JP2005217696A - Membrane reflector and manufacturing method thereof - Google Patents

Membrane reflector and manufacturing method thereof Download PDF

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JP2005217696A
JP2005217696A JP2004020881A JP2004020881A JP2005217696A JP 2005217696 A JP2005217696 A JP 2005217696A JP 2004020881 A JP2004020881 A JP 2004020881A JP 2004020881 A JP2004020881 A JP 2004020881A JP 2005217696 A JP2005217696 A JP 2005217696A
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reflector
membrane
mirror surface
membrane reflector
coupling component
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Hiroyuki Shigemasa
裕之 重政
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Mitsubishi Electric Corp
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Abstract

<P>PROBLEM TO BE SOLVED: To provide a membrane reflector for an artificial satellite giving less effect on the mirror surface accuracy due to a temperature change and needing less number of components. <P>SOLUTION: The membrane reflector for mount on the artificial satellite includes: the membrane reflector; a coupling component 3 formed to be a closed shape adhered to a rear side of the membrane reflector; and a rear face structure 2 of the membrane reflector inserted and located to the coupling component 3 perpendicularly to the rear side of the membrane reflector. Thus, the effect on the mirror surface accuracy due to a temperature change is reduced and the number of coupling components is decreased. <P>COPYRIGHT: (C)2005,JPO&NCIPI

Description

この発明は、人工衛星に搭載するメンブレンリフレクタの構造およびその製造方法に関するものである。   The present invention relates to a structure of a membrane reflector mounted on an artificial satellite and a manufacturing method thereof.

現在、人工衛星に搭載されているリフレクタについては各種の方式があることは周知のところである。   It is well known that there are various types of reflectors currently mounted on artificial satellites.

このような各種のリフレクタの中に軽量化を目的とし鏡面部に強化繊維による2軸または3軸織物を強化材とする複合材料からなる薄板状の面を反射鏡面として持つメンブレンリフレクタがあり、その背面構造部分と鏡面部分の結合方法についてはL字型、箱型や円筒状部品と板の組み合わせの部品が知られている(例えば、特許文献1参照。)。   Among these various reflectors, there is a membrane reflector that has a thin plate-like surface made of a composite material with a biaxial or triaxial woven fabric made of reinforcing fibers as a reinforcing material for the purpose of weight reduction. As a method for connecting the back structure portion and the mirror surface portion, L-shaped, box-shaped, or a combination of a cylindrical component and a plate is known (for example, see Patent Document 1).

特開平10−270922号公報(第1−3図、第7図)Japanese Patent Laid-Open No. 10-270922 (FIGS. 1-3 and 7)

最近の通信容量の増大によるリフレクタの高周波数化やリフレクタに対するコスト削減要求により、より簡易に、かつ、高周波数に対応できる構造様式のメンブレンリフレクタが要求されてきているが、従来のメンブレンリフレクタでは安価なL字型の部品か、高価な箱型や円筒状部品と板の組み合わせ部品を用いて背面構造と鏡面を結合している。特許文献1に記載のように積層複合材料製のL字型部品はその面内方向と面外方向の熱膨張係数が異なるため、温度変化によってその角度が変化し、リフレクタの鏡面精度を劣化させる懸念があり、箱型や円筒状部品と板の組み合わせ部品による結合は部品点数が増るという問題点があった。   Due to the recent trend to increase the frequency of reflectors due to the increase in communication capacity and cost reduction requirements for reflectors, there has been a demand for membrane reflectors that are simpler and can handle high frequencies. However, conventional membrane reflectors are inexpensive. The back structure and the mirror surface are combined using a large L-shaped part or an expensive box-shaped or cylindrical part-plate combination part. As described in Patent Document 1, an L-shaped component made of a laminated composite material has different coefficients of thermal expansion in the in-plane direction and in the out-of-plane direction, so that the angle changes due to a temperature change and deteriorates the mirror surface accuracy of the reflector. There is a concern, and there is a problem that the number of parts increases when the box or cylindrical part is combined with the combination part of the plate.

この発明は、係る課題を解決するために成されたものであり、メンブレンリフレクタの鏡面部分と背面構造部分の結合を安価に、かつ、温度変化に対してリフレクタ鏡面精度への影響が少ないように結合することを目的としており、さらに、この結合部品をより安価に製造する方法を提供することを目的としている。   The present invention has been made to solve the above-described problems, and is intended to reduce the influence on the mirror accuracy of the reflector with respect to temperature changes at a low cost by combining the mirror surface portion and the back structure portion of the membrane reflector. It aims at joining, and also aims at providing the method of manufacturing this joining component cheaply.

この発明のメンブレンリフレクタは、人工衛星搭載用のメンブレンリフレクタにおいて、反射鏡面を有する反射鏡面部と、閉曲面形状を成す樹脂または金属板で形成され、当該閉曲面の一部が、上記反射鏡面部における反射鏡面の裏面側に接着された複数の結合部品と、上記反射鏡面部の裏面側に配置され、上記それぞれの結合部品における上記閉曲面の一部と対向する他の面の側で接着されて、上記反射鏡面部を支持する背面構造とを備えたものである。   The membrane reflector of the present invention is a membrane reflector for an artificial satellite, and is formed of a reflecting mirror surface portion having a reflecting mirror surface and a resin or metal plate having a closed curved surface shape, and a part of the closed curved surface is formed by the reflecting mirror surface portion. A plurality of coupling parts bonded to the back surface side of the reflecting mirror surface, and disposed on the back surface side of the reflecting mirror surface portion, and bonded to the other surface side facing a part of the closed curved surface in each of the coupling components. And a back surface structure that supports the reflecting mirror surface portion.

この発明のメンブレンリフレクタの製造方法は、メンブレンリフレクタ鏡面の成形型の上に離型性のあるフィルムを敷き、その上に未硬化の樹脂を含浸させたクロス材をセットする第1の工程と、未硬化の樹脂を含浸させたクロス材の上に表面を離型処理した成形型をセットし、その上に背面構造をセットする第2の工程と、成形型を包むように、未硬化の樹脂を含浸させたクロス材を持ち上げ、背面構造に接着し、硬化後に成形型を抜き取る第3の工程と、背面構造と一体化している結合部品と鏡面部の間に接着剤の塗布し、接着する第4の工程とから成るものである。   The manufacturing method of the membrane reflector of the present invention includes a first step of setting a cloth material in which a film having releasability is laid on a mold for the mirror reflector mirror surface and impregnated with an uncured resin thereon, A second step of setting a mold having a surface release treatment on a cloth material impregnated with an uncured resin, and setting a back structure on the mold, and an uncured resin to wrap the mold Lifting the impregnated cloth material, adhering it to the back structure, removing the mold after curing, applying the adhesive between the connecting part integrated with the back structure and the mirror surface part, and adhering 4 steps.

この発明の閉じた形状の結合部品によっては、その部品の面内方向と面外方向の熱膨張係数に差があっても温度変化による形状変化が少なく、メンブレンリフレクタが温度が変動した場合においてもその背面構造と鏡面部の関係を狂わすことなく結合させることができるので、安価で、かつ、温度変化に対してリフレクタ鏡面精度への影響が少ないように結合することができるという効果がある。   Depending on the closed shape coupling component of this invention, even if there is a difference in the thermal expansion coefficient between the in-plane direction and the out-of-plane direction of the component, there is little change in shape due to temperature change, and even when the temperature of the membrane reflector fluctuates. Since the back surface structure and the mirror surface portion can be coupled without deviating from each other, there is an effect that the coupling can be performed at low cost and with little influence on the reflector mirror surface accuracy with respect to temperature change.

実施の形態1.
図1はこの発明の実施の形態1を説明するための図であり、図1(a)は実施の形態1によるメンブレンリフレクタの鏡面部と背面構造の結合部分を示すもの、図1(b)および図1(c)はリフレクタの異なる位置での結合部の断面図を示すものである。
図1において、メンブレンリフレクタの鏡面部1が背面構造2に閉じた形状の結合部品3で結合されている。
Embodiment 1 FIG.
FIG. 1 is a diagram for explaining Embodiment 1 of the present invention, and FIG. 1 (a) shows a connecting portion between a mirror surface portion and a back surface structure of a membrane reflector according to Embodiment 1, FIG. 1 (b). And FIG.1 (c) shows sectional drawing of the coupling | bond part in a different position of a reflector.
In FIG. 1, the mirror surface portion 1 of the membrane reflector is coupled to the back structure 2 by a coupling component 3 having a closed shape.

このように閉じた形状の結合部品においては、その部品のメンブレンリフレクタの鏡面部1に平行な方向である面内方向とメンブレンリフレクタの鏡面部1に垂直な方向である面外方向の熱膨張係数に差があっても温度変化による形状変化が少ない。従ってメンブレンリフレクタが温度が変動した場合においてもその背面構造と鏡面部の関係を狂わすことなく結合させることができる。ここで、面内方向の熱膨張係数は0〜3ppm程度、面外方向の熱膨張係数は20〜60ppm程度である。よって、温度変化により、結合部品の面内方向と面外方向での熱膨張の相違により歪みが発生するので、背面構造と鏡面部がリジットに構成されている場合はメンブレンリフレクタの鏡面部1に歪みを生じることに成るが、本発明のように結合部品にバネ性を有すると歪みを吸収できる。   In such a closed joint component, the thermal expansion coefficient in the in-plane direction that is parallel to the mirror surface portion 1 of the membrane reflector and in the out-of-plane direction that is perpendicular to the mirror surface portion 1 of the membrane reflector. Even if there is a difference, there is little shape change due to temperature change. Therefore, even when the temperature of the membrane reflector fluctuates, the membrane reflector can be coupled without upsetting the relationship between the back surface structure and the mirror surface portion. Here, the thermal expansion coefficient in the in-plane direction is about 0 to 3 ppm, and the thermal expansion coefficient in the out-of-plane direction is about 20 to 60 ppm. Therefore, distortion occurs due to the difference in thermal expansion between the in-plane direction and the out-of-plane direction of the coupling component due to the temperature change. Therefore, when the back structure and the mirror surface portion are configured to be rigid, the mirror surface portion 1 of the membrane reflector Although distortion will occur, the distortion can be absorbed if the coupling component has springiness as in the present invention.

また、この結合部品は樹脂で成型して製作され、背面構造の両側を一つの部品で構成しているため、従来のL字型結合部品や箱型や円筒状部品と板の組み合わせ部品による結合部品に比べて部品点数が少なく低コストで製作することができる。   In addition, this joining part is manufactured by molding with resin, and both sides of the back structure are composed of one part, so it can be joined by conventional L-shaped joining parts or combination parts of box-shaped or cylindrical parts and plates Compared to parts, it has fewer parts and can be manufactured at lower cost.

実施の形態2.
図2は実施の形態2によるメンブレンリフレクタの鏡面部と背面構造の結合部分を示すものである。
図2において、メンブレンリフレクタの鏡面部1が背面構造2に閉じた形状の結合部品3で結合されている。
Embodiment 2. FIG.
FIG. 2 shows a joint portion between the mirror surface portion and the back surface structure of the membrane reflector according to the second embodiment.
In FIG. 2, the mirror surface portion 1 of the membrane reflector is coupled to the back structure 2 by a coupling component 3 having a closed shape.

このように閉じた形状の結合部品においては、その部品のメンブレンリフレクタの鏡面部1に平行な方向である面内方向とメンブレンリフレクタの鏡面部1に垂直な方向である面外方向の熱膨張係数に差があっても温度変化による形状変化が少ない。従ってメンブレンリフレクタが温度が変動した場合においてもその背面構造と鏡面部の関係を狂わすことなく結合させることができる。ここで、面内方向の熱膨張係数は0〜3ppm程度、面外方向の熱膨張係数は20〜60ppm程度である。   In such a closed joint component, the thermal expansion coefficient in the in-plane direction that is parallel to the mirror surface portion 1 of the membrane reflector and in the out-of-plane direction that is perpendicular to the mirror surface portion 1 of the membrane reflector. Even if there is a difference, there is little shape change due to temperature change. Therefore, even when the temperature of the membrane reflector fluctuates, the membrane reflector can be coupled without upsetting the relationship between the back surface structure and the mirror surface portion. Here, the thermal expansion coefficient in the in-plane direction is about 0 to 3 ppm, and the thermal expansion coefficient in the out-of-plane direction is about 20 to 60 ppm.

また、この結合部品は背面構造の両側を一つの部品で構成し、かつ、鏡面部に対する接着面積の小さな結合部品においては、鏡面部と背面構造との為す角度に依存せず同一の部品となるため、従来のL字型結合部品や箱型や円筒状部品と板の組み合わせ部品による結合部品に比べて部品点数が少なく低コストで製作することができる。   In addition, this connecting part is composed of one part on both sides of the back structure, and in a connecting part having a small adhesion area to the mirror surface part, it is the same part regardless of the angle between the mirror surface part and the back structure. Therefore, the number of parts can be reduced and the manufacturing cost can be reduced as compared with the conventional L-shaped connecting parts, box-shaped parts, and connecting parts made of a combination of cylindrical parts and plates.

実施の形態3.
図3は、閉じた形状の結合部材を未硬化の樹脂をクロス材に含浸させて成形している製造工程を示すものである。
(イ)第1工程(図3(a)参照):メンブレンリフレクタ鏡面の成形型4の上に離型性のあるフィルム5を敷き、その上に未硬化の樹脂を含浸させたクロス材6をセットする。
(ロ)第2工程(図3(b)参照):未硬化の樹脂を含浸させたクロス材6の上に表面を離型処理した成形型7をセットし、その上に背面構造2をセットする。
(ハ)第3工程(図3(c)参照):成形型7を包むように、未硬化の樹脂を含浸させたクロス材6を持ち上げ、背面構造に接着し、硬化後に成形型を奥行き方向から抜き取る。
(ニ)第4工程(図3(d)参照):背面構造と一体化している結合部品と鏡面部の間に接着剤8の塗布し、接着する。
Embodiment 3 FIG.
FIG. 3 shows a manufacturing process in which a coupling member having a closed shape is molded by impregnating an uncured resin with a cloth material.
(A) First step (see FIG. 3 (a)): a film 5 having releasability is laid on a mold 4 on the mirror reflector mirror surface, and a cloth material 6 impregnated with an uncured resin is placed thereon. set.
(B) Second step (see FIG. 3 (b)): A molding die 7 whose surface is subjected to mold release treatment is set on a cloth material 6 impregnated with uncured resin, and a back structure 2 is set thereon. To do.
(C) Third step (see FIG. 3 (c)): Lift the cloth material 6 impregnated with uncured resin so as to wrap the molding die 7, adhere to the back structure, and after curing, remove the molding die from the depth direction. Pull out.
(D) Fourth step (see FIG. 3 (d)): Adhesive 8 is applied and bonded between the coupling part integrated with the back structure and the mirror surface part.

上記のような結合部材の製造方法によれば、背面構造と鏡面部とがなす角度がリフレクタの各場所によって異なっていようとも、同一の成形型を使用して結合部材を安価に製造することが出来る。   According to the manufacturing method of the coupling member as described above, the coupling member can be manufactured at low cost using the same mold even if the angle formed by the back surface structure and the mirror surface portion varies depending on each location of the reflector. I can do it.

この発明の実施の形態1を説明するための図である。It is a figure for demonstrating Embodiment 1 of this invention. この発明の実施の形態2を説明するための図である。It is a figure for demonstrating Embodiment 2 of this invention. この発明の実施の形態3を説明するための図である。It is a figure for demonstrating Embodiment 3 of this invention.

符号の説明Explanation of symbols

1 メンブレンリフレクタ鏡面部、 2 メンブレンリフレクタ背面構造、 3 結合部品、 4 メンブレンリフレクタ鏡面成形型、 5 離型性のあるフィルム、 6 未硬化の樹脂を含浸させたクロス材、 7 結合部品用の成形型、 8 結合部品とメンブレンリフレクタ鏡面を結合する接着剤。   DESCRIPTION OF SYMBOLS 1 Membrane reflector mirror surface part, 2 Membrane reflector back structure, 3 Joining parts, 4 Membrane reflector mirror molding mold, 5 Releasable film, 6 Cross material impregnated with uncured resin, 7 Mold for joining parts , 8 Adhesive that joins the coupling part and the mirror reflector mirror surface.

Claims (7)

人工衛星搭載用のメンブレンリフレクタにおいて、
反射鏡面を有する反射鏡面部と、
閉曲面形状を成す樹脂または金属板で形成され、当該閉曲面の一部が、上記反射鏡面部における反射鏡面の裏面側に接着された複数の結合部品と、
上記反射鏡面部の裏面側に配置され、上記それぞれの結合部品における上記閉曲面の一部と対向する他の面の側で接着されて、上記反射鏡面部を支持する背面構造と
を備えたメンブレンリフレクタ。
In membrane reflectors for satellite installations,
A reflecting mirror surface portion having a reflecting mirror surface;
A plurality of coupling parts formed of a resin or metal plate having a closed curved surface shape, and a part of the closed curved surface bonded to the back surface side of the reflecting mirror surface in the reflecting mirror surface portion;
A membrane provided on the back surface side of the reflecting mirror surface portion and bonded to the other surface facing the part of the closed curved surface in each of the coupling parts, and a back surface structure for supporting the reflecting mirror surface portion Reflector.
上記結合部品は、上記閉曲面の一部における、上記反射鏡面部との接合面に垂直な方向と面方向にばね性を有し、上記閉曲面における他の面に開口部を有し、当該開口部に上記背面構造が挿入されて固定されることを特徴とする請求項1記載のメンブレンリフレクタ。 The coupling component has a spring property in a direction perpendicular to the joint surface with the reflecting mirror surface portion and a surface direction in a part of the closed curved surface, and has an opening in the other surface of the closed curved surface, 2. The membrane reflector according to claim 1, wherein the back structure is inserted into and fixed to the opening. 上記結合部品が複合材料製であることを特徴とする請求項2記載のメンブレンリフレクタ。 The membrane reflector according to claim 2, wherein the coupling component is made of a composite material. 上記結合部品がバネ性の在る袋状であることを特徴とする請求項2記載のメンブレンリフレクタ。 3. The membrane reflector according to claim 2, wherein the coupling component is a bag having a spring property. 上記結合部品と上記メンブレンリフレクタの裏面及び上記結合部品とメンブレンリフレクタの背面構造の間の一部あるいは全てが接着で結合されていることを特徴とする請求項1〜請求項4のいづれか1項に記載のメンブレンリフレクタ。 5. The structure according to claim 1, wherein a part or all of the coupling component and the back surface of the membrane reflector and a part or all of the coupling component and the back surface structure of the membrane reflector are bonded together. The membrane reflector described. 上記結合部品と上記メンブレンリフレクタの裏面の間に一定の間隙が在り、上記結合部品とメンブレンリフレクタの背面構造の間の隙間が極力小さいことを特徴とする請求項1〜請求項5のいづれか1項に記載のメンブレンリフレクタ。 6. A device according to claim 1, wherein there is a certain gap between the coupling component and the back surface of the membrane reflector, and the gap between the coupling component and the back surface structure of the membrane reflector is as small as possible. The membrane reflector described in 1. メンブレンリフレクタ鏡面の成形型の上に離型性のあるフィルムを敷き、その上に未硬化の樹脂を含浸させたクロス材をセットする第1の工程と、
未硬化の樹脂を含浸させたクロス材の上に表面を離型処理した成形型をセットし、その上に背面構造をセットする第2の工程と、
成形型を包むように、未硬化の樹脂を含浸させたクロス材を持ち上げ、背面構造に接着し、硬化後に成形型を抜き取る第3の工程と、
背面構造と一体化している結合部品と鏡面部の間に接着剤の塗布し、接着する第4の工程と
から成ることを特徴とするメンブレンリフレクタの製造方法。
A first step in which a film having releasability is laid on the mold of the mirror reflector mirror surface, and a cloth material impregnated with an uncured resin is set thereon;
A second step of setting a mold having a surface release treatment on a cloth material impregnated with an uncured resin, and setting a back structure thereon;
A third step of lifting the cloth material impregnated with uncured resin so as to wrap the mold, adhering it to the back structure, and extracting the mold after curing;
A method of manufacturing a membrane reflector, comprising: a fourth step of applying and bonding an adhesive between a connecting part integrated with a back structure and a mirror surface portion.
JP2004020881A 2004-01-29 2004-01-29 Membrane reflector and manufacturing method thereof Pending JP2005217696A (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010016747A (en) * 2008-07-07 2010-01-21 Mitsubishi Electric Corp Membrane reflector and method of manufacturing the same
JP2014195233A (en) * 2013-03-29 2014-10-09 Mitsubishi Electric Corp Antenna reflector, and method of manufacturing the same
EP4223649A1 (en) * 2022-02-02 2023-08-09 Deutsches Zentrum für Luft- und Raumfahrt e.V. Spacecraft membrane coupling device and spacecraft membrane unit

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010016747A (en) * 2008-07-07 2010-01-21 Mitsubishi Electric Corp Membrane reflector and method of manufacturing the same
JP2014195233A (en) * 2013-03-29 2014-10-09 Mitsubishi Electric Corp Antenna reflector, and method of manufacturing the same
EP4223649A1 (en) * 2022-02-02 2023-08-09 Deutsches Zentrum für Luft- und Raumfahrt e.V. Spacecraft membrane coupling device and spacecraft membrane unit

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