• 제목/요약/키워드: holding mechanism

검색결과 119건 처리시간 0.027초

열선분리방식을 이용한 힌지구동형 구속분리장치 비행모델의 발사 및 궤도환경 검증시험 (Launch and On-orbit Environment Verification Test of Flight Model of Hinge Driving Type Holding and Release Mechanism based on the Burn Wire Release)

  • 이명재;이용근;강석주;오현웅
    • 한국항공우주학회지
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    • 제44권3호
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    • pp.274-280
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    • 2016
  • 2015년 발사예정인 우주기반기술 검증용 큐브위성 STEP Cube Lab.의 주요 탑재체인 열선절단방식 힌지구동형 구속분리장치는 높은 체결력 및 저충격 구현의 장점으로 초소형위성 전개구조물의 구속/분리에 적용이 용이하며, 기존 나일론선 절단방식의 낮은 체결력 및 복수구조물 적용에 따른 시스템 복잡화의 단점을 극복가능하다. 본 논문에서는 인증모델 검증시험이 완료된 구속분리장치의 궤도검증 임무수행을 목적으로 체결력 검증 및 전개 확인 신호 획득이 가능한 비행모델을 설계/제작하였으며, 탑재체 레벨에서의 발사 및 궤도환경 검증시험을 수행하여 설계 유효성을 입증하였다.

원자로 제어봉구동장치의 동작 검출을 통한 안전한 이중유지 방법 (The Method of safe double holding by detecting movements of Control Rod Drive Mechanism)

  • 천종민;김춘경;이종무;박민국;권순만
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2005년도 제36회 하계학술대회 논문집 D
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    • pp.2655-2657
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    • 2005
  • When a fault relating to the urgent alarm occurs, we must prevent control rods from dropping and make one of two grippers in Control Rod Drive Mechanism (CRDM) grip the drive rod taking a control rod assembly. To enhance the reliability of holding control rods, we order two grippers to hold the drive rod. This action is called the double holding. In the middle of the movement of the drive rod, the latching of the drive rod can cause friction between a gripper and the drive rod. This state may give damage to both the gripper and the drive rod. In this paper, we have devised the method which can have two grippers hold the drive rod more stably, without damaging the equipment.

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Mechanism for Efficient Use of Server's Resource on the Web

  • 이윤정;박남섭;김태윤
    • 한국정보처리학회:학술대회논문집
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    • 한국정보처리학회 2001년도 춘계학술발표논문집 (상)
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    • pp.507-510
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    • 2001
  • HTTP/1.1 standard reduces latencies and overhead from closing and re-establishing connections by supporting persistent connections as a default, which encourage multiple transfers of objects over one connection. HTTP/1.1, however, does not define explicitly connection-closing time but specifies a certain fixed holding time model. This model may induce wasting server's resource when server maintains conn ection with the idle-state client that requests no data for a certain time. This paper proposes the mechanism of a heuristic connection management supported by the client-side under persistent HTTP, in addition to HTTP/1.1's fixed holding time model on server-side. The client exploits the tag information within transferred HTML page so that decides connection-closing time. As a result, the mechanism allows server to use server's resource more efficiently without server's efforts.

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나일론선 절단 방식에 기반한 Pin-puller형 큐브위성용 태양전지판 구속분리장치의 기능검증 (Functional Verification of Pin-puller-type Holding and Release Mechanism Based on Nylon Wire Cutting Release Method for CubeSat Applications)

  • 고지성;손민영;오현웅
    • 항공우주시스템공학회지
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    • 제15권5호
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    • pp.81-88
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    • 2021
  • 일반적으로 큐브위성용 전개형 태양전지판을 수납 및 전개시키기 위해 사용되는 구속분리장치는 비폭발식 나일론선 절단방식이 적용된다. 그러나 상기 방식은 태양전지판 수납 상태에서 큐브위성의 배터리 충전, PCB 및 탑재체의 전기적 점검 및 시험 등을 위한 접근 포트 연결 시 분리장치의 구속해제 및 재채결 작업이 반복적으로 요구된다. 따라서, 기존의 구속분리장치는 위성체 내부 접근을 위해서는 작업자의 번거로움 및 일관된 나일론선 체결작업 공정 유지의 어려움이 존재한다. 본 연구에서는 나일론 선 절단 없이 구속 핀 분리만으로 자유롭게 태양전지판 전개 및 수납이 가능한 Pin-puller형 태양전지판 구속분리장치를 제안하였으며, 기능 및 성능검증을 위한 분리장치의 전개시험 및 최대 분리하중 측정 시험을 통해 분리장치 설계의 유효성을 입증하였다.

BONDING PHENOMENON IN TRANSIENT LIQUID PHASE BONDING OF NI BASE SUPERALLOY GTD-111

  • Kang, Chung-Yun;Kim, Dae-Up;Woo, In-Soo
    • 대한용접접합학회:학술대회논문집
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    • 대한용접접합학회 2002년도 Proceedings of the International Welding/Joining Conference-Korea
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    • pp.798-802
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    • 2002
  • Metallurgical studies on the bonded interlayer of directionally solidified Ni-base superalloy GTD111 joints were carried out during transient liquid phase bonding. The formation mechanism of solid during solidification process was also investigated. Microstructures at the bonded interlayer of joints were characterized with bonding temperature. In the bonding process held at 1403K, liquid insert metal was eliminated by well known mechanism of isothermal solidification process and formation of the solid from the liquid at the bonded interlayer were achieved by epitaxial growth. In addition, grain boundary formed at bonded interlayer is consistent with those of base metal. However, in the bonding process held at 1453K, extensive formation of the liquid phase was found to have taken place along dendrite boundaries and grain boundaries adjacent to bonded interlayer. Liquid phases were also observed at grain boundaries far from the bonding interface. This phenomenon results in liquation of grain boundaries. With prolonged holding, liquid phases decreased gradually and changed to isolated granules, but did not disappeared after holding for 7.2ks at 1473K. This isothermal solidification occurs by diffusion of Ti to be result in liquation. In addition, grain boundaries formed at bonded interlayer were corresponded with those of base metal. In the GTD-ll1 alloy, bonding mechanism differs with bonding temperature.

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일방향응고 Ni기초내열합금 GTD-111의 천이액상확산접합(I) (Transient Liquid Phase Bonding of Directionally Solidified Ni Base Superalloy, GTD-111(I) - Bonding Phenomena and Mechanism -)

  • 강정윤;권민석;김인배;김대업;우인수
    • Journal of Welding and Joining
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    • 제21권2호
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    • pp.82-88
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    • 2003
  • The bonding phenomenon and mechanism in the transient liquid phase bonding(TLP Bonding) of directionally solidified Ni base superalloy, GTD-111 was investigated. At the bonding temperature of 1403K, liquid insert metal was eliminated by isothermal solidification which was controlled by the diffusion of B and Si into the base metal and solids in the bonded interlayer grew epitaxially from mating base metal inward the insert metal. The number of grain boundaries formed at the bonded interlayer was corresponded with those of base metal. The liquation of grain boundary and dendrite boundary occurred at 1433K. At the bonding temperature of 1453K which is higher than liquation temperature of grain boundary, liquids of the Insert metal were connected with liquated grain boundaries and compositions in each region mixed mutually. In Joints held for various time at 1453t phases formed at liquated grain boundary far from the interface were similar to those of bonded interlayer. With prolonged holding time, liquid phases decreased gradually and liquids of continuous band shape divided many island shape. But liquid phases did not disappeared after holding for 7.2ks at 1453k. Isothermal solidification process at the bonding temperature which is higher than the liquation temperature of the grain boundary was controlled by diffusion of Ti to be result in liquation than B or Si. in insert metal. (Received January 15, 2003)

Mechanism for Fairness Service of Web Server

  • Rhee, Yoon-Jung;Park, Nam-Sup;Hyun, Eun-Sil;Kim, Jeong-Beom;Lee, Young-Ji;Yun, Ma-Ru;Hyeok Kang;Kim, Young-Jun;Kim, Tai-Yoon
    • 한국정보과학회:학술대회논문집
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    • 한국정보과학회 2001년도 봄 학술발표논문집 Vol.28 No.1 (A)
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    • pp.355-357
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    • 2001
  • HTTP/1.1 standard reduces latencies and overhead from closing and re-establishing connections by supporting persistent connections as a default, which encourage multiple transfers of objects over one connection. HTTP/1.1, however, does not define explicitly connection-closing time but specifies a certain fixed holding time model. This model may induce wasting server’s resource when server maintains connection with the idle-state client that requests no data for a certain time. This paper proposes the mechanism of a heuristic connection management supported by the client-side under persistent HTTP, in addition to HTTP/1.1’s fixed holding time model on server-side. The client exploits the tag information within transferred HTML page so that decides connection-closing time. As a result, the mechanism allows server to use server’s resource more efficiently without server’s efforts.

우주발사체 지상고정장치 유압시스템 설계 및 해석 (Design and simulation of hydraulic system for launch vehicle holding device)

  • 김대래;양성필;이재준;김범석;이영신
    • 한국항공우주학회지
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    • 제44권12호
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    • pp.1087-1094
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    • 2016
  • 발사체 지상고정장치는 지상운용시 발사패드에 기립된 발사체를 견고하게 지지하다가 발사시점에서 고정장치를 해제하여 발사체를 이륙하도록 하는 장치이다. 엔진점화이후 발사체 최대추력에서 발사체 고정의 급격한 해제는 Ka Doing a Doing a Doing 현상을 발생시켜 발사체 구조에 심각한 손상을 초래한다. 따라서, 발사체 지상고정장치는 고정력을 점진적으로 해제하기위한 기능이 요구된다. 또한 총 4개 고정장치의 해제 동작은 대단히 정밀하게 동시에 작동 하여야 한다. 본 연구에서는 복잡한 유압기기 없이 축압기 및 파이로 밸브에 의해 유압구동기의 속도를 발생시키고 오리피스로 속도를 제어함으로써 요구조건들을 충족하는 유압시스템을 제안하였다. 다물체 동역학 해석 및 Amesim을 이용한 유압시스템 해석을 통하여 유압구동기 목표속도를 도출하고 목표 속도를 만족하기 위한 오리피스의 단면적을 산출하였다. 이와 같은 연구를 통하여 복잡한 유압기기 없이 동작하는 신뢰도 높은 유압시스템을 설계하였다.

큐브위성용 포고핀 기반 열선절단 분리장치의 열적 거동 분석 및 검증 (Numerical and Experimental Thermal Validation on Pogo-pin based Wire Cutting Mechanism for CubeSat Applications)

  • 손민영;채봉건;오현웅
    • 항공우주시스템공학회지
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    • 제17권2호
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    • pp.94-102
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    • 2023
  • 큐브위성용 태양전지판 분리장치는 열선 또는 저항소자의 발열로 나일론선을 절단하여 구조물의 구속을 해제하는 나일론선 절단방식 구속분리장치가 주로 적용되고 있다. 일반적으로 태양전지판 조립체의 발사하중을 고려한 구조해석을 수행하여 구속분리장치의 설계가 이루어지고 있으나, 발사 이후 궤도 열환경에 대한 구속분리장치의 열적 검토 및 분석사례는 전무한 실정이다. 따라서, 본 논문에서는 현재 개발중인 큐브위성 STEP Cube Lab-II에 적용되는 나일론선 절단 기반 구속분리장치의 열적 안정성 평가를 수행하고자 한다. 위성이 POD (Picosatellite Orbital Deployer)에서 사출되고 태양전지판이 전개되기까지의 분리장치 온도 분포를 검토하여 분리장치의 허용온도 범위 내에서 안정적인 구속 분리가 될 수 있도록 분리장치에 대한 궤도 열해석을 수행하였다. 또한, 열해석 결과를 기반으로 열진공시험을 수행하여 분리장치의 설계를 검증하였다.

전자기 교반한 알루미늄합금 빌렛의 재가열시 고액공존구역에서의 조직변화 (Microstructural Evolution of Electromagnetically Stirred Al alloy Billet During Isothermal Reheating at the Solid-liquid State)

  • 이덕영
    • 한국주조공학회지
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    • 제28권3호
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    • pp.129-135
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    • 2008
  • The reheating stage of electromagnetically stirred Al billet is a critical factor in the thixoforming process. When reheated to the solid-liquid state, the microstructure evolves to a more globular and more homogeneous structure by a coarsening mechanism, the kinetics depending on the initial microstructure. Microstructural evolution has been characterized by conventional parameters (mean size of particle and shape factor) as a function of holding time in the solid-liquid state. The aim of this study is to report experimental results concerning microstructural evolution in the solid-liquid state of electromagnetically stirred Al billet. The material was elaborated in the form of continuously cast bars solidified with electromagnetic stirring to degenerate the dendritic structure. The choice of the reheating conditions is determined by a dendritic ripening and coalescence mechanism, involving variations of both the shape and size of the particles. The reheating time has to be long enough to allow a minimum degree of spheroidizing, but has to be limited as much as possible in order to avoid excessive ripening. The optimum microstructure was obtained at the reheating temperature of near $584^{\circ}C$ and the holding time of 5 min. The only means of combining high productivity with good casting quality was to use feedstock billets whose microstructure showed rapid transformation characteristics.