SAE ARP 4404C-2013 Aircraft Electrical Installations《飞机电气设备》.pdf
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1、_SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising theref
2、rom, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions.Copyright 2013 SAE International All rights reserved. No part of this pub
3、lication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-4970
4、(outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/ARP4404CAEROSPACERECOMMENDED PRACTICEARP4404 REV. CIssued 1992-03 Revised 2013-11 Su
5、perseding ARP4404B Aircraft Electrical Installations RATIONALEImprove conductor voltage drop values by including an estimated conductor temperature formula to 9.3.4.2.FOREWORDThe acceptability of the electric wiring system for a transport aircraft depends to a large degree on the consideration, in t
6、he preliminary design stages, given to such factors as electrical load analysis, generating equipment characteristics, location of centers of load distribution, and general wire routing. Good detail electrical design, including proper equipment and wire selection and installation, coupled with the p
7、roper evaluation of the reliability of circuitry to be used, are necessary steps in assuring a good system. In general, the material in this document applies specifically to 28 V DC and 115/200 V AC electric systems. It is recognized that detail design considerations must vary with each type of airc
8、raft. With the development of improved techniques, there will be differences within given types. Therefore, this document has been prepared on the basis of a general guide, and no attempt has been made to cover exact details of installation. It is believed that this method of presentation will allow
9、 the designers maximum opportunity to exercise their best judgment and ingenuity to make the system in their aircraft as simple, safe, and reliable as possible. The various phases of transport aircraft electrical design, as related to reliability of operation and reduction of hazards, are set forth
10、on the following pages. These factors should be considered throughout the design stages from preliminary design to the completed aircraft. It is felt that the application of the principles in this guide will provide a safe and satisfactory electric system installation for transport type aircraft. SA
11、E INTERNATIONAL ARP4404C Page 2 of 111 TABLE OF CONTENTS 1. SCOPE 92. APPLICABLE DOCUMENTS 92.1 SAE Publications . 92.2 Military Publications 102.3 Other Documents 113. CIRCUIT PROTECTION . 123.1 Definitions, Principles, and General Recommendations 123.1.1 Circuit Protectors. 123.1.2 Scope of Protec
12、tion . 123.1.3 Equipment Protection 123.1.4 Dual Protection 123.2 Circuit Breakers. 133.2.1 Definitions, Principles, and General Recommendations 133.2.2 Interrupting Capacity of Circuit Breakers 143.2.3 Trip-Free Circuit Breakers . 143.2.4 Non-Trip-Free Circuit Breakers . 153.2.5 Automatic Reset Cir
13、cuit Breakers . 153.2.6 Remote Circuit Breakers . 153.2.7 Magnetic Circuit Breakers. 163.2.8 High Voltage Applications of Circuit Breakers 163.2.9 Multiple-Pole Circuit Breakers . 163.3 Fuses 173.3.1 Definitions, Principles, and General Recommendations 173.3.2 Application of Fuses 183.3.3 Fuse Speci
14、fications and Designations 183.3.4 Fuse Types . 183.3.5 Fuse Materials . 183.3.6 Connections for Fuses 193.3.7 Fuse Time-Current Characteristics . 193.4 Limiters 193.4.1 Definitions, Principles, and General Recommendations 193.4.2 Types of Limiters . 213.4.3 Limiter Time-Current Characteristics 223.
15、5 Aircraft Wire and Circuit Protector Coordination . 223.6 Power System Protection 243.6.1 Definitions, Principles, and General Recommendations 243.6.2 Generation System Protection 273.6.3 Conversion System Protection 283.6.4 Distribution System Protection 293.6.5 Utilization System Protection 303.6
16、.6 External Power Circuit Protection . 304. FAIL-SAFE FEATURES IN ELECTRIC CIRCUITS 304.1 General Probability Consideration for Failure Analysis 304.1.1 Wiring Failures 304.1.2 Equipment Failures . 304.1.3 Design Considerations 314.2 Definitions, Principles, and General Recommendations 314.2.1 Defin
17、ition . 324.2.2 Circuit Analysis 324.3 Fire Detection Circuits . 324.3.1 Integrity of Fire Detector Circuits 324.3.2 Selection of Components for Fire Detector Circuits . 324.3.3 Shorted or Open Wire Effects on Fire Detector Circuits . 324.3.4 Coordination and Interconnection of Fire Detector Circuit
18、s 32SAE INTERNATIONAL ARP4404C Page 3 of 111 4.4 Propeller Circuits . 334.4.1 Interconnection of Propeller Control Circuits 334.4.2 Failure of Propeller Control Circuits 334.5 Thermal Anti-Icing and Deicing Circuits 334.5.1 Overheat Control in Thermal Anti-Icing and Deicing Circuits . 334.5.2 Symmet
19、rical Anti-Icing and Deicing Control . 334.6 Fire Extinguishing Control Circuits 334.6.1 Selection and Protection of Fire Extinguishing Control Components. 334.6.2 Circuit Connection for Fire Extinguishing Control Components . 334.7 Fluid Shutoff Valve Circuits . 344.7.1 Selection of Fluid Shutoff V
20、alves 344.7.2 Engine Oil Valve Control . 344.8 Other Circuits 344.8.1 Circuits Recommended for Fail-Safe Consideration 345. CIRCUITS FOR ESSENTIAL EQUIPMENT . 355.1 Definitions and General Principles 355.1.1 Essential Circuits. 355.1.2 Emergency Circuits . 355.2 Dual Power Sources . 355.2.1 Selectio
21、n of Alternate Power Supplies 355.2.2 Types of Self-Contained Emergency Power Supplies 355.2.3 Use of Main Engines . 365.3 Electrical Isolation . 365.3.1 Individual Circuit Protection for Essential Circuits 365.3.2 Emergency Circuit Power Sources . 365.4 Types of Circuit Protection 365.4.1 Protectio
22、n for Essential Circuits 365.5 Sequence Operation . 365.5.1 Sequence Operation of Relays and Switches 365.6 Special Consideration in Wire Routing . 365.6.1 Wire Routing . 365.7 Special Considerations in Fire Areas 375.7.1 Fire Wall and Fire Seal Connections 375.7.2 Fire Detector Circuits 375.7.3 Fai
23、rleads on Fire Walls . 375.7.4 Dielectric Materials 375.7.5 Electric Equipment 375.8 Flight Instruments 375.8.1 Multipower Sources for Flight Instruments . 376. MULTI-ENGINE RELIABILITY 386.1 General Principles and Recommendations 386.2 Power Source (Generators) 386.2.1 Low Engine Revolutions Per Mi
24、nute Operation of Generators . 386.2.2 Capacity of Generators . 386.3 Separate Routing of Wiring . 386.3.1 Instrument Wire Routing . 386.3.2 Generator Feeder and Control Wiring 387. CONNECTORS AND OTHER TERMINATIONS 397.1 General Recommendation 397.2 Studs and Insulators . 397.2.1 Current Carrying S
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