接线保护件3的下侧,且临近接线保护件3设置,所述接线保护件3为沿长度方向开口的筒形结构,所述卫星天线馈源输出线经所述条形口后卡设在接线保护件3内。The side of the cylindrical
进一步地,本发明中,还包括F头接口,所述F头接口的一端与天线馈源信号输出线连接,所述F头接口设置在在接线保护件3内。Further, the present invention also includes an F-head interface, one end of the F-head interface is connected to the antenna feed signal output line, and the F-head interface is arranged in the
进一步地,本发明中,还包括卡夹4,所述卡夹4卡接在接线保护件3上,用于对天线馈源信号输出线进行固定。Further, in the present invention, a
进一步地,本发明中,三个固定支架2通过螺丝与馈源支架固定。Further, in the present invention, the three
进一步地,本发明中,筒形防护罩1为透明塑料制成。Further, in the present invention, the cylindrical
本发明首先依据实际使用的卫星天线尺寸确定馈源接线转换罩的尺寸进行加工。将加工好的馈源接线转换罩先与馈源出线端口进行连接,然后将转换罩安装的馈源上,并用三个固定支架进行固定,将户外电缆连接到转换器处并用接线保护器固定好电缆,最后将电缆沿着馈线支架固定好并引出。In the present invention, the size of the feed wiring conversion cover is firstly determined according to the size of the actually used satellite antenna for processing. Connect the processed feed source wiring conversion cover to the feed source outlet port first, then install the conversion cover on the feed source, and fix it with three fixing brackets, connect the outdoor cable to the converter and fix it with a wiring protector Finally, fix the cable along the feeder bracket and lead it out.
虽然在本文中参照了特定的实施方式来描述本发明,但是应该理解的是,这些实施例仅仅是本发明的原理和应用的示例。因此应该理解的是,可以对示例性的实施例进行许多修改,并且可以设计出其他的布置,只要不偏离所附权利要求所限定的本发明的精神和范围。应该理解的是,可以通过不同于原始权利要求所描述的方式来结合不同的从属权利要求和本文中所述的特征。还可以理解的是,结合单独实施例所描述的特征可以使用在其他所述实施例中。Although the invention is described herein with reference to specific embodiments, it should be understood that these embodiments are merely illustrative of the principles and applications of the invention. It is therefore to be understood that numerous modifications may be made to the exemplary embodiments and that other arrangements may be devised without departing from the spirit and scope of the invention as defined by the appended claims. It shall be understood that different dependent claims and features described herein may be combined in a different way than that described in the original claims. It will also be appreciated that features described in connection with individual embodiments can be used in other described embodiments.
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Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
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JP2012124714A (en) * | 2010-12-08 | 2012-06-28 | Nippon Antenna Co Ltd | Antenna device |
CN108511871A (en) * | 2018-02-28 | 2018-09-07 | 浙江联品电子科技有限公司 | A kind of sucker car antenna |
CN208111660U (en) * | 2018-02-09 | 2018-11-16 | 四川公众监理咨询有限公司 | A kind of omnidirectional volumetric antenna |
CN208767464U (en) * | 2018-10-29 | 2019-04-19 | 李楠 | A kind of satellite earth antenna device |
CN209056600U (en) * | 2018-12-29 | 2019-07-02 | 深圳市大疆创新科技有限公司 | RTK antenna assembly and its shell structure and unmanned plane |
CN216698729U (en) * | 2021-12-20 | 2022-06-07 | 长江三峡通航管理局 | Marine big dipper antenna protection device |
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- 2022-09-09 CN CN202211104560.2A patent/CN115360550A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2012124714A (en) * | 2010-12-08 | 2012-06-28 | Nippon Antenna Co Ltd | Antenna device |
CN208111660U (en) * | 2018-02-09 | 2018-11-16 | 四川公众监理咨询有限公司 | A kind of omnidirectional volumetric antenna |
CN108511871A (en) * | 2018-02-28 | 2018-09-07 | 浙江联品电子科技有限公司 | A kind of sucker car antenna |
CN208767464U (en) * | 2018-10-29 | 2019-04-19 | 李楠 | A kind of satellite earth antenna device |
CN209056600U (en) * | 2018-12-29 | 2019-07-02 | 深圳市大疆创新科技有限公司 | RTK antenna assembly and its shell structure and unmanned plane |
CN216698729U (en) * | 2021-12-20 | 2022-06-07 | 长江三峡通航管理局 | Marine big dipper antenna protection device |
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Inventor after: Tian Yuan Inventor after: Du Wei Inventor after: Cui Chun Inventor after: Pan Xiangrong Inventor after: Jin Jingshan Inventor after: Wang Yilei Inventor after: Cui Xintian Inventor after: Wang Shengli Inventor after: Yang Shumin Inventor after: Li Zhefu Inventor before: Tian Yuan Inventor before: Cui Chun Inventor before: Jin Jingshan Inventor before: Wang Yilei Inventor before: Cui Xintian Inventor before: Wang Shengli Inventor before: Yang Shumin Inventor before: Li Zhefu Inventor before: Du Wei |