PREN 2282 : 200P1
Withdrawn
AEROSPACE SERIES - CHARACTERISTICS OF AIRCRAFT ELECTRICAL SUPPLIES
Hardcopy , PDF
English
07-23-2013
0 Introduction
1 Scope
2 Normative references
3 Definitions
4 Requirements common to all electrical power systems
4.1 General requirements for electrical power generation
4.2 General requirements for utilization equipment
5 A.C. power system
5.1 General
5.2 Supply characteristics for category A (CF) system
5.3 Supply characteristics for category A (NF) system
5.4 Supply characteristics for category A (WF) system
5.5 Requirements relating to utilization equipment
6 D.C. power system 28 V
6.1 General
6.2 Supply characteristics for 28 V systems
6.3 Requirements relating to utilization equipment
Specifies the characteristics of electrical power supplied to the terminals of equipment installed in the aircraft. Also defines the supply system and compatibility requirements for equipment together with the special systems with constant and variable frequency. Applicable to a.c. and d.c. on-board or ground systems.
| Committee |
C2
|
| DocumentType |
Draft
|
| Pages |
24
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Withdrawn
|
| PREN 3372-001 : 200P1 | AEROSPACE SERIES - CONNECTORS, ELECTRICAL, CIRCULAR, MEDIUM AND HIGH CONTACT DENSITY, SCOOP-PROOF WITH BAYONET COUPLING, OPERATING TEMPERATURES -65 DEGREES C TO 175 DEGREES C OR 200 DEGREES C CONTINUOUS - PART 001: TECHNICAL SPECIFICATION |
| 09/30212621 DC : 0 | BS EN 3682-001 - AEROSPACE SERIES - CONNECTORS, PLUG AND RECEPTACLE, ELECTRICAL, RECTANGULAR, INTERCHANGEABLE INSERT TYPE, RACK TO PANEL, OPERATING TEMPERATURE 150 DEGREE C CONTINUOUS - PART 001: TECHNICAL SPECIFICATION |
| EN 2592:1990 | Aerospace series - Three-pole circuit breakers temperature compensated rated currents up to 25 A - Product standard |
| EN 2495:1990 | Aerospace series - Single-pole circuit breakers temperature compensated rated currents up to 25 A - Product standard |
| STANAG 3456 : 0 | AIRCRAFT ELECTRICAL POWER SYSTEM CHARACTERISTICS |
| ISO 1540:2006 | Aerospace — Characteristics of aircraft electrical systems |
| PREN 3830 : 200P1 | AEROSPACE SERIES - ELECTRICAL SYSTEM - LOAD ANALYSIS |
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