• Title/Summary/Keyword: 역방향선회

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Effect of friction and eccentricity on rebbing phenomenon (회전마멸현상에서의 마찰과 편심의 영향)

  • 최연선;김준모;정호권
    • Journal of KSNVE
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    • v.6 no.6
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    • pp.819-825
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    • 1996
  • Nonlinear dynamic characteristics of rubbing phenomenon in rotor dynamics are investigated experimentally and numerically. Rubbing phenomenon occurs when rotor contacts with stator during whirling and causes the large amplitude of vibration, high whirl frequencies, and possibly catastrophic failure. Rubbing has various types of forward whirl, backward rolling, backward slipping, and partial rub depending on the system parameters of rotating machinery and running speed. Experiments are performed for forward whirl and backward whirl. And numerical analysis are conducted to explain the changes between backward rolling and backward slipping. Experimental and numerical results show that the types of whirling motion depends on the friction coefficient between rotor and stator and the eccentricity of rotor.

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Development of Hybrid/Dual Jet Combustor for a MGT (Part I: Experimental Study on Geometric Optimization) (마이크로 가스터빈용 하이브리드/이중 선회제트 연소기 개발 (Part I: 형상 최적화를 위한 실험연구))

  • Park, Tae-Joon;Hwang, Cheol-Hong;Lee, Kee-Man
    • Journal of the Korean Society of Propulsion Engineers
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    • v.17 no.5
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    • pp.60-69
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    • 2013
  • An optimum configuration of the hybrid/dual swirl jet combustor for a micro-gas turbine was investigated experimentally. Location of pilot nozzle, angle and direction of swirler vane were varied systematically as main parameters under the conditions of constant thermal load. The results showed that the variation in locations of inner fuel nozzle and pilot burner resulted in significant change in flame shape and swirl intensity due to the changes in recirculating flow pattern and minimum flow area near burner exit, in particular, with the significant reduction of CO emission near lean-flammability limit. In addition, it was observed that the co-swirl configuration produced less CO and NOx emissions compared to the counter-swirl configuration.

Development of Gasoline Direct Swirl Injector (직접분사식 가솔린 선회분사기 개발에 관한 연구)

  • Park, Yong-Guk;Lee, Chung-Won
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.25 no.1
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    • pp.78-86
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    • 2001
  • The Gasoline Direct Injection(GDI) system has been highlighted due to the improvement of fuel consumption and the control of exhaust emission from gasoline engines. The GDI system includes a high injection pressure, smaller mean diameter, good spray characteristics and stability. We were interested in the development for gasoline direct swirl injector(GDSI) in which the swirler is specially designed with an incident angle. Nymerical analysis was utilized to investigate the internal flow of GDSI with a goal to determine the swirl incident angle and needle lift. Accordingly, it describes characteristics of a GDSI in which the flowrate and spray characteristics are satisfied. especially the spray tip penetration decreases, compared with other type GDI, mean diameter of droplets is from 20${\mu}{\textrm}{m}$ to 25${\mu}{\textrm}{m}$ and spray angle ranges from 64$^{\circ}$to 66$^{\circ}$.