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AIR5271
A Guideline for Application of High-Density Fiber Optic Interconnects to Aerospace Platforms
A Guideline for Application of High-Density Fiber Optic Interconnects to Aerospace Platforms
0001-01-01
有效
【范围】 This SAE Aerospace Information Report (AIR5271) covers the basic attributes of a second-generation robust, reliable high-density fiber optic interconnect system for aerospace applications. The intent is to take advantage of recent commercial developments in materials, components and manufacturing methods to develop rugged high-density fiber optic interconnects optimized for aerospace and automotive applications, which can accommodate a variety of optical fiber waveguide types. These waveguide types include single mode and multi-mode glass/glass fibers and waveguides, plastic clad silica fibers and waveguides, and all polymer fibers and waveguides. This second generation interconnect system should represent a dramatic improvement over first generation. The cable should be extremely robust eliminating any concerns over cable damage or fiber breakage in an aerospace environment. A high-density fiber optic interconnect system provides the physical medium for optical data and control communication in aerospace vehicles. As such, it consists of the cables and harnesses, connectors, splices, backplane interfaces, transceivers, fiber optic couplers, and includes test and maintenance concepts for these items. Also included are manufacturing, installation and repair tools, processes and training programs. The high-density format should provide for both redundant serial data transmission or parallel data transfer by providing a scaleable fiber count. Connectors should provide an extremely small footprint, with low mass connector shells and array inserts, and accommodate both single and multi-mode fibers. Fiber spacing and cladding diameter should be standardized and coatings utilized to guarantee long term reliability. The cable connector interface shall be optimized to preclude damage during installation and/or maintenance actions as well as ease of termination. All elements of the cable plant should be compatible including splices and couplers with minimum weight, volume and footprint. This optimized cable plant shall serve as an integrated information distribution system capable of transferring all information on military and commercial aircraft with dramatic improvements in affordability, reliability, fault tolerance, EMI/EMP immunity and safety. Utilization of this cable plant will improve aircraft performance and fuel economy, providing operational cost effectiveness while reducing new aircraft certification costs.strRefField
【与前一版的变化】

引用文件/被引文件

Fiber Optic Test Methods and Instrumentation
Connector
Connector
Electrical Equipment
Microcircuits
Test Methods for Electrical Connectors
Test methods for Electrical and Electronic Component Parts
Aircraft/Stores Electrical Interconnection System
General Specification for Single Terminus Fiber optic Connectors
General Specification for Fiber Optic Cable-Shipboard
General Specification for Optical Fiber
General Specification for Removable Fiber Optic Termini
Requirements for the Control of Electro-magnetic Interference Emissions and Susceptibility
Measurement of Electro-magnetic Interference Characteristics
Wiring
Fiber Optics Mechanization of an Aircraft Linear Time Division Command/Response Multiplexed Data Bus
Guidelines for Testing of Aerospace Fiber Optic Inter-Connection Systems
Air Transport Equipment Cases and Racking
Air Transport Avionics Equipment Interfaces
Cabin Equipment Interfaces (CEI) Part 6 Fiber Optic Cable Assembly General Specification
Multi-Transmitter Data Bus
Multi-Transmitter Data Bus
Onboard Local Area Network (OLAN)
Backplane Data Bus
Generic Requirements for Single-Mode Optical Fiber Connectors
General Specification for Single Terminus Fiber Optic Connectors
Environmental Conditions and Test Procedures for Airborne Equipment
Fiber Optic Test procedures (FOTPs)
Optical Fiber System Test Procedures (OFSTPs)
Fiber Optic Connector Inter-mateability Standards (FOCIS)
General Requirements for WDM Backbone Networks

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包含图表

Cross Section of a F
Typical Attenuation
Typical Attenuation
Optical Properties o
Most Dominant Radiat
Cross Section of an
Cross Section Of An
A Non-Encapsulated R
An Encapsulated Fibe
An Armored Circular
A Commercial Stacked
Cross Section Of A S
A Photomicrograph of
A Silicon V-Groove C
A Molded MT Array Fe
A Molded Connector (
Ribbon Preparation P
Ribbon Preparation P
Ribbon Preparation P
Ribbon Preparation P
Ribbon Preparation P
Ribbon Preparation P
Ferrule Termination
Ferrule Termination
Ferrule Termination
Ferrule Termination
Ferrule Termination
Ferrule Termination
Computerized Connect
A High Density Conne
Cross Sectional View
Top View of a Planar
Isometric View of a
A Photomicrograph of
A Molded V-Groove Co
A Silicon Integrated
A Packaged Transceiv
An Optical Backplane
The Optical Backplan
Butt Coupled Optical
MT Optical Connector
MT Connector Transmi
An Optical/Electrica
An Optical Backplane
Housing for the MT C
Expanded Beam Optica
A Generation I Lens
An Embedded Optical
Optical Backplane Me
Edge Emitting Laser3
Cross Section of Imp
Temperature Dependen
Schematic Of Double-
A Single Quantum Wel
A Multiple Quantum W
Schematic of a Lithi
Transfer Function of
Schematic of a Quant
Packaged Lithium Nio
Lap Sheath Tube Cabl
Isometric View of MF
Isometric View of th
Provides Isometric V
Cross-Sectional View
Exploded Isometric V
Top View of the Opti
A Handtool for Batch
Common Network Topol
SCM/WDM LAN Example
A Proposed SCM/WDM B
SCM LAN Example
Proposed SCM/WDM Lan
Optical Interconnect
Optical Interconnect
Elements in a Rack-t
Optical Link Using T

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