Thermodynamic Characteristic Study of a High-temperature Flow-rate Control Valve for Fuel Supply of Scramjet Engines

Thermodynamic characteristics are of great importance for the performance of a high-temperature flow-rate control valve, as high-temperature environment may bring problems, such as blocking of spool and increasing of leakage, to the valve. In this paper, a high-temperature flow-rate control valve, pilot-controlled by a pneumatic servo system is developed to control the fuel supply for scramjet engines. After introducing the construction and working principle, the thermodynamic mathematical models of the valve are built based on the heat transfer methods inside the valve. By using different boundary conditions, different methods of simulations are carried out and compared. The steady-state and transient temperature field distribution inside the valve body are predicted and temperatures at five interested points are measured. By comparing the simulation and experimental results, a reasonable 3D finite element analysis method is suggested to predict the thermodynamic characteristics of the high-temperature flow-rate control valve.

[1]  Giovanni Tanda,et al.  Heat transfer in rectangular channels with transverse and V-shaped broken ribs , 2004 .

[2]  Gilbert F. Froment,et al.  Kinetic modeling of the thermal cracking of hydrocarbons. 1. Calculation of frequency factors , 1988 .

[3]  F. A. Williams,et al.  Acoustic-instability boundaries in liquid-propellant rockets - Theoretical explanation of empirical correlation , 1996 .

[4]  George S. Dulikravich,et al.  Simultaneous Prediction of External Flow-Field and Temperature in Internally Cooled 3-D Turbine Blade Material , 2000 .

[5]  Yong Hong Li,et al.  Thermodynamic Analysis of Friction Pairs inside a High Temperature Flow Rate Control Valve for Scramjet Engines , 2008 .

[6]  Jerald R. Brevick,et al.  Prediction of Thermal Fatigue in Tooling for Die‐casting Copper via Finite Element Analysis , 2004 .

[7]  B Y Lee,et al.  Thermal analysis of a liquid-petroleum-liquid injection engine piston using the inverse heat conduction method , 2008 .

[8]  Tong Hong Wang,et al.  Transient Thermal Analysis for Board-Level Chip-Scale Packages Subjected to Coupled Power and Thermal Cycling Test Conditions , 2006 .

[9]  Ma Chongfang,et al.  Turbulent convective heat transfer with molten salt in a circular pipe , 2009 .

[10]  Carlos G. Rodriguez Computational Fluid Dynamics Analysis of the Central Institute of Aviation Motors/NASA Scramjet , 2003 .

[11]  Viacheslav A. Vinogradov,et al.  Russian Research on Experimental Hydrogen-Fueled Dual-Mode Scramjet: Conception and Preflight Tests , 2001 .

[12]  Shirish Raichintala,et al.  Heat exchanger switchover in a refrigeration system: Thermodynamic modeling of a reversing valve , 2005 .

[13]  Michael Goldfarb,et al.  Design and Characterization of a Rotary Actuated Hot Gas Servovalve , 2004 .

[14]  Vigor Yang,et al.  Liquid rocket engine combustion instability , 1995 .

[15]  Lin Wang,et al.  Transient Analysis of a Spring-Loaded Pressure Safety Valve Using Computational Fluid Dynamics (CFD) , 2010 .

[16]  J. K. Hedrick,et al.  Modeling and Validation of Automotive Engines for Control Algorithm Development , 1992 .

[17]  Braham Prakash,et al.  High temperature friction and wear characteristics of various coating materials for steam valve spindle application , 2000 .

[18]  Th. Eggers,et al.  Design Studies of the JAPHAR Experimental Vehicle for Dual Mode Ramjet Demonstration , 2001 .

[19]  M. S Söylemez On the optimum heat exchanger sizing for heat recovery , 2000 .

[20]  E. T. Curran,et al.  Scramjet Engines: The First Forty Years , 2001 .

[21]  Abbas Elmualim,et al.  Performance Evaluation of a Wall Mounted Convector for Pre-heating Naturally Ventilated Spaces , 2003 .

[22]  W. Rohsenow,et al.  Thermally Optimum Spacing of Vertical, Natural Convection Cooled, Parallel Plates , 1984 .

[23]  John J. Moskwa,et al.  Engine Control Using Estimated Parameters From a Real Time Model of an Engine With Variable Valve Actuation , 2005 .

[24]  A. Roudakov,et al.  Recent Flight Test Results of the Joint CIAM-NASA Mach 6.5 Scramjet Flight Program , 1998 .

[25]  Mica Grujicic,et al.  Heat Transfer and Effective Thermal Conductivity Analyses in Carbon-Based Foams for Use in Thermal Protection Systems , 2005 .

[26]  LU Xi-yun LARGE EDDY SIMULATION OF PARTICLE TRANSPORT IN FULLY DEVELOPED VERTICAL TURBULENT CHANNEL FLOW , 2004 .