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198252

Modelling and transient response study of hydraulic servo actuator

Article

Last updated: 24 Dec 2024

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Abstract

This paper presents a mathematical model of electro hydraulic servo system (EHS) using two-stage electrohydraulic servovalve (EHSV), by the aim of Matlab-simulink-simscape multibody to predict the flow characteristics (pressure/flow rate) with changing the parametric configuration of (EHSV), these parameters could be used to estimate the error at different operating conditions. It includes establishing mathematical model, controller model and validating the performance of the (EHSV) by experimental result of published work using the data of servovalve labelled B.31.210.12.1000.U2V (mechanical feedback) manufactured by PPT – Trstenik. The effect of changing servovalve orifice diameter (0.25, 0.30, and 0.35) mm, show that increasing the orifice diameter of the servovalve leads to increase the transient time but decrease the system overshoot. The pressure behaviour is plotted and shows that increasing the
orifice diameter leads to increasing the pressure inside the system as to reach the relieve pressure.

DOI

10.1088/1757-899X/1172/1/012037

Authors

First Name

E

Last Name

Ibrahim

MiddleName

E

Affiliation

Department of Mechanical Power & Energy, Military technical college, Cairo, Egypt.

Email

ezzbos@gmail.com

City

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First Name

T

Last Name

Elnady

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Affiliation

Department of Mechanical Power & Energy, Military technical college, Cairo, Egypt.

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City

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Orcid

-

First Name

I

Last Name

Saleh

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Affiliation

Department of Mechanical Power & Energy, Military technical college, Cairo, Egypt.

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Orcid

-

First Name

S

Last Name

Hassan

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-

Affiliation

Department of Mechanical Power & Energy, Military technical college, Cairo, Egypt.

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-

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-

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-

Volume

19

Article Issue

19

Related Issue

27988

Issue Date

2021-04-01

Receive Date

2021-10-05

Publish Date

2021-04-01

Page Start

1

Page End

9

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_198252.html

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https://asat.journals.ekb.eg/service?article_code=198252

Order

39

Type

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

Modelling and transient response study of hydraulic servo actuator

Details

Type

Article

Created At

22 Jan 2023