• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2003년도 춘계학술대회논문집
• /
• pp.950-955
• /
• 2003

This paper introduces an enhanced condition monitoring and diagnosis system recently developed for rotating machinery. In the system, the data aquisition/monitoring signal processing, machine condition classifier, case-based reasoning and demonstration modules are effectively integrated with user-friendliness so that machine operators can easily monitor and diagnose the status of rotating machinery in operation. Some of the new features include the directional spectrum, case-based reasoning and neural network techniques. And the demonstrator modules for fault diagnosis of a Bear driving system and for basic understanding of the rotor dynamics are provided to help the potential users better understand the system.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2013년도 추계학술대회 논문집
• /
• pp.585-588
• /
• 2013

Electric motor with reduction gear systems are being adopted recently as main propulsion on the special-purposed ships. These specialized ships or offshore vessels require higher power rating generators for propulsion and accommodation power supply. This study investigated the cause of exciter components failure in the view of excessive vibration, force or abnormal ship motion in service. Countermeasures are proposed to address the exciter component failure. A 1.4 MW class dual-fuel engine generator using rigid foundation for a LNG carrier was used as research model.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 1997년도 추계학술대회논문집; 한국과학기술회관; 6 Nov. 1997
• /
• pp.70-75
• /
• 1997

Power driving shaft systems with reduction gear are frequently equipped with elastic couplings to protect reduction gears and to relieve the torsional vibration problems. In this study, torsional vibration characteristics for the engine shafting system with elastic couplings are investigated and the calculating program is developed. It is confirmed that torsional vibration can be controled by careful selection of a elastic coupling with suitable characteristics and the suitability of a elastic coupling can only be determined as a result of a complete torsional vibration analysis including engine conditions such as misfring for shafting system.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2004년도 추계학술대회논문집
• /
• pp.508-512
• /
• 2004

This paper described operation and vibration characteristics of 'Tail-Fan' performance test system. KARI(Korea Aerospace Research Institute) developed 'Tail-Fan' system as a kind of helicopter anti-torque system(ATS) and designed ATS performance test-rig for Tail-Fan system performance test. Test-rig consists of driving parts, supporting parts and rotating parts. For Tail-Fan system performance tests, firstly, test-rig operation tests were carried out for verification of design specifications. Secondly, natural frequencies of fan blade and test-rig were measured respectively. Lastly, to find the operation rotating speed for performance tests, vibration tests using accelerometers on tail gear box(TGB) were carried out. Through the fanplot and vibration test results, Tail-Fan performance test conditions to avoid a resonance were found and performance tests were well done safely.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2004년도 추계학술대회논문집
• /
• pp.1056-1061
• /
• 2004

The vibration of rotor systems is caused by various factors, such as misalignment, unbalance, gear meshing, error of assembly, etc. Modal test and TDA/ODS analysis were done. The dynamic analysis of the armature was done with SAMCEF which is a commercial software for finite element and kinematic analysis. The transient response of the armature is calculated by the SAMCEF with the consideration of magnetic force and bearing stiffness, which are the essential elements for the design of high speed cutter. Main frequency of the vibration is due to the unbalance of the armature. The FEM analysis model considering unbalance and the high speed cutter have same vibration properties. The vibration sources of the high speed cutter is proved to be unbalance.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2005년도 춘계학술대회논문집
• /
• pp.692-697
• /
• 2005

좋은 날개 실속특성 및 실속/스핀의 특성이 입증된 선미익형 항공기를 현재 개발중에 있다. 전에 개발된 1호기 및 2호기 시제기는 코어 샌드위치 형식으로 날개 전체가 채워지고 고정식 착륙장치로 제작되었다. 새로이 개발될 반디호는 접개식 착륙장치와 날개와 동체에 일반적인 폼 코아 샌드위치층이 장착될 예정이다. 제작을 위해 시편 시험을 포함한 복합 소재 제작 공정이 연구되었고 적층 몰드를 이용하여 유리 섬유 천으로 폼 코어 위로 상온 적충하는 방식이 채택되었으며, 복합소재 부품들은 실온과 대기압하에 경화시킨다. 일반적으로, 몰드부품들은 양산에 적합한 매끄러운 표면 조도와 표준 품질을 보여주었다. 본 연구에서는 소형 항공기 반디호 몰드 기술과 개발 상황을 기술하였다.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2006년도 추계학술대회논문집
• /
• pp.523-530
• /
• 2006

A rotordynamic analysis was performed with a dry vacuum pump, which is a major equipment in modern semiconductor and LCD manufacturing processes. The system is composed of screw rotors, lobes picking air, helical gears, driving motor, and support rolling element hearings of rotors and motor. The driving motor-screw rotor system has a rated speed of 6,300rpm, and was modeled utilizing a rotordynamic FE method for analysis, which was verified through the results of its 3-D finite element model. As loadings on the bearings due to the gear action were significant in the system considered, each resultant bearing load was calculated determinately and indeterminately by considering the generalized forces of the gear action as veil as the rotor itself. Each resultant hearing loading was used in calculating each stiffness of rolling element bearings. Design goals are to achieve wide separation margins of critical speeds and favorable unbalance responses of the rotor in the operating range. Then, a complex rotordynamic analysis of the system was carried out to evaluate its forward synchronous critical speeds, whirl natural frequencies and mode shapes, and unbalance responses under various unbalance locations. Results show that the entire system is well designed in the operating range. In addition, the procedure of rotordynamic analysis for dry vacuum pump rotor-bearing system was proposed and established.

• 한국항공우주학회지
• /
• 제48권11호
• /
• pp.837-847
• /
• 2020

본 논문에서는 20g급 날갯짓 초소형 비행체의 정지 비행 시의 날갯짓 효율을 증가시키기 위한 날갯짓 속도 분포 최적화를 진행하였다. 비원형 기어를 이용하여 다양한 날갯짓 속도 분포를 나타내는 메커니즘을 설계하였으며, 실증 기체를 이용하여 실험적으로 날갯짓 속도 분포 최적화를 진행하였다. 최적화 모델은 노이즈를 포함한 Kriging을 사용하였으며 불확실성에 의한 오차를 반영하였다. 날갯짓 속도 분포를 네 개의 파라미터로 나타내어 각 파라미터에 대한 최적화를 진행하였고. 최적화 결과 추력-파워비가 11.3% 증가하였다. 추력-파워비가 증가한 이유에 대해 탄성력에 의해 이전 스트로크에서의 각운동에너지가 일부 보존되어 다음 스트로크에서 사용되어 효율이 높아진 것으로 분석하였다.

• 한국소음진동공학회논문집
• /
• 제17권10호
• /
• pp.967-975
• /
• 2007

A rotordynamic analysis was performed with a dry vacuum pump, which is a major equipment in modern semiconductor and LCD manufacturing processes. The system is composed of screw rotors, lobes picking air, helical gears, driving motor, and support rolling element bearings of rotors and motor. The driving motor-screw rotor system has a rated speed of 6,300 rpm, and was modeled utilizing a rotordynamic FE method for analysis, which was verified through 3-D FE analysis and experimental modal analysis. As loadings on the bearings due to the gear action were significant in the system considered, each resultant bearing load was calculated by considering the generalized forces of the gear action as well as the rotor itself. Each resultant bearing loading was used in calculating each stiffness of rolling element bearings. Design goals are to achieve wide separation margins of lateral and torsional critical speeds, and favorable unbalance responses of the rotor in the operating range. Then, a complex rotordynamic analysis of the system was carried out to evaluate its forward synchronous critical speeds, whirl natural frequencies and mode shapes, unbalance responses under various unbalance locations, and torsional interference diagram. Results show that the entire system is well designed in the operating range. In addition, the procedure of rotordynamic analysis for dry vacuum pump rotor-bearing system was proposed and established.

• 비파괴검사학회지
• /
• 제36권3호
• /
• pp.195-201
• /
• 2016

금속성부품의 자동화 생산라인 상에서 결함검사는 통상 시스템 가격이 합리적이고 고속검사가 가능한 와전류검사(ECT, eddy current testing) 기법이 많이 사용된다. 이러한 금속성 피검사체 가운데 특별히 스플라인 샤프트(spline shaft)의 스플라인 기어부(spline gear)와 같이 표면이 고르지 못한 피검사 대상에 대하여 ECT검사를 적용할 경우 주파수 분포도가 유사하면서 동시에 상대적으로 큰 표면신호로 인해 센서로부터 획득한 원신호와 결함에 의해 발생한 신호를 분리해내기가 어렵다. 이러한 스플라인 기어부의 결함신호 검출을 용이하게 하기 위해서는 주변 잡음신호에서 결함신호만을 구분해낼 수 있는 고차필터의 구현이 필수적이고 동시에 각 생산라인과 피검사체의 상황에 따라 필터의 통과대역을 조절할 수 있어야 한다. 이러한 통과대역 조절이 가능한 고차필터 구현을 위해 디지털 방식 중 하나인 IIR (infinite impulse filter) 필터에 의한 구현방안을 검토하고, 신호검출을 위해 시스템 레벨에서 설계요소들의 최적화를 통해 결함신호검출을 시도하였다.