日本航空宇宙学会論文集
Online ISSN : 2432-3691
Print ISSN : 1344-6460
ISSN-L : 1344-6460
論文
金属製冷却配管を材料の弾性力により固定した C/C複合材冷却構造の冷却特性
竹腰 正雄植田 修一
著者情報
ジャーナル フリー

2006 年 54 巻 626 号 p. 129-135

詳細
抄録
A new cooling structure of C/C composites was made to use in high temperature environment over 2000K. A stainless steel tube was used as a cooling channel. The stainless steel tube was fixed to the C/C composites by the elastic force of each material. The performance of the cooling structure was evaluated by heating tests and numerical analysis. In the result of the numerical analysis, it was shown that the surface can be cooled below 2000K under the condition of surface heat flux of 10MW/m2. However, it was shown experimentally that the cooling performance gets extremely worse due to the plastic deformation of the tube when the temperature of the tube rises more than 600K.
著者関連情報
© 2006 The Japan Society for Aeronautical and Space Sciences
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