• Title/Summary/Keyword: 허브 베어링

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Current Technology Status of Bearingless Rotor Hub system for Helicopter (헬리콥터 무베어링 로터 허브 시스템 기술동향)

  • Kim, Deog-Kwan;Yun, Cheol-Yong;Song, Keun-Woong;Kim, Seung-Bum;Kim, Seung-Ho
    • Current Industrial and Technological Trends in Aerospace
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    • v.8 no.1
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    • pp.118-130
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    • 2010
  • In this paper, it is described the current technology status of bearingless rotor hub system for helicopter which is one of major rotor hub system. First, the advantages and disadvantages of major helicopter rotor hub system are described and compared each other. The unique characteristics of bearingless rotor hub system are described compared to other types of rotor hub systems. Next, the main function, role and characteristics of the sub-components of bearingless rotor hub system are described. Furtherly, recent helicopters which adopt this bearingless rotor hub system are described and introduced.

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Aerodynamic Drag Prediction of a Bearingless Rotor Hub (무베어링 로터 허브의 공기역학적 항력 예측)

  • Kang, Hee-Jung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.8
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    • pp.655-661
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    • 2012
  • In this study, aerodynamic drag of a bearingless rotor hub was predicted by computational fluid dynamics methodology using unstructured overset mixed meshes. The calculated results showed that the drag due to pressure forces rather than the viscous drag act as a major factor on both the fuselage and rotor hub, and the drag acting on the torque tube accounted for the largest portion in the hub drag. It was also found the hub drag accounted for 39 ~ 41% of the fuselage drag. Finally, the result confirmed the drag of the designed rotor hub satisfied the requirement of the aerodynamic hub drag by comparing with the drag trend of developed helicopter.

Design of an Elastomeric Bearing for a Helicopter Rotor Hub by Non-linear Finite Element Method (비선형 유한요소법을 이용한 헬리콥터 로터허브용 탄성체베어링 설계)

  • Kim, Hyun-Duk;Yoo, Si-Yoong;Park, Jung-Sun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.38 no.6
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    • pp.612-619
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    • 2010
  • In this paper, an elastomeric bearing for a helicopter rotor hub is designed using nonlinear finite element method. The elastomeric bearing is the main component of the helicopter rotor hub that acts as a hinge to three motions(flapping, lagging and pitching) of rotor blade. The elastomeric bearing consists of rubber and metal plates. The stiffness design of the elastomeric bearing is important because elastic deformation of rubber is served to hinge. Accordingly, the elastomeric bearing is designed to satisfy the stiffness requirements for rotor hub bearing. In this study, a FE model generation algorithm is developed and stiffness characteristic of a rubber plate is analyzed for an efficient design of the spherical elastomeric bearing. It is proven that the elastomeric bearing satisfies stiffness requirements of the spherical bearing for a helicopter rotor hub.

Requirement Analysis and Drag Prediction for the Aerodynamic Configuration of a Bearingless Rotor Hub (무베어링 로터 허브 형상에 대한 요구도 분석 및 항력 예측)

  • Kang, Hee-Jung
    • Aerospace Engineering and Technology
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    • v.11 no.1
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    • pp.19-26
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    • 2012
  • The requirement for the aerodynamic hub drag, allocated from the system requirement of development of a bearingless rotor hub, was analyzed and embodied to be substantiated by the methodology assigned from the requirement. Drag prediction for the initial hub configuration was carried out by hand calculation using aerodynamic drag coefficients and the design change about the sectional shape of torque tube was suggested to satisfy the requirement. Finally, drag prediction was performed for the changed hub configuration by using unstructured overset mesh technique and parallel computation and the calculated result satisfied the requirement of the aerodynamic hub drag. It was found that the drag of final hub configuration was also within the range of drag inferred from the trendline of developed helicopter.

Fatigue Safe Life Analysis of Helicopter Bearingless Rotor Hub Composite Flexbeam (헬리콥터 무베어링 로터 허브 복합재 유연보 피로 안전수명 해석)

  • Kim, Taejoo;Kee, Youngjoong;Kim, Deog-Kwan;Kim, Seung-Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.7
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    • pp.561-568
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    • 2013
  • After we designed Bearingless rotor hub system for 7,000lb class helicopter, flexbeam fatigue analysis was conducted for validation of requirement life time 8,000 hours. sectional structural analysis method applying elastic beam model was used. Fatigue analysis for two sections of flexbeam which were expected to weak to fatigue damage from result of static analysis was conducted. Extension, bending and torsion stiffness of flexbeam section shape was calculated using VABS for structure analysis. S-N curve of two composite material which composed flexbeam was generated using wohler equation. Load analysis of bearingless rotor system was conducted using CAMRAD II and load analysis result was applied HELIX/FELIX standard load spectrum to generate bearingless rotor system load spectrum which was used flexbeam fatigue safe life analysis.

Fatigue Safe Life Analysis of Helicopter Rotor Bearingless Hub System Composite Components (헬리콥터 로터 무베어링 허브 시스템 복합재 구성품 피로 안전수명 해석)

  • Kim, Taejoo;Kee, Youngjoong;Kim, Deog-Kwan
    • Aerospace Engineering and Technology
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    • v.13 no.1
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    • pp.10-19
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    • 2014
  • We designed bearingless rotor hub system which replace mechanical hinge/bearing with composite beam component and conducted fatigue analysis for flexbeam and torque tube. Extension/bending/torsional stiffness was calculated from 2D section analysis using VABS and 2D section structure analysis was applied for strain calculation. S-N curve of each composite material was generated using Wohler equation and fatigue analysis was conducted on weakness section which was decided from static structure analysis. CAMRAD II was used for load analysis and load analysis result was applied HELIX/FELIX standard load spectrum to generate bearingless rotor system load spectrum which was used fatigue safe life analysis.

Faults Detection Method Unrelated to Signal to Noise Ratio in a Hub Bearing (신호대 잡음비에 무관한 허브 베어링 결함 검출 방법)

  • Choi, Young-Chul;Kim, Yang-Hann;Ko, Eul-seok;Park, Choon-Su
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.14 no.12
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    • pp.1287-1294
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    • 2004
  • Hub bearings not only sustain the body of a cat, but permit wheels to rotate freely. Excessive radial or axial load and many other reasons can cause defects to be created and grown in each component. Therefore, nitration and noise from unwanted defects in outer-race, inner-race or ball elements of a Hub bearing are what we want to detect as early as possible. How early we can detect the faults has to do with how the detection algorithm finds the fault information from measured signal. Fortunately, the bearing signal has Periodic impulse train. This information allows us to find the faults regardless how much noise contaminates the signal. This paper shows the basic signal processing idea and experimental results that demonstrate how good the method is.

Faults Detection in Hub Bearing with Minimum Variance Cepstrum (최소 분산 켑스트럼을 이용한 자동차 허브 베어링 결함 검출)

  • 박춘수;최영철;김양한;고을석
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2004.05a
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    • pp.593-596
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    • 2004
  • Hub bearings not only sustain the body of a car, but permit wheels to rotate freely. Excessive radial or axial load and many other reasons can cause defects to be created and grown in each component. Therefore, vibration and noise from unwanted defects in outer-race, inner-race or ball elements of a Hub bearing are what we want to detect as early as possible. How early we can detect the faults has to do with how the detection algorithm finds the fault information from measured signal. Fortunately, the bearing signal has periodic impulse train. This information allows us to find the faults regardless how much noise contaminates the signal. This paper shows the basic signal processing idea and experimental results that demonstrate how good the method is.

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A Study on Transfer Process Design on Hot Forging of Bearing Hub (베어링 허브의 트랜스퍼 열간 단조 공정 설계에 관한 연구)

  • Byun H.S.;Kim B.M.;Ko D.C.
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2005.10a
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    • pp.993-996
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    • 2005
  • This paper is concerned with transfer process on hot forging of bearing hub. Workers on hot forging have difficulty in working by high temperature and weight workpiece. And In conventional got forging of bearing hub, the material wasted to the flash accounts approximately 10% of the original workpiece. It is need manufacture automation and reduce the cost of forged products. Surface treatment of die and lubricant are investigated from experiment and FE-simulation for analysis of forming simulation. In order to hot forging process design considered flash thickness and blocker geometry and initial temperature of die and billet. This transfer process gave comparatively good results compared with actual products.

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Development of Diagnosis System for Hub Bearing Fault in Driving Vehicle (차량 주행 상태에서 허브 베어링 이상을 진단할 수 있는 장치 개발)

  • Im, Jong-Soon;Park, Ji-Hun;Kim, Jin-Yong;Yun, Han-Soo;Cho, Yong-Bum
    • Transactions of the Korean Society of Automotive Engineers
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    • v.19 no.2
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    • pp.72-77
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    • 2011
  • In this paper, we propose effective diagnosis algorithm for hub bearing fault in driving vehicle using acceleration signal and wheel speed signal measured in hub bearing unit or knuckle. This algorithm consists of differential, envelope and power spectrum method. We developed diagnosis system for realizing proposed algorithm. This system consists of input device including acceleration sensor and wheel speed sensor, calculation device using Digital Signal Processor (DSP) and display device using Personal Digital Assistant (PDA). Using this diagnosis system, a driver can see hub bearing fault(flaking) from the vibration in driving vehicle. With early repairing, he can keep good ride feeling and prevent accident of vehicle resulting from hub bearing fault.