WEKO3
アイテム
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航空機による微小重力実験:二相流体式排熱システム用蒸発器. 二相流動観察実験 その2
https://jaxa.repo.nii.ac.jp/records/39870
https://jaxa.repo.nii.ac.jp/records/398701aaa66b7-9fa0-47f6-91b1-1072aeb8c4a9
名前 / ファイル | ライセンス | アクション |
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00788002.pdf (525.7 kB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 航空機による微小重力実験:二相流体式排熱システム用蒸発器. 二相流動観察実験 その2 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | MU-300型航空機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | パラボリックフライト | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 微小重力環境 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 二相流体 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 二相流体排熱システム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 蒸発器 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 2連グルーブ管 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ステンジャ型蒸発器 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 圧力差制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 蒸発表面 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | MU 300 aircraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | parabolic flight | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | microgravity environment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | two phase fluid | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | two phase fluid loop thermal control system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | evaporator | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | grooved double pipe | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | mesh wick pipe evaporator | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | pressure difference control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | evaporative surface | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Evaluation of evaporators for two-phase fluid loop thermal control system through observation of flow pattern under microgravity condition aboard aircraft | |||||
著者 |
古川, 正夫
× 古川, 正夫× 板垣, 春昭× 石井, 康夫× 山本, 隆宣× 味村, 一樹× 古浜, 功吉× 宮崎, 芳郎× 小森, 実× Furukawa, Masao× Itagaki, Haruaki× Ishii, Yasuo× Yamamoto, Takanori× Mimura, Kazuki× Furuhama, Kokichi× Miyazaki, Yoshio× Komori, Minoru |
|||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属 | ||||||
東芝 | ||||||
著者所属 | ||||||
東芝 | ||||||
著者所属 | ||||||
東芝 | ||||||
著者所属 | ||||||
東芝 | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
著者所属(英) | ||||||
en | ||||||
Toshiba Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
Toshiba Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
Toshiba Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
Toshiba Corporation | ||||||
出版者 | ||||||
出版者 | 宇宙開発事業団 | |||||
出版者(英) | ||||||
出版者 | National Space Development Agency of Japan (NASDA) | |||||
書誌情報 |
宇宙開発事業団技術報告 en : NASDA Technical Memorandum p. 10-19, 発行日 1997-01-31 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | MU-300型航空機上での重力低減条件において、二相流体式排熱システムに用いられる流量制御法の研究を行った。蒸発器は2連グルーブ管式とステンジャ型の2種類で、下記3種類の制御方式を試験するために試作したものである。(1)蒸発器の出口端でのクオリティ制御を行う。(2)蒸発器表面(熱源の直下)と蒸気の間の温度差を制御する。(3)蒸発器中の蒸気と液体間の圧力差を制御する。制御方式の評価は、蒸発器中の余剰液の挙動および並列運転中の蒸発器の熱的性能によって行った。この目的のため、蒸発器にはすべて、蒸発表面の流動様式の観測用窓を取り付ける。これらの方式はすべて、軌道上操作で有効に使用できることを示したが、制御方式とハードウェア構成が簡略になるという点で(3)型を推奨する。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Flow rate control methods for a two-phase fluid loop thermal control system, are studied under reduced gravity condition aboard MU-300 aircraft. Two types of evaporators, grooved double pipes and mesh wick pipes, are fabricated to examine the following three types of control logic: (1) one which controls quality at an outlet of an evaporator; (2) one which controls difference in temperature between evaporator surface (just below heat sources) and vapor; and (3) one which controls difference in pressure between vapor and liquid in an evaporator. Evaluation of control logic is made through the behavior of excess liquid in the evaporators and the thermal performances of the evaporators under parallel operation. For this purpose every evaporator is equipped with the windows for flow pattern observation of evaporative surfaces. Although all of the logic exhibited potential for an in-orbit operation, the type (3) is recommended because of the simplicity of both control logic and hardware configuration. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1345-7888 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00364784 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0000788002 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NASDA-TMR-960026 |