• 제목/요약/키워드: force margin

검색결과 83건 처리시간 0.026초

전투기 날개 수리를 위한 기계적 체결의 형상 선정에 관한 연구 (A Study on the Shape Selection of Mechanical Fastening for the Repair of Fighter Wing)

  • 최동수
    • 한국군사과학기술학회지
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    • 제24권5호
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    • pp.467-474
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    • 2021
  • A study on optimal shape selection of a mechanical fastening for the repair of crack defect of ROK Air Force F-5 fighter wing was conducted. The crack defect occurred in the spar of the wing, and the technical manual does not specify the repair method. However, ROK Air Force decided to develop a repair technology for this defect in consideration of various logistic conditions. Three repair shapes for the proper repair were devised and the finite element analysis was performed to examine the structural safety of these three connection members. As a result of the structural safety review, two connection members except one were structurally safe with safety margins over zero because the calculated stress values were at or below the yield strength level. Therefore, two connection members were determined to be able to use for repair under the condition that the aircraft operated within the design limit load. The results of this study would be very useful if the same defect occurs in long-term aircraft operated by the ROK Air Force.

가스터빈 블레이드 MODAL TEST를 위한 실험적 방법에 관한 연구 (An Experimental Study on the Modal Test of Gas Turbine Blade Integrity)

  • 조철환;양경현;김성휘
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2001년도 추계학술대회논문집 II
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    • pp.1388-1392
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    • 2001
  • In this paper, an experimental method of several modal analyses was devised to iify the vibration characteristics of G/T blade in power plants. Also, it is being applied this method to establish the standard category of natural frequency of new developed blades. So acceptance margin to avoid resonance due to nozzle waking force is being established for new blades. It is expected to improve the availability of G/T blades by using the result of this study.

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가스터빈 블레이드의 건전성 평가를 위한 실험적 연구 (An Experimental Study on Evaluation of Gas Turbine Blade Integrity)

  • 조철환;양경현;원종범;김성휘
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2000년도 추계학술대회논문집
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    • pp.618-622
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    • 2000
  • An experimental method is devised to identify the vibration characteristics of G/T blade in power plants. The acceptance margin to avoid resonance due to nozzle waking force is established and evaluated by suggested method. It is expected that improvement of turbine availability and the localization of blade can be achieved by using the result of this study.

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Design and Analysis of A Mini Linear Optical Pickup Actuator

  • Park, Joon-Hyuk;Baek, Yoon-Su;Park, Young-Pil
    • Journal of Mechanical Science and Technology
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    • 제17권11호
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    • pp.1616-1627
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    • 2003
  • This paper describes a mini linear optical pickup actuator. To reduce the size, inner yokes are designed to guide the mover and outer yokes of permanent magnets are removed. Magnetic circuit method is used to determine the thrust force. Virtual path method is proposed to analyze the open magnetic circuit analysis. The magnetic circuit of the proposed actuator can be a closed circuit due to the virtual path model of the outer magnetic flux. The validity of virtual path method is evaluated by comparing to the FEM analysis. Structural vibration is investigated using FEM and the design of the mover is modified to improve the vibration characteristic. Dynamic characteristic experiments shows that the performance of the proposed actuator is enough to be used as a coarse and fine seeking actuator simultaneously and the thrust force margin for loading a focusing actuator is guaranteed.

A Study on the Rotordynamic Stability of Turbo Pump Unit

  • Kwak, Hyun-Duck;Lee, Yong-Bok;Kim, Chang-Ho;Ha, Tae-Woong;Yoo, Woo-Chul
    • KSTLE International Journal
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    • 제4권1호
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    • pp.1-7
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    • 2003
  • A turbo pump unit provides high pressure oxygen and fuel in a space shuttle main engine (SSME). This paper focused on rotordynamics, investigating its characteristics based on a numerical simulation of turbo pump finite element model. Speeds up to 50,000 rpm are considered, as well as the special problems related to elastic-ring, seal hydrodynamic force, shroud force and clearance-excitation farce. The rotordynamic prediction shows that the elastic-ring which is inserted between the casing and the outer race of ball bearing allows far an acceptable separate margin of first critical speed. Additionally, the results show that the floating ring seal, which have a peculiar ring, adds substantial stiffness and damping to the system as well as exhibits superior performance in terms of rotordynamic stability of system compared to the plain seal.

운동용 힘 발생기를 위한 리니어 모터의 전류제어 (Linear Motor Current Control for a Force Generator)

  • 이세한
    • 한국산업융합학회 논문집
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    • 제18권1호
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    • pp.1-9
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    • 2015
  • This research dealt with a two-degree-of-freedom controller which was used for 2-dimensional force generator based on an linear motor. The gain margin of the controller may be reduced when the time constant is near to the sampling time of a discrete controller. In case of low gain controller, it cannot satisfy the control performance. A two-degree-of-freedom controller based on PI-control was proposed. It can manage performance and stability respectively. It also had a kind of a feed-forward control. This scheme can not only lessen gain of conventional PI controller in order to stability but also obtain high tracking performance.

KSLV-I 페이로드 페어링 구조시험 (Structural test of KSLV-I Payload fairing)

  • 이종웅;공철원;은세원;남기원;장영순;심재열;이영신
    • 한국항공우주학회지
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    • 제41권11호
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    • pp.900-907
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    • 2013
  • 페이로드 페어링은 위성과 부품들을 외부환경으로부터 보호하며, 위성분리 전에 페이로드 페어링은 분리된다. 페이로드 페어링은 굽힘 강성과 무게에 비해 강도 비율이 우수한 복합재 샌드위치 재료로 제작 되었다. 페이로드 페어링은 비행 중에 압축, 굽힘 그리고 전단하중을 받게 된다. 본 연구에서는 PLF와 연결구조물의 강도를 확인하기 위하여 액추에이터와 치구를 사용하여 PLF 구조시험을 수행하였다. 구조시험의 목적은 분리 스프링의 힘이 PLF에 가해진 상태에서 조합하중이 PLF에 작용할 때 PLF의 건전성을 확인하는 것이다. 구조시험 결과에서는 분리 스프링 하중과 조합하중에 의한 PLF의 구조 건전성을 확인하였다.

균형상살 검출 알고리즘에서 검출과 관련된 설계변수의 민감도 해석 몇 최적화 (Sensitivity Analysis and Optimization of Design Variables Related to an Algorithm for Loss of Balance Detection)

  • 고병규;김광훈;손권
    • 대한의용생체공학회:의공학회지
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    • 제32권1호
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    • pp.7-14
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    • 2011
  • This study suggested an optimized algorithm for detecting the loss of balance(LOB) in the seated position. And the sensitivity analysis was performed in order to identify the role of each design variable in the algorithm. The LOB algorithm consisted of data processing of measured signals, an internal model of the central nervous system and a control error anomaly(CEA) detector. This study optimized design variables of a CEA detector to obtain improved values of the success rate(SR) of detecting the LOB and the margin time(MT) provided for preventing the falling. Nine healthy adult volunteers were involved in the experiments. All the subjects were asked to balance their body in a predescribed seated posture with the rear legs of a four-legged wooden chair. The ground reaction force from the right leg was measured from the force plate while the accelerations of the chair and the head were measured from a couple of piezoelectric accelerometers. The measured data were processed to predict the LOB using a detection algorithm. Variables S2, h2 and hd are related to the detector: S2 represents a data selecting window, h2 a time shift and hd an operating period of the LOB detection algorithm. S2 was varied from 0.1 to 10 sec with an increment of 0.1 sec, and both h2 and hd were varied from 0.01 to 1.0 sec with an increment of 0.01 sec. It was found that the SR and MT were increased by up to 9.7% and 0.497 sec comparing with the previously published case when the values of S2, h2 and hd were set to 4.5, 0.3 and 0.2 sec, respectively. Also the results of sensitivity analysis showed that S2 and h2 had considerable influence on the SR while these variables were not so sensitive to the MT.

정전형 마이크로 액추에이터를 이용한 초고밀도 HDD용 Dual-Stage 서보 시스템 (Dual-Stage Servo System using Electrostatic Microactuator for Super-High Density HDD)

  • 김승한;성우경;이효정;이종원;최정훈;안영재;전국진;김봉환
    • 대한전기학회논문지:전기물성ㆍ응용부문C
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    • 제48권2호
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    • pp.153-160
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    • 1999
  • Dual-stage servo system for super-high density HDD has the chances of being composed of the coarse actuator(VCM) for track-seeking control and the fine actuator(microactuator) for-following control in near future. This paper presents the concept design of dual-stage servo system and the track-following control using an electrostatic microactuator for super-high density HDD. The electrostatic microactuator is designed and fabricated by MEMS(micro-electro-mechanical system) process. Both the nonlinear plant(voltage/displacement-to-electrostatic force) and the linear plant(electrostatic force-to-displacement) of the microactuator are established. Inverse function of the nonlinear plant is employed for a feedforward nonlinear compensator design. And feedforward control effect of this compensator is shown by time-domain experiments. A track-following feedback controller is designed using the feedback nonlinear compensator which is derived from the feedforward nonlinear compensator. The track-following control experiment is done to show the control efficiency of the proposed control system. And, excellent track-following control performance(2.21kHz servo-bandwidth, 7.51dB gain margin, $50.98^{\circ}$phase margin) is achieved by the proposed control system.

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한국 자유무역협정의 동태적 교역효과 분석: 무역외연효과를 중심으로 (The Dynamic Trade Effect of Korea's Free Trade Agreements: Extensive Margins of Trade)

  • 정재욱
    • 무역학회지
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    • 제48권1호
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    • pp.307-329
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    • 2023
  • 본 논문은 2021년 말까지 발효된 한국의 자유무역협정(FTA) 총 17건의 동태적 교역효과를 확인하기 위해 1996년부터 2021년까지 한국의 HS 10단위 상품 및 국가별 수입액 패널자료를 계량분석하였다. FTA의 협상개시, 협상타결 및 서명, 비준 및 발효 등의 무역정책 전환기(transition period)동안 동태적 교역효과를 분석한 결과, 협정의 발효 시점에 수입이 증가하는 효과는 뚜렷하며 특히, 새로운 교역상품의 등장에 따른 무역외연효과(extensive margin)가 중요한 역할을 하였다. 또한, 외연효과는 FTA의 발효에 따라 관세가 인하되기 이전부터 증가하는 추세를 보였다. 이는 최근 선행연구에서 확인된 잠재적 수출기업의 수출시장 조기진입현상을 뒷받침하는 중요한 결과이다. 특히, 이런 선행효과는 FTA 협상 개시 이후에 뚜렷하게 나타나, 정책 불확실성의 감소와 시장 조기진입현상의 관련성을 시사한다.