SAE AIR4982A
Current
The latest, up-to-date edition.
Aerospace Fly-by-Light Actuation Systems
Hardcopy , PDF
English
18-12-2014
1. SCOPE
2. REFERENCES
3. BACKGROUND
4. OPTIC ACTUATION INTERFACES
This SAE Aerospace Information Report (AIR) has been prepared to provide information regarding options for optical control of fluid power actuation devices.
DocumentType |
Standard
|
Pages |
20
|
ProductNote |
This standard is now stabilized
|
PublisherName |
SAE International
|
Status |
Current
|
Supersedes |
This SAE Aerospace Information Report (AIR) has been prepared to provide information regarding options for optical control of fluid power actuation devices. It is not intended to establish standards for optical fluid power control, but rather is intended to provide a baseline or foundation from which standards can be developed. It presents and discusses approaches for command and communication with the actuation device via electro-optic means.The development of standards will require industry wide participation and cooperation to ensure interface commonality, reliability, and early reduction to practice. To facilitate such participation, this document provides potential users of the technology a balanced consensus on its present state of development, the prospects for demonstration of production readiness, and a discussion of problem areas within this technology. The intent is to inform the user/designer of the options available for interfacing photonics (optics) to hydraulic power control actuators used in aerospace applications. Specifically, power and signal interfaces such as control, status and BIT (built in test) are considered. Mechanical interfaces such as optical connectors and fibers are also discussed. Other issues covered include the benefits of optics, reliability of components, and system architectures.The document draws on the expertise of numerous investigators who develop demonstration hardware, are familiar with photonics and specialize in hydraulic actuation, or are cognizant of aerospace fluid control systems. Contributions and suggestions have been supplied by members and attendees of the A-6D Committee.
SAE AIR 6258 : 2015 | FIBER OPTIC SENSORS FOR AEROSPACE APPLICATIONS |
SAE ARP 1281 : 2002 | ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
ARINC 629 : 90 SUPP 5 | MULTI TRANSMITTER DATA BUS - TECHNICAL DESCRIPTION |
ANSI Z136.2 : 2012 | SAFE USE OF OPTICAL FIBER COMMUNICATION SYSTEMS UTILIZING LASER DIODE AND LED SOURCES |
MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
SAE AS 1773 : 1995 | FIBER OPTICS MECHANIZATION OF A DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS |
MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
MIL-STD-1773 Base Document:1988 | FIBER OPTICS MECHANIZATION OF AN AIRCRAFT INTERNAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS |
SAE ARD 50024 : A2003 | FIBER OPTIC COUPLED SENSORS FOR AEROSPACE APPLICATIONS |
SAE ARD 50020 : A2003 | FIBER-OPTIC INTERCONNECTION HARDWARE FOR AEROSPACE APPLICATIONS |
SAE ARP4386C | Terminology and Definitions for Aerospace Fluid Power, Actuation and Control Technologies |
ARINC 429 : 2001 | ELECTRONIC DISKETTE COPY OF DATA LABELS IN MICROSOFT WORD AND EXCEL FORMATS |
SAE ARP490F | Electrohydraulic Servovalves |
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