Reduction of Hydraulic System Pressure Spikes Through Limiting of Servovalve Current Change Rate 985561
Fast closing of actuator servovalves in airplane hydraulic systems can often cause unacceptably high pressure spikes in these systems. This paper describes and discusses a method of reducing these hydraulic system pressure spikes by suitable limiting of the rate at which the servovalve current can change. Analytical and test results are presented to show that with this method, the pressure spikes can be reduced without significantly affecting the actuator dynamic response characteristics.
Citation: Trikha, A., "Reduction of Hydraulic System Pressure Spikes Through Limiting of Servovalve Current Change Rate," SAE Technical Paper 985561, 1998, https://doi.org/10.4271/985561. Download Citation
Author(s):
Arun K. Trikha
Pages: 8
Event:
World Aviation Congress & Exposition
ISSN:
0148-7191
e-ISSN:
2688-3627
Also in:
SAE 1998 Transactions - Journal of Aerospace-V107-1
Related Topics:
Hydraulic systems
Pressure
Sensors and actuators
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