• Title/Summary/Keyword: Chill-down

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A Study of Chill-down Process in 30 tonf Turbopump-Gas Generator Coupled Tests (30톤급 터보펌프-가스발생기 연계시험에서 예냉 절차 연구)

  • Moon, Yoon-Wan;Nam, Chang-Ho;Kim, Seung-Han
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2012.05a
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    • pp.447-450
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    • 2012
  • An analysis of chill-down process was performed for 30 tonf Turbopump-Gas generator coupled tests. The chill-down process must be fulfilled before liquid rocket engine test using cryogenic propellant. Cavitation, damage and/or combustion instability due to bubble of propellant must be eliminated by chill-down process in a test specimen, especially cryogenic pump. The analysis of test data obtained by 30 tonf TP-GG coupled tests was performed in order to be based on the test process of KSLV-II liquid propellant rocket engine which will be developed. To macroscopically understand the process of chill-down from the viewpoint of test procedure the temperatures of important part and total time of chill-down process were analyzed.

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Investigation of Chill Down Characteristics of Liquid Oxygen Feeding System in 75 Tonf-class Liquid Rocket Engine Firing Test (75톤급 액체로켓엔진 연소시험에서의 액체산소 공급부 예냉특성 고찰)

  • Seo, Daeban;Cho, Namkyung;Han, Yeoungmin
    • Journal of the Korean Society of Propulsion Engineers
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    • v.22 no.4
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    • pp.108-116
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    • 2018
  • A firing test of the 75 tonf-class liquid rocket engine to be used as the first and second stage engines of the KSLV-II was carried out at the rocket engine test facility(RETF). Since this engine uses liquid oxygen as the oxidizer, which is a cryogenic fluid, it is essential that the chill down of the supply pipe line and engine proceed for the firing test; thus, the given inlet requirements must be met. Moreover, it is important to understand the chill down characteristics of the facility and the engine and the amount of liquid oxygen consumed in the chill down process for efficient test operation in the future. In this paper, chill down characteristics of the supply pipe and the engine were evaluated through the investigation of the chill down process of the 75 tonf-class liquid rocket engine at each stage before and after run tank pressurization. In addition, the amount of liquid oxygen consumed was also evaluated.

Improvement of a Flow Coefficient for the Recirculation Chill-down Flow in a Main Oxidizer Shut-off Valve (연소기 산화제 개폐밸브 재순환예냉 유로의 유량계수 개선)

  • Hong, Moongeun
    • Journal of the Korean Society of Propulsion Engineers
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    • v.21 no.4
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    • pp.89-95
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    • 2017
  • The improvement of a flow coefficient for the recirculation chill-down flow in a main oxidizer shut-off valve has been presented. The flow coefficient, which is mainly affected by the recirculation outlet port size and the configuration inside the valve, has been predicted with measured flow coefficient values. The comparison of experimentally measured flow coefficient with the predicted value shows the effect of valve inside configuration on the flow coefficient. Consequently, the flow coefficient is twice the previous value and about 75% of the pressure loss assigned to the main oxidizer shut-off valve can be used for additional pressure losses for other components in the recirculation chill-down system of a launch vehicle.

A Study on Cryogenic Line Chill Down Characteristics of LNG (극저온 LNG 배관냉각 특성에 대한 연구)

  • BYEONGCHANG, BYEON;KYOUNG JOONG, KIM;SANGKWON, JEONG;MO SE, KIM;SANGYOON, LEE;KEUN TAE, LEE;DONGMIN, KIM
    • Journal of Hydrogen and New Energy
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    • v.33 no.6
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    • pp.808-818
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    • 2022
  • In this research paper, we investigated the cryogenic line chill down characteristics of liquefied natural gas (LNG). A numerical analysis model was established and verified so that it can calculate the precise cooling characteristics of cryogenic fluid for the stable and safe utilization especially such as LNG and liquid hydrogen. The numerical modeling was programmed by C++ as an one-dimensional homogeneous model. The thermohydraulic cooling process was simulated using mass, momentum, energy conservation equations and appropriate heat transfer correlations. In this process, the relevant heat transfer correlations for nuclear boiling, transition boiling, film boiling, and single-phase heat transfer that can predict the experimental results were implemented. To verify the numerical modeling, several cryogenic line chill down experiments using LNG were conducted at the Korea Institute of Machinery & Materials (KIMM) LNG and Cryogenic Technology Center.

Effect of geometry on shrinkage of cryostats for HTS cables

  • de Souza Isaac;Jadkar Ninad;Gour Abhay Singh;Vasudeva Rao Vutukuru
    • Progress in Superconductivity and Cryogenics
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    • v.25 no.4
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    • pp.32-39
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    • 2023
  • One of the main problems faced in developing India's first HTS power cable was that of shrinkage in length of the double-walled vacuum-insulated cryostat. The shrinkage was due to the evacuation of the annular vacuum space which results in a shorter working cable length. This work reports experimentally observed contraction during evacuation and analyses corrugated pipes/bellows which house the cable core of HTS cables. The effect of corrugation geometry including length, corrugation pitch and depth, diameters of corrugated pipes and thicknesses of pipes is studied numerically to realize the degree of shrinkage due to vacuum as well as chill down. Finally, necessary length compensation and associated cost is determined to tackle the shrinkage issue.

Soundscapes of Soswaewon Represented in Kim In-Hu's 48 Poems (김인후의 48영에 표상된 소쇄원의 소리풍경)

  • Han, Myung-Ho;Cheon, Deuk-Youm
    • Journal of architectural history
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    • v.24 no.6
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    • pp.21-33
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    • 2015
  • This study aims to rediscover the meaning and value of Soswaewon construction represented in Kim In-Hu's 48 poems on the basis of the concept and idea of soundscape. It classified the landscape resources through the various emotional elements such as the sense of sight, hearing, smell, touch, taste, and warmth described in the 48 poems of Soswaewon, and also interpreted the meaning and value of Soswaewon construction. Appreciating various sounds of Soswaewon, Kim In-Hu understood a sound as an important element of the landscape. Also, he abundantly wrote down the interesting changes of Soswaewon which vary depending on time or seasons. The 48 poems contain the scent and feel of Soswaewon as well as the soundscapes which can be heard with ears. A variety of sounds heard in Soswaewon are the whole senses which are combined with the chill of Soswaewon, the fragrance of trees and the mystery of the mountain, etc, and they mean the wider world much more than the value of physical sounds. Soundscapes of Soswaewon are becoming an emotional space which intactly conveys not only the musical inspiration but also the scent of life to us.

A Study on the Mechanical Properties of High-P, High-Si Ductile Cast Iron (고인(高燐), 고규소(高硅素) 구상흑연주철(球狀黑鉛鑄鐵)의 기계적(機械的) 성질(性質)에 관(關)한 연구(硏究))

  • Kim, Ha-Young
    • Journal of Korea Foundry Society
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    • v.8 no.3
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    • pp.296-309
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    • 1988
  • In this study the mechanical properties of ferritic ductile cast iron in as-cast are discussed by metallographic considering the effect of phosphorus content(about 0 - 0.8wt.%). In ferritic S.G. cast iron containing about 4.2wt.% Si, 0.5wt.% Ni, 0.02wt.%B, these samples are investigated for castability, microstructure, machinability, wear resistance, mechanical and thermal properties. The main results are summarized as follows. 1) The chill depth increased greatly with P addition up to about 0.6wt.% but the tensile strength and the elongation are decreased smoothly. 2) The size of S.G. and the amount of steadite increase with increasing P content. This means the tendency of increasing the number of S.G. 3) The maximum value of wear by mechanical fracture was appeared at the abrasion speed of 1.14m/sec and the plastic Flow layers are stretched longly on the wear surface with decreasing P content. 4) Although the coefficient of thermal expansion increased with P addition, the cast iron growth was slowing down extremely at 0.6w.% P or more.

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Thermomechanical Analysis of a 75ton Thrust Turbopump Assembly (75톤급 터보펌프의 조립체 열응력 거동 해석)

  • Yoon, Suk-Hwan;Jeon, Seong-Min;Kim, Jin-Han
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.11a
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    • pp.409-412
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    • 2009
  • A 75ton thrust turbopump system for liquid rocket engine was analyzed thermally and mechanically. A 2D axisymmetric model of the turbopump assembly was created. In the analysis operation cycle including chill-down, operation and post operation steps were considered. Appropriate heat transfer conditions for each step were modeled and applied. Transient temperature distribution was calculated, consequent mechanical analysis was conducted to predict stress and deformation. Effects of external heat insulators and heat dissipation at the bearings were considered in the heat transfer analysis.

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A literratual study on correlation of Pehuh(肺虛), Peson(肺損), Pero(肺勞) (폐허(肺虛) 폐손(肺損) 및 폐노(肺勞)의 상호관계(相互關係)에 대(對)한 문헌적(文獻的) 고찰(考察))

  • Lee, Han-Goo;Jung, Sung-Gi;Rhee, Hyung-Koo
    • The Journal of Internal Korean Medicine
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    • v.3 no.1
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    • pp.41-48
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    • 1986
  • 1. The cause of Pehuh is deficiency of Peki(肺氣). Symptoms are tachypnea, thirst and deafness of hemoptysis. In treatment, control it's Ki(氣). 2. The cause of Peson is in addition to Pehuh Pimo(皮毛) is demaged by heat and cold. Symptoms are alopecia, cough, sputum, fever and chill. In treatment, supply it's Ki. 3. The cause of Pero is it's Ki which is demaged by lie down for a long time or because of anxiety Sang Ryum Hueng Kum(上炎刑金). Symptoms are tachypnea, chest and back pain, cough and sputum. In treatment, supply Sinki(腎氣). 4. In correlation of Pehuh, Peson and Pero, Pehuh is progressed from Kihuh(氣虛), Peson is progressed from Pehuh and Pero is progressed from Peson. 5. The treatment of Lung disease showed by chapter Huhro(虛勞). In early stage, control it's Ki. In middle stage, supply it's Ki. The last stage, supply Sinki(腎氣).

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Turbopump+Gas generator Open-loop coupled test (터보펌프+가스발생기 개회로 연계시험)

  • Kim, Seung-Han;Nam, Chang-Ho;Kim, Cheul-Woong;Moon, Yoon-Wan;Seol, Woo-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.11a
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    • pp.125-128
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    • 2008
  • As a interstage of the 30tonf level LOx/kerosene liquid rocket engine development, turbopump-gas generator open-loop coupled tests are performed. Test schematic and test results of open-loop coupled tests are presented. In engine system operation environment simulating combustion chamber by flow control orifice, chill-down procedure, startup characteristics, nominal operability of turbopump+gas generator open-loop coupled Test Plant are confirmed The results of open-loop coupled test were used for the preparation on turbopump+gas generator closed-loop test.

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