JP2001153576A - Carbon fiber skin heat pipe panel and heat pipe - Google Patents
Carbon fiber skin heat pipe panel and heat pipeInfo
- Publication number
- JP2001153576A JP2001153576A JP33128799A JP33128799A JP2001153576A JP 2001153576 A JP2001153576 A JP 2001153576A JP 33128799 A JP33128799 A JP 33128799A JP 33128799 A JP33128799 A JP 33128799A JP 2001153576 A JP2001153576 A JP 2001153576A
- Authority
- JP
- Japan
- Prior art keywords
- heat pipe
- carbon fiber
- skin
- panel
- fiber skin
- 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.)
- Pending
Links
Landscapes
- Laminated Bodies (AREA)
Abstract
Description
【0001】[0001]
【発明の属する技術分野】この発明は、例えば人工衛星
を構成する構体パネルの一部として使用される炭素繊維
表皮ヒートパイプパネルに関するものである。人工衛星
は通常このような複数のサンドイッチ構造体のパネルか
ら構成されており、なかでも炭素繊維表皮ヒートパイプ
パネルは、送信用の電力増幅器などの特に高発熱機器が
取り付けられるパネルとして使用されている。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a carbon fiber skin heat pipe panel used, for example, as a part of a structural panel constituting an artificial satellite. Satellites usually consist of a plurality of such sandwich-structured panels, of which carbon fiber skin heat pipe panels are used as panels to which particularly high heat-generating equipment such as power amplifiers for transmission are attached. .
【0002】[0002]
【従来の技術】図2は一般的な炭素繊維表皮ヒートパイ
プパネルを示すもので、1はインナ表皮(人工衛星構体
内面側)、2はアウタ表皮(人工衛星外面側)、3はヒ
ートパイプ、4はハニカムコアである。炭素繊維表皮ヒ
ートパイプパネルは、金属性のヒートパイプと表皮材の
炭素繊維の熱膨張係数の差によって生じる熱応力による
破壊を防ぐため、ヒートパイプと表皮の間に可とう性5
の接着剤を、他の部分にはより接着強度が高い構造用接
着剤6を使用するのが一般的である。2. Description of the Related Art FIG. 2 shows a typical carbon fiber skin heat pipe panel, wherein 1 is an inner skin (on the inner surface of the artificial satellite), 2 is an outer skin (the outer surface of the artificial satellite), and 3 is a heat pipe. 4 is a honeycomb core. The carbon fiber skin heat pipe panel is made of a flexible material between the heat pipe and the skin in order to prevent breakage due to thermal stress caused by a difference in thermal expansion coefficient between the metal heat pipe and the skin material carbon fiber.
In general, the structural adhesive 6 having higher adhesive strength is used for the other parts.
【0003】[0003]
【発明が解決しようとする課題】しかしながら、可とう
性接着剤の接着強度は他の構造用接着剤と比較すると強
度的に劣るため、ヒートパイプとインナ表皮、及びヒー
トパイプとアウタ表皮の接着に限定して使用するのが一
般的である。また、例えば、ヒートパイプがパネルの面
内で湾曲部を持っている場合などの理由で、表皮とヒー
トパイプの線膨張係数の差による熱応力がその部分の表
皮に集中することによって表皮に座屈が生じる可能性が
高くなるため、そのようなヒートパイプをパネルに埋め
込む際には、ヒートパイプと表皮間を接着する可とう性
接着剤の接着層を厚くせざるを得なかった。しかしなが
ら、可とう性接着剤を厚くした場合は、ヒートパイプと
表皮間の熱伝導率が低下するため、炭素繊維表皮ヒート
パイプパネル本来の熱的な性能が低下すると共に、構造
用接着剤に比べ接着力が弱い可とう性接着剤の接着層が
厚くなるため、構造的な強度も低下することとなってし
まう。However, since the adhesive strength of the flexible adhesive is inferior to other structural adhesives in terms of strength, it is difficult to bond the heat pipe to the inner skin and the heat pipe to the outer skin. It is common to use it in a limited manner. In addition, for example, when the heat pipe has a curved portion in the plane of the panel, thermal stress due to the difference in linear expansion coefficient between the skin and the heat pipe concentrates on the skin in that part, so that the seat is seated on the skin. When such a heat pipe is embedded in a panel, the adhesive layer of a flexible adhesive for bonding between the heat pipe and the skin must be thickened because the possibility of bending is increased. However, when the thickness of the flexible adhesive is increased, the thermal conductivity between the heat pipe and the skin is reduced, so the thermal performance inherent in the carbon fiber skin heat pipe panel is reduced, and compared with the structural adhesive. Since the adhesive layer of the flexible adhesive having a weak adhesive force becomes thick, the structural strength is also reduced.
【0004】この発明はかかる課題を解決するためにな
されたものであり、表皮との間に熱応力が発生すると予
想される部分のみヒートパイプを薄く加工することによ
って、必要な場所のみ表皮とヒートパイプの間の接着に
使用する可とう性接着剤の接着層を厚くすることができ
る。また、この場合、他の部分の可とう性接着剤の接着
層の厚さが厚くなることはないため、従来と比較して熱
的性能及び構造的強度が高い炭素繊維表皮ヒートパイプ
パネルを提供するものである。SUMMARY OF THE INVENTION The present invention has been made to solve such a problem, and a heat pipe is thinned only at a portion where thermal stress is expected to occur between the heat pipe and the skin, so that the heat pipe is heated only at a necessary place. The thickness of the adhesive layer of the flexible adhesive used for bonding between pipes can be increased. Further, in this case, since the thickness of the adhesive layer of the flexible adhesive in other portions does not increase, a carbon fiber skin heat pipe panel having higher thermal performance and structural strength than the conventional one is provided. Is what you do.
【0005】[0005]
【課題を解決するための手段】この発明は、表皮と接着
した場合に大きな熱応力が発生する部分のヒートパイプ
に段差を設けたものである。According to the present invention, a step is provided in a portion of a heat pipe where a large thermal stress is generated when the heat pipe is bonded to a skin.
【0006】[0006]
【発明の実施の形態】実施の形態1.図1は、この発明
の実施形態1を示す炭素繊維表皮ヒートパイプパネル用
ヒートパイプの模式図である。図1により詳細を説明す
る。(a)に示すように、表皮1,2との接着部に大き
な熱応力が発生するヒートパイプ3に段差7加工を行な
うことによって、(b)に示すように、ヒートパイプ3
の他の部分と表皮1,2間の接着層厚さを増やさずに炭
素繊維表皮ヒートパイプパネルを構造することができ
る。DESCRIPTION OF THE PREFERRED EMBODIMENTS Embodiment 1 FIG. 1 is a schematic diagram of a heat pipe for a carbon fiber skin heat pipe panel showing Embodiment 1 of the present invention. Details will be described with reference to FIG. As shown in (a), a step 7 is formed on the heat pipe 3 in which a large thermal stress is generated at a bonding portion between the heat pipe 3 and the skin 1, 2 as shown in (b).
The carbon fiber skin heat pipe panel can be structured without increasing the thickness of the adhesive layer between the other parts and the skins 1 and 2.
【0007】[0007]
【発明の効果】この発明によれば、熱応力が集中する部
分のみ可とう性接着剤の接着層を厚くすることができる
ため、従来の炭素繊維表皮ヒートパイプパネルと比較し
て熱的性能と構造的強度が高い炭素繊維表皮ヒートパイ
プパネルを製造することができる。According to the present invention, the adhesive layer of the flexible adhesive can be thickened only in the portion where the thermal stress is concentrated, so that the thermal performance and the heat performance can be improved as compared with the conventional carbon fiber skin heat pipe panel. A carbon fiber skin heat pipe panel having high structural strength can be manufactured.
【図1】 この発明による実施形態1を示す図である。FIG. 1 is a diagram showing a first embodiment according to the present invention.
【図2】 一般的な炭素繊維表皮ヒートパイプパネルの
模式図である。FIG. 2 is a schematic view of a general carbon fiber skin heat pipe panel.
1 インナ表皮、2 アウタ表皮、3 ヒートパイプ、
4 ハニカムコア、5構造用接着剤、6 可とう性接着
剤、7 段差。1 inner skin, 2 outer skin, 3 heat pipes,
4 Honeycomb core, 5 structural adhesive, 6 flexible adhesive, 7 steps.
Claims (2)
およびハニカムコアを挟み込み構成するサンドイッチ構
造体の炭素繊維表皮ヒートパイプパネルにおいて、表皮
とヒートパイプの線膨張係数の差による熱応力が集中す
る部分の表皮の下のヒートパイプの一部に段差を設ける
ことを特徴とする炭素繊維表皮ヒートパイプパネル。In a carbon fiber skin heat pipe panel having a sandwich structure in which a heat pipe and a honeycomb core are sandwiched between an inner skin and an outer skin, a portion where thermal stress due to a difference in linear expansion coefficient between the skin and the heat pipe is concentrated. A carbon fiber skin heat pipe panel, wherein a step is provided in a part of the heat pipe below the skin.
生する部分のみ薄くしてあることを特徴とするヒートパ
イプ。2. A heat pipe characterized in that only a portion where thermal stress is generated between the heat pipe and the skin of the heat pipe is thinned.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP33128799A JP2001153576A (en) | 1999-11-22 | 1999-11-22 | Carbon fiber skin heat pipe panel and heat pipe |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP33128799A JP2001153576A (en) | 1999-11-22 | 1999-11-22 | Carbon fiber skin heat pipe panel and heat pipe |
Publications (1)
Publication Number | Publication Date |
---|---|
JP2001153576A true JP2001153576A (en) | 2001-06-08 |
Family
ID=18242010
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP33128799A Pending JP2001153576A (en) | 1999-11-22 | 1999-11-22 | Carbon fiber skin heat pipe panel and heat pipe |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2001153576A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10340092A1 (en) * | 2003-08-30 | 2005-05-04 | Ohb Orbitale Hochtechnologie B | Radiator with sandwich structure for use in satellites, includes integral loop heat pipe comprising flanged aluminum profiles |
DE102005039783B3 (en) * | 2005-08-22 | 2007-03-22 | Orbitale Hochtechnologie Bremen-System Ag | Sandwich structure with resin-embedded carbon fiber-reinforced layers and integrated metal tube, useful e.g. in spacecraft, has thermal and structural optimization sandwich layers with differently oriented fibers |
DE102006025733B4 (en) * | 2006-05-31 | 2010-09-02 | Orbitale Hochtechnologie Bremen-System Ag | Reduction of the thermal expansion coefficient in metallic heat pipes |
-
1999
- 1999-11-22 JP JP33128799A patent/JP2001153576A/en active Pending
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10340092A1 (en) * | 2003-08-30 | 2005-05-04 | Ohb Orbitale Hochtechnologie B | Radiator with sandwich structure for use in satellites, includes integral loop heat pipe comprising flanged aluminum profiles |
DE10340092B4 (en) * | 2003-08-30 | 2005-09-01 | Ohb Orbitale Hochtechnologie Bremen--System Ag | Sandwich structure with carbon fiber reinforced facings and integrated metallic condensing tubes |
DE102005039783B3 (en) * | 2005-08-22 | 2007-03-22 | Orbitale Hochtechnologie Bremen-System Ag | Sandwich structure with resin-embedded carbon fiber-reinforced layers and integrated metal tube, useful e.g. in spacecraft, has thermal and structural optimization sandwich layers with differently oriented fibers |
DE102006025733B4 (en) * | 2006-05-31 | 2010-09-02 | Orbitale Hochtechnologie Bremen-System Ag | Reduction of the thermal expansion coefficient in metallic heat pipes |
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