• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2013년도 춘계학술대회 논문집
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• pp.1329-1330
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• 2013

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2009년도 춘계학술대회 논문집
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• pp.465-466
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• 2009

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2011년도 춘계학술대회 논문집
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• pp.1153-1154
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• 2011

• 대한기계학회논문집A
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• 제40권7호
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• pp.637-646
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• 2016

실온에서 인코넬 718의 UNSM(Ultrasonic nanocrystal surface modification)처리재, 수소취화재(100 bar, $300^{\circ}C$에서 120 h) 및 수소취화재의 UNSM처리재의 회전굽힘피로시험에 의해 얻어진 결과, 수소취화재는 미처리재의 S-N곡선보다 피로수명이 약 10~20 % 감소하며 부식피로나 비철재료처럼 피로한도 없이 점진적으로 감소하였다. 표면균열수는 수소취화의 영향으로 평균입경($13{\mu}m$)보다 작은 균열의 비율이 약 80 %를 차지하였다. 결정입계, 표면 흠 등에 수소침투에 의한 취화현상으로 티어링(tearing)하면서 복수로 발생한 작은 표면균열은 불규칙적으로 분포하며 티어링하면서 성장, 합체되어 피로수명이 감소하는 것으로 추정된다. 미처리재에 비해서 UNSM처리재의 피로수명은 전 영역에서 크게 증가하였고, 수소취화된 시험편을 UNSM 처리한 후 피로시험을 실시하면 700 MPa에서 10배 이상, 600 MPa에서 20배 이상 증가하였다.

• 대한기계학회논문집A
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• 제40권11호
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• pp.935-941
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• 2016

고온기기의 부재로 널리 사용되는 인코넬 718을 사용하여 UNSM 표면처리법에 의한 처리효과를 기기의 사용조건을 고려한 실온, $300^{\circ}C$, $500^{\circ}C$ 및 $600^{\circ}C$ 의 세 가지 온도레벨하의 대기 중에서 고온피로 시험을 실시하여 각 시험편의 온도에 따른 피로특성을 연구하였다. 이때 고온회전굽힘피로시험(R=-1)은 할로겐(Halogen) 램프를 사용한 집광식인 가열방식을 선택한 새로운 피로시험기를 사용하였다. 인코넬 718의 고온피로강도는 상온에 비하여 감소하였다. 그러나 설계응력레벨에서는 상온의 내구한도와 유사한 경향을 나타내었다. UNSM 처리된 고온피로특성은 미처리재에 비하여 설계응력레벨에서 크게 향상되었다. 미처리재의 $300^{\circ}C$와 $500^{\circ}C$ 사이의 온도 영향은 거의 없었지만, $600^{\circ}C$에서는 높은 응력레벨에서 피로수명이 짧아졌지만, 낮은 설계응력레벨에서는 상온의 S-N선도보다 피로수명이 증가되는 경향을 나타내었다.

• 한국기계가공학회지
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• 제18권2호
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• pp.96-101
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• 2019

This paper presents a machinability evaluation of Inconel 718 material when using a new uniform-temperature indirect cooling method that incorporates constant-pressure liquid nitrogen (LN2). The flank wear of a TiAlN coated tool used with this indirect cooling system was much lower than that of the tool used with dry machining under all machining conditions. Also, the surface roughness resulting from machining with this indirect method was far less than that of a dry machined surface after the same cutting time. Reduced heat generation and uniform temperature in turning operations play important roles in tool life and surface quality.

• 한국생산제조학회지
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• 제19권1호
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• pp.1-6
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• 2010

Inconel 718 alloy has been applied to high temperature, high load and corrosion resistant environments due to its superior properties. However, This alloy is a difficult-to-cut nickel-based superalloy and the chipping or notch wear is mainly generated on the cutting edge of the tool. In this study, the machinability of Inconel 718 is investigated to improve tool life under various cutting conditions with TiCN-based coated ball-end mills. The cutting conditions can be suggested to improve both the tool life and machined surface quality in Inconel 718 high speed machining.

• 한국생산제조학회지
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• 제21권6호
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• pp.982-987
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• 2012

Inconel 718 alloy has been widely used in the aerospace, heavy industry and electronic industry. However, the machinability of this alloy is very poor, which is attributed to their inherent high strength that is maintained at elevated temperatures. The tool life is dominant problem in machining difficult-to-cut materials, so it is necessary to select the efficient cutting conditions for the improvement of tool life. In this study, the cutting force, tool wear and surface roughness are investigated in end milling machining under various cutting conditions. By this experiment, the efficient machining condition of this alloy is suggested to adopt in various industries.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2000년도 추계학술대회 논문집
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• pp.814-817
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• 2000

This paper has two purposes. One is to investigate the effect of the helix angle of endmilling cutter on the cutting haracteristics of inconel 718 in down endmilling. To this end a newly developed cutting force model in down end milling process is presented. Using this cutting force components of 4-tooth endmills with various helix angles have been predicted. Predicted values of cutting force components are well coincide with the measured ones. The other is to compare the down endmilling characteristics of lnconel 718 with those of the up milling previously presented. In up endmilling as the helix angle becomes larger the radial and tangential components of the specific cutting force ($K_1 and K_r$) decrease. While in down milling $K_1 and K_r$ become smaller as the helix angle decrease.

• 한국기계가공학회지
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• 제8권4호
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• pp.48-53
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• 2009

Inconel 718 alloy, widely used as material of aircraft engine, has a good mechanical property in high temperature, strong anti-oxidation characteristics in oxidated current over $900^{\circ}C$, and also is not easily digested in the air containing sulfur, therefore, its usage as mechanical component is expanding rapidly. Even though Inconel alloy 718 is difficult to machine, it requires highly precise processing/machining to sustain its component quality of high accuracy. In this paper, general turning operation conditions are tested to select the best cutting process condition by measuring surface roughness through implementing experiments with orthogonal array of cutting speed, feeding speed and cutting depth as processing parameters based on the Taguchi method. Optimal turning operation conditions are extracted from the proposed experimental models.