Art

J-GLOBAL ID：201702236970745617   Reference number：17A0164151

An improved calculation model for forward slip in rolling compressor blade

改良型圧縮機ブレードのためのGunYaの前の計算モデルを提案した。【JST・京大機械翻訳】

Author (6)： Jin Qichao (The Key Laboratory of Contemporary Design and Integrated Manufacturing Technology, Ministry of Education, Northwestern Polytechnical University) ,  Wang Wenhu (The Key Laboratory of Contemporary Design and Integrated Manufacturing Technology, Ministry of Education, Northwestern Polytechnical University) ,  Jiang Ruisong (The Key Laboratory of Contemporary Design and Integrated Manufacturing Technology, Ministry of Education, Northwestern Polytechnical University) ,  Zhao Dezhong (The Key Laboratory of Contemporary Design and Integrated Manufacturing Technology, Ministry of Education, Northwestern Polytechnical University) ,  Cui Kang (The Key Laboratory of Contemporary Design and Integrated Manufacturing Technology, Ministry of Education, Northwestern Polytechnical University) ,  Xiong Yifeng (The Key Laboratory of Contemporary Design and Integrated Manufacturing Technology, Ministry of Education, Northwestern Polytechnical University)
Material： Hangkong Xuebao  (Acta Aeronautica et Astronautica Sinica)
Volume： 37  Issue： 10  Page： 3178-3185  Publication year： 2016 
JST Material Number： W1470A  ISSN： 1000-6893  Document type： Article
Article type： 原著論文  Country of issue： China (CHN)  Language： CHINESE (ZH)

Abstract/Point： In the process of roll forming...

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Thesaurus term： three dimension ,  rotational frequency ,  *compressor ,  rigidity ,  *computation model
Semi thesaurus term： 不規則性 ,  数値シミュレーション ,  CADモデル ,  航空エンジン , 【Automatic Indexing@JST】

Author keywords (5)： compressor blade ,  roll forming ,  section curve ,  forward slip model ,  FEM

JST classification (2)： Gas turbines  (PB02040Y) ,  Blowers,compressors,wind turbines  (QD03000U)

Terms in the title (4)： 圧縮機 ,  ブレード ,  計算モデル ,  提案