• Title/Summary/Keyword: 펌프 배관

Search Result 131, Processing Time 0.027 seconds

펌프 위치 선정 (배관내 압력분포)

  • 정진문
    • 월간 기계설비
    • /
    • s.61
    • /
    • pp.23-29
    • /
    • 1995
  • 열원기기와 공조기등을 연결하는 물배관식에는 여러 가지 방식이 있으며, 이는 배관의 기능 및 용도에 따른 각종 설계요소를 비롯하여 에너지 절약 측면 또는 내구성 향상을 위한 배려등에 의하여 결정되어지고 있다. 그러면 강제순환 배관계통에서 장치내의 펌프위치는 어떤 영향이 미치는지 한사례를 통하여 펌프가 열원기기의 전$\cdot$후에 설치되었을때 배관내의 압력분포도를 작성하고, 이에 대한 분석을 통하여 우리가 간과하기 쉬운 펌프 위치선정에 대한 주의점 및 배관내의 압력분포에 대한 유의사항등을 알아 보기로 한다.

  • PDF

Experimental Study on the Blade Excitation Frequency for the Natural Frequence of Centrifugal Pump Piping Systems (원심펌프 배관계 진동에 영향을 주는 블레이드 가진주파수의 실험적 고찰)

  • 김윤제;신호길
    • Journal of Energy Engineering
    • /
    • v.10 no.4
    • /
    • pp.335-341
    • /
    • 2001
  • Pressure pulsations generated by the blade-tongue interaction induce vibration of the piping systems and the structure connected to pumps, resulting in the severe noise and fatigue fracture. Experiments were made on the natural frequencies of liquid columns in piping systems with a single suction, single stage, centrifugal volute pump. Experimental results show that the natural frequencies of the liquid columns in the pump piping systems depend on the dimensions of the pipes and the impeller shapes, and are not affected substantially by the rate of discharge and the rotating speed of the pump.

  • PDF

CFD Modeling of Unsteady Gas-Liquid Flow in a Small Scale Air-Lift Pump (소형 공기 양수 펌프의 불규칙한 가스-액체 흐름의 CFD 모델링)

  • Li, X.S.;Jeong, H.M.;Chung, H.S.
    • Journal of Power System Engineering
    • /
    • v.16 no.1
    • /
    • pp.30-37
    • /
    • 2012
  • 공기 양수 펌프는 재생 에너지 분야, 부식 및 마모 특성의 유체의 활용 등 높은 신뢰성과 낮은 유지보수 비용을 필요로 하는 분야에서 그 사용이 증대되고 있다. 본 연구에서는 소형 공기 양수 펌프의 성능 평가 및 기초 데이터를 얻기 위한 연구로, D=0.012~0.019m, L=0.933m인 배관의 침수 깊이(${\beta}$=0.55,0.60,0.65,0.70)에 따른 수치해석을 수행하였다. 수치 해석 및 실험 결과는 유사성을 뛰었으며, 펌프의 사양과 효율은 공기의 질량 유속 비, 침수 깊이 비와 양수 배관의 길이에 관한 함수로 나타났다. 그리고 최대 물과 공기 질량 유속의 비는 각 배관에서 서로 다른 침수 깊이의 비로 나타났으며, 공기 양수 펌프의 최대 효율이 발생되는 운전조건은 슬러그(slug)와 슬러그 교반 정도(slug-churn flow regime)에 따라 나타남을 알 수 있었다.

Basic Design of High Pressure LOx Lines for a Liquid Rocket Engine (액체로켓엔진 액체산소 고압 배관부 기본설계)

  • Moon, Il-Yoon;Yoo, Jae-Han;Moon, In-Sang
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2009.11a
    • /
    • pp.107-110
    • /
    • 2009
  • A basic design for a Technical Development Model (TDM) of liquid oxygen lines from the turbopump exit to the oxidizer valves of the combustion chamber and the gas generator was conducted to develop a turbopump-fed liquid rocket engine. The TDM is composed of straight lines, elbows, bellows, a branch, an orifice, flanges and a heat insulator. Materials were determined by consideration of operation conditions, weight constraint and manufacturing procedures. The size and the location of each component were determined by flow analysis of the required flowrate and the pressure loss. Basic designs of the components were conducted by consideration of the operating temperature and the maximum expectation operating pressure. The safety factors were evaluated by structural analysis of design of each component.

  • PDF

경제적인 배관과 PUMP의 시방결정

  • 박승열
    • 월간 기계설비
    • /
    • s.13
    • /
    • pp.180-184
    • /
    • 1991
  • 펌프는 최근 산업의 급속한 발달로 성능, 재질, 구조 등 여러 면에서 새로운 기술을 가미한 각종 펌프가 개발되어 여러 산업분야나 공공사업에 쓰이고 있다. 따라서 펌프계획시나 사용시 여러가지 경우에 대하여 검토하므로써 보다 경제적인 계획을 할 수 있으므로 다음과 같이 주로 물을 취급하는 펌프에 대한 기초적인 이론 및 경제성에 대하여 고찰해 보기로 한다.

  • PDF

Development of Propellant On-Board Feeding System of Pump-fed Liquid Rocket Propulsion System (터보펌프식 발사체 추진기관의 기체공급계 개발)

  • Cho, Nam-Kyung;Jeong, Yong-Gahp;Kwon, Oh-Sung;Han, Sang-Yeop;Kim, Young-Mog
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2006.11a
    • /
    • pp.122-126
    • /
    • 2006
  • Two types of pressurization system and low weight feeding piping system are developed. With sub-system tests, ullage pressure control performance was verified for 1 step and 2 step pressurization system and the feeding performance of feeding piping system was also verified. The weight of the feeding piping system is low enough for the application of launch vehicle. In addition, LOX conditioning system is developed for avoiding geysering and LOX temperature rise. Integrated performance was verified through integrated on-board feeding system performance tests.

  • PDF

High Frequency Signal Analysis of Fuel Pump for Liquid Rocket Engine under Cavitating Condition (캐비테이션 환경에서의 액체로켓엔진용 연료펌프의 고주파 신호 분석)

  • Kim, Dae-Jin;Kang, Byung Yun;Choi, Chang-Ho
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2017.05a
    • /
    • pp.1099-1102
    • /
    • 2017
  • High frequency signals are analyzed which are measured at the inlet / outlet pipeline and pump casing during cavitation tests of the fuel pump for the liquid rocket engine. RMS values of each data are shown according to the cavitation number and compared with those of the LOx pump tests and the impact of the cavitation instability is also explored. Analogies about the cavitation number are confirmed between high frequency data of both pumps. In addition, the cavitation instability is found in all the signals and has an affect on the outlet pressure pulsation of the fuel pump.

  • PDF

High Frequency Signal Analysis of LOx Pump for Liquid Rocket Engine under Cavitating Condition (캐비테이션 환경에서의 액체로켓엔진용 산화제펌프의 고주파 신호 분석)

  • Kim, Dae-Jin;Kang, Byung Yun;Choi, Chang-Ho
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2017.05a
    • /
    • pp.1093-1098
    • /
    • 2017
  • High frequency signals are analyzed which are measured at the inlet / outlet pipeline and pump casing during cavitation tests of the LOx pump for the liquid rocket engine. RMS values of data are shown according to the cavitation number. RMS values of the synchronous frequency, its harmonic frequencies and frequencies of cavitation instabilities are also calculated. The pressure pulsations of the inlet and outlet pipeline are affected by cavitation instabilities. 3x component is predominant in the outlet pulsation sensor since 3x component generated at the inducer is amplified at the impeller. The cavitation instability is also found at the accelerometer signal of the casing.

  • PDF

Features and Cost Reduction Effect of High Pressure LNG Pipeline Network (고압 LNG 배관망의 특성 및 비용절감 효과)

  • Kim, Ho-Yeon;Hong, Young-Soo;Noh, Joo-Young;Eom, Yun-Seong;Kim, Cheol-Man
    • Journal of Energy Engineering
    • /
    • v.17 no.3
    • /
    • pp.139-144
    • /
    • 2008
  • Recently due to march as the high oil price, It is necessary for Korea to grope a plan, which is to increase the energy efficiency of existing facilities as well as to develop overseas gas and oil resources. With this point, this work carried out to approach the high pressure LNG pipeline network of Inchon receiving terminal with Newton method as corrective flowrate. We found that the high pressure network mainly depends on FCVs(Flow Control Valves). The high pressure pump showed the maximum efficiency at the FCVs of 50% opening and could discharge LNG only above the LNG head of 1,500m from a system curve obtained. The operating cost of pumps was estimated from their operating points. We compared the operating cost under normal operation with the operating cost under maximum efficiency. Especially, we obtained the day savings of a year as wells as the hour savings of a day. From the results, the high pressure network win be able to reduce the operating cost of 138 million wons in a year. This means that a pump can reduce the operating cost of 9,823 thousands won. Consequently, this work could find the operating features of the pumps under the complicated high pressure LNG network and the savings effect of the pump operating cost. Also, the results will be able to macroscopically contribute the heightening of national energy competitiveness as well as to microscopically contribute the future effective operation of LNG receiving terminal.