タービン諸特性(回転部重量，翼応力，動翼共振回避，Thomas Force)を考慮したロケットターボポンプ用タービンの多目的最適化

Material type: 文書・図像類

Author: 瀧田, 純也ほか

Publisher: 宇宙航空研究開発機構(JAXA)

Publication date: 2013-01-31

Material Format: Digital

Capacity, size, etc.: -

NDC: -

View All

Notes on use

Note (General)：: Because rocket turbopump turbine blades have higher loading, there is a possibility of shaft vibration problem due to "Thomas Force". In order to redu...

Search by Bookstore

Holdings of Libraries in Japan

This page shows libraries in Japan other than the National Diet Library that hold the material.

List of Cooperating Institutions and Databases

Please contact your local library for information on how to use materials or whether it is possible to request materials from the holding libraries.

other

JAXA Repository
Digital
You can check the holdings of institutions and databases with which 学術機関リポジトリデータベース（IRDB）（機関リポジトリ） is linked at the site of 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）.
JAXA Repository

Search by Bookstore

Bibliographic Record

You can check the details of this material, its authority (keywords that refer to materials on the same subject, author's name, etc.), etc.

Digital

Material Type: 文書・図像類
Title: タービン諸特性(回転部重量，翼応力，動翼共振回避，Thomas Force)を考慮したロケットターボポンプ用タービンの多目的最適化
Author/Editor: 瀧田, 純也
福田, 太郎
宇山, 遼一
船﨑, 健一
内海, 政春
Takida, Junya
Fukuda, Taro
Uyama, Ryoichi
Funazaki, Kenichi
Uchiumi, Masaharu
Author Heading: 瀧田, 純也
福田, 太郎
宇山, 遼一
船﨑, 健一
内海, 政春
Takida, Junya
Fukuda, Taro
Uyama, Ryoichi
Funazaki, Kenichi
Uchiumi, Masaharu
Publication, Distribution, etc.: 宇宙航空研究開発機構(JAXA)
Publication Date: 2013-01-31
Publication Date (W3CDTF): 2013-01-31
Alternative Title: Multi-Objective Optimization of a Rocket Turbopump Turbine Considering the Turbine Characteristics: i.e., Rotor Weight, Blade Stress, Avoidance of Blade Resonance and Thomas Force
Periodical title: 宇宙航空研究開発機構研究開発資料 = JAXA Research and Development Memorandum
No. or year of volume/issue: JAXA-RM-12-007
Volume: JAXA-RM-12-007
Pages: 1-11
ISSN (Periodical Title): ISSN : 1349-1121
Text Language Code: jpn
Subject Heading: Multi-Objective Genetic Algorithm (MOGA)
Parameter Design
Rocket Turbopump
Self-Organizing Map(SOM)
Thomas Force
Target Audience: 一般
Note (General): Because rocket turbopump turbine blades have higher loading, there is a possibility of shaft vibration problem due to "Thomas Force". In order to reduce shaft vibrations, it is important to keep "Thomas Force" small. In the previous report, validity of optimization process for the reduction of Thomas Force was confirmed by performing Parameter Design and Multi-Objective Genetic Algorithm (MOGA). In this paper, by increasing the number of objective functions, the results of multi-objective optimization for reduction of Thomas Force and the considering the feasibility of blade structure are discussed. It was found that optimized blade reduced 10% in weight, 30% in Thomas Force, compared from the original blade.
形態: カラー図版あり
Physical characteristics: Original contains color illustrations
資料番号: AA0065514000
レポート番号: JAXA-RM-12-007
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=2525&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=2525&item_no=1&attribute_id=31&file_no=1
Access Restrictions: 限定公開
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ