• 제목/요약/키워드: Flange-Shaft Assembly

검색결과 3건 처리시간 0.018초

드럼세탁기 축계의 피로수명 평가 (Fatigue Life Evaluation for Flange-Shaft Assembly of Front Loading Washing Machine)

  • 김대진;위우택;석창성;이근호;민제홍
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2006년도 춘계학술대회 논문집
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    • pp.429-430
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    • 2006
  • To estimate the fatigue life of flange-shaft assembly, fatigue test for flange material and bending fatigue test for flange-shaft assembly were conducted. Also, finite element analysis for flange-shaft assembly was conducted. Then, we have changed the obtained P-N curve to S-N curve using the finite element analysis results which were stress values at the location of fracture. The S-N curve of flange material itself was almost consistent with that of flange-shaft assembly, so it seems that the fatigue life of flange-shaft assembly could be estimated by using S-N curve for flange material and the stress at the location of fracture calculated by finite element methods.

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발전용 축계 결합용 커플링 볼트 설계에 관한 연구 (Study on Design of Coupling Bolt for Shaft in Power Plant)

  • 정호승;손창우;조종래;김태형
    • 대한기계학회논문집A
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    • 제37권5호
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    • pp.707-713
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    • 2013
  • 커플링 볼트는 조립, 분해 시 작업자의 안전이 고려되는 부분이나 공정 중단의 비용이 중요한 부분에서 기존의 일반볼트를 대체한다. 해양과 발전분야에서 세계적으로 광범위하게 적용되어, 회전하는 플랜지 결합에 사용되어 왔고, 국제적인 국가 선급 협회나 규제기관의 사용을 승인받아 왔었다. 커플링 볼트는 유압식으로 인장되어 플랜지 사이를 안정적으로 단단히 결합한다. 본 논문에서는 발전소 커플링 볼트의 국산화를 위해, 역설계를 통해 현재 사용 중인 볼트의 치수를 측정, 역학적인 수식을 통해 권장 체결하중의 기준을 살펴보았다. 마찰계수는 실험을 통해 선정하였고, 구조해석을 통해 체결상태를 확인하였다. 형상변수에 따른 접촉압력의 변화를 볼트 재설계시 참고할 수 있도록 나타내었다.

터보차져용 터빈의 스핀 테스트를 위한 로터다이나믹 특성분석 (Rotordynamic Characteristics Analysis of Turbocharger Turbine for Spin Test)

  • 김병옥;양성진;이명호
    • 한국유체기계학회 논문집
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    • 제14권6호
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    • pp.91-95
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    • 2011
  • This paper deals with the detail rotordynamic analysis for the assembly rotor composed of turbine wheel, turbine shaft, connecting arbor, and flange & spindle in order to perform the spin test of turbocharger turbine. Prior to rotordynamic analysis, the 1st spin test was performed but the test was failed by excess vibration in the neighborhood rated speed. It is the reason for this fail that the separation margin between the rated speed and critical speed is not enough, confirmed by rotordynamic analysis results. Since then, the dimension of turbine shaft was modified and the critical speeds were again reviewed for modified assmebly rotor. In results, the separation margin between the rated speed and critical speed is over 20% and then the 2nd spin test was performed successfully. In preparing spin test for turbine, compressor wheels and etc., the geometry design of connecting arbor and dimension of rough machining should be reviewed by considering rotordynamic results, and the separation margin should be enough for successful spin test.