Hydraulic-To-Pneumatic Power Supply for Aircraft Fluidic Systems.
Abstract
The program activities encompassed analysis, development, design, fabrication, and test of a hydraulic-to-pneumatic power supply suitable for use in supplying the total power required for any of a number of different aircraft fluidic systems. The unit uses a hydrofluidic oscillator to drive a double-ended reciprocating bellows compressor. The input is Type MIL-H-5606 hydraulic fluid at a supply pressure of 3,000 psi. The pneumatic output is at a discharge pressure of 30 psia with a flow of 0.25 lb per minute. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 01, 1974
- Accession Number
- AD0778764
Entities
People
- J. T. Cox
- R. S. Mccarty