• 대한기계학회논문집A
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• 제30권3호
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• pp.349-355
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• 2006

The gas turbine components is used on high temperature conditions which under severely circumstance with start-up and stop several times. Therefore, it is used nickel-base superalloys like and GTD-111DS. Damaged buckets on the t긴ade tip during operating are repaired per 24,000 hr to three times according to repair specification of manufacture. It is applied pre-heat, HIP(hot isostatic pressing) and post-heat treatment to support welding repair on blade tip effectively. On this study, It is utilize of $WRAP^{TM}$ (welding repair advanced process) method to make tension test specimens for this study, And then, material strength and characteristic for GTD-111DS was analyzed.

• 대한용접접합학회:학술대회논문집
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• 대한용접접합학회 2009년 추계학술발표대회
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• pp.108-108
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• 2009

니켈기지의 석출강화 초내열합금은 가스터빈의 고온부 부품 제조에 널리 사용되고 있다. 장시간 동안 부품의 강성 유지와 구조적 안정성을 확보하기 위해서는 니켈기지의 합금에 감마프라임 생성을 위한 원소를 첨가하는데 이에 따른 용접성의 저하 때문에 보통 초합금의 용접은 고온에서 수행하게 된다. 그러나 레이저용접의 경우는 용접변수 및 입열제어가 용이해 상온에서 초합금의 용접이 가능한 장점이 있다. 본 연구에서는 일반적인 재료로 연성이 좋은 STS304 판재와 실제 블레이드의 재료로 사용되는 니켈계 석출강화 합금인 GTD 111DS 모재에 $CO_2$ 레이저를 이용하여 용접을 실시하였고 적용파우더와 파워, 용접속도 및 파우더 공급량 등을 달리 하였다. STS304 판재 사용시 Rene 80과 IN 625 파우더 모두 용접부에서 균열이 발생하지 않았다. 그러나 GTD 111DS 모재의 경우 IN 625 파우더에서는 결함이 없었으나 Rene 80 파우더를 사용시에는 용접부에 균열이 발생하였다. IN 625 파우더는 모재보다 기계적 성질이 떨어지는 문제가 있으나 Rene 80은 모재와 동등 이상의 기계적 성질을 보유하고 있기 때문에 Rene 80 의 적용을 위해 균열이 발생하지 않는 용접변수의 제어를 시도하였다. 용접변수의 조정 결과 레이저 파워와 파우더 공급량을 낮추고 용접속도를 높여 균열이 발생하지 않는 최적의 용접변수를 설정할 수 있었다. 최적화된 용접변수를 적용, 용접한 시편의 인장값을 보면 GTD 111DS 모재에 Rene 80 파우더로 용접된 시편의 인장강도가 상온/고온($760^{\circ}C$)의 조건에서 각각 GTD 111DS 모재의 인장강도 보다 높은 값을 나타내었다.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2005년도 춘계학술대회 논문집
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• pp.1358-1362
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• 2005

The Ni-base superalloy GTD-111DS was designed in the 1970s and is widely used as the material of the first stage blade under a severe combination of temperature and pressure in gas turbines. But because GTD-111DS is distributed in the shape of blade and blade has a unique figure and many cooling channels, it is hard to manufacture the test specimen. In this reason, there are little data on the microstructure and mechanical properties of the alloy. Therefore through the microstructure analysis, present paper observed that the shape of $\gamma{'}$ did not change even if aging time was increased but the amount and volume of the deposition of secondary $\gamma{'}\;rose\;and\;secondary\;\gamma{'}\;grew\;among\;primary\;\gamma{'}$. Also, by tensile test for different temperature, there was difference between yield strength and tensile strength in room temperature on heat treatment and extracting region but the more increasing temperature, the more decreasing difference between yield strength and tensile strength.

• 한국정밀공학회지
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• 제26권3호
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• pp.19-24
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• 2009

• Journal of Welding and Joining
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• 제25권5호
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• pp.45-50
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• 2007

The Ni-base superalloy GTD111 DS is used in the first stage blade of high power land-based gas turbines. Advanced repair technologies of the blade have been introduced to the gas turbine industry over recent years. The effect of the filler metal powder on Transient Liquid Phase bonding phenomenon and tensile mechanical properties was investigated on the GTD111 DS superalloy. At the filler metal powder N series, the base metal powders fully melted at the initial time and a large amount of the base metal near the bonded interlayer was dissolved by liquid inter metal. Liquid filler metal powder was eliminated by isothermal solidification which was controlled by the diffusion of B into the base metal. The solids in the bonded interlayer grew from the base metal near the bonded interlayer inward the insert metal during the isothermal solidification. The bond strength of N series filler metal powder was over 1000 MPa. and ${\gamma}'$ phase size of N series TLP bonded region was similar with base metal by influence of Ti, Al elements. At the insert metal powder M series, the Si element fluidity of the filler metal was good but microstructure irregularity on bonded region because of excessive Si element. Nuclear of solids formed not only from the base metal near the bonded interlayer but also from the remained filler metal powder in the bonded interlayer. When the isothermal solidification was finished, the content of the elements in the boned interlayer was approximately equal to that of the base metal. But boride and silicide formed in the base metal near the bonded interlayer. And these boride decreased with the increasing of holding time. The bond strength of M series filler metal powder was about 400 MPa.

• 대한기계학회논문집A
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• 제41권8호
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• pp.765-770
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• 2017

Ni기 초내열합금인 GTD111 DS는 가스터빈 블레이드에 사용된다. 본 논문에서는 실제 운전조건과 유사한 조건을 설정하여 GTD111 DS의 저주기 피로시험을 실시하였다 상온, $760^{\circ}C$, $870^{\circ}C$의 온도범위와 다양한 변형률에서 저주기 피로시험을 수행하였다. 실험결과 총 변형률이 증가함에 따라 피로수명은 감소하였다. 상온 및 $760^{\circ}C$에서는 주기적 경화반응이 나타났으며 $870^{\circ}C$에서는 주기적 연화반응이 나타났다. $870^{\circ}C$에서 응력완화 현상은 유지시간에 따른 크리프의 영향으로 나타났다. 피로수명과 총 변형률의 관계는 Coffin-Manson 식을 통해 얻었다. 파단면은 SEM을 통해 초기균열 및 피로진전지역을 관찰하였다.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2006년도 추계학술대회 논문집
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• pp.627-628
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• 2006

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2008년도 춘계학술대회 논문집
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• pp.411-412
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• 2008

• 대한기계학회논문집A
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• 제31권4호
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• pp.525-531
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• 2007

The operating temperature has been increased to improve the efficiency of gas turbine. The most advanced Gas turbine is operated at above $1,500^{\circ}C$. Improvement in material and cooling method permit hot gas path component to run at increased temperature. But, the repair of blades which are developed with advanced manufacture technique is difficult to use normal welding. Most of gas turbine blades are made of precipitation harden nickel base superalloy, which is very hard to weld. Therefore, the employment of welding filler on blade is solid solution nickel base superalloy(Hastelloy X, Inconel 617). In this study, Tensile test in high temperature was conducted on welded GTD111DS with GTD111 to evaluate effect of variation of pre, post treatment. The result of this study showed that the specimen was treated with optimum pre and post treatment(preweld HT($1200^{\circ}C$), Post treatment($1100^{\circ}C$ HIP, $1200^{\circ}C$ + $1100^{\circ}C$ + $800^{\circ}C$ HT) is mush superior.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2007년도 추계학술대회 논문집
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• pp.381-382
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• 2007