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SAE ARD 50024 : A2003

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

FIBER OPTIC COUPLED SENSORS FOR AEROSPACE APPLICATIONS

Withdrawn date

15-07-2003

Published date

12-01-2013

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1 SCOPE
2 REFERENCES
   2.1 SAE publications
   2.2 U.S. Government Publications
   2.3 Other Documents
   2.4 Definitions
3 FIBER-OPTIC COUPLED SENSOR CONCEPTS
   3.1 Introductory statements
   3.2 Discussion
   3.3 General considerations
   3.4 Diagnostics, Self-Test, and Fault Monitoring
   3.5 Flight History; Problem Encountered
4 SENSOR TYPES
   4.1 Time Division Encoded Sensors, DIGITAL
   4.2 Time Division Encoded Sensors, ANALOG
   4.3 Wavelength Division Encoded Sensors, DIGITAL
   4.4 Wavelength Division Encoded Sensors, ANALOG
   4.5 Direct Wavelength Encoded Sensors
   4.6 Frequency Output Sensors
   4.7 Magneto-Optic Sensors
   4.8 Self Luminous Sensors
   4.9 Hybrid Sensors
   4.10 Time rate of decay sensors
   4.11 Interferometric Fiber Optic Sensing
5 CONCLUSIONS
   5.1 Summary of Identified Needs
6 RECOMMENDATIONS
7 KEY WORDS
APPENDIX A PRINCIPAL CONTRIBUTIONS
APPENDIX B BIBLIOGRAPHY
FIGURES
TABLES

Includes concepts for all general purpose fiber optic coupled sensing schemes that are applicable to the aerospace industry: a) to define certain terms related to sensors; b) to consider interconnection related aspects of these sensor schemes; c) to consider diagnostics and self-test; d) to provide a compendium of problem areas; e) to discuss possible resolution of problem areas; and f) to provide a brief bibliography of salient technical references.

Committee
AS-3
DocumentType
Standard
PublisherName
SAE International
Status
Withdrawn

SAE AIR 4982 : 2014 AEROSPACE FLY-BY-LIGHT ACTUATION SYSTEMS
SAE AIR 4922A : 2015 PRIMARY FLIGHT CONTROL HYDRAULIC ACTUATION SYSTEM INTERFACE DEFINITION

SAE ARP 4258 : 1990 APPLICATION OF LOW SPEED AVIONIC SYSTEM DISCRETE SIGNAL INTERFACES
MIL C 83723 : E CONNECTORS, ELECTRICAL (CIRCULAR, ENVIRONMENT RESISTING) RECEPTACLES AND PLUGS GENERAL SPECIFICATION FOR
MIL-HDBK-217 Revision F:1991 RELIABILITY PREDICTION OF ELECTRONIC EQUIPMENT
MIL-STD-1773 Base Document:1988 FIBER OPTICS MECHANIZATION OF AN AIRCRAFT INTERNAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS
SAE AIR 4508 : 1992 MIL-STD-1773 USERS HANDBOOK
SAE ARD 50020 : A2003 FIBER-OPTIC INTERCONNECTION HARDWARE FOR AEROSPACE APPLICATIONS

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