DocumentCode
3049349
Title
Thermodynamic characteristics analysis of a high temperature fuel flow-rate control valve
Author
Song, Kai ; Li, Songjing
Author_Institution
Fluid Control & Autom. Dept., Harbin Inst. of Technol., Harbin, China
fYear
2010
fDate
8-10 June 2010
Firstpage
1333
Lastpage
1338
Abstract
High temperature flow-rate control valve is a key component to control the flow rate of fuel supply for aerospace engines. A high temperature fuel flow-rate control valve, pilot-controlled by a high pressure pneumatic system, is developed in this paper. The construction and working principle of the valve are introduced. The thermodynamic mathematical models of the valve are built and the thermodynamic characteristics are simulated by using the 3D finite element analysis method under the condition that the material of the valve elements is a high temperature alloy. Then both of the steady-state and transient temperature field distribution inside the spool and valve body are studied. Also the thermal stress and thermal strain of the valve are calculated.
Keywords
aerospace engines; finite element analysis; flow control; fuel systems; pneumatic systems; pressure control; temperature control; temperature distribution; thermal stresses; thermodynamics; valves; 3D finite element analysis; aerospace engine; fuel supply; high pressure pneumatic system; high temperature alloy; high temperature fuel flow-rate control valve; pilot-control; spool; steady-state temperature field distribution; thermal strain; thermal stress; thermodynamic characteristics analysis; thermodynamic mathematical model; transient temperature field distribution; valve body; Finite element methods; Heat transfer; Heating; Strain; Stress; Thermal stresses; Valves; finite element analysis; flow-rate control valve; high temperature fuel; thermal strain;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location
Harbin
Print_ISBN
978-1-4244-6043-4
Electronic_ISBN
978-1-4244-7505-6
Type
conf
DOI
10.1109/ISSCAA.2010.5633602
Filename
5633602
Link To Document