Hydraulic generation system on helicopter generally consists of flight control hydraulic actuating circuit, landing gear retraction/extension hydraulic circuit, and wheel brake circuit. This paper studies on a volumetric speed control system applied in helicopter flight control actuating system. The system performance curve, deduced from the modeling, simulation and testing of the tail-actuating system, reveals that this volumetric speed control system meets the requirements of helicopter control system actuating.
The Modeling and Simulation of Hydraulic Actuated Control System of Helicopter in Volumetric Speed Control
Applied Mechanics and Materials ; 779 ; 169-174
2015-07-30
6 pages
Article (Journal)
Electronic Resource
English
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