• Title/Summary/Keyword: 데이타획득장비

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Marking network connections by DICOM & PACS

  • Kim, Gwang-Yeol;Lee, An-Bae;Park, Dong-Hun
    • Korean Journal of Digital Imaging in Medicine
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    • v.3 no.1
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    • pp.72-73
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    • 1997
  • Medical imaging device에서 이미지 정보의 교환은 PACS의 성공을 결정짓는 중요한 요소이다. 즉 이미지 정보를 획득한다는 것은 네트워크상에서 정보를 신속 정확히 얻을 수 있다는 장점을 말한다. 더욱 중요한 것은 이미지파일의 호환성이다. 의료영상저장전달시스템 즉 PACS는 병원의 모든 정보와 서로 연동될 수 있어야 한다. 데이타 통합과 시스템의 안정성은 PACS에 있어서 가장 중요한 필수요건이다. 위에 언급한 요구조건들을 모두 만족시키기 위해서는 시스템 상호간을 네트워크할 수 있는 공통의 통합 프로토콜이 필요하다. 이와같은 문제를 해결하기 위해서 The American College of Radiology(ACR)과 National Electrical Manufacturers Association(NEMA)는 1983년초에 업체간의 장비공유와 방사선 실무자들의 통합되는 프로토클을 제정하기 위해 위원회를 설립하였다. 여기서 제정된 프로토콜을 DICOM이라 정하였다. DICOM의 역사적 배경, 의미, 필요성과 시스템상에서 어떻게 역활해왔는가와 DICOM을 통한 PACS시스템의 실제 활용예에 대하여 알아보겠다.

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Evaluation of Structural Integrity of Aircraft External Fuel Tank for Separation Loads (분리하중에 대한 항공기용 외부연료탱크 구조 건전성 평가)

  • Hyun-gi Kim;Sungchan Kim;Min-su Park;Su-hong An
    • Journal of Aerospace System Engineering
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    • v.18 no.1
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    • pp.64-71
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    • 2024
  • The external fuel tank of an aircraft is a main component that can increase the cruising range of the aircraft. It must be able to be stably separated from the pylon in an emergency situation. At this time, a separation load is applied to the fin and the pivot of the external fuel tank. To stably separate the external fuel tank, the structural soundness of the fin and the pivot must be confirmed. In this study, structural tests were conducted to verify the structural integrity of the external fuel tank pin and pivot when the external fuel tank was separated from the aircraft. Results are then presented. In this paper, a test configuration diagram consisting of the hydraulic and load control equipment, data acquisition system, and pneumatic supply unit used in the structural test was explained. Test installation and test load application plan for each test condition were provided. As results of the structural test, it was found that test load and internal pressure of the test specimen were properly controlled within the allowable range in each test. It was confirmed that serious structural defects in the test specimen did not occur under required load conditions. In conclusion, through structural test for design limit load and design ultimate load, it was proven that the fin and pivot of the external fuel tank for aircraft covered in this study had sufficient structural strength.

Development of a Simple In-Situ Data Logger (간단한 현장 데이타 수집장치의 개발에 관한 연구)

  • Yeo, Woo-Kwang;Yoon, Byung-Man;Lee, Jong-Kuk
    • Water for future
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    • v.29 no.2
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    • pp.249-260
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    • 1996
  • There have been easily found a number of examples that misleading or unreasonable measuring data set of physical variables are often produced in the field and the laboratory. The primary reason is that the specific requirements of civil engineers are initially disregarded in designing the experimental apparatus. It results from a lack of mutual understanding and co-operating between the user group and the maker. Therefore, their fundamental knowledge and apprehension become indispensible in order to obtain measuring data with high confidence and good quality In this study it is shortly explained the basic structure and the operation system of the experimental equipments commonly used at the present. A simple measuring set is developed which is quite easy for a general civil engineer to design and operate without any other specialty of mostly electricity electronics. Based upon this requirement, one of data logger named PPDL8 is newly designed by making use of the parallel port in the personal computer, consisting of multi-channels able to measure 8 different point values simultaneously. It can also use many valuable sub-programs existing in PC because the user makes his own programs necessary for measurement, by himself. Of all things, it has a great advantage to increase the applicability of field measurements much larger when adopting the notebook computer to operate with small battery only. In addition this study gives, in fact, the excellent agreements of in-situ field variables by showing their measuring results of temperature, distance and turbidity.

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Color Gamut Mapping and Dithering for Ink-Jet Color Printing (잉크젯 칼라 프린팅을 위한 색역 사상과 디더링)

  • Lee, Chae-Soo;Kim, Kyeong-Man;Lee, Cheol-Hee;Ha, Yeong-Ho
    • Journal of the Korean Institute of Telematics and Electronics S
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    • v.35S no.6
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    • pp.137-146
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    • 1998
  • Recently many devices print electronic images in a variety of ways. The reproduced color, however, is different from the original color because of the difference of hardware characteristics. To maintain device independent color, gamut mapping method is proposed. The proposed color gamut mapping uses nonlinear intensity mapping and clipping for saturation mapping on HSI color space. In the dithering operation, expanded nonlinear ordered dithering and modified error diffusion are proposed. The proposed ordered dithering uses expanded nonlinear quantization which considers overlapping phenomena of neighbored printing dots. In the modified error diffusion, quantization errors to be diffused are adjusted to improve both image blur and color change produced in the error diffusion. So, the printed image is similar to the image of monitor. Our results indicate that proposed algorithm can produce high quality image in the low bit color devices.

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A Realistic Modeling and Rendering of Cloth Textures by Photometry (사진 측정에 의한 옷감의 질감 모델링 및 사실적 렌더링)

  • Kim, Min-Soo;Kim, Dae-Hyun;Kim, Myoung-Jun
    • Journal of KIISE:Computer Systems and Theory
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    • v.35 no.2
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    • pp.84-93
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    • 2008
  • Modeling and rendering of cloth texture have been regarded as one of the most important factors to enhance reality of the contents in the digital contents industry. So far, however, two major approaches to realistically describe the cloth texture were developed: building analytical reflectance model for target cloth and sometimes thread itself and obtaining overall reflectance model using optical equipments. However, yielding a plausible analytic reflection model satisfying many subtle characteristics of a cloth is not an easy task; moreover, fine-detailed modeling of the cloth pattern across the target clothes should also be accompanied by huge amount of computation. The method to obtain overall reflectance model needs expensive measurement equipments and data size becomes huge. Since it applies in the end the reflectance model obtained at one point of a cloth to across whole the visible area of the target clothes, it cannot properly reproduce the pattern of the clothes nor the texture. To address the aforementioned problems, this paper proposes a simple low cost camera rig and a novel method for realistic modeling and rendering of the cloth texture by analyzing photos taken by the proposed camera rig, which can reproduce even the texture pattern applied to the whole clothes, overcoming the one-point reflectance model.

Verification of the Reliability of the Numerical Analysis for the Crash Impact Test of Rotorcraft Fuel Tank (회전익항공기용 연료탱크 충돌충격시험에 대한 수치해석 신뢰성 검증)

  • Kim, Sungchan;Kim, Hyun-Gi
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.19 no.12
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    • pp.918-923
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    • 2018
  • The main function of a fuel tank is to store fuel. On the other hand, the structural soundness of the fuel tank is related directly to the survival of the crew in an emergency situation, such as an aircraft crash, and the relevant performance is demonstrated by a crash impact test. Because crash impact tests have a high risk of failure due to the high impact loads, various efforts have been made to minimize the possibility of trial and error in the actual test at the beginning of the design. Numerical analysis performed before the actual test is a part of such efforts. For the results of numerical analysis to be reflected in the design, however, the reliability of numerical analysis needs to be ensured. In this study, the results of numerical analysis and actual test data were compared to ensure the reliability of numerical analysis for the crash impact test of a rotorcraft fuel tank. For the numerical analysis of a crash impact test, LS-DYNA, crash analysis software, was used and the ALE (arbitrary Lagrangian Eulerian) technique was applied as the analysis method. To obtain actual test data, strain gages were installed on the metal fittings of the fuel tank and linked to the data acquisition equipment. The strain and stress of the fuel tank fitting were calculated by numerical analysis. The reliability of the numerical analysis was enhanced by assessing the error between the strain measurement of the upper fitting obtained from an actual fuel tank and the strain calculated from numerical analysis.