JPH0710097A - Equipment mounting structure for artificial satellite - Google Patents
Equipment mounting structure for artificial satelliteInfo
- Publication number
- JPH0710097A JPH0710097A JP5155285A JP15528593A JPH0710097A JP H0710097 A JPH0710097 A JP H0710097A JP 5155285 A JP5155285 A JP 5155285A JP 15528593 A JP15528593 A JP 15528593A JP H0710097 A JPH0710097 A JP H0710097A
- Authority
- JP
- Japan
- Prior art keywords
- panel
- heat pipe
- mounting structure
- artificial satellite
- equipment
- 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.)
- Granted
Links
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
Landscapes
- Non-Reversible Transmitting Devices (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明は、人工衛星の機器実装構
造に関し、特に機器配置設計を容易にする機器実装構造
に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a device mounting structure for an artificial satellite, and more particularly to a device mounting structure that facilitates device layout design.
【0002】[0002]
【従来の技術】従来、人工衛星の機器実装構造は、単一
パネル面上に機器,導波管,同軸ケーブル,ハーネスが
実装されている。また、パネル内にヒートパイプが実装
されている。2. Description of the Related Art Conventionally, in a device mounting structure of an artificial satellite, a device, a waveguide, a coaxial cable and a harness are mounted on a single panel surface. Also, a heat pipe is mounted in the panel.
【0003】図2は、従来の人工衛星の機器実装構造の
一例を示す分解斜視図である。高発熱機器はヒートパイ
プが設けられた機器パネル1および2に搭載され、低発
熱機器はヒートパイプを必要としない機器パネル3に搭
載される。FIG. 2 is an exploded perspective view showing an example of a conventional artificial satellite device mounting structure. The high heat generating device is mounted on the device panels 1 and 2 provided with the heat pipe, and the low heat generating device is mounted on the device panel 3 which does not require the heat pipe.
【0004】機器パネル面上に搭載されている機器4間
を接続するための導波管5,同軸ケーブル6,ハーネス
7も同一面上に配置されている。A waveguide 5, a coaxial cable 6 and a harness 7 for connecting the devices 4 mounted on the device panel surface are also arranged on the same surface.
【0005】また、機器パネル1および2において機器
の発する熱を排熱するため、パネル内にヒートパイプ9
が埋め込まれており、パネル内に熱を分散させ、宇宙空
間へ放出するようになっている。Further, in order to exhaust the heat generated by the devices in the device panels 1 and 2, the heat pipe 9 is provided in the panels.
Is embedded in the panel to dissipate the heat and release it into outer space.
【0006】[0006]
【発明が解決しようとする課題】この従来の人工衛星の
機器実装構造は、機器,導波管,同軸ケーブル,ハーネ
ス,ヒートパイプが同一パネル面上に配置されるため、
機器,導波管,ハーネスをパネルに取り付けるねじ位置
とヒートパイプとの干渉や、同軸ケーブルルートとハー
ネスルートとの干渉が問題となり、機器配置とヒートパ
イプの設計,同軸ケーブルとハーネスルートの設計が並
行して進められなかった。In the conventional equipment mounting structure of the artificial satellite, since the equipment, the waveguide, the coaxial cable, the harness, and the heat pipe are arranged on the same panel surface,
Interference between the screw position where the equipment, waveguide, and harness are attached to the panel and the heat pipe, and interference between the coaxial cable route and the harness route become problems. I could not proceed in parallel.
【0007】本発明の目的は、パネルに実装される機
器,導波管,同軸ケーブル,ハーネス,ヒートパイプの
配置設計を容易にする機器実装構造を提供することにあ
る。An object of the present invention is to provide a device mounting structure that facilitates the layout design of devices mounted on a panel, a waveguide, a coaxial cable, a harness, and a heat pipe.
【0008】[0008]
【課題を解決するための手段】本発明は、パネル上に、
機器,導波管,同軸ケーブル,ハーネス,ヒートパイプ
を実装する人工衛星の機器実装構造において、ヒートパ
イプ専用のパネルを外側に設け、内側のパネル両面に、
機器,導波管,同軸ケーブル,ハーネスを実装すること
を特徴とする。SUMMARY OF THE INVENTION The present invention provides a panel with:
In the equipment mounting structure of the artificial satellite that mounts equipment, waveguide, coaxial cable, harness, and heat pipe, a panel dedicated to the heat pipe is provided on the outside and both sides of the inner panel are
It is characterized by mounting devices, waveguides, coaxial cables, and harnesses.
【0009】[0009]
【作用】本発明の人工衛星の機器実装構造では、ヒート
パイプを実装するパネルを別に設け、機器,導波管,同
軸ケーブルおよびハーネスとの干渉を避けている。ま
た、従来パネルの片面に実装していた機器,導波管,同
軸ケーブル,ハーネスを両面に実装する。例えば、片面
に機器とハーネスを実装し、他方の面に導波管と同軸ケ
ーブルを実装することにより、同軸ケーブルとハーネス
との干渉を避けている。In the device mounting structure of the artificial satellite of the present invention, a panel for mounting the heat pipe is separately provided to avoid interference with the device, the waveguide, the coaxial cable and the harness. Also, the equipment, waveguide, coaxial cable, and harness that were conventionally mounted on one side of the panel are mounted on both sides. For example, the equipment and the harness are mounted on one surface, and the waveguide and the coaxial cable are mounted on the other surface to avoid interference between the coaxial cable and the harness.
【0010】[0010]
【実施例】次に、本発明の実施例について図面を参照し
て説明する。Embodiments of the present invention will now be described with reference to the drawings.
【0011】図1は、本発明の一実施例を示す分解斜視
図である。本実施例の機器実装構造では、機器パネル1
および2の内面に、機器4とハーネス7だけを実装す
る。機器パネル1および2の外面に、導波管5と同軸ケ
ーブル6だけを実装する。FIG. 1 is an exploded perspective view showing an embodiment of the present invention. In the device mounting structure of this embodiment, the device panel 1
Only the device 4 and the harness 7 are mounted on the inner surfaces of and 2. Only the waveguide 5 and the coaxial cable 6 are mounted on the outer surfaces of the device panels 1 and 2.
【0012】機器4と導波管5および同軸ケーブル6と
の接続は、機器パネル1および2に一部貫通孔を設ける
ことにより行う。The connection between the device 4 and the waveguide 5 and the coaxial cable 6 is made by partially forming through holes in the device panels 1 and 2.
【0013】ヒートパイプ8,9はそれぞれヒートパイ
プパネル10,11に実装される。The heat pipes 8 and 9 are mounted on the heat pipe panels 10 and 11, respectively.
【0014】機器パネル1,2は、これらパネルの外側
に設けられたヒートパイプパネル10,11に熱伝導の
良い連結金具12で組付けられる。The equipment panels 1 and 2 are assembled to the heat pipe panels 10 and 11 provided on the outer sides of these panels with a coupling fitting 12 having good heat conduction.
【0015】低発熱機器は従来技術と同様にヒートパイ
プを必要としない機器パネル3に搭載される。The low heat generating device is mounted on the device panel 3 which does not require a heat pipe as in the prior art.
【0016】[0016]
【発明の効果】以上説明したように、本発明による人工
衛星の機器実装構造は、ヒートパイプを配置するパネル
を別に設けることにより、機器パネルへの機器配置と、
ヒートパイプレイアウトとのインタフェースが簡略化さ
れるとともに、並行して設計作業が行える。As described above, in the device mounting structure of the artificial satellite according to the present invention, by disposing the panel for disposing the heat pipe separately, the device disposition on the device panel,
The interface with the heat pipe layout is simplified, and design work can be performed in parallel.
【0017】また、機器配置が決まった後に、機器パネ
ルとヒートパイプパネルとの連結金具でインタフェース
をとることになり、ヒートパイプパネルの標準化が計れ
る。Further, after the arrangement of the equipment is decided, an interface is taken by a connecting metal fitting between the equipment panel and the heat pipe panel, and the heat pipe panel can be standardized.
【0018】機器パネルの内面側に機器とハーネスを実
装し、外面側に導波管,同軸ケーブルを実装するため、
同軸ケーブルとハーネスの干渉がないため、それぞれが
最短ルートで接続されることになり、電気的な損失が少
なく、かつ重量も軽減できる。また、機器の実装面積も
広くとれる。Since the equipment and the harness are mounted on the inner surface side of the equipment panel and the waveguide and the coaxial cable are mounted on the outer surface side,
Since there is no interference between the coaxial cable and the harness, they will be connected by the shortest route, reducing electrical loss and reducing weight. In addition, the mounting area of the device can be wide.
【図1】本発明による人工衛星の機器実装構造を示す分
解斜視図である。FIG. 1 is an exploded perspective view showing a device mounting structure of an artificial satellite according to the present invention.
【図2】従来の人工衛星の機器実装構造を示す分解斜視
図である。FIG. 2 is an exploded perspective view showing a conventional device mounting structure of an artificial satellite.
1,2,3 機器パネル 4 機器 5 導波管 6 同軸ケーブル 7 ハーネス 8,9 ヒートパイプ 10,11 ヒートパイプパネル 12 連結金具 1,2,3 Equipment panel 4 Equipment 5 Waveguide 6 Coaxial cable 7 Harness 8,9 Heat pipe 10,11 Heat pipe panel 12 Connecting fitting
Claims (2)
ル,ハーネス,ヒートパイプを実装する人工衛星の機器
実装構造において、 ヒートパイプ専用のパネルを外側に設け、内側のパネル
両面に、機器,導波管,同軸ケーブル,ハーネスを実装
することを特徴とする人工衛星の機器実装構造。1. A device mounting structure for an artificial satellite, wherein a device, a waveguide, a coaxial cable, a harness, and a heat pipe are mounted on a panel. , A device mounting structure for an artificial satellite characterized by mounting a waveguide, a coaxial cable, and a harness.
ル,ハーネス,ヒートパイプを実装する人工衛星の機器
実装構造において、 機器パネルと、この機器パネルに対向して配置されたヒ
ートパイプパネルとを備え、 前記機器パネルの、前記ヒートパイプパネルとは反対側
の面上に、機器とハーネスを実装し、前記ヒートパイプ
パネルに対向する面上に、導波管と同軸ケーブルを実装
し、 前記機器パネルとヒートパイプパネルとは、熱伝導の良
い部材で連結されている、ことを特徴とする人工衛星の
機器実装構造。2. In a device mounting structure of an artificial satellite in which devices, waveguides, coaxial cables, harnesses, and heat pipes are mounted on a panel, the device panel and a heat pipe panel arranged so as to face the device panel. And, on the surface of the device panel opposite to the heat pipe panel, the device and the harness are mounted, on the surface facing the heat pipe panel, the waveguide and the coaxial cable are mounted, The device mounting structure for an artificial satellite, wherein the device panel and the heat pipe panel are connected by a member having good heat conduction.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP5155285A JP2565089B2 (en) | 1993-06-25 | 1993-06-25 | Device mounting structure for satellite |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP5155285A JP2565089B2 (en) | 1993-06-25 | 1993-06-25 | Device mounting structure for satellite |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH0710097A true JPH0710097A (en) | 1995-01-13 |
| JP2565089B2 JP2565089B2 (en) | 1996-12-18 |
Family
ID=15602564
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP5155285A Expired - Lifetime JP2565089B2 (en) | 1993-06-25 | 1993-06-25 | Device mounting structure for satellite |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2565089B2 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2012529402A (en) * | 2009-06-12 | 2012-11-22 | ザ・ボーイング・カンパニー | Method and apparatus for aircraft wireless communication using fuselage stringers |
-
1993
- 1993-06-25 JP JP5155285A patent/JP2565089B2/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2012529402A (en) * | 2009-06-12 | 2012-11-22 | ザ・ボーイング・カンパニー | Method and apparatus for aircraft wireless communication using fuselage stringers |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2565089B2 (en) | 1996-12-18 |
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