B-10 単結晶材料の高熱流束バーナーリグ評価試験(伝熱・計測,一般講演)

• 松下 政裕

  宇宙航空研究開発機構

• 福山 佳孝

  宇宙航空研究開発機構

• 藤沢 良昭

  宇宙航空研究開発機構

• 青木 祥宏

  石川島播磨重工業

書誌事項

タイトル別名

• B-10 Evaluation Test of Single Crystal Superalloy by High Heat Flux Burner Rig Test Equipment

抄録

Experimental equipment had been built to evaluation for high heat-resistant materials under the condition of turbine blade. As this equipment, a circular straight pipe was rounded on the central axis for uniform circumferential heating, and the position control of burners was programmable for the cyclic heating test which simulated the engine condition. By this equipment, two single crystal superalloys, CMSX-2 and TMS138, were tested by only thermal stress at about 1000 degree of maximum material temperature for 100 cycles (3 minutes heating and 3 second cooling).

収録刊行物

• ガスタービン定期講演会講演論文集

  ガスタービン定期講演会講演論文集 (33), 159-164, 2005-09-01

  公益社団法人日本ガスタービン学会

キーワード

• Single Crystal
• Supperalloy
• Thermal Stress
• Turbine blade

詳細情報

• CRID: 1572261552168706816
• NII論文ID: 110006173599
• NII書誌ID: AN10255898
• ISSN: 09191941
• 本文言語コード: ja
• データソース種別:
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