Coupled Deformation Properties of Anti-Symmetrical Laminate Composites

• HOJO Masahiro

  JAXA Aerospace Research Center

• HASHIMOTO Ryosaku

  JAXA Aerospace Research Center

• OGAWA Akinori

  JAXA Aerospace Research Center

抄録

Anti-symmetrical laminate composites exhibit a coupling effect between tensile stress and twisting deformation, and are very attractive as blade materials for aircraft engines. Blades made of anti-symmetrical laminate composites can automatically adjust their stagger angle to a better aerodynamic configuration with changing rotational speed. Thus, the aerodynamic efficiency and stability of aircraft engines can be greatly improved. In this study, the coupled deformation properties of anti-symmetrical laminate composites were evaluated with tensile tests. Two kinds of specimens fabricated from carbon/epoxy laminate composites with different anti-symmetrical stacking sequences were tested. On the basis of the tensile-test results, the anti-symmetrical laminate composites were then used as blade materials. The coupled deformation of the test blades at high rotational speed was evaluated by spin tests and FEM analyses. It was demonstrated that test blades twisted about 4° at 10000rpm.

収録刊行物

• JSME International Journal Series A Solid Mechanics and Material Engineering

  JSME International Journal Series A Solid Mechanics and Material Engineering 49 (1), 43-47, 2006

  一般社団法人 日本機械学会

キーワード

• Coupled Deformation
• Anti-Symmetrical Laminate Composite
• Composite Blade

詳細情報

• CRID: 1390282681471485952
• NII論文ID: 110004082842
• NII書誌ID: AA11179396
• DOI: 10.1299/jsmea.49.43
• ISSN: 13475363
• ISSN: 13447912
• NDL書誌ID: 7769012
• Web Site: http://id.ndl.go.jp/bib/7769012
• Web Site: https://ndlsearch.ndl.go.jp/books/R000000004-I7769012
• Web Site: http://www.jstage.jst.go.jp/article/jsmea/49/1/49_1_43/_pdf
• 本文言語コード: en
• データソース種別:
  • JaLC
  • NDL
  • Crossref
  • CiNii Articles
• 抄録ライセンスフラグ: 使用不可