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SAE ARP5584

Current

Current

The latest, up-to-date edition.

Document for Electric Power Management

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

16-05-2011

€134.60
Excluding VAT

1 SCOPE
2 REFERENCES
3 SYSTEM ARCHITECTURE CONSIDERATIONS
  3.1 Types of Power
       3.1.1 AC Considerations
       3.1.2 Low and High Voltage DC Considerations
       3.1.3 Capacity Requirements
       3.1.4 Types of Loads
       3.1.5 Load Shedding
       3.1.6 Distribution Architecture
  3.2 Redundancy
       3.2.1 Survivability
       3.2.2 Reconfiguration
  3.3 Reliability
  3.4 Control and Decision Making
       3.4.1 Autonomous Control
       3.4.2 Central Control
       3.4.3 Local (Distributed Control)
       3.4.4 Hard-Wired Discrete Versus Multiplex Bus
       3.4.5 Multiplex Power Management System
       3.4.6 Human Control Interface
       3.4.7 Vehicle Management System Integration
  3.5 Fault Detection and Isolation
       3.5.1 Maintainer Interface
  3.6 Multifunction Controls
  3.7 Thermal Management/Efficiency
  3.8 Fault Isolation
  3.9 Fault Trip Coordination
  3.10 Electromagnetic Compatibility/Lightning
  3.11 Bonding and Grounding
       3.11.1 Isolation
4 POWER SWITCHING APPLICATION CONSIDERATIONS
  4.1 Wire and Equipment Protection
  4.2 Circuit/Load Considerations
       4.2.1 Voltage Drop
       4.2.2 Leakage Current
       4.2.3 Dead-Facing Requirements
       4.2.4 Reverse Current
  4.3 Efficiency and Power Dissipation
       4.3.1 Nominal and Peak Power Requirements
       4.3.2 Thermal Management
  4.4 Interface
       4.4.1 Control Interfaces
       4.4.2 Status Interfaces
       4.4.3 Power Interfaces
       4.4.4 Load Interfaces
  4.5 Initialization State and Sequencing
  4.6 Default State
  4.7 Built-In Test (BIT)
       4.7.1 Initialization BIT
       4.7.2 Periodic BIT
       4.7.3 Failure Monitoring
  4.8 Electrical Test Requirements
  4.9 Environmental Test Requirements
  4.10 Fault Current, Rupture Current
       4.10.1 Solid State Power Controllers
       4.10.2 Electromechanical Devices
  4.11 Uninterruptible Power
5 POWER SWITCHING AND PROTECTIVE DEVICES
  5.1 Power Controllers
       5.1.1 Solid State Power Controllers (SSPC)
       5.1.2 Solid State Relays
       5.1.3 Electromechanical Relays and Contactors
       5.1.4 Hybrid Power Controllers
       5.1.5 Remote Controlled Circuit Breakers
       5.1.6 Circuit Breakers
       5.1.7 Electromechanical Power Controller
  5.2 Power Switching and Protective Devices Optional
       Characteristics
       5.2.1 Feedback Signals
       5.2.2 Built-In Test
       5.2.3 Current Limiting
       5.2.4 Off-State Output Voltage Crowbar
6 SOFTWARE AND FIRMWARE CONSIDERATIONS
  6.1 Central Versus Local
  6.2 Fixed Versus Programmable Logic
  6.3 Growth Capacity
  6.4 Programming Languages
7 GLOSSARY OF TERMS

This SAE Aerospace Recommended Practices (ARP) covers the definitions, functions and broad application guidelines of modern aerospace vehicle electric power management systems.

DocumentType
Standard
Pages
26
PublisherName
SAE International
Status
Current
Supersedes

This SAE Aerospace Recommended Practices (ARP) covers the definitions, functions and broad application guidelines of modern aerospace vehicle electric power management systems. As aerospace control systems have become more sophisticated and autonomous, the electric power subsystem no longer is just a generation and distribution bus control system. New electric power systems include integration of individual load logic control, protection, generation, distribution, and load management. This system can report to a higher level control system, typically a vehicle management system, or can be an autonomous system within itself reporting and responding to operator commands.

ISO 1540:2006 Aerospace — Characteristics of aircraft electrical systems
SAE ARP1199B Selection, Application, and Inspection of Electric Overcurrent Protective Devices
MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
SAE AS1212A Electric Power, Aircraft, Characteristics and Utilization of
ARINC 629 : 90 SUPP 5 MULTI TRANSMITTER DATA BUS - TECHNICAL DESCRIPTION
SAE AS15531A Digital Time Division Command/Response Multiplex Data Bus
SAE AS 1831 : 1997 ELECTRICAL POWER, 270 V DC, AIRCRAFT, CHARACTERISTICS AND UTILIZATION OF
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
ARINC 429 : 2001 ELECTRONIC DISKETTE COPY OF DATA LABELS IN MICROSOFT WORD AND EXCEL FORMATS
MIL-STD-1553 Revision B:1978 DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA

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