New Developments in Fluidics for Aircraft High-Pressure Hydraulic System Applications 700784
The new technology of hydraulic fluidics has been applied to the control of aircraft hydraulic systems in three areas: hydraulic circuit damage isolation, control column artificial feel computation, and the sequencing of landing gear motion. Successful development is demonstrated, and hydraulic fluidics are shown to produce considerable improvements to hardware in specific instances.
Citation: Smith, D. and Church, R., "New Developments in Fluidics for Aircraft High-Pressure Hydraulic System Applications," SAE Technical Paper 700784, 1970, https://doi.org/10.4271/700784. Download Citation
Author(s):
David H. Smith, Royce F. Church
Affiliated:
Commercial Airplane Div., The Boeing Co.
Pages: 12
Event:
National Aeronautic and Space Engineering and Manufacturing Meeting
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Hydraulic systems
Hardware
Aircraft
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