CN205248451U - Plane of reflection that leads to satellite communication antenna in quiet - Google Patents

Plane of reflection that leads to satellite communication antenna in quiet Download PDF

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Publication number
CN205248451U
CN205248451U CN201521065713.2U CN201521065713U CN205248451U CN 205248451 U CN205248451 U CN 205248451U CN 201521065713 U CN201521065713 U CN 201521065713U CN 205248451 U CN205248451 U CN 205248451U
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CN
China
Prior art keywords
hasp
reflecting surface
panel
quiet
satellite communication
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
Application number
CN201521065713.2U
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Chinese (zh)
Inventor
高峰
秦文科
刘鑫
贾弛
付轶轩
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.)
Space Star Technology Co Ltd
Original Assignee
Space Star Technology Co 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.)
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Publication date
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Priority to CN201521065713.2U priority Critical patent/CN205248451U/en
Application granted granted Critical
Publication of CN205248451U publication Critical patent/CN205248451U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The embodiment of the utility model provides a plane of reflection that leads to satellite communication antenna in quiet, the plane of reflection is central panel (1), zhonghuan panel (2), outer loop panel (3) from interior past exterior division, the center panel (1) with between zhonghuan panel (2) zhonghuan panel (2) with all through hasp (4) fixed connection between outer loop panel (3). The embodiment of the utility model provides an in central panel (1) be the main support part of plane of reflection, central panel (1), zhonghuan panel (2), outer loop panel (3) are respectively through hasp fixed connection to the quick assembly disassembly's of plane of reflection mesh has been realized.

Description

A kind of reflecting surface of quiet middle communication satellite communication antenna
Technical field
The utility model relates to technical field of satellite communication, specifically based on the quiet middle communication satellite communication of oneThe reflecting surface of antenna.
Background technology
Quiet middle communication satellite communication antenna is to build mobile satellite communication network, and Support, Command information is transmitted rapidlyA visual plant, be used for the function transmitting and receiving of command information.
Quiet middle communication satellite communication antenna comprises reflecting surface, the structure of reflecting surface want can meet fast demountable,Lightweight requirement. The antenna of travel position is in collecting state, and Reflector Panel is by artificial unloading, when workFast Installation according to demand.
But the surface of emission of the prior art when mounted, due to complex structure, can not carry out Fast Installation.
Utility model content
In view of this, the utility model provides a kind of reflecting surface of quiet middle communication satellite communication antenna, to solveIn prior art, the surface of emission when mounted, due to complex structure, can not carry out the problem of Fast Installation, its skillArt scheme is as follows:
A reflecting surface for quiet middle communication satellite communication antenna, described reflecting surface is from the interior the center panel that is divided into outward(1), middle anchor ring plate (2), outer shroud panel (3);
Between described the center panel (1) and described middle anchor ring plate (2), described middle anchor ring plate (2) and instituteState between outer shroud panel (3) and be all fixedly connected with by hasp (4).
Wherein, described the center panel (1) inside comprises built-in fitting.
Wherein, described the center panel (1) is provided with luffing mechanism connector and fixture (5).
Wherein, described the center panel is provided with alignment pin on (1), on described middle anchor ring plate (2), is provided withWith the pin-and-hole that the alignment pin on described the center panel (1) coordinates, it is fixed on described middle anchor ring plate (2), to be provided withPosition pin, is provided with the pin coordinating with the alignment pin on described middle anchor ring plate (2) on described outer shroud panel (3)Hole.
Wherein, described reflecting surface be shaped as the paraboloid of revolution, described reflecting surface is aluminium honeycomb interlayer carbon fiberThe surface of emission of covering composite.
Wherein, the thickness of described reflecting surface is 50mm.
Wherein, described hasp (4) comprises sub-hasp and female hasp, and described sub-hasp is provided with alignment pin,On described female hasp, be provided with the pin-and-hole corresponding with alignment pin on described sub-hasp, or described female hasp is establishedBe equipped with alignment pin, on described sub-hasp, be provided with the pin-and-hole corresponding with alignment pin on described female hasp.
Wherein, described hasp (4) comprises adjusting nut, and the degree of tightness of described hasp (4) can be passed through described tuneJoint nut regulates.
Wherein, described hasp (4) is high strength hasp.
Technique scheme has following beneficial effect:
The main support part that the center panel 1 in the utility model embodiment is reflecting surface, the center panel 1,Middle anchor ring plate 2, outer shroud panel 3 are fixedly connected with by hasp respectively, thereby have realized the fast dismantling of reflecting surfaceThe object of dress.
Brief description of the drawings
The structure of the reflecting surface of a kind of quiet middle communication satellite communication antenna that Fig. 1 provides for the utility model embodimentSchematic diagram;
The enlarged drawing of a kind of high strength hasp that Fig. 2 provides for the utility model embodiment;
Side-looking in the reflecting surface of the quiet middle communication satellite communication antenna that Fig. 3 provides for the utility model embodimentFigure.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the utility model embodiment, to the technical side in the utility model embodimentCase is clearly and completely described, and obviously, described embodiment is only that the utility model part is realExecute example, instead of whole embodiment. Based on the embodiment in the utility model, ordinary skill peopleMember, not making the every other embodiment obtaining under creative work prerequisite, belongs to the utility modelThe scope of protection.
Refer to Fig. 1, the reflection of a kind of quiet middle communication satellite communication antenna providing for the utility model embodimentThe structural representation of face, reflecting surface from interior be divided into outward the center panel 1, anchor ring plate 2, outer shroud panel 3.
Wherein, between described the center panel 1 and described middle anchor ring plate 2, described middle anchor ring plate 2 with described outsideBetween anchor ring plate 3, be all fixedly connected with by hasp 4.
Hasp (4) is high strength hasp.
In order to allow those skilled in the art more understand the utility model embodiment, refer to Fig. 2, be this realityThe enlarged drawing of a kind of hasp providing by new embodiment.
The main support part that the center panel 1 in the utility model embodiment is reflecting surface, the center panel 1,Middle anchor ring plate 2, outer shroud panel 3 are fixedly connected with by hasp respectively, thereby have realized the fast dismantling of reflecting surfaceThe object of dress.
Fixing main the center panel 1 that relies on of entirety of the surface of emission is realized, so the center panel 1 preferablyThickening type panel, the center panel 1 inside comprises built-in fitting.
In the reflecting surface embodiment of above-mentioned arbitrary quiet middle communication satellite communication antenna, the center panel 1 is provided with bowsFace upward mechanism's connector and fixture 5, the entirety that realizes reflecting surface with this is fixed and pitch regulation.
Refer to Fig. 3, in the reflecting surface of the quiet middle communication satellite communication antenna providing for the utility model embodimentSide view.
Fixture 5 has been shown in Fig. 3.
In the reflecting surface embodiment of above-mentioned arbitrary quiet middle communication satellite communication antenna, in order to install more fastReflecting surface can be provided with alignment pin on described the center panel 1, on described middle anchor ring plate 2, be provided withThe pin-and-hole that alignment pin on described the center panel 1 coordinates, is provided with alignment pin, institute on described middle anchor ring plate 2State and on outer shroud panel 3, be provided with the pin-and-hole coordinating with the alignment pin on described middle anchor ring plate 2.
Or can on described middle anchor ring plate 2, be provided with alignment pin, on described the center panel 1, be provided withThe pin-and-hole that alignment pin on described middle anchor ring plate 2 coordinates, is provided with alignment pin on described outer shroud panel 3, instituteState and on anchor ring plate 2, be provided with the pin-and-hole coordinating with the alignment pin on described outer shroud panel 3.
Alignment pin refers in the mould being made up of two parts or more parts, makes the adjacent two parts of mould accurateLocate and the pin of design.
In the reflecting surface embodiment of above-mentioned arbitrary quiet middle communication satellite communication antenna, the shape of described reflecting surface canThink the paraboloid of revolution, described reflecting surface is the surface of emission of aluminium honeycomb interlayer carbon fiber skin composite.
According to the weight requirement of quiet middle communication satellite communication antenna, reflecting surface can adopt the composite that density is littleProcessing and fabricating forms, and plate thickness should be able to meet some strength requirement. In the utility model embodiment, reflectFace can be made by aluminium honeycomb interlayer carbon fiber skin composite, and the gross thickness of reflecting surface can be50mm. In addition, the cross section of reflecting surface is nomianl para-curve, and can meet multifrequency in design simultaneouslyThe transmitting-receiving demand of segment signal.
Reflecting surface in the utility model embodiment adopts the little composite of density, for example aluminium honeycomb interlayer carbonFabric jacket composite, has realized reflecting surface high strength and light-weighted object.
In order to meet the demand of fast assembling-disassembling, between the center panel 1, middle anchor ring plate 2, outer shroud panel 3, adoptBe connected and fixed by the form of hasp 4, hasp stress can be adjusted by the adjusting nut of bucklingJoint, after assembling and setting completes, fixes adjusting nut.
In the reflecting surface embodiment of above-mentioned arbitrary quiet middle communication satellite communication antenna, described hasp 4 comprises that son takesButton and female hasp, described sub-hasp is provided with alignment pin, on described female hasp, be provided with described sub-hasp onPin-and-hole corresponding to alignment pin, or described female hasp is provided with alignment pin, on described sub-hasp, be provided withPin-and-hole corresponding to alignment pin on described female hasp.
Between described sub-hasp and female hasp, position the assembling that improves reflecting surface with this by alignment pinPrecision.
The method that the above-mentioned surface of emission is installed is as follows: reflecting surface is installed under the state of looking up to heaven, first by median planePlate 1 is fixed, anchor ring plate 2, outer shroud panel 3 in then installing successively. When installation, according to debuggingInstallation site, each piecemeal panel is installed to assigned address. The center panel 1, middle anchor ring plate 2, outer shroudInstallation between panel 3 can be docked by alignment pin, then uses snap lock.
The reflecting surface embodiment of above-mentioned quiet middle communication satellite communication antenna can be applied in medium caliber quiet logicalIn satellite antenna system. In general medium caliber quiet, logical satellite antenna system is mostly vehicle-mounted antenna system,Its volume is large, Heavy Weight, arrives work object required time longer, or for without vehicle transport conditionExtreme regions cannot enter work. Adopt the utility model embodiment to address the above problem.
In this description, each embodiment adopts the mode of going forward one by one to describe, and what each embodiment stressed isWith the difference of other embodiment, between each embodiment identical similar part mutually referring to.
Also it should be noted that, in this article, term " comprises ", " comprising " or its any other variantBe intended to contain comprising of nonexcludability, thus make to comprise a series of key elements process, method, article orEquipment not only comprises those key elements, but also comprises other key elements of clearly not listing, or also comprisesBy the intrinsic key element of this process, method, article or equipment. In the situation that there is no more restrictions,The key element being limited by statement " comprising ... ", and be not precluded within comprise described key element process, method,In article or equipment, also there is other identical element.
To the above-mentioned explanation of provided embodiment, make professional and technical personnel in the field can realize or use thisUtility model. To be aobvious and easy for those skilled in the art to the multiple amendment of these embodimentSee, General Principle as defined herein can be in the situation that does not depart from spirit or scope of the present utility modelUnder, realize in other embodiments. Therefore, the utility model will can not be restricted to shown in this article theseEmbodiment, but to meet the widest scope consistent with principle provided in this article and features of novelty.

Claims (9)

1. a reflecting surface for quiet middle communication satellite communication antenna, is characterized in that, described reflecting surface is from interior pastBe divided into the center panel (1), middle anchor ring plate (2), outer shroud panel (3) outward;
Between described the center panel (1) and described middle anchor ring plate (2), described middle anchor ring plate (2) and instituteState between outer shroud panel (3) and be all fixedly connected with by hasp (4).
2. the reflecting surface of quiet middle communication satellite communication antenna according to claim 1, is characterized in that,
Described the center panel (1) inside comprises built-in fitting.
3. according to the reflecting surface of quiet middle communication satellite communication antenna described in claim 1 or 2, it is characterized in that,
Described the center panel (1) is provided with luffing mechanism connector and fixture (5).
4. according to the reflecting surface of quiet middle communication satellite communication antenna described in claim 1 or 2, it is characterized in that,
Described the center panel is provided with alignment pin on (1), on described middle anchor ring plate (2), is provided with describedThe pin-and-hole that alignment pin on the center panel (1) coordinates, is provided with alignment pin on described middle anchor ring plate (2),On described outer shroud panel (3), be provided with the pin-and-hole coordinating with the alignment pin on described middle anchor ring plate (2).
5. according to the reflecting surface of quiet middle communication satellite communication antenna described in claim 1 or 2, it is characterized in that,Described reflecting surface be shaped as the paraboloid of revolution, described reflecting surface is aluminium honeycomb interlayer carbon fiber skin composite woodThe surface of emission of material.
6. according to the reflecting surface of quiet middle communication satellite communication antenna described in claim 1 or 2, it is characterized in that,The thickness of described reflecting surface is 50mm.
7. according to the reflecting surface of quiet middle communication satellite communication antenna described in claim 1 or 2, it is characterized in that,Described hasp (4) comprises sub-hasp and female hasp, and described sub-hasp is provided with alignment pin, described female haspOn be provided with the pin-and-hole corresponding with alignment pin on described sub-hasp, or described female hasp is provided with alignment pin,On described sub-hasp, be provided with the pin-and-hole corresponding with alignment pin on described female hasp.
8. according to the reflecting surface of quiet middle communication satellite communication antenna described in claim 1 or 2, it is characterized in that,
Described hasp (4) comprises adjusting nut, and the degree of tightness of described hasp (4) can be passed through described adjusting nutRegulate.
9. according to the reflecting surface of quiet middle communication satellite communication antenna described in claim 1 or 2, it is characterized in that,
Described hasp (4) is high strength hasp.
CN201521065713.2U 2015-12-18 2015-12-18 Plane of reflection that leads to satellite communication antenna in quiet Expired - Fee Related CN205248451U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201521065713.2U CN205248451U (en) 2015-12-18 2015-12-18 Plane of reflection that leads to satellite communication antenna in quiet

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201521065713.2U CN205248451U (en) 2015-12-18 2015-12-18 Plane of reflection that leads to satellite communication antenna in quiet

Publications (1)

Publication Number Publication Date
CN205248451U true CN205248451U (en) 2016-05-18

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107240757A (en) * 2017-04-22 2017-10-10 西安电子科技大学 It is a kind of new from resilience reconfigurable satellite-borne deployable antenna

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107240757A (en) * 2017-04-22 2017-10-10 西安电子科技大学 It is a kind of new from resilience reconfigurable satellite-borne deployable antenna
CN107240757B (en) * 2017-04-22 2019-12-31 西安电子科技大学 Novel self-resilience reconfigurable satellite-borne deployable antenna

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C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160518

Termination date: 20191218

CF01 Termination of patent right due to non-payment of annual fee