Hydraulic-To-Pneumatic Power Supply for Aircraft Fluidic Systems.

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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

Author(s):
Mccarty, R. S. ; Cox, J. T.
Author Organization(s):
AIRESEARCH MFG CO OF ARIZONA PHOENIX
Descriptive Note:
Final rept. 2 Feb 73-25 Jan 74,
Pagination:
0068

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
74-410484
Contract/Grant Number(s):
N00019-73-C-0311
Project Number(s):
AIR-52022
 Subject Terms
Communities of Interest:
Air Platforms
Descriptor(s):
*AIRCRAFT, *FLUIDICS, *POWER SUPPLIES, FLUIDIC AMPLIFIERS, HYDRAULIC EQUIPMENT, HYDRAULIC FLUIDS, PNEUMATIC EQUIPMENT, BISTABLE DEVICES, EXPERIMENTAL DESIGN
Field(s)/Group(s):
Aircraft, Fluidics and Fluerics
Keyword(s):
*Hydrofluidic devices
Report Date:
1974 Feb 01