• Title/Summary/Keyword: Gas-liquid injector

Search Result 157, Processing Time 0.025 seconds

Numerical Study for Kerosene Surrogate Model in Supercritical Swirl Injector (초임계 스월 인젝터에서의 케로신 Surrogate 모델에 대한 수치적 연구)

  • Kim, Kuk-Jin;Heo, Jun-Young;Sung, Hong-Gye
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2010.11a
    • /
    • pp.19-23
    • /
    • 2010
  • Injection characteristics of a kerosene swirl injector of liquid rocket engine operating at supercritical environment have been investigated. Kerosene surrogate models are proposed to model the kerosene properties. Turbulent numerical model is based on large eddy simulation and contains Soave modification of Redlich-Kwong equation of state and Chung's model. Numerical analysis results at supercritical environment are compared with the one at transcritical condition. Differences of density and viscosity are analyzed at both liquid film and core gas in the swirl injector.

  • PDF

Injection Condition Effects of a Pintle Injector for Liquid Rocket Engines on Atomization Performances (액체로켓 핀틀 인젝터의 분사조건이 미립화 성능에 미치는 영향)

  • Son, Min;Yu, Kijeong;Koo, Jaye;Kwon, Oh Chae;Kim, Jeong Soo
    • Journal of ILASS-Korea
    • /
    • v.20 no.2
    • /
    • pp.114-120
    • /
    • 2015
  • Effects of injection conditions on a pintle injector which is proper to recent liquid rocket engines requiring low cost, low weight, high efficiency and reusability were studied. The pintle injector with a typical moving pintle was used for atmospheric experiment using water and air. Injection pressures of water were considered 0.5 and 1.0 bar, 0.1 to 1.0 bar for injection pressures of air and 0.2 to 1.0 mm for pintle opening distance. Sauter mean diameters (SMD) of spray was measured at 50 mm distance from a pintle tip and SMD was treated as a representative parameter in this study. As a result, because of shape characteristics of the pintle injector, there was a transient region between the pintle opening distances of 0.6 and 0.7 mm and this region affected to mass flow rates and SMDs. Also, Reynolds numbers for gas, Weber numbers and momentum ratios were adopted as major non-dimensional paramters and the momentum ratio has strong correlation with SMD.

Spray Characteristics of Swirl-coaxial Injector According to the Recess Length and Injection Pressure Variation (리세스 길이 및 분사압력 변이에 따른 스월 동축형 인젝터의 분무특성)

  • Bae, Seong Hun;Kwon, Oh Chae;Kim, Jeong Soo
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.20 no.4
    • /
    • pp.68-76
    • /
    • 2016
  • This research is carried out for the performance evaluation of the injector that is one of the critical components of bipropellant-rocket-engine. Spray characteristics are investigated in detail according to the recess length and injection pressure on the swirl-coaxial-injector using gaseous methane and liquid oxygen as propellants. A visualization is conducted by the Schlieren photography that is composed of a light source, concave mirrors, knife, and high-speed-camera. A hollow-cone-shape is identified in the liquid spray that is spread only by inner injector and the spray angle is decreased due to the diminution of swirl strength in accordance with the increase of the length of injector orifice. When the injector sprays the liquid through the inner injector with the aid of gas through the outer injector, the spray angle in external mixing region tends to increase with rise of the recess length, while in internal mixing region, it is decreased. It is also confirmed that the same tendency of the spray angle with recess length appears irrespective of the injection pressure of liquid spray.

A Study on Performance Improvement in Durability and Reliability of LPi Injector (LPI 인젝터의 성능 및 내구성 개선에 관한 연구)

  • Park, Cheol-Woong;Kim, Chang-Up;Choi, Kyo-Nnam;Baik, Seung-Kook;Shin, Moon-Sung
    • Journal of the Korean Institute of Gas
    • /
    • v.16 no.2
    • /
    • pp.38-44
    • /
    • 2012
  • In recent years, the need for more fuel-efficient and lower-emission vehicles has driven the technical development of alternative fuels such as LPi (Liquid phase LPG injection) which uses pump for the high pressure supply of liquid LPG fuel and is able to meet the limits of better emission levels while it has an advantage of higher power. Although it has the advantage of power and lower emission levels, the characteristics of LPG, such as high vapor pressure, lower viscosity and surface tension than gasoline fuels makes it difficult design system. Therefore most fuel pumps and injectors are imported. In the present study, in order to domestically develop LPG injector which guarantees flow rates and optimal operation, the experimental investigation on leakage and flow rate characteristics of developed prototype injector was carried out at the bench test rig for developed injector.

Hot-firing Test Results of Subscale Gas Generator for 75 ton-class Liquid Rocket Engine (75톤급 액체로켓엔진 축소형 가스발생기 연소시험 결과)

  • Kim, Mun-Ki;Ahn, Kyu-Bok;Lim, Byoung-Jik;Kim, Jong-Gyu;Seo, Seong-Hyeon;Choi, Hwan-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2010.11a
    • /
    • pp.726-728
    • /
    • 2010
  • A subscale gas generator was designed and manufactured to investigate the effect of design parameters on discharge coefficients of injectors for a 75 ton-class gas generator and hot-firing tests were successfully performed. The test results showed that discharge coefficients of fuel and liquid oxygen injectors remained nearly constant irrespective of variations of a mixture ratio and a chamber pressure. When the post diameter of the liquid oxygen injector was reduced, the discharge coefficient was increased as the pressure drop of the injector was decreased.

  • PDF

Atomization Characteristics of shear coaxial twin fluid injector (동축형 인젝터의 미립화 특성)

  • Han, J.S.;Kang, G.T.;Kim, Y.;Kim, S.J.
    • Journal of ILASS-Korea
    • /
    • v.5 no.4
    • /
    • pp.40-46
    • /
    • 2000
  • To understand the basic the structure of the spray field and to obtain the initial conditions for computational models for shear coaxial twin-fluid injectors. the atomization characteristics under different flow and geometric conditions were examined. The spray characteristics such as SMD, mean axial and radial velocities, Dia. of droplets and volume flux with a P.D.P.A. Water and nitrogen gas under atmospheric conditions were used as a test fluids. The drops produced by shear coaxial injectors continue to disintegrate along the spray axis and decrease their sizes. SMD was the maximum at the spray center of spray and decreased with increasing radial distance. The results of this parametric study showed that SMD decreased with increasing gas injection velocity as well as with decreasing liquid injection mass flow rate, The relative velocity between gas and liquid flow played a significant role resulted in decreasing SMD and in spreading the spray. Recessing the liquid orifice resulted decreasing SMD and a spreading the spray. Recess of liquid orifice by 5.0mm showed best atomization characteristics in this experiment. Although drop diameter changes, shear coaxial injector sprays had constant velocity and exhibited a high degree of radial symmetry.

  • PDF

Combustion Performance Tests of Fuel-Rich Gas Generator for Liquid Rocket Engine Using an Impinging Injector (충돌형 분사기 형태의 액체로켓엔진용 가스발생기 연소성능시험)

  • 한영민;김승한;문일윤;김홍집;김종규;설우석;이수용;권순탁;이창진
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.8 no.2
    • /
    • pp.10-17
    • /
    • 2004
  • The results of the combustion performance tests of gas generator which supplies hot gas into the turbine of turbo-pump for liquid rocket engine and uses LOx and kerosene as propellant are described. The gas generator consists of a injector head with F-O-F impinging injector, a water cooled combustion chamber, a gas torch igniter, a turbulence ring and an instrument ring. The effect of turbulence ring and combustion chamber length on performance of gas generator are investigated. The ignition and combustion at design point are stable and the pressure and gas temperature at gas generator exit meets the target. The turbulence ring installed at middle of chamber effectively mixes hot gas with cold gas and the effect of residence time of hot gas in gas generator on combustion efficiency is small. Test results show that the main parameter controlling the gas temperature at gas generator exit is overall O/F ratio.

Improvement of Leakage Performance of LPG Injector (LPG인젝터의 누설성능 향상에 관한 연구)

  • Kim, Changup;Shin, Moonsung;Baik, SeungKook
    • Journal of the Korean Institute of Gas
    • /
    • v.16 no.6
    • /
    • pp.23-28
    • /
    • 2012
  • The LPG engine technology in Korea has made significant advances with the mass production of LPG vehicle with liquid phase LPG injection system, and have reached to satisfy the SULEV emission regulations. As of now, domestic production of LPG fuelled vehicles in Korea have reached more than 2.4 millions, which is the best in the world. But in the technical point of view, the key technologies for fuel injection system of LPG fuelled engine are mainly dependent on foreign license. Especially, fuel injector in the liquid phase LPG injection system has been imported from C company, which supplies LPG injector worldwide in the name of model D. In the context, it is quite urgent to develop the LPG injector technology in Korea. In this study, WCC coating which is key technology to develop LPG injector by reducing the fuel leakage was developed and tested. Considering the fuel leakage of 0.06cc/min in commercial LPG injector, fuel leakage was reduced down to 0.04cc/min with WCC coating technology and optimization of injector structure.

A Study on Spray Characteristics of Deteriorated Mechanical Injectors (노후 기계식 인젝터의 분무특성 연구)

  • Jeong, Minuk;Yu, Young Soo;Yang, Seungho;Choi, Minhoo;Park, Sungwook
    • Journal of ILASS-Korea
    • /
    • v.26 no.3
    • /
    • pp.111-119
    • /
    • 2021
  • Deteriorated agricultural diesel engines using mechanical fuel injection systems have low fuel injection pressures. And they are not equipped with an exhaust gas abatement device, so it produces a lot of exhaust gas. Remanufactured used injectors can reduce emissions because spray characteristics are improved. In addition, remanufacturing is environmentally friendly and economical compared to producing new parts. For efficient injector remanufacturing, it is necessary to conduct a comparison experiment on the spray characteristics of an used mechanical injector and a new injector of the same model. In this study, the spray characteristics of the two injectors were compared by performing an injection quantity measurement and a spray visualization experiment. As a result, the used injector had a larger injection quantity, a shorter spray tip penetration, a wider spray angle and a smaller spray area than the new injector.

A study on the structure of a diesel spray and the Improvement of the Injection System by the Exciplex Method (EXCIPLEX법에 의한 디젤분무의 구조와 분사계 개선에 관한 연구)

  • 김덕줄;차건종
    • Transactions of the Korean Society of Mechanical Engineers
    • /
    • v.19 no.9
    • /
    • pp.2373-2385
    • /
    • 1995
  • The goals of this study are to apply exciplex method to the visualization of the fuel spray of a diesel engine and to investigate the liquid phase of fuel spray that injected at the various tips of a fuel injector. This study provides the informations for the improvement of the diesel injection system and the structures of diesel spry with the boiling of fuel droplets in combustion chamber by the exciplex method. Hexame was used as fuel for approximation to injection condition of the engine. And naphthalene and TMDP were added to the fuel for the visualization by exciplex method. Experimental injectors were 4hole, 8hole, and 1hole impinging injectors. In the injection condition of actual engine the exciplex was sufficient to catch the liquid phase signal. The spray penetration of impinging injector was small than that of actual 4 and 8hole injector but atomization was better. The upper bound of impinging injector was determined by the geometry of a cylinder head and the lower bound was determined by spray angle. On impinging injector the atomization was better at the edge of disk than at center of disk and also the mixing with environmental gas was better.