• 제목/요약/키워드: engine facility

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Study on the Emergency Protection System of Liquid Rocket Engine (액체로켓엔진 비상보호시스템 연구)

  • Kim, Seung-Han;Han, Yeoung-Min
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.97-103
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    • 2011
  • This paper describes the main considerations for the development of engine emergency protection system and applications to preliminary engine development tests. Emergency protection system performed its role without failure to shutdown test very quickly for the prevention of development of malfunctioning of test articles, which protected test articles and test facility in all abnormal situation occurred during preliminary engine development test program. This results will be used for the development of engine emergency protection system.

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Development of Small-sized Gas Turbine Engine Control System for Power Generation (발전용 소형가스터빈엔진 제어시스템 개발)

  • Hong, Seong-Jin;Kim, Seung-Min;Yook, Sim-Kyun;Nam, Sam-Sik
    • The KSFM Journal of Fluid Machinery
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    • v.14 no.4
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    • pp.52-56
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    • 2011
  • Small-sized gas turbine engine could be applied to various fields such as propulsion, power generation, machine driving, etc., and Doosan has been developing 5MW class gas turbine engine for power generation since 2005. To verify its design performance and operating characteristics, a gas turbine engine test facility was constructed, and control system was also established to satisfy rapid and reliable control performance. In this paper, the hardware specification and structure of control system for gas turbine engine are introduced, and test result for starting characteristics analysis and loading is also presented.

Development of Test Stand for Altitude Engine Test of Reciprocating Engine (왕복동 엔진의 고도성능시험을 위한 시험장치 개발)

  • Lee, KyungJae;Yang, InYoung;Kim, ChunTaek;Kim, DongSik;Baek, Cheulwoo;Yang, GyaeByung
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.563-571
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    • 2017
  • Test stand for altitude engine test of reciprocating engine was designed, manufactured and validated by preliminary test and simple calculation. These test stand designed to interface with Altitude turbo-shaft engine test facility of Korea Aerospace Research Institute. Many limiting condition for altitude test of reciprocating engine are assumed and test stand was developed to satisfy those limits. Test stand design specially focused on a altitude, Mach number and fuel temperature control for reciprocating engine altitude test with smaller air and fuel flow than turbo-shaft engine.

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Pressure Drop Changes at Engine Fuel Inlet Filter according to Water Contents Management of KSLV-II Liquid Rocket Fuel (한국형발사체 액체로켓 연료의 수분관리에 따른 엔진 연료입구필터 차압의 변화)

  • Hwang, Changhwan;Kim, Inho;Park, Jaeyoung;Kim, Seonglyong;Yoo, Byungil;Cho, Namkyung;Han, Yeoungmin
    • Journal of the Korean Society of Propulsion Engineers
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    • v.24 no.6
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    • pp.120-125
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    • 2020
  • 75 tonf liquid rocket engine combustion test was performed at Naro space center Engine Combustion Test Facility for KSLV-II. A gradual pressure drop was observed during off-design combustion test turbopump inlet condition using cooled kerosene at 271 K. It was found that the water content inside kerosene could cause pressure drop at 40 ㎛ grade filter through the water contests analysis of kerosene, kerosene cooling test and dehydration of kerosene.

Economic Feasibility Analysis on Construction Facility Improvement Project of North Korea Considering Technology Application Period (국내 기술의 적용시기를 고려한 북한 건축시설 개선사업의 경제적 타당성 분석)

  • Kim, Min Ju;Kim, Chang-Won;Lee, Dongyoun;Cho, Hunhee;Kang, Kyung-In
    • Proceedings of the Korean Institute of Building Construction Conference
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    • 2016.05a
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    • pp.68-69
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    • 2016
  • North Korean market created by reunification of the Korean Peninsula is expected to serve as a new growth engine to the already-developed construction industry of South Korea. Improvement on deteriorated construction facility of North Korea is a project in urgent need at the initial stage of reunification. Prior to market entry of the Korean peninsula under these circumstances, economic feasibility analysis on construction technology application must be preceded by considering reunification period. Therefore, this study conducts an economic feasibility analysis on construction facility improvement project of North Korea considering application period of technology developed by South Korea. Results of this study are expected to be utilized in future reunification process as the basis for establishing relevant guidelines for construction facility improvement project of North Korea.

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Technical Review of Heavy Test Facilities of Liquid Rocket Propulsion System (액체추진기관 대형시험설비 기술동향)

  • Yu, Byung-Il;Kim, Ji-Hoon;Oh, Seung-Hyub
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.11a
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    • pp.814-815
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    • 2010
  • Korea Aerospace Research Institute plan to develop propulsion system test facilities for combustor, engine system, propulsion systems of KSLV-II propulsion system in process of Korea Space Launch Vehicle project. By review for heavy test facilities specifications of foreign technically developed nations of the world, it will be referenced for test facility development plan of Korea Space Launch Vehicle project in the future.

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Designing an expert system for library classification (문헌분류 전문가시스팀의 설계에 대한 연구)

  • 김정현
    • Journal of Korean Library and Information Science Society
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    • v.21
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    • pp.459-483
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    • 1994
  • The purpose of the study is to design and implement a prototype expert system for library classification in the literature field of the DDC 20. The system was largely consisted of a knowledge base, an inference engine, a knowledge acquisition facility, an explanation facility and an user interface facility. The knowledge base was represented by inference rules and frames. The name file for authors and titles was designed separately. The forward chaining technique was chosen for the inference engine and the menu-driven dialog technique was also taken for the user interface. The conclusions of the study can be summarized as follows: 1) The difficulty of document classification work is due to the complex and stringent classification rules. Such problems can be considerably alleviated by using the present system. 2) Even the novice with a knowledge about the DDC 20 can easily access the system. And also librarian other than the professional classifier can easily be accustomed to the classification work. 3) The system can be used as an online classification scheme. 4) By adding any local language other than English or Hangeul on the menu screen, the language problem relating classification can be overcome. 5) The system can be employed as the intensification tool for the education of classification as well as library automation.

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A Study on the Characteristics of the Oil-free Turbocharger for Diesel Engine Vehicles (디젤 엔진 차량의 무급유 터보차져의 성능 평가에 관한 연구)

  • Park, Dong-Jin;Kim, Chang-Ho;Lee, Yong-Bok
    • Transactions of the Korean Society of Automotive Engineers
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    • v.16 no.4
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    • pp.47-55
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    • 2008
  • Turbocharger has a main purpose on recycling of the exhaust gas from the engine cylinder. On the basis of the facility characteristics, the turbocharger supported on floating ring bearings has some problems such as the large volume, oil supplement for lubrication and high power loss due to high operating torque. The air foil bearing has been studied as the bearing element to be able to alternate the floating ring bearing without the problems of the floating ring bearing. In this study, the air foil bearing has 2 parts; journal and thrust bearings, and the test facility consists of the engine, exhaust and intake parts. In addiction, the specification of the turbocharger follows a small turbocharger for SUV engine. The engine speed is varied from 750 (idle rpm) to 2,500 rpm and then, the rotating speed of the turbocharger rotor is accelerated from 0 to 100,000 rpm. From those experiments, the comparison between the performances of the air foil bearing and floating ring bearing is conducted and the results show that the air foil bearing has less power loss, maximum 770 watt, than the floating ring bearing, maximum 5,110 watt. This result verifies that the air foil bearing is more efficient and able to output more power under the same condition of the input power.

Implementation of HL7 Interface Engine for Medical Information Exchange (의료정보 공유를 위한 HL7 인터페이스 엔진 구현)

  • Hwang, Deuk-Young
    • Journal of the Korea Society of Computer and Information
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    • v.15 no.8
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    • pp.89-98
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    • 2010
  • Recently supply of Internet is bringing a important change in medical environments. The hospitals which had a different system is required the system that can efficiently share and exchange medical information. In order to transmission medical information between systems, the Health Level Seven(HL7) interface engine development that can convert medical data to HL7 messages is necessary. The HL7 is a standard protocol for data exchange in healthcare environments. In this paper, I implemented HL7 interface engine for Alzheimer's disease in elderly care facility. The interface engine is composed of the client system and the server system. The client system inputs user's medical care data for the aged, and builds them into HL7 message stream. HL7 messages in the client system transmitted over TCP/IP protocol to the server system. The server system parses and validates this messages stream to the segments and fields and then transmits acknowledgement to the client system. I implemented it using the Java and JavaCC. The study of interface engine implementation can be used meaningfully in electronic health record, telemedicine system, and medical information sharing among various healthcare institutions.