• Transactions of the Korean Society of Mechanical Engineers
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• v.10 no.4
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• pp.519-528
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• 1986

본 연구에서는 우선 1차적으로 한국중공업에서 제조한 실제의 터어빈 회전자 축에서 시편을 채취하여 화력발전소 터어빈의 작동 온도에서의 크리이프 거동을 실험 하고, Larson-Miller 법 및 Orr-sherby-Dorn 법에 의하여 수명을 예상하엿으며 열처리 조건의 변화에 따른 크리이프 특성 변화를 고찰하였다.

• Transactions of the Korean Society of Mechanical Engineers
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• v.12 no.3
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• pp.513-519
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• 1988

Constant load creep tests have been carried out over a range of stresses at high temperatures. The experimental equations of the steady-state creep rate and creep-rupture life were respectively found to be related to the normalized applied-stress and temperature as ln.epsilon.$_{s}$ =6.10 on.sigma./ $E_{T}$-12.81*10$^{3}$ 1/T+15.98 (h $r^{-1}$) ln $t_{R}$=-6.24ln.sigma./ $E_{T}$+15.08*10$^{3}$1/T-23.66 (hr) and the equation of creep-rupture life had a good agreement with the expression of the Minimum-Commitment Method (MCM). However, the relationship between the steady-state creep rate and the creep-rupture life, noted by Monkman and Grant, lnt/snb R/ = mln.epsilon.$_{S}$+b made a considerable deviation against the present creep-rupture data. It is believed that this problem is to be discussed and investigated continually.lly.lly..