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成層圏プラットフォーム飛行船の推進性能とプロペラ特性の検討
https://jaxa.repo.nii.ac.jp/records/2235
https://jaxa.repo.nii.ac.jp/records/22351abc3da0-35aa-4d64-af74-597be0b49d2d
名前 / ファイル | ライセンス | アクション |
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49490000.pdf (6.0 MB)
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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 | 成層圏プラットフォーム飛行船の推進性能とプロペラ特性の検討 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 成層圏プラットフォーム飛行船 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 成層圏 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 推進性能 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | プロペラ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ロータ/機体相互作用 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 船体-プロペラ系 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低Reynolds数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算流体力学 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stratospheric platform airship | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stratosphere | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | propulsion performance | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | propeller | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | rotor body interaction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hull-propeller system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low Reynolds number | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computational fluid dynamics | |||||
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 | Study of propulsion performance and propeller characteristics for stratospheric platform airship | |||||
著者 |
奥山, 政広
× 奥山, 政広× 柴田, 眞× 横川, 彰寛× 木村, 校優× Okuyama, Masahiro× Shibata, Makoto× Yokokawa, Akihiro× Kimura, Koyu |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 航空プログラムグループ | ||||||
著者所属 | ||||||
航空宇宙技術振興財団 | ||||||
著者所属 | ||||||
住友精密工業 | ||||||
著者所属 | ||||||
三井造船昭島研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Aviation Program Group | ||||||
著者所属(英) | ||||||
en | ||||||
Foundation for Promotion of Japanese Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Sumitomo Precision Products Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Akishima Laboratories (Mitsui Zosen) Inc. | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構研究開発報告 en : JAXA Research and Development Report 巻 JAXA-RR-05-056, 発行日 2006-03-31 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 成層圏プラットフォーム飛行船の実現に向けて、推進系に係わる船体-プロペラ系の推進性能とプロペラ特性を本報告で取り上げる。船体-プロペラ系の取り扱いと、多発プロペラの効率をはじめに示した。推進性能解析では、船舶工学の手法と研究開発実績により船体-プロペラ系の相互干渉解析を実施し、船体プロペラ配置形態の推進性能を推算すると共に、プロペラによる船体干渉の様子を示した。プロペラ特性の解析では、成層圏条件で運用するプロペラにおいて、プロペラの製造実績を生かし空力と構造を解析し、プロペラの多発化および軽負荷化を検討した。また、求められる成層圏用の低レイノルズ数プロペラを設計し、その運用について検討した。検討の結果、船尾プロペラによる推進効率の向上が確認された。さらに、設計された低レイノルズ数プロペラにより、成層圏における低回転数の制限が緩和された。また、プロペラの重量軽減が成された。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The propulsion performance and propeller characteristics on hull-propellers system within the propulsion system are taken up in this paper toward the realization of the stratospheric platform airship. First of all, the efficiencies of multi-propellers were studied. Next, the mutual interference analysis of the hull-propellers system was carried out by the method of ship engineering on the propulsion performance. Furthermore, the propulsion performance of the propellers that were arranged to the hull was calculated, and the hull interference by the propellers was shown. In the end, propeller characteristics used at stratosphere were analyzed in the aerodynamics and structure. In addition multi-propellers and light loading propeller were examined. As a result, the low Reynolds number propeller for stratosphere was designed and examined for use. The improvement of the propulsion efficiency by the stern propeller was confirmed as a result of the examination. Furthermore, the relaxation of the low revolutions of propeller in stratosphere was improved by the designed low Reynolds number propeller. Also the weight reduction of this propeller was attained. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-1113 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA1192675X | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0049490000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-RR-05-056 |