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JPH0422362B2 - - Google Patents
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JPH0422362B2 - - Google Patents

Info

Publication number
JPH0422362B2
JPH0422362B2 JP27476184A JP27476184A JPH0422362B2 JP H0422362 B2 JPH0422362 B2 JP H0422362B2 JP 27476184 A JP27476184 A JP 27476184A JP 27476184 A JP27476184 A JP 27476184A JP H0422362 B2 JPH0422362 B2 JP H0422362B2
Authority
JP
Japan
Prior art keywords
antenna reflector
support device
back support
rectangular
parabolic
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
Application number
JP27476184A
Other languages
Japanese (ja)
Other versions
JPS61157004A (en
Inventor
Masahiro Minoke
Katsumi Kaneoka
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.)
Toshiba Corp
NTT Inc
Original Assignee
Toshiba Corp
Nippon Telegraph and Telephone Corp
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 Toshiba Corp, Nippon Telegraph and Telephone Corp filed Critical Toshiba Corp
Priority to JP27476184A priority Critical patent/JPS61157004A/en
Publication of JPS61157004A publication Critical patent/JPS61157004A/en
Publication of JPH0422362B2 publication Critical patent/JPH0422362B2/ja
Granted legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q15/00Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
    • H01Q15/14Reflecting surfaces; Equivalent structures
    • H01Q15/16Reflecting surfaces; Equivalent structures curved in two dimensions [2D], e.g. paraboloidal

Landscapes

  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Aerials With Secondary Devices (AREA)
  • Support Of Aerials (AREA)

Description

【発明の詳細な説明】 [発明の技術分野] この発明は、例えば宇宙基地等に用いられる展
開型アンテナ反射鏡に係り、特に、その背面支持
装置に関する。
DETAILED DESCRIPTION OF THE INVENTION [Technical Field of the Invention] The present invention relates to a deployable antenna reflector used, for example, in a space base, and particularly to a back support device thereof.

[発明の技術的背景] 一般に、アンテナ反射鏡は、その鏡面部が背面
支持装置に取付けられ、この背面支持装置を介し
て所定の位置に設置される。そして、このような
アンテナ反射鏡を支持する背面支持装置において
は、近時、アンテナの分野において開発されつつ
ある開口径が10m〜数100mに達する超大口径の
組立型アンテナに好適するように改良することが
要請されている。この改良するため手段として
は。トラス構造やラーメン構造等の骨組構造で、
アンテナ反射鏡に対応するパラボラ近時曲面を持
つ背面支持装置を構成することが考えられてい
る。
[Technical Background of the Invention] Generally, an antenna reflector has its mirror surface attached to a back support device, and is installed at a predetermined position via the back support device. The back support device that supports such an antenna reflector is improved to be suitable for ultra-large-diameter assembled antennas with apertures ranging from 10 m to several 100 m, which have recently been developed in the field of antennas. This is requested. As a means to improve this. With frame structures such as truss structures and rigid frame structures,
It has been considered to construct a rear support device with a parabolic recently curved surface corresponding to the antenna reflector.

[背景技術の問題点] ところが、上記のような骨組構造の背面支持装
置では、例えば使用周波数が20GHz以上で、開口
径が数mの展開型アンテナに適用した場合、各種
の不具合を有する。
[Problems with Background Art] However, the above-mentioned back support device having a frame structure has various problems when applied to a deployable antenna with a working frequency of 20 GHz or higher and an aperture diameter of several meters, for example.

すなわち、アンテナ反射鏡の鏡面輪郭はパラボ
ラ面(回転放物面)と回転軸に平行な円筒との交
線(即ち、楕円)として定義される。この結果、
このような背面支持装置にあつては、その骨組構
造で形成される1つの基本形状(立体セル)を細
かく分割しないと、鏡面形状に適合するパラボラ
近似曲面の形成が困難となる。従つて、設計的に
非常に難しく、製作が非常に面倒となると共に、
接合箇所が非常に多くなり、重量が重くなるとい
う問題を有する。特に、重量の問題は、特に宇宙
基地等の宇宙空間に構築するアンテナ反射鏡に適
用する場合に大きな問題となる。
That is, the specular contour of the antenna reflector is defined as an intersection line (ie, an ellipse) between a parabolic surface (paraboloid of revolution) and a cylinder parallel to the axis of rotation. As a result,
In the case of such a back support device, unless one basic shape (three-dimensional cell) formed by the frame structure is divided into small pieces, it becomes difficult to form a parabolic approximation curved surface that matches the mirror surface shape. Therefore, it is very difficult to design, very troublesome to manufacture, and
The problem is that there are a large number of joints and the weight is heavy. In particular, the problem of weight becomes a big problem especially when applied to an antenna reflector constructed in outer space such as a space base.

[発明の目的] この発明は、上記の事情に鑑みてなされたもの
で、簡易な構成で、軽量化を促進し得ると共に、
製作性を向上し得、かつ鏡面形状との高精度な整
合を実現し得るようにしたアンテナ反射鏡の背面
支持装置を提供することを目的とする。
[Object of the Invention] The present invention was made in view of the above circumstances, and has a simple configuration and can promote weight reduction.
It is an object of the present invention to provide a back support device for an antenna reflector that can improve manufacturability and realize highly accurate matching with a mirror surface shape.

[発明の概要] すなわち、この発明は、同心円筒面上の周方向
に等分割された点群でなるものであつて、略平行
に配置された矩形状の上部面及び矩形状の下部面
を有した台形状の立体セルを複数個組合わせ全体
としての略同心曲面状を形成し、前記矩形状の上
部面及び矩形状の下部面の一方面側をアンテナ反
射鏡設置面とするように構成したものである。
[Summary of the Invention] That is, the present invention consists of a point group equally divided in the circumferential direction on a concentric cylindrical surface, and has a rectangular upper surface and a rectangular lower surface arranged substantially parallel to each other. A plurality of trapezoidal three-dimensional cells are combined to form a substantially concentric curved surface as a whole, and one side of the rectangular upper surface and the rectangular lower surface is configured to be an antenna reflector installation surface. This is what I did.

[発明の実施例] 以下、この発明の実施例について、図面を参照
して詳細に説明する。
[Embodiments of the Invention] Hereinafter, embodiments of the present invention will be described in detail with reference to the drawings.

第1図はこの発明の一実施例に係るアンテナ反
射鏡の背面支持装置を示すもので、例えばオフセ
ツトフイード形アンテナ反射鏡(図示せず)のパ
ラボラ面に対応して第1〜第3のブロツク10,
11,12に3分割されている。これら第1〜第
3のブロツク10,11,12は略同様の基本構
造で構成されるもので、その各鏡面側の面(以
下、上部面という)及び鏡面より遠い面(以下、
下部面という)が同一中心軸を有する曲面となる
ように形成されている。このうち第1及び第3の
ブロツク10,12は、その各端部から中央部方
向に上記アンテナ反射鏡(図示せず)のパラボラ
面に対応するように成形される。そして、これら
の第1及び第3のブロツク10,12の周囲部に
は傾斜部101,102及び121,122が上
記アンテナ反射鏡(図示せず)の外形に対応する
ように形成されている。
FIG. 1 shows a back support device for an antenna reflector according to an embodiment of the present invention. Block 10,
It is divided into three parts, 11 and 12. These first to third blocks 10, 11, and 12 are constructed with substantially the same basic structure, and have a surface on the mirror surface side (hereinafter referred to as the upper surface) and a surface farther from the mirror surface (hereinafter referred to as the upper surface).
The lower surface) is formed to be a curved surface having the same central axis. Of these, the first and third blocks 10 and 12 are shaped from each end toward the center so as to correspond to the parabolic surface of the antenna reflector (not shown). Slanted portions 101, 102 and 121, 122 are formed around the first and third blocks 10, 12 so as to correspond to the outer shape of the antenna reflector (not shown).

ここで、第2図は上記第2のブロツク11の基
本セルパターンを取り出して示すもので、その曲
面方向に台形状の略同様の複数のセル13が配置
されている。この複数の立体セル13はトラス構
造等の骨組構造により第3図に示すように、点
aehd及び、点dhgcを結び面(以下、側部面Aと
いう)が略台形状で、その他の面、即ち、点
aehd、及び点bfgcを結ぶ面(以下、側部面Bと
いう)と、点abcd、及び点efghを結ぶ面(以下、
上部面及び下部面という)の全て矩形(長方形及
び正方形)状に形成される。この立体セル13の
部材長及び部材のなす角度は ad=eh=bc=fg、ae=dh=bf=cg、 ab=dc、ef=hg ∠abe=∠bef=∠baf=∠afe=∠dch=∠chg
=∠cdg=∠dgh、 ∠ade=∠deh=∠dah=∠ahe=∠bcf=∠cfg
=∠cbg=∠bgh、 の関係が成立する。
Here, FIG. 2 shows the basic cell pattern of the second block 11, in which a plurality of substantially similar trapezoidal cells 13 are arranged in the direction of the curved surface. As shown in FIG.
The surface connecting aehd and point dhgc (hereinafter referred to as side surface A) is approximately trapezoidal, and the other surface, that is, the point
A surface connecting aehd and point bfgc (hereinafter referred to as side surface B) and a surface connecting point abcd and point efgh (hereinafter referred to as side surface B)
The upper and lower surfaces are all rectangular (rectangular and square). The lengths of the members of this three-dimensional cell 13 and the angles formed by the members are: ad=eh=bc=fg, ae=dh=bf=cg, ab=dc, ef=hg ∠abe=∠bef=∠baf=∠afe=∠dch =∠chg
=∠cdg=∠dgh, ∠ade=∠deh=∠dah=∠ahe=∠bcf=∠cfg
=∠cbg=∠bgh, the following relationship holds true.

上記複数の立体セル13はそれぞれの側部面A
及び側部面Bを介して互いに対向する側に接して
いる。従つて、任意の点間を結ぶ斜材の追加を考
慮しても、各立体セル13の点群a、b、c、d
(あるいはe、f、g、h)における各上部面
(あるいは下部面)のなす角は、面全体で同一と
することができるので、1つの曲面を1種類で構
成することができる。
Each of the plurality of three-dimensional cells 13 has a side surface A
and are in contact with mutually opposing sides via the side surface B. Therefore, even if the addition of diagonal members connecting arbitrary points is considered, the point groups a, b, c, d of each three-dimensional cell 13
The angles formed by the upper surfaces (or lower surfaces) in (or e, f, g, h) can be the same for the entire surface, so one curved surface can be composed of one type.

すなわち、上記アンテナ反射鏡の背面支持装置
は、1種類の立体セル13を周知のヒンジ構造等
により連続的(横及び周方向)に組合わせて第1
〜第3のブロツク10,11,12を形成する。
そして、これら第1〜第3のブロツク10,1
1,12は相互間をヒンジ構造等により結合さ
れ、第1図に示すようなパラボラ近似曲面が形成
される。このパラボラ近似曲面としては、例えば
焦点距離3024mm、開口径3500mm、鏡面中心と焦点
軸との距離276.09のアンテナ反射鏡(図示せず)
のパラボラ面に対応するように形成した場合、該
パラボリ面との最大距離誤差が、約40.1mm程度と
なることが確認される。
That is, the antenna reflector back support device is constructed by continuously (laterally and circumferentially) combining one type of three-dimensional cells 13 using a well-known hinge structure or the like.
- form third blocks 10, 11, 12;
And these first to third blocks 10,1
1 and 12 are connected to each other by a hinge structure or the like, and a parabolic approximate curved surface as shown in FIG. 1 is formed. This parabolic approximation curved surface is, for example, an antenna reflector (not shown) with a focal length of 3024 mm, an aperture diameter of 3500 mm, and a distance of 276.09 mm between the center of the mirror surface and the focal axis.
When formed to correspond to a parabolic surface, it is confirmed that the maximum distance error from the parabolic surface is approximately 40.1 mm.

[発明の効果] 以上詳述したように、この発明によれば、同心
筒面上の周方向に等分割された点群でなるもので
あつて、略平行に配置された矩形状の上部面及び
矩形状の下部面を有した台形状の立体セルを複数
個組合わせ全体として略同心曲面状を形成し、そ
の上部面側をパラボラ面を設置するアンテナ反射
鏡設置面とするように構成したことにより、その
アンテナ反射鏡設置面として、アンテナ反射鏡の
パラボラ面との高精度な整合が可能なパラボラ近
似曲面を容易に形成し得るアンテナ反射鏡の背面
支持装置を提供することができる。そして、これ
によれば、骨組構造で形成される複数の立体セル
の標準化が実現され、その設計を含む製作の簡略
化が図れるという効用を有する。
[Effects of the Invention] As detailed above, according to the present invention, the rectangular upper surface is formed of a group of points equally divided in the circumferential direction on a concentric cylindrical surface, and is arranged substantially in parallel. A plurality of trapezoidal three-dimensional cells each having a rectangular lower surface are combined to form a substantially concentric curved surface as a whole, and the upper surface thereof is configured to be an antenna reflector installation surface on which a parabolic surface is installed. As a result, it is possible to provide a back support device for an antenna reflector that can easily form a parabolic approximation curved surface that can be highly accurately matched with the parabolic surface of the antenna reflector as the antenna reflector installation surface. According to this, it is possible to standardize a plurality of three-dimensional cells formed with a frame structure, and there is an effect that the manufacturing including the design thereof can be simplified.

なお、この発明は上記実施例に限ることなく、
その他、この発明の要旨を逸脱しない範囲で種々
の変形を実施し得ることは勿論のことである。」
Note that this invention is not limited to the above embodiments,
It goes without saying that various other modifications can be made without departing from the spirit of the invention. ”

【図面の簡単な説明】[Brief explanation of drawings]

第1図はこの発明の一実施例に係るアンテナ反
射鏡の背面支持装置を示す斜視図、第2図及び第
3図は第1図の詳細を説明するために示した詳細
図である。 10……第1のブロツク、11……第2のブロ
ツク、12……第3のブロツク、13……立体セ
ル。
FIG. 1 is a perspective view showing a back support device for an antenna reflector according to an embodiment of the present invention, and FIGS. 2 and 3 are detailed views shown for explaining the details of FIG. 1. 10...first block, 11...second block, 12...third block, 13...three-dimensional cell.

Claims (1)

【特許請求の範囲】[Claims] 1 同心円筒面上の周方向に等分割された点群で
なるものであつて、略平行に配置された矩形状の
上部面及び矩形状の下部面を有した台形状の立体
セルを複数備え、この複数の立体セルを組合わせ
全体として略同心曲状を形成し、前記矩形状の上
部面及び矩形状の下部面の一方面側をアンテナ反
射鏡設置面としたことを特徴とするアンテナ反射
鏡の背面支持装置。
1 It is made up of a group of points equally divided in the circumferential direction on a concentric cylindrical surface, and includes a plurality of trapezoidal three-dimensional cells each having a rectangular upper surface and a rectangular lower surface arranged approximately in parallel. , an antenna reflection characterized in that the plurality of three-dimensional cells are combined to form a substantially concentrically curved shape as a whole, and one side of the rectangular upper surface and the rectangular lower surface is an antenna reflection mirror installation surface. Mirror back support device.
JP27476184A 1984-12-28 1984-12-28 Rear face supporting device for antenna reflecting mirror Granted JPS61157004A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP27476184A JPS61157004A (en) 1984-12-28 1984-12-28 Rear face supporting device for antenna reflecting mirror

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP27476184A JPS61157004A (en) 1984-12-28 1984-12-28 Rear face supporting device for antenna reflecting mirror

Publications (2)

Publication Number Publication Date
JPS61157004A JPS61157004A (en) 1986-07-16
JPH0422362B2 true JPH0422362B2 (en) 1992-04-16

Family

ID=17546208

Family Applications (1)

Application Number Title Priority Date Filing Date
JP27476184A Granted JPS61157004A (en) 1984-12-28 1984-12-28 Rear face supporting device for antenna reflecting mirror

Country Status (1)

Country Link
JP (1) JPS61157004A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110290388A1 (en) * 2006-07-13 2011-12-01 Radulescu Robert C Tire with side features for resisting irregular shoulder wear
CN102099637B (en) 2008-06-06 2016-10-19 日出Csp股份有限公司 Improvement of Solar Thermal Collector

Also Published As

Publication number Publication date
JPS61157004A (en) 1986-07-16

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