• 제목/요약/키워드: Different frequency whirl

검색결과 5건 처리시간 0.03초

Experimental investigation of the whirl and generated forces of rotating cylinders in still water and in flow

  • Chen, Wei;Rheem, Chang-Kyu;Lin, Yongshui;Li, Ying
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제12권1호
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    • pp.531-540
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    • 2020
  • The whirl and generated forces of rotating cylinders with different diameters placed in still water and in flow are studied experimentally. For the rotating cylinders in still water, the Same Frequency Whirl (SFW) and Different Frequency Whirl (DFW) have been identified and illustrated. The corresponding SFW and DFW areas are divided. The Root Mean Square (RMS) values of the generated force coefficient dramatically increase in the defined ranges of Resonance I and Resonance II. For the rotating cylinders in flow, the hydrodynamics, SFW and DFW are illustrated. The hydrodynamic, SFW and DFW areas are divided. The RMS values of the generated forces in the range of Resonance II are much smaller than those in still water due to the generated lift forces. The discussion suggests that the frequency of the DFW may equal multiple times or one-multiple times that of the rotating frequency: the whirl direction of the DFW with multiple times the frequency of the rotating frequency is the same as the rotating direction. The whirl direction of the DFW with one-multiple times frequency of the rotating frequency is opposite to the rotating direction.

기어박스로 구동되는 축-저널베어링계의 동적특성에 관한 연구 (Dynamic Characteristics of a Rotor-Journal Bearing System Driven by Gearboxes)

  • 박상규
    • 소음진동
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    • 제5권4호
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    • pp.565-575
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    • 1995
  • Gearboxes are often used in the petrochemical and electrical power plants to transmit mechanical power between two branches of a machinery train rotating at different speeds. When the gearboxes are connected with rotors supported by journal bearings, bearing loads vary in magnitude and direction with rotor speed and torque transmitted by the gearboxes. In this study, dynamic characteristics of the system which consists of gearboxes and a rotor supported by journal bearings are investigated analytically and experimentally by employing the polynomial transfer matrix method and modal analysis under different speeds and torque levels. Journal bearing loads due to the transmitted torque are claculated analytically and the stiffness and damping coefficient of the journal bearings are obtained using finite element method. Comparison of the analytical and experimental results shows that the cross coupled stiffness coefficients increase with increasing rotor speed, while the cross coupled damping coefficients decrease. This generates the oil whirl instability in the journal bearings. As the transmitted torque level goes up, the stiffness coefficients of the journal bearing and the first horizontal natural frequency increase. High levels of the transmitted torque produce high bearing stiffness since the contact loads of the mating gear teeth increase. The logarithmic decrement, which is a stability indicator, is shown to decrease with increasing speed and decreasing torque. Thus, at the low torque level, the system become unstable even at the low shaft speed.

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Vibration Attenuation in Helicopters using an Active Trailing-edge Flap Blade

  • Natarajan, Balakumaran;Eun, WonJong;Shin, SangJoon
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2013년도 춘계학술대회 논문집
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    • pp.347-352
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    • 2013
  • Seoul National University Flap (SNUF) blade is a small-scaled rotor blade incorporating a small trailing-edge flap control surface driven by piezoelectric actuators at higher harmonics for vibration attenuation. Initially, the blade was designed using two-dimensional cross-section analysis and a geometrically exact one-dimensional beam analysis, and material configuration was finalized. Flap deflection angle of ${\pm}45^{\circ}$ was established as the criterion for better vibration reduction performance based on an earlier simulation. Flap linkage mechanism design is carried out and static bench tests are conducted to verify the flap actuation mechanism performance. Different versions of test beds are developed and tested with the flap and chosen APA 200M piezoelectric actuators. Through significant improvements, a maximum deflection of ${\pm}3.7^{\circ}$ was achieved. High frequency experiments are conducted to evaluate the performance and transfer function of the test bed is determined experimentally. As the static tests are almost completed, rotor power required for testing the blade in whirl tower (centrifugal environment) is calculated and further preparations are under way.

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와권(渦卷) 노즐의 무화기구(霧化機構)에 관(關)한 연구(硏究) (A Study on the Atomizing Mechanism for the Swirl Nozzle)

  • 이상우;판정순;석원앙
    • 농업과학연구
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    • 제14권1호
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    • pp.81-97
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    • 1987
  • 병충해방제(病蟲害防除)에 있어서 효율적(效率的)인 분무립자(噴霧粒子)의 크기는 $20{\mu}m$ 이내(以內)이지만 비산(飛散)의 해(害)를 감안하여 $140{\sim}200{\mu}m$를 추천하고 있다. 그러나 우리나라 수도방제기(水稻防除機)의 주종(主種)인 총포노즐의 경우 입자(粒子)크기는 $220{\sim}750{\mu}m$로 과대(過大)한 실정(實情)이다. 우리나라에서 널리 이용(利用)되고 있는 과권(過卷) 노즐의 구조(構造)를 Figure 2와 같이 고안(考案)하여 공기(空氣)를 혼합(混合)시킨 약액(藥液)을 이용(利用)함으로써 과실내(過室內)에서의 예비무화효과(豫備霧化效果), 약액(藥液)의 감소된 표면장력(表面張力) 및 점주(粘住), 분사액(噴射液)의 증가된 주파수(周波數)의 효과(效果)를 이용(利用)하여 분무립자(噴霧粒子)를 개선(改善)하고저 실시(實施)된 실험결과(實驗結果)는 다음과 같다. 분무립자(噴霧粒子) 크기는 분무압력(噴霧壓力)(본(本) 실험(實驗)에서는 $0.70kg/cm^2$부터 $6.33kg/cm^2$까지 실시(實施)) 이 증가(增加)됨에 따라서 점차로 미립화(微粒化)되었고 이 경향(傾向)은 표준(標準)노즐의 결과(結果)와 같다. 동일(同一)한 분무압력하(噴霧壓力下)에서 분무립자(噴霧粒子)의 크기 및 분포상태(分布狀態)를 표준(標準)노즐의 비교(比較)할 때 체적평균직경(體積平均直徑)이 작아졌고 입자(粒子)크기 분포(分布)도 개선(改善)되었다. 입자(粒子)크기 분포(分布)는 분무형(噴霧型)의 중심(中心)으로부터 외측(外側)으로 향(向)하면 체적평균직경(體積平均直徑)이 작아지는 현상(現象)이었다.

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SNUF뒷전 플랩 블레이드 메커니즘의 설계 개선 (Enhancement of SNUF Active Trailing-edge Flap Blade Mechanism Design)

  • ;은원종;신상준
    • 한국소음진동공학회논문집
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    • 제23권7호
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    • pp.645-653
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    • 2013
  • SNUF(Seoul National University flap) 블레이드는 고주파 영역에서 진동 감쇠를 위하여, 압전작동기에 의해 움직이는 뒷전 플랩이 장착되어 있는 축소형 로터 블레이드이다. 이 블레이드를 설계하기 위하여 2차원 단면 해석과 1차원 기하학적 정밀 보 해석이 수행되었고, 사용할 재료의 특성을 확인하였다. 이전 연구자들의 실험을 참조하여, ${\pm}4^{\circ}$의 플랩 변위각을 진동감쇠를 위한 설계요건으로 선정하였다. 플랩의 연결 메커니즘을 설계하고, 설계된 메커니즘의 성능을 확인하기 위하여 정적 벤치 시험을 수행하였다. 개선된 버전의 플랩 장치를 설계하고 시험하였으며, 압전작동기로는 APA 200M을 선정하였다. 장비의 개선을 통하여, 최대 플랩변위가 ${\pm}3.7^{\circ}$에 도달하였다. 성능을 평가하기 위하여 고주파 실험을 수행하였으며, 플랩 장치의 전달 함수를 실험적으로 결정하였다. 정적 시험을 완료하여, 훨타워 시험을 위하여 필요한 로터의 요구마력을 계산하였고, 그 이외의 준비가 진행 중에 있다.