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26013

HYDRAULIC ACTUATORS STEP RESPONSE CONSIDERING FLUID LINES INERTIAL EFFECTS

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Last updated: 04 Jan 2025

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Abstract

A convenient simple model for a high velocity fluid line, connecting a hydraulic actuator to a 4/3 zero lapped valve, is presented. The conditions under which the proposed model is valid, are deduced. The system mathema-tical model, in case of constant supply pressure operation and pure inertial external load, shows that the actuator response to step opening of the valve depends on two parameters; the system dimensionless inertial resistance and its dimensionless capacitance. The former equals the ratio between the fluid line inertial resistance and that of the load, while the latter accounts for the system capacitance, valve resistance, load inertial resistance, and the supply pressure. Numerical solution of the system governing equations verifies that at small values of the dimensionless capacitance, cavitation occurs at certain values of the dimensionless inertial resistance, a phenomenon that can not be predicted when the fluid line inertial resistance is ignored. At small dimensionless capacitances, the fluid line inertial resistance is shown to have considerable effect on the transient response, and can be made use of to improve the system performance. Ale combination of dimensionless capacitance and inertial resistance, at which minimum settling time and reasonable values of overshoot and delay and rise times occur, is determined.

DOI

10.21608/asat.1987.26013

Authors

First Name

S.

Last Name

KASSEM

MiddleName

A.

Affiliation

Associate Professor, Department of Mechanical Design and Production, Faculty of Engineering, Cairo University, Cairo, Egypt.

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Volume

2

Article Issue

A.S.A.T. CONFERENCE 21-23 April 1987 , CAIRO

Related Issue

4700

Issue Date

1987-04-01

Receive Date

2019-01-27

Publish Date

1987-04-01

Page Start

355

Page End

365

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_26013.html

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https://asat.journals.ekb.eg/service?article_code=26013

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22

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Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

HYDRAULIC ACTUATORS STEP RESPONSE CONSIDERING FLUID LINES INERTIAL EFFECTS

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Article

Created At

22 Jan 2023