Flight Control Actuator System Development.

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Abstract:

This report describes the following research tasks The test and evaluation of a quadruplex redundant Pitch Axis Test Rig PATR to fully describe the hydraulic, mechanical and electronic technology contained therein and the design of a Roll Axis Test Rig RATR to permit hardware simulation of quad redundant, force sharing, active standby, median select and split surface flight control system mechanizations that have high dynamic response.

Author(s):
Bazill, Dale G. ; Schreadley, Harry S. ; Earley, B. H.
Author Organization(s):
LEAR SIEGLER INC OKLAHOMA CITY OKLA MANAGEMENT SERVICES DIV
Descriptive Note:
Final rept. 24 Nov 72-18 Dec 73,
Pagination:
0226

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
AFFDL-TR-74-82
Contract/Grant Number(s):
F33615-73-C-3024
Task Number(s):
822510
Project Number(s):
AF-8225
Monitor Series:
TR-74-82
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*FLIGHT CONTROL SYSTEMS, *JET FIGHTERS, *ACTUATORS, ELECTRONIC EQUIPMENT, SERVOMECHANISMS, ELECTRICAL EQUIPMENT, TEST FIXTURES, HYDRAULIC ACTUATORS
Field(s)/Group(s):
Attack and Fighter Aircraft, Test Facilities, Equipment and Methods
Keyword(s):
F 4 aircraft
Report Date:
1974 Aug 01