DocumentCode :
1828027
Title :
Modal analysis of two typical fluid-filled pipes in aircraft
Author :
Li, Xin ; Wang, Shaoping ; Liang, Ran
Author_Institution :
Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
fYear :
2011
fDate :
17-20 Aug. 2011
Firstpage :
462
Lastpage :
466
Abstract :
The vibration of hydraulic pipe poses a severe safety concern in aircraft. Aiming at this problem, the two typical pipelines (straight pipe and curved pipe) were analyzed using the Finite Element Method (FEM) in ADINA software. Compared with the experiment, the results from ADINA simulation are close to the experiment data. Based on the simulation results, we concluded that adjusting the clamped-end length or consolidating the pipe are effective ways to change the natural frequencies of fluid-filled pipe and prevent the drastic vibration of the pipeline system in aircraft when the natural frequencies of the fluid-filled pipe fall into the frequency range of vibration source.
Keywords :
aircraft; finite element analysis; hydraulic systems; modal analysis; pipelines; vibrations; ADINA software; FEM; aircraft safety; curved pipelines; finite element method; fluid-filled pipes; hydraulic pipes; modal analysis; natural frequencies; straight pipelines; vibration; Finite element methods; Fluids; Modal analysis; Pumps; Resonant frequency; Shape; Vibrations; finite element method; fluid-filled pipe; modal analysis; pipe vibration;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Fluid Power and Mechatronics (FPM), 2011 International Conference on
Conference_Location :
Beijing
Print_ISBN :
978-1-4244-8451-5
Type :
conf
DOI :
10.1109/FPM.2011.6045809
Filename :
6045809
Link To Document :
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