• Title/Summary/Keyword: SFC 프로그램

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Use of HCI Program for Optimization of Operating Conditions in Analytical and Preparative Chromatography (분석 및 분리용 크로마토그래피에서 조업조건의 최적화를 위한 HCI 프로그램의 이용)

  • Lee, Ju-Won;Lee, Min-U;No, Gyeong-Ho
    • KSBB Journal
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    • v.14 no.4
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    • pp.408-413
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    • 1999
  • To separate mixtures analytically and preparatively by LC (Liquid Chormatography), the operating conditions of analytical chromatography should be determined. The HCI program was utilized to find the optimum operating condition accurately and rapidly, and to reduce the number of experiments. In an analytical chromatography, based on the resolution and analysis time, the experimental conditons of deoxyribonucleosides and phopholipids were fixed in terms of taxol was calculated, and the collection time was predicted for the mixture of 5'-IMP and 5'-GMP from the elution profile when and purity wer known.

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Development of an Software Programmable Logic Control Compiler based on SPC-10 (SPC-10기반 소프트웨어 PLC 컴파일러 개발)

  • Cho Young Im
    • Proceedings of the Korean Institute of Intelligent Systems Conference
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    • 2005.04a
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    • pp.206-209
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    • 2005
  • 본 논문에서는 국내에서 상용화되고 있는 삼성전자의 SPC-10의 IEC1131-3 표준 언어(LD, SFC, FBD, ST)가 상호 호환성을 갖도록 목적 언어인 IL로 변환하여 컴파일 될 수 있는 IL 컴파일러를 개발하고자 한다. 개발하려는 IL 컴파일러는 IL언어의 활용성을 매우 높여주며, 실제네트워크 디바이스에 다운로드 하여 사용할 수 있는 IL 언어를 생성하고 실행시키는 점이 특징이다. 이 시스템은 SPC-10에서 많이 사용되는 언어를 패턴인식에 의해 클러스터링하여 자동적으로 IL 언어로 변환이 되며, 컴파일에 의해 PLC 프로그램의 동작이 가능하다. 이 시스템에서는 또한 사용자가 발생할 수 있는 문법오류는 물론 논리오류를 지능적 에이전트에 의해 검색하여 수정함으로써 최적화된 환경에서 PC 기반 제어가 가능하도록 해준다.

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Small Turbojet Engine Test and Uncertainty Analysis (소형 터보제트 엔진 시험 및 불확도 분석)

  • Jun, Yong-Min;Yang, In-Young;Nam, Sam-Sik;Kim, Chun-Taek;Yang, Soo-Seok;Lee, Dae-Sung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.30 no.5
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    • pp.118-126
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    • 2002
  • The Altitude Engine Test Facility(AETF) was built at the Korea Aerospace Research Institute and has been being operated for the gas turbine engines in the class of 3,000 lbf thrust. To enhance the confidence level of AETF to the international level, a series of studies and facility modification have been conducted to improve the measurement uncertainty and reliability. In this paper, some part of the facility evaluation tests performed with a single spool turbojet engine are introduced. Tests were performed simulating the flight conditions as steady state, sea level for various flight speeds (i.e., Mn=0.3, 0.5, 0.7, 0.9). The obtained test results are compared with the predicted values of the engine DECK. The measurement uncertainties of airflow, net thrust, fuel flow and SFC showed 0.791~0.914%, 0.851~1.706%, 1.372~7.348% and 1.642~5.205%, respectively. Thus, from this research, the improvement methods of uncertainties on AETF has been confirmed.