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New Developments in Fluidics for Aircraft High-Pressure Hydraulic System Applications
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English
Abstract
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.
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Authors
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.Also In
References
- Kelley L. R. Boothe W. A. “Hydraulic Fluids.” ASME Winter Annual Meeting and Energy Systems Exposition Dec. 1968
- Boeing Control Specification 60B00055
- General Electric Co.'s P4 Fluidic Modules Literature