Fluidics - Feasibility Study Electro/Hydraulic/Fluidic Direct Drive Servo Valve.

reportActive / Technical Report | Accession Number: ADA069798 | Open PDF

Abstract:

The feasibility of providing a fluidic back-up control for the Navys Advanced flight control actuation system AFCAS was investigated and potential design concepts were evaluated. A prelim. spec. for an electrohydraulicfluidic direct drive servo valve was proposed. Technical data and supplier hardware was reviewed. A design concept for an electrohydraulicfluidic servo control valve was selected and a prelim. design drawing was prepared. The study confirms the feasibility of providing a fluidic back-up for the AFCAS direct drive servo valve. Author

Author(s):
Biafore, Louis P. ; Holland, Bernie
Author Organization(s):
ROCKWELL INTERNATIONAL COLUMBUS OHIO COLUMBUS AIRCRAFT DIV
Descriptive Note:
Final rept. 11 Apr-29 Dec 78,
Pagination:
0071

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
NR78H-126, NADC-78033-60
Contract/Grant Number(s):
N62269-78-C-0176
Task Number(s):
WF41400000
Project Number(s):
F41400
Monitor Series:
78033-60
 Subject Terms
Joint Capability Areas:
JCA_5_Command and Control; JCA_1.2.6_Concepts; JCA_5.3_Planning; JCA_5.3.3_Develop Strategy; JCA_5.3.4_Develop Courses of Action; JCA_5.3.5_Analyze Courses of Action; JCA_5.6.3_Assess Achievement of Objectives; JCA_5.6_Monitor; JCA_1.2.5_Lessons Learned; JCA_5.5.2_Task; JCA_5.5_Direct
Modernization Areas:
Quantum Science and Computing
Communities of Interest:
Weapons Technologies
Descriptor(s):
*FLIGHT CONTROL SYSTEMS, *HYDRAULIC SERVOMECHANISMS, *HYDRAULIC VALVES, *SERVOVALVES, EXPERIMENTAL DESIGN, ACTUATORS, DRIVES(ELECTRONICS), BACKUP SYSTEMS, FLUIDIC CONTROL, MECHANICAL DRAWING, ELECTROHYDRAULIC VALVES
Field(s)/Group(s):
Aircraft, Fluidics and Fluerics, Pumps, Filters, Pipes, Tubing, Fittings and Valves
Keyword(s):
PE62241N, WUZA606
Report Date:
1979 Mar 01