• 제목/요약/키워드: Imbalanced vibration

검색결과 5건 처리시간 0.016초

스트레인 게이지법을 이용한 4,700 DWT 선박의 우현 전타시 프로펠러 편심추력이 축 거동에 미치는 영향 연구 (The Effect of Transient Eccentric Propeller Forces on Shaft Behavior Measured Using the Strain Gauge Method During Starboard Turning of a 4,700 DWT Ship)

  • 이재웅;김홍렬;임긍수
    • 해양환경안전학회지
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    • 제24권4호
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    • pp.482-488
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    • 2018
  • 선박 축계는 프로펠러 하중의 영향으로 선미관 후부베어링의 국부하중 증가가 현저히 나타나 축계 선미관 베어링 손상의 위험이 증대된다. 이를 방지하기 위해 수행된 추진축계 정렬연구는 주로 준정적 상태(quasi-static condition)에서 축과 지지베어링간의 상대적 경사각을 감소시키는데 중점을 두어 진행되어 왔다. 그러나 보다 상세한 평가를 위해서는 동적상태를 추가로 고려하는 것이 필요하다. 4,700 DWT 선박을 대상으로 NCR로 운전중 급속으로 우현 전타할 때 추진축계가 받는 영향에 대해 연구하였다. 연구결과 선미 유동장 변화에 의해 프로펠러 편심추력이 과도 상태가 되어 프로펠러에 불평형 진동이 유발되는 것을 확인하였다. 우현 전타시의 프로펠러 편심추력은 NCR 조건대비 축을 선미관 베어링으로부터 들어 올리는 힘으로 작용하여 선미관 베어링 하중완화에 기여하고 있음을 확인하였다.

회전자 편심을 가지는 IPM, SPM 전동기 진동 특성 비교: (1) 영구 자석에 의한 전자기력 (Comparison of Vibration Characteristics in IPM and SPM BLDC Motors with Rotor Eccentricity : (1) Electro-magnetic Force Due to PM)

  • 황근배;김경태;황상문
    • 한국소음진동공학회논문집
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    • 제11권9호
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    • pp.454-461
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    • 2001
  • Acoustic noise and vibration of a BLDC motor is a coupled phenomenon between mechanical characteristics and electromagnetic origins through the motor air-gap. When a relative misalignment of rotor in the air-gap center exists on the assemblage, it is considered to influence the motor system characteristics. In this paper, the back electro motive force(BEMF) is analyzed by Finite Element Method(FEM) and verified by experiments for the SPM and IPM type motors. For magnetic field analysis, a FEM is used to account for the magnetic saturation. Using these results, the FEM is made to determine the appropriate electromagnetic field analysis in BLDC motors with rotor eccentricity ratio. A radial magnetic imbalance force of BLDC motor with rotor eccentricity is analyzed. Results demonstrate that the imbalance force is increased according to the degree of misalignment. An IPM motor, mostly chosen to realize high-speed operation, shows a worse effect on magnetic unbalanced forces and dynamic responses compared with SPM motor due to magnetic saturation when the rotor eccentricity exists.

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Random vibration-based investigation of required separation gap between adjacent buildings

  • Atefeh Soleymani;Denise-Penelope N. Kontoni;Hashem Jahangir
    • Earthquakes and Structures
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    • 제26권4호
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    • pp.285-297
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    • 2024
  • Due to the imbalanced vibration of the adjacent buildings, the pounding phenomenon occurs as a result of an insufficient gap between them. Providing enough gap between adjacent structures is the most efficient approach to preventing the pounding effect. This paper calculated the required separation gaps between adjacent buildings, including two, four, eight, twelve and twenty stories steel moment-resisting frames, and investigated their related influencing parameters such as time periods, damping ratios, and the number of bays. The linear and nonlinear dynamic time-history analyses under real seismic event records were conducted to calculate the required separation gaps by obtaining relative displacement and velocity functions of two adjacent frames. The results showed that the required separation gap increased when the time periods of adjacent frames were not the same. The resulting separation gaps values of linear and nonlinear analyses were similar only for two and four stories frames. In other frames, the resulting separation gap values of linear analyses surpassed the corresponding nonlinear analyses. Although increasing the damping ratios in adjacent frames causes a decrease in the required separation gaps, the number of bays had no significant effect on them.

이단 왕복동 공기압축기 구조에 따른 관성력 비교 (Inertia Force Comparison of 2 Stage Reciprocating Air Compressors)

  • 김영철;안국영
    • 한국유체기계학회 논문집
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    • 제12권4호
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    • pp.23-29
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    • 2009
  • For the purpose of high outlet pressure, compactness and low vibration and noise, 2 stage reciprocating air compressors can have various cylinder arrangement: opposed, in-line, and V type. This paper presents an effective method to calculate the inertia forces and to design counter weight. This method is based on the complex representation for the orbital behavior of the compressor shaft. This method helps to find the optimal balancing rate easily to reduce the inertial force or moment. This paper shows that the residual inertia forces of the single throw shafts and the residual inertia moments of the double throw shafts remain to be imbalanced.