• Title/Summary/Keyword: 회전체-베어링계

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Dynamic Behavior Analysis of Rotor-Bearing System for Rotary Compressor (로터리 압축기 회전체-베어링계의 동적 거동해석)

  • 김태학
    • Journal of Advanced Marine Engineering and Technology
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    • v.23 no.2
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    • pp.244-251
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    • 1999
  • Large dynamic loads act on the rotor in rotary compressors. There are unbalance forces due to eccentric rotation parts and gas forces induced by the pressure difference between compression and suction gases. Rotor-journal bearing system is nonlinear since the stiffness and damping coef-ficients of the lubrication oil film are not constant in the bearings. in this paper the program for predicting the behaviors of rotor-journal bearing system of rotary compressor is developed. Finite element modeling is used to analyze the flexible rotor. The numerical results are compared with experimental results.

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Steady State Response of a Rotor Supported on Cavitated Squeeze Film dampers (공동 스퀴즈 필름 댐퍼에 지지된 회전체의 정상상태 응답 해석)

  • 정시영;정재천;심상규
    • Proceedings of the Korean Society of Tribologists and Lubrication Engineers Conference
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    • 1992.06a
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    • pp.77-81
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    • 1992
  • 스퀴즈 필름 댐퍼 (Squeeze Film Damper, SFD)는 구조가 단순하면서도 감쇠성능이 우수하여 구름베어링에 지지된 고속회전체의 댐퍼로 이용되고 있으며 특히 대부분의 항공기용 터보엔진에 장착되어 고속회 전체의 댐퍼로서의 우수성을 보여주고 있다. 또한 동력기계의 단위 무게당 고출력화 경향으로 인하여 회전체의 경량화와 고속회전은 더욱 절실히 요구되고 있다. 이에따라 기계의 회전속도를 제 1차 또는 제 2차 위험속도(critical speed)이상까지 상승시켜야 하므로 SFD의 활용범위는 앞으로도 점차 증가할 것이다. 본 논문에서는 Swift-Stieber 경계조건을 적용하여, 공동현상이 발생하는 무한 폭 SFD의 유막력과 감쇠계수를 구한 후 강성 및 유연회전체의 정상상태 응답을 해석함으로써 공동현상이 회전체-SFD계의 진동에 미치는 영향을 연구하고자 한다.

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A Comparison of Dynamics of Rotor Systems for Different Internal Damping Models (분포 내부 감쇠 모형에 따른 회전체 계 동특성 비교 연구)

  • 박종혁;전봉석;강중옥;홍성욱
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2001.11b
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    • pp.838-843
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    • 2001
  • Internal damping plays an important role in some rotor dynamic systems with the use of various materials for shafts, for example, composite material. However, although the effects of internal damping have been investigated for a couple of decades, there are several different internal damping models in use, none of which are accepted as the most reliable model. The purpose of this paper is to compare the results of dynamic analysis of rotor systems with several different internal damping models. The exact dynamic element method is used to formulate and analyze the problem. The simulation results provided in this paper may be useful for the dynamic analysis of high rotor systems subject to significant internal damping.

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Isotropic Control of Rotor Bearing System (회전체 베어링계의 등방 제어)

  • 김철순;이종원
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 1993.04a
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    • pp.101-106
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    • 1993
  • A new rotor control scheme, the isotropic control of anisotropic rotor bearing system in complex state space, is proposed, which utilizes the concepts on the eigenstructure of the isotropic rotor system. Then the control scheme is applied to an active magnetic bearing system and the control performance is investigated in relation to control energy, transient response, and unbalance response. In particular, it is shown that the proposed method is efficient for control of unbalance response.

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Development of Dynamic Vibration Absorber to Reduce Unbalance Response in Flexible Rotor-Bearing System (탄성 회전체 베어링 계의 불균형 응답 저감을 위한 동흡진기 개발)

  • Yu, Tae-Gyu;Bae, Gyu-Hyun;Kim, Kil-Hwan;Hong, Seong-Wook
    • Journal of the Korean Society of Manufacturing Technology Engineers
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    • v.21 no.1
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    • pp.175-181
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    • 2012
  • This paper presents a novel dynamic vibration absorber (DVA) to suppress the unbalance response of flexible rotor-bearing systems. The DVA unit consists of two DVAs, an adapter to place the DVAs and an adapter frame to locate the adapter. The essential feature of the proposed DVA unit is to place itself on any desirable location of the shaft without disassembling the rotor-bearing system under consideration. A simulation with a 3D element based commercial rotor dynamic software is made to test the possibility of the proposed DVA on the suppression of unbalance response in rotor-bearing systems. Experiments are performed to validate the proposed DVA unit. The simulation and experiments show that the proposed DVA unit is very effective to suppress the unbalance response in rotor-bearing system at designated rotational speeds of interest.

A Study on the Vibration of Rotordynamic System Structured Rotor-Bearing and Rotor-Bearing-Stator (로터-베어링/로터-베어링-스테이터로 구성된 회전체 진동에 관한 연구)

  • 주성현;김광식;김창호;이성철
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 1990.10a
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    • pp.173-178
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    • 1990
  • 로터-베어링축계는 증기및 가스터빈, 터보 발전기, 압축기등 거의 모든 산업 기계류에서 동력 전달의 기본 도구로써 사용되고 있다. 즉 회전에 의한 동력 의전달은 비교적 간단히 대용량의 동력을 효율적으로 전달할 수 있다. 이에 따라 회전기계류에 대한 연구는 산업 혁명 이후 꾸준히 발전되어 온바, 특히 근래에 들어와 산업기계류의 경쟁이 치열하여짐에 따라 산업기계류의 고정 밀화, 고속화, 고신뢰화 요구가 증대하고 있는 현실을 비추어 볼때, 산업 기 계류의 근간을 이루고 있는 로터-베어링 축계의 안정성을 포함한 진동에 관 한 문제는 회전기계류 설계의 주요 기술로써 연구.개발의 필요성이 매우 높 다 하겠다. 회전축계 진동 관련 연구는 두 분야로 대별될 수 있는데 언밸런 스(Unbalance)에 의한 Synchronous진동과 여러가지 원인에 의해 계의 불안 정성을 유발시키는 Nonsynchronous진동으로 나눌 수 있다. 본 연구에서는 이들 연구의 기본이 되는 회전축-베어링계 동특성 해석 프로그램을 개발하 였다. 여러가지 방법이 있으나 여기서는 Holzer가 비틀림 진동에 적용하고, Mykiestad(2)와 Prohl(3)에 의하여 회전축의 횡 진동에 적용된 이후 Lund(4) 등에 의하여 베어링의 영향등이 첨가된 전달 매트릭스 (Transfer Matrix) 방 법을 이용하여 임계속도(Critical Speed), 모우드 형태(Mode shapes)를 예측 하고 불안정 판정(Instability Criteria)등을 할 수 있는 프로그램을 개발하였 다. 특히 Murphy(1)의 다항식 방법(Polynomial Method)에 기본을 두어 기존 의 전달 매트릭스가 가지고 있던 반복, 수렴 시간 문제와 빠뜨리는 임계속도 예측에 대한 개선을 이루었으며 기존 논문과 실험 결과와의 비교 검토를 통 하여 개발된 프로그램의 신뢰성을 검토하였다. 특히, 각종 회전 기계의 소형 화, 경량화 추세에 따라 지반이나 케이싱이 경량이거나 유연하여 회전축과 동적으로 연성된 경우 회전축-베어링-지반으로 이루어진 2중구조의 회전축 계 동특성을 해석할 수 있는 프로그램을 개발하므로서 회전 기계류의 진동 전반에 걸친 문제점에 대한 그 원인과 현상을 명확히 분석하여 국내의 전기 계류의 보다 신뢰성있는 설계 및 제작자료를 확보하는데 기여할 수 있게 하 였다.

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Idetification of Parameter for Bearing Using Sensitivity Analysis Method (민감도 해석 기법을 이용한 베어링 파라미터 규명)

  • 이경백;김영배
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2001.04a
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    • pp.354-357
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    • 2001
  • The developed method is proposed to identify rotor dynamic parameters. The method known imbalance vector, which renders over-determined linear system equation. The solution of the system equation can be obtained using least square method. The sensitivity analysis is performed to extract optimized solution, which is considered to be insensitive to inherent measurement errors. As an alternative approach to identify the parameters of bearings and rotor, adding a known imbalance to the rotor produces another equation set to make the system equations over-determined and linearly independent.

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Identification of Parameter for Bearing Using Orbit Shapes (궤도형상 데이터를 이용한 베어링 파라미터 규명)

  • 이경백;김영배
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 1997.10a
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    • pp.672-675
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    • 1997
  • This paper presents the identification of rotor dynamic parameters. The solution of the system equation can be obtained using least square method. The sensitivity analysis is performed to extract optimized solution, which is considered to be insensitive to inherent measurement errors. The cosine and sine term of orbit shapes can be obtained by experiment the orbit analysis at a different speed after doing orbit analysis at an arbitrary selected speed. This values measured time domain used to search the stiffness and damping coefficients of rotor bearing.

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Estimation of the Unmeasured Unbalance Responses and Identification of Bearing Parameters in Flexible Rotor-Bearing Systems (회전체 베어링계의 불균형응답 간접추정과 베어링 매개변수 규명)

  • 홍성욱;이종원
    • Journal of KSNVE
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    • v.2 no.3
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    • pp.193-202
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    • 1992
  • The unbalance response analysis is one of the essential area in the forced vibration analysis of rotor bearing systems because of it usefulness in balancing and diagnosis as well as identification of parameters involved in rotor bearing systems. However some unbalance responses are not measurable due to the fact that rotor bearing systems are often encapsulated by fixtures or safety protectors. In the present paper, an efficent estimation scheme for unmeasured unbalance responses in rotor bearing systems is developed. The fundamental fearture of the proposed method is characterized by the linear formulae to estimate the unbalance responses from the measured unbalance responses and the finite element auxilliary model equation which is constructed to be identical to the prototype excluding the uncertain parameters such as bearing coefficients. The identification formulae for bearing parameters are also derived by using the unbalance response and the finite elements auxiliary model. Simulation is provided to verify the effectiveness of the proposed method.

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Identification of parameter for Bearing Using Orbit Data (궤도형상 데이터를 이용한 베어링 파라미터 규명)

  • 이경백;정찬범;김영배
    • Journal of the Korean Society for Precision Engineering
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    • v.20 no.3
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    • pp.112-119
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    • 2003
  • This paper presents the identification of rotor dynamic parameters. The solution of the system equation can be obtained using least square method. The sensitivity analysis is performed to extract optimized solution, which is considered to be insensitive to inherent measurement errors. The cosine and sine term of orbit shapes can be obtain ed through the by experiment of the orbit analysis at a different speed after doing orbit analysis at an arbitrary selected speed. This values measured time domain are used to search the stiffness and damping coefficients of rotor bearing.