• Title/Summary/Keyword: 3 분력

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The Effect of the Bolted Joint Stiffness on the Thrust Measurement Stand (볼트의 체결 강성이 추력 시험대에 미치는 영향)

  • Lee, Kyujoon;Jung, Chihoon;Ahn, Dongchan
    • Journal of the Korean Society of Propulsion Engineers
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    • v.20 no.5
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    • pp.31-39
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    • 2016
  • This paper is studied on the effect of the bolt joint stiffness on the Thrust Measurement Stand(TMS). TMS is a test stand for thrust performance of the propulsion system, which depends on two factors: The $1^{st}$ is the parallel degree between directions of the thrust vector and action lines of the corresponding measuring load cells for the vector, and the $2^{nd}$ is the orthogonality between action lines of the measuring load cells. Therefore, it is essential to maintain the original shape of the TMS under operating conditions. In this paper, it is examined how the geometric tolerance of the bolt joints and threads of the load cell trains affect the performance of the TMS. Also, some techniques to overcome related problems are proposed.

Design and Strain Analysis of Precision 3-component Load Cell (정밀 3분력(Fz, Fy, Mz) 로드셀의 설계 및 변형률해석)

  • Kim, Gab-Soon;Rhee, Se-Hun;Um, Ki-Woan
    • Journal of the Korean Society for Precision Engineering
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    • v.16 no.3 s.96
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    • pp.222-232
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    • 1999
  • This paper describes the development of a precision 3-component load cell with plate beams which may be used for measuring forces Fx, Fy and moment Mz simultaneously in industry. We have derived equations to predict the bending strains on the surface of the beams under forces or moment. We have also determined the attachment location of strain gages of each sensor and fabricated 3-component load cell. To evaluate the rated strain and interference error of each sensor, we have carried out characteristic test of precision 3-component load cell. It reveals that the rated strain calculated from the derived equations are good agreement with the results from Finite Element Method analysis.

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A Study of Development for Contact CMM Probe using Three-Component Force Sensor (3 분력 힘 센서를 이용한 CMM 용 접촉식 프로브의 개발에 관한 연구)

  • 송광석;권기환;박재준;조남규
    • Journal of the Korean Society for Precision Engineering
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    • v.20 no.8
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    • pp.101-107
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    • 2003
  • A new mechanical probe for 3-D feature measurement on coordinate measuring machines (CMMs) is presented. The probe is composed of the contact stylus and the three-component force sensor. With the stylus mounted on the force sensor, the probe can not only measure 3-D features, but also detect contact force acting on the stylus tip. Furthermore, the probing direction and the actual contact position can be determined by the relationship among three components of contact force to be detected. In this paper, transformation matrix representing the relationship between the external force acting on the stylus tip and the output voltages of measurement gauges is derived and calibrated. The prototype of probe is developed and its availability is investigated through the experimental setup for calibration test of the probe. A series of experimental results show that the proposed probe can be an effective means of improving the accuracy of touch probing on CMM.

Modeling Scheme for the Six-components Force Measurements of Solid-propellant Rocket Motors (고체 추진기관 6분력 시험대의 모델링 기법)

  • 박익수;이규준;윤일선;김중근
    • Journal of the Korean Society of Propulsion Engineers
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    • v.5 no.3
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    • pp.79-86
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    • 2001
  • The six-components force measurements systems for rocket motors are used to measure multi components force generated by TVC(Thrust Vector Control) motors. This paper suggested the modeling scheme which is used in preliminary design and test analysis procedure and which can be applied to the existing other test stand in operation. The model whose parameters are determined by least square method makes the design engineer build the test stand to satisfy all kinds of requirements such as accuracy, operating condition and structural stability without tradeoff among the requirements. The experimental results shows that the proposed model has better accurate performances than those of other existing model.

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Development of 6-component Force/Moment Calibration Machine (6분력 힘/모멘트 교정기의 개발)

  • 김갑순;강대임
    • Journal of the Korean Society for Precision Engineering
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    • v.15 no.9
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    • pp.127-134
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    • 1998
  • This paper describes the design of a 6-component force/moment calibration machine with having the maximum capacities of 500 N in forces and 50 Nm in moments. To be used for the characteristic of a multi-component load cell. this machine consists of a body, a fixture, a force generating system, a moment generating system and weights. We have also evaluated the accuracy of the calibration machine. Test results show that the expanded relative uncertainty for force components $\pmFx,\;\pmFy\;and\;moment\;components\;\pmMx,\;\pmMy\;are\;less\; than\;8.6\times10^{-4}$, and force components +Fz, -Fz and moment components $\pmMz\;is\;less\;than\;1.6\times10^{-3},\;2.0\times10^{-5},\;1.7\times10^{-3}$ respectively.

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Effects of Lug Design Factors of Driving Wheel on Soil Reaction (러그의 설계요인(設計要因)이 구동륜하(驅動輪下)의 토양반력(土壤反力)에 미치는 영향(影響))

  • Kim, J.H.;Chung, S.W.;Kim, C.S.;Lee, K.M.
    • Journal of Biosystems Engineering
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    • v.12 no.1
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    • pp.14-19
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    • 1987
  • Lug design factors of a driving wheel were proved to have a significant effect on its traction. The effects of lug taper angle, lug angle, and lug width were experimentally analyzed. The results were summarized as follows: 1. Increasing wheel slippage increased the horizontal soil reaction force. 2. Significant improvement of traction was made when lug taper angle was 23 degrees. 3. Excellent traction was obtained in the range of lug angles of 60 to 74 degrees. 4. Lug width in 20 to 30 mm range has no effect on traction.

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Design of 3-component Force/Moment Sensor with Force/Moment Ratio of Wide Range (넓은 범위의 힘/모멘트비를 갖는 3분력 힘/모멘트 센서 설계)

  • Kim, Gap-Sun
    • Journal of the Korean Society for Precision Engineering
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    • v.18 no.2
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    • pp.214-221
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    • 2001
  • This paper describes the design of 3-component force/moment sensor with the force and moment ratio of wide range. It can measure the x-direction force Fx, y-direction force Fy and z-direction moment Mz simultaneously. In order to accurately measure forces and moment using 3-component force/moment sensor, it should get suitable force and moment ratio(the ratio of force Fx=200 N and moment Mz=20 Nm is ten to one), and small interference error. In this paper, in order to design the 3-component force/moment sensor with the force and moment ratio of wide range, the procedures are performed as follow : 1) the derivation of the equations to predict the bending strains on the surfaces of the plate-beams under the force or the moments, 2) the determination of the size of the sensing elements of the force/moment sensor by using the derived equations, 3) the Finite Element Method(FEM) analysis and the characteristic test for confirming the strains from the theory analysis, 4) the selection of the attachment locations of the strain gages of each sensor, 5) the analysis of the rated strain and the interference error at the attachment location of strain gages. It reveals that the rated strains calculated from the derived equations make a good agreement with the results from the Finite Element Method analysis and the characteristic test.

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Gait Initiation in a Patient With Spastic Hemiplegia Cerebral Palsy With and Without a Dynamic Ankle Foot Orthosis: A Pilot Study (강직성 편측 뇌성마비 환자의 보행 기시에 미치는 동적 단하지 보조기의 효과: 사전연구)

  • Jeon, Hye-Seon;Senesac, Claudia;Kaufman, Elizabeth
    • Physical Therapy Korea
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    • v.7 no.4
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    • pp.39-46
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    • 2000
  • 본 연구는 강직성 편측 뇌성마비 환자의 보행 기시(gait initiation)의 특성을 파악하고, 동적 단하지 보조기(dynamic ankle foot orthosis : DAFO)가 이런 환자들의 보행 기시에 미치는 영향을 알아보기 위하여 실시하였다. 연구대상자는 19세 선천성 강직성 우측 뇌성마비를 가진 여자 대학생이었다. 연구대상자는 4개의 다른 보행 기시 조건에서 각 조건당 7회의 보행 기시를 하였는데, 각각의 보행 기시 조건은: 1) 보조기 없이 좌측 하지로 보행 기시; 2) 우측 하지 보조기 착용 상태에서 좌측하지로 보행 기시; 3) 보조기 없이 우측 하지로 보행 기시; 4) 우측 하지 보조기 착용 상태에서 우측 하지로 보행 기시였다. 두개의 힘 판(force plate) 위에서 본인이 선택한 가장 편안한 방법과 속도로 2 m를 걷도록 하였다. 연구대상자가 보행 기시를 하는 동안 양쪽 가자미근과 앞정강근에 부착된 4개의 표면 전극으로부터 근 전도 신호와 보행 기시를 하는 연구 대상의 양 발 아래 놓인 두개의 힘 판의 자료를 분석하여 체중(body weight : BW)으로 정량화 하였다. 실험결과는 각 조건마다 7회 실시된 측정값들의 평균을 이용하였다. 본 사전연구의 결과는 다음과 같다. 1. 보행 기시 전 양다리로 선 상태에서 환측보다 건측으로 많은 체중지지를 하였으나(환측 42.57%BW, 건측 58.03%BW) 보조기의 착용이 환측으로의 체중지지를 향상시켰다(환측 44.46%BW, 건측 55.54%BW). 2. 보행 기시 중 가자미근과 앞정강근의 동시수축(coactivation)이 계속되었는데 이러한 양상은 보조기의 착용 유무에 따라 크게 달라지지 않았다. 3. 힘 판에서 들어온 지면 반발력(ground reaction force)의 수직 분력(vertical element, Fz)과 전후 분력(anterior-posterior element, Fx)을 분석한 결과, 건측 다리로 보행 기시를 할 때 보조기 착용은 가속을 촉진시켜 역학적으로 유리하였다. 이상의 연구 결과는 보조기의 착용이 건측 다리로 보행 기시를 할 때 미치는 신경학적, 역학적 장점들에 대한 구체적 연구의 필요성 및 근거를 제시하고, 환자들의 보행훈련 접근에 보다 효율적인 보행방법을 소개하는데 이용될 수 있다.

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Experimental Study on the Static Stability of a Sounding Rocket Model in the Supersonic Wind Tunnel (과학로켓 모델의 정적 안정성에 대한 초음속풍동 실험연구)

  • Lee, Sang-Hyun;Cho, Hwan-Kee;Sung, Hong-Gye;Kim, Jin-Kon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.38 no.9
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    • pp.856-861
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    • 2010
  • In this work, experiments on hybrid sounding rocket were conducted to investigate the aerodynamic characteristics and analyze longitudinal static stability. Tests were performed on 1/10 scale models of sounding rocket through Mach number ranging from 1.75 to 2.5 and for angle of attack from $0^{\circ}$ to $6^{\circ}$. Aerodynamic forces and moments were measured by means of a 4 component internal balance. With measured forces and moments, static stability characteristics of rocket were calculated. Tests were made for three models with different length to determine the effect of body length. The visualization of shock waves was carried out by Schlieren optical system to observe variations of shock waves with Mach number and angle of attack.

A Study on the Detection of Tool Wear by Use of Cutting Force Component in Orthogonal Cutting (선삭가공에서 절삭분력을 이용한 공구의 마멸검출에 관한 연구)

  • Kim, Ki-Choong;Hyun, Chung-Nam
    • Journal of the Korean Society for Precision Engineering
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    • v.3 no.4
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    • pp.30-42
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    • 1986
  • On the analysis of cutting mechanics in orthogonal cutting, each cutting force component can be predicted. By adding the flank face wear term to the prediction equation for cutting force components, complete equations are obtained. Using these equations, it is shown that cutting force components are increased linearly as flank face wear land is developed, in theory and experiment. By making non-dimensional term ie. Fv/Fc, the width of variation of output signal Fv/Fc is greately decreased compared with each cutting force component as cutting condition is varied. Among these conditions, the variation of chip width in the range of more than 1mm and that of cutting velocity have little effect on the output signal Fv/Fc, that of Flank face werr land can be detected without difficulty.

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