• 제목/요약/키워드: Vacuum test

검색결과 1,002건 처리시간 0.031초

이중펄스 추진기관의 펄스분리장치 파열압력 분석기법 연구 (A Study of Rupture Pressure for Membrane Type Pulse Separation Device of Dual Pulse Rocket Motor)

  • 김세일
    • 한국추진공학회지
    • /
    • 제26권1호
    • /
    • pp.98-106
    • /
    • 2022
  • 고고도에서 작동하는 신뢰성 있는 이중펄스 추진기관을 개발하기 위해서는 안정적인 진공 점화 기술과 펄스분리장치(PSD, Pulse Separation Device) 설계기술이 요구된다. 본 연구에서는 이중펄스 추진기관 격막형 펄스분리장치(Membrane Type Pulse Separation Device)의 파열압력 분석기법을 개발하였다. 변형률-압력 관계를 이용하여 PSD 파열압력에 대한 관계식을 도출하였다. 고고도 진공환경을 모사할 수 있는 PSD 진공파열 시험장치와 PSD 1초급 진공점화 시험장치를 개발하였다. PSD 진공파열시험을 수행하여 파열압력을 분석하고 PSD 설계 값을 도출하였다. 최종적으로 PSD 1초급 진공점화 시험을 통해 이중펄스 추진기관의 PSD 설계 파열압력과 추진제 진공점화 성능을 확인하였다.

함수다공질층의 진공건조에 관한 실험적 연구 (Ⅰ) (An Experimental Study on Vacuum Drying of Water-Saturated Porous Media)

  • 박형진;김경근;김명환
    • Journal of Advanced Marine Engineering and Technology
    • /
    • 제20권5호
    • /
    • pp.68-75
    • /
    • 1996
  • The vacuum drying characteristics of water-saturated porous media were studied experimentally. The water-saturated porous media, water-saturated sand layer, was heated by the isothermal bottom wall of the rectangular vessel. The vacuum drying rate and temperature distribution of the sand layer were measured and calculated under a variety of conditions of heated wall temperature, vacuum rate, and thickness of the test material. It was found that the drying rate due to the heat and mass teansfer is greatly influenced by the heated wall temperature, vacuum rate, and thickness of the test material.

  • PDF

하이브리드 타입 진공펌프의 동특성 및 최적화 (Optimization and dynamic characteristics of the hybrid type vacuum pump)

  • 김용휘;이종명;안병현;하정민;최병근
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2014년도 추계학술대회 논문집
    • /
    • pp.306-310
    • /
    • 2014
  • The purpose of this study is the stability evaluation of a vacuum pump through modal test and rotor dynamics. Eigenvalue was solved by the finite-element method(FEM) using 2D and 3D models, then the modal test result was compared with the FEM result. According to the comparison, the analysis result using the 2D was more accurate than the 3D model. Therefore, rotor dynamics was performed by the 2D model. Campbell diagram and root-locus maps, which were calculated by complex-eigenvalue analysis, were used to evaluate the stability of the rotors of the vacuum pump. And displacement solved by unbalance response analysis was compared with the minimum clearance between two rotors of the vacuum pump. Thus, the vacuum pump is assumed operated under steady state through the evaluation of the rotor dynamics.

  • PDF

루츠타입 진공펌프 동특성의 해석적 평가 (Analytical Evaluation of Rotor Dynamic Characteristic of Roots Type Vacuum Pump)

  • 이종명;김용휘;하정민;구동식;최병근
    • 한국소음진동공학회논문집
    • /
    • 제21권12호
    • /
    • pp.1112-1119
    • /
    • 2011
  • The goal of this study is the stability evaluation of a vacuum pump through modal test and rotor dynamics. Roots type vacuum pump, which is a dry vacuum pump, is necessary for the manufacturing process of the semiconductor and the display. Eigenvalue was solved by the finite-element method(FEM) using 2D and 3D models, then the modal test result was compared with the FEM result. According to the comparison, the analysis result using the 2D was more accurate than the 3D model. Therefore, rotor dynamics was performed by the 2D model. Campbell diagram and root-locus maps, which were calculated by complex-eigenvalue analysis, were used to evaluate the stability of the rotors of the vacuum pump. And displacement solved by unbalance response analysis was compared with the minimum clearance between two rotors of the vacuum pump. Thus, the vacuum pump is assumed operated under steady state through the evaluation of the rotor dynamics.

육상 및 해양 시추용 디개서 시스템의 진공펌프 성능해석 (A Study on the Performance Analysis of Degasser System with Vacuum Pump for Onshore and Offshore Drilling)

  • 권성용;박성규;신철순;김승찬;임희연
    • 한국산업융합학회 논문집
    • /
    • 제25권6_2호
    • /
    • pp.1063-1069
    • /
    • 2022
  • In modern industry, vacuum has grown into an indispensable industrial field. The performance of the vacuum pump in the degasser system among mud treatment system facilities was verified by a numerical analysis method. The degasser system is an equipment for removing the gas contained in the mud, and it is a work process that requires a vacuum. This study analyzed the vacuum pump performance of the degasser used in drilling for resource development of onshore and offshore plants. The vacuum pump used in the degasser system was designed with a discharge rate of 0.099kg/s. The DM(Design Modeler) program of ansys workbench 17.2 was used to modify the model of the vacuum pump used in the degasser system. And for performance analysis, CFX, which is known to be suitable for rotating system analysis, was used. Finally the performance analysis results of the vacuum pump and the prototype performance test results were compared and analyzed.

대형우주모사장비(${\Phi}8m{\times}L10m$) 열교환 슈라우드 설계 (Thermal Shroud Design of a Large Space Simulator(${\Phi}8m{\times}L10m$))

  • 조혁진;문귀원;이상훈;서희준
    • 대한기계학회:학술대회논문집
    • /
    • 대한기계학회 2004년도 추계학술대회
    • /
    • pp.1236-1240
    • /
    • 2004
  • Thermal vacuum test for satellites should be performed before launch to verify the feasibility of satellites' operation in a harsh space environment which is represented as an extremely cold temperature and vacuum condition. A large space simulator(${\Phi}8m{\times}L10m$) has been demanded to accomplish the thermal vacuum test for the huge satellites designed in compliance with the national space program of Korea. In this paper, the design and calculation of thermal shroud which is the core part of large space simulator were discussed. The characteristics of the large space simulator being constructed at Korea Aerospace Research Institute(KARI) were depicted.

  • PDF

우주 열환경 모사용 소형 극저온 블로워 설계 및 성능평가 (Design and Performance Test of a Cryogenic Blower for Space Thermal Environment Simulation)

  • 서희준;안성민;허환일
    • 한국항공우주학회지
    • /
    • 제41권10호
    • /
    • pp.833-839
    • /
    • 2013
  • 위성체는 지상에서 우주환경시험을 거쳐 기능 및 작동상태를 점검해야 하며, 이를 위해서는 우주환경을 모사 할 수 있는 우주환경 모사장비가 필요하다. 위성체 및 위성체의 부품 성능을 검증하기 위해 사용되는 열진공 챔버는 진공용기, 진공시스템, 열제어 시스템 등으로 구성이 된다. 특히, 고온 및 극저온의 열환경을 모사하는 열제어 시스템이 열진공 챔버의 핵심이라고 할 수 있으며, 열제어 시스템의 성능은 극저온 블로워의 성능에 의해 결정된다. 본 논문에서는 극저온 블로워의 유동 해석과 블레이드의 구조해석을 통해 원심팬을 설계 하였으며, 구동부와 유체부의 열전달 방지를 위한 열장벽, 모터의 과열 방지를 위한 냉각 시스템 등이 설계되었으며, 이는 열해석을 통해 검증 되었다. 최종적으로 성능실험을 수행하여 극저온 블로워의 성능을 확인하였다.

Improvement of soft clay at a site in the Mekong Delta by vacuum preloading

  • Quang, N.D.;Giao, P.H.
    • Geomechanics and Engineering
    • /
    • 제6권5호
    • /
    • pp.419-436
    • /
    • 2014
  • Soil improvement by preloading with PVD in combination with vacuum is helpful when a considerable load is required to meet the desired rate of settlement in a relative short time. To facilitate the vacuum propagation, vertical drains are usually employed in conjunction. This ground improvement method is more and more applied in the Mekong delta of Vietnam to meet the needs of fast infrastructure development. This paper reports on a pilot test that was carried out to investigate the effect of ground improvement by vacuum and PVD on the rate of consolidation at the site of Saigon International Terminals Vietnam (SITV) in Ba Ria-Vung Tau Province, Viet Nam. Three main aspects of the test will be presented, and namely, instrumentation and field monitoring program, calculation of consolidation settlement and back-analysis of soil properties to see the difference before and after ground improvement.