• Title/Summary/Keyword: Hydraulic powerpack

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A Study on the Application and Economical Efficiency of Electric Driven Cargo Pumping System (전동기 구동 카고펌프의 적용 및 경제성 연구)

  • Cho, Dong-Ju;Kim, Kyung-Bae;Park, Myung-Kyu
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.24 no.1
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    • pp.85-89
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    • 2012
  • This study has been conducted to compare two cargo handling systems on MR tanker and Panamax tanker. Submerged hydraulic cargo pumps with hydraulic power packs and frequency converter controlled electric deepwell pumps will be investigated and compared on all aspects of initial cost, installation, operation and maintenance. The result of investigation shows Electric Systems have less manufacturing costs, higher environmental friendliness and reliable operation compare to Hydraulic Systems. Furthermore, the present experimental data will provide important database for Electric Systems onboard new ships and practical and empirical guidelines are constructed for further determine the design of the Electric Systems.

Pressure Control of Staged Combustion Liquid Rocket Engine (다단연소사이클 액체 로켓엔진의 압력제어에 대한 연구)

  • Hwang, Changhwan;Lee, Kwangjin;Woo, Seongphil;Im, Ji-Hyuk;Jeon, Junsu;Lee, Jungho;Yoo, Byungil;Han, Yeoungmin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.88-93
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    • 2017
  • For the control of pre-burner combustion pressure, the open angle of TTR(Throttle for Thrust Regulation) valve was varied from $143^{\circ}$ to $185^{\circ}$ while testing of cold flow, ignition, combustion. The major performance variables of rocket engine and hydraulic performance of TTR valve regarding the open angle was verified. However the controllability of pre-burner combustion pressure was not verified due to the limitations of test. The comprehensive research will be done after supplementing these problems.

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Pressure Control of Staged Combustion Liquid Rocket Engine (다단연소사이클 액체 로켓엔진의 압력제어에 대한 연구)

  • Hwang, Changhwan;Lee, Kwangjin;Woo, Seongphil;Im, Ji-Hyuk;Jeon, Junsu;Lee, Jungho;Yoo, Byungil;Han, Yeoungmin
    • Journal of the Korean Society of Propulsion Engineers
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    • v.22 no.4
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    • pp.18-23
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    • 2018
  • For the control of pre-burner combustion pressure, the open angle of the TTR (Throttle for Thrust Regulation) valve was varied from $143^{\circ}$ to $185^{\circ}$ while testing cold flow, ignition, and combustion. The major performance variables of rocket engines and hydraulic performance of the TTR valve regarding the open angle were verified. However, the controllability of pre-burner combustion pressure was not verified due to the limitations of the test. Comprehensive research will be done after addressing these problems.