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62042000.pdf1.65 MB
titleQFD援用によるロケットターボポンプ多領域最適化設計
Other TitleMultidisciplinary optimal design for rocket turbopump by employing QFD
Author(jpn)弘松, 純; 内海, 政春; 島垣, 満; 川崎, 聡; 瀧田, 純也; 中村, 智也
Author(eng)Hiromatsu, Jun; Uchiumi, Masaharu; Shimagaki, Mitsuru; Kawasaki, Satoshi; Takida, Junya; Nakamura, Tomoya
Author Affiliation(jpn)宇宙航空研究開発機構宇宙輸送ミッション本部宇宙輸送系推進技術研究開発センターエンジン研究開発グループ(JAXA); 宇宙航空研究開発機構宇宙輸送ミッション本部宇宙輸送系推進技術研究開発センターエンジン研究開発グループ(JAXA); 宇宙航空研究開発機構宇宙輸送ミッション本部宇宙輸送系推進技術研究開発センターエンジン研究開発グループ(JAXA); 宇宙航空研究開発機構宇宙輸送ミッション本部宇宙輸送系推進技術研究開発センターエンジン研究開発グループ(JAXA); 宇宙航空研究開発機構宇宙輸送ミッション本部宇宙輸送系推進技術研究開発センターエンジン研究開発グループ(JAXA); 宇宙航空研究開発機構宇宙輸送ミッション本部宇宙輸送系推進技術研究開発センターエンジン研究開発グループ(JAXA)
Author Affiliation(eng)Engine System Research and Development Group, Space Transportation Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA); Engine System Research and Development Group, Space Transportation Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA); Engine System Research and Development Group, Space Transportation Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA); Engine System Research and Development Group, Space Transportation Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA); Engine System Research and Development Group, Space Transportation Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA); Engine System Research and Development Group, Space Transportation Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA)
Issue Date2013-10-31
Publisher宇宙航空研究開発機構(JAXA)
Japan Aerospace Exploration Agency (JAXA)
Publication title宇宙航空研究開発機構研究開発資料
JAXA Research and Development Memorandum
VolumeJAXA-RM-13-007
Start page1
End page10
Publication date2013-10-31
Languagejpn
eng
AbstractA rocket turbopump, high-speed, high-power turbomachinery, has suffered from various rotor vibration problems up to the present time. Establishment of an integrated design method consisting of turbopump components is eagerly expected to suppress the rotor vibration. We are now studying the design method of optimal rotor system by using multidisciplinary optimization due to information-sharing of turbopump components (pump, bearing, seal and turbine). A quality function deployment (QFD) is employed to visualize of the relation between turbopump components.
Description形態: カラー図版あり
Physical characteristics: Original contains color illustrations
KeywordsTurbopump; Design of form; Multidisciplinary optimal design; Dynamics design; QFD
Document TypeTechnical Report
JAXA Category研究開発資料
NASA Subject CategorySpacecraft Propulsion and Power
ISSN1349-1121
NCIDAA11983593
SHI-NOAA0062042000
Report NoJAXA-RM-13-007
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/20784


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