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Design of a Hydraulic Actuator for Active Control of Rotating Machinery PUBLIC ACCESS

[+] Author Affiliations
Majid Rashidi

Cleveland State University

Eliseo Dirusso

NASA Lewis Research Center

Paper No. 91-GT-246, pp. V005T14A038; 8 pages
doi:10.1115/91-GT-246
From:
  • ASME 1991 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award; General
  • Orlando, Florida, USA, June 3–6, 1991
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7902-3
  • Copyright © 1991 by ASME

abstract

A Hydraulic actuator was designed and is described herein. This actuator consists of: a pump which generates the nominal pressure, a hydraulic servo-valve, and a thin elastic plate which transduces the generated pressure variations into forces acting on a mass which simulates the bearing of a rotor system. An actuator characteristic number is defined to provide a base for an optimum design of force actuators with combined weight, frequency, and force considerations. This characteristic number may also be used to compare hydraulic and electromagnetic force actuators. In tests this actuator generated 182.3 Newton force at a frequency of 100. Hz. and a displacement amplitude of 5.8×10−5 meter.

Copyright © 1991 by ASME
Topics: Machinery , Actuators , Design
This article is only available in the PDF format.

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