• 비파괴검사학회지
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• 제28권2호
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• pp.177-183
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• 2008

고온-고압의 장시간 사용으로 나타나게 되는 재료열화현상을 이해하고 구조건전성 모니터링을 위한 기초연구로 사용하고자 대표적인 로터용 내열강인 2.25CrMo 강과 9CrMo 강 그리고 12CrW 강을 연구하였다. 재료열화를 모니터링하기 위해 2.25CrMo 강은 등온열화 시험을 9CrMo 강은 크리프-피로 시험을 그리고 12CrW 강은 크리프 시험을 각 단계별로 수행하였다. 이들 각 손상재에 대한 초음파전파특성, 비저항측정 그리고 보자력측정을 통하여 미세조직 의존성을 고찰하였고 이들 파라미터는 특정 미세조직의 변화에 상당히 민감하게 작용하였다.

• 한국정밀공학회지
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• 제26권6호
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• pp.90-96
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• 2009

Ultrasonic method using SH(shear horizontal) wave has been developed to determine the surface damage in fatigued material. Fatigue damages based on propagation energy were analyzed by multi-regression analysis in interrupted fatigue test specimen including CrMoV and 12Cr alloy steel. From the test results, as the fatigue damage increased the propagation time of the launched waves increased and amplitude of wavelet decreased. Also, analysis for the waveform modulation showed a reliable estimation, with confidence limit of 97% for 12Cr steel and 95% for CrMoV steel, respectively. Therefore, It is thought that SH ultrasonic wave technique can be applied to determine fatigue damage of in-service component nondestructively.

• 대한기계학회논문집
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• 제16권10호
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• pp.1861-1868
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• 1992

본 연구에서는 발전소의 터빈 블레이드는 물방울에 의해서 부식이 발생한다는 사실은 널리 알려져 있다. 부식을 방지하기위해서 보통 12%-Cr 강으로 만들며 표면 을 고주파 유도경화법에 의해서 표면을 경화시킨다. 고주파유도 경화법은 경화층 깊 이가 마모 특성을 가장 좋게 하는 깊이보다 훨씬 깊게 경화되며, 열응력이 과대하게 생기고, 처리시간이 많이 걸리며, 표면경화 처리후 기계가공이 필요하다. 12%-Cr 강 의 레이저 표면경화를 연속파 3kw CO$_{2}$ 레이저로 실험하여 금속조직과 경도분포에 대해서 연구하여 레이저 표면경화 가능성을 고찰하였다.

• 기계저널
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• 제26권4호
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• pp.284-289
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• 1986

이들 기기, 장치는 대부분 철강재가 그 근간을 이루고 있지만, 특히 고온부를 형성하는 부재는 내열용 철강과 합금이다. 강을 모재로 하고 고온에서의 강도유지를 위하여 유용한 소랴의 Cr, Mo 등을 합금시킨 저합금내열강이 1차적으로 사용되어 왔으나 사용조건이 고도화 되면서 이들 합금성분 량이 늘어나 주로 Cr 성분을 증가시킨 고 Cr 페라이트계, 그리고 Ni 성분을 다량으로 첨가한 오스테나이트계 내열강이 제 2차, 제 3차대상이 되어 연구 발전되어 왔다. 그 사용한계는 사용 가스등 환경의 영향과 고온의 크리이프나 피로, 파괴에 대한 저항성등에 크게 좌우되지만, 대개 2.25Cr-1Mo 강의 저합금강에서 $550^{\circ}C$, 9~12% Cr인 페라이트계 내열강에서 $^650{\circ}C$ 까지가 한도이며 그 이상온도에서는 오스테나이트계 내열강이 고려의 대상이 되고 있는 것 같다. 이들 고온부에 사용되는 철강 재료를 중심으로 최근의 동향을 주로 금속학적 입장에서 살펴보기로 한다.

• 한국원자력학회:학술대회논문집
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• 한국원자력학회 2001년도 추계학술발표회요약집
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• pp.263.2-263
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• 2001

• 동력기계공학회지
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• 제15권2호
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• pp.49-54
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• 2011

Effect of tempering treatment on the mechanical properties of 12Cr heat resistant steel with ferrite phase was investigate in this study. As time and temperature of tempering treatment were increase, C and Cr contents in matrix structure were decreased. Due to increase of the amount of Cr26C6 type carbides. It was confirmed in mechanical properties experimental that tensile strength and hardness were decreased, while elongation and impact value were, increased with increasing the time and temperature.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 추계학술대회논문집A
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• pp.322-327
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• 2000

This paper investigates the time-dependent crack growth in X20CrMoV 12 1 steel weld joints. Crack growth test are carried out $545^{\circ}C$ on side-grooved 1/2T CT specimens under static loads. A simulated material is produced for the intercritical HAZ, where fracture normally occurs. Constitutive properties are obtained for the simulated HAZ material as well as for the base metal and weld metal. Finite element analyses of crack growth are performed on the models with and without a HAZ layer, using the experimental crack length-time history. The inclusion of HAZ layer increase the load line velocities significantly. The crack growth rates are correlated reasonably well with $C^*$. The smallest crack size for the validity of $C^*$ is found much smaller than the ASTM crack initiation size for 1T CT specimen of creep ductile materials.

• 대한기계학회논문집
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• 제17권6호
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• pp.1321-1329
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• 1993

본 연구에서는 이들보다 매우 간단한 IS법, 즉 초기 변형률법(ISM: initial strain method)에 의한 크리프 수명예측식을 고안하여, 현재 화력발전용 고압 로터강 에 사용되고 있는 1%Cr-Mo-V강과 발전소 효율향상을 위해 최근 국내최초로 개발된 12% Cr강에 대하여 도출하였고, 이 도출식이 앞에서 언급한 여러 파라메트에 의한 결과와 비교 평가하여 장시간 강도 및 수명예측식으로 사용될 수 있음을 입증하였다.

• 한국해양공학회지
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• 제3권2호
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• pp.125-137
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• 1989

To check technical improvement in the soundness and strength of 12% Cr steel rotor, a 25 tons of rotor with 65 tons of ingot was made in real size and was cut to pieces to take test samples, and the various mechanical tests such as impact, tensile, creep, and fatigue were carried out. The strengths are compared with those of 1% Cr-Mo-V rotor of same size. Microstructures of the samples are examined and reviewed. The results can be summarized as follows. 1) Fracture appearance transition temperatures are 80.deg. C at the center part and 60.deg. C near surface of 12% Cr rotor, and 8.deg. C near surface of 1% Cr-Mo-V rotor. 2) Comparative rapid softening occurs at higher temperatures above 600.deg. C for 12% Cr steel and 550.deg. C for 1% Cr-Mo-V steel in tension tests. 3) Fatigue crack propagation rate of 12% Cr steel is almost same as that of 1% Cr-Mo-V steel at the same corresponding surface part of the rotors. The crack growth rate of center part of 12% Cr rotor is faster than near surface part of the rotor, and the crack growth rate at the load condition of R=0.04 is slower than that of the load condition of R=0.5 for both 12% Cr steel and 1% Cr-Mo-V steel. 4) Crack growth rate of radial direction near surface of 12% Cr rotor is faster than that of transverse direction at the same part because of the difference in residual stresses. 5) Both creep and fatigue strengths of 12% Cr steel are superior to those of 1% Cr-Mo-V steel and the difference is thought the effect of climb and glide controlled creep by solid solution of alloying elements and dispersion of carbides.

• 한국해양공학회지
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• 제3권2호
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• pp.625-625
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• 1989

To check technical improvement in the soundness and strength of 12% Cr steel rotor, a 25 tons of rotor with 65 tons of ingot was made in real size and was cut to pieces to take test samples, and the various mechanical tests such as impact, tensile, creep, and fatigue were carried out. The strengths are compared with those of 1% Cr-Mo-V rotor of same size. Microstructures of the samples are examined and reviewed. The results can be summarized as follows. 1) Fracture appearance transition temperatures are 80.deg. C at the center part and 60.deg. C near surface of 12% Cr rotor, and 8.deg. C near surface of 1% Cr-Mo-V rotor. 2) Comparative rapid softening occurs at higher temperatures above 600.deg. C for 12% Cr steel and 550.deg. C for 1% Cr-Mo-V steel in tension tests. 3) Fatigue crack propagation rate of 12% Cr steel is almost same as that of 1% Cr-Mo-V steel at the same corresponding surface part of the rotors. The crack growth rate of center part of 12% Cr rotor is faster than near surface part of the rotor, and the crack growth rate at the load condition of R=0.04 is slower than that of the load condition of R=0.5 for both 12% Cr steel and 1% Cr-Mo-V steel. 4) Crack growth rate of radial direction near surface of 12% Cr rotor is faster than that of transverse direction at the same part because of the difference in residual stresses. 5) Both creep and fatigue strengths of 12% Cr steel are superior to those of 1% Cr-Mo-V steel and the difference is thought the effect of climb and glide controlled creep by solid solution of alloying elements and dispersion of carbides.