1、 AEROSPACE STANDARD ARC FAULT CIRCUIT BREAKER - AIRCRAFT, TRIP FREE, 1-20 AMP, TYPE I AS5692/2Copyright 2014 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photoco
2、pying, 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 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org ISSUED 2007-01REAFFIRMED 2014-09THIR
3、D ANGLE PROJECTION CUSTODIAN: AE-8/AE-8B1 FEDERAL SUPPLY CLASS 5925 AS5692/2 SHEET 1 OF 4 PROCUREMENT SPECIFICATION: AS5692SAE Technical Standards Board Rules provide that: “This report ispublishedby SAE toadvance thestate of technicalandengineeringsciences.The useofthis reportisentirelyvoluntary, a
4、ndits applicability and suitability forany particular use,including any patent infringement arising therefrom, isthe soleresponsibilityofthe user.”SAE reviews eachtechnicalreport at least every five years at which time itmay berevised,reaffirmed, stabilized, orcancelled. SAE invites yourwrittencomme
5、nts andsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/PRODCODE RATIONALE AS5692/2 HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY. THE REQUIREMENTS FOR PROCURING THE PRODUCT DESCRIBED HEREIN SHALL
6、 CONSIST OF THIS SPECIFICATION SHEET AND THE LATEST ISSUE OF: SAE AS5692. FIGURE 1 REF. LINE A REPRESENTS THE LOCATION OF THE INTERFACE BETWEEN THE AFCB AND THE PANEL. DIMENSIONS REFERENCED FROM “REF. LINE A” ARE THE DIMENSION FROM THE BACK OF THE PANEL TO THE DIMENSIONED FEATURE. AEROSPACE STANDARD
7、 AS5692/2 SHEET 2 OF 4 ARC FAULT CIRCUIT BREAKER - AIRCRAFT, TRIP FREE, 1-20 AMP, TYPE I TABLE 1 - ELECTRICAL AND MECHANICAL CHACTERISTICS ENDURANCE CYCLES OPERATING FORCE MAX (LB) RESISTIVE INDUCTIVE DASH NO. NOMINAL AMPERAGE RATING (A) VOLTAGE DROP MAX (V) WEIGHT MAX (LB) PULLOUT RESET AC AC MECH
8、NO LOAD CYCLES 1 1 1.10 1- 1.5 (1-) 0.80 2 2 0.75 2- 2.5 (2-) 0.70 3 3 0.55 4 4 0.45 5 5 0.35 7- 7.5 (7-) 0.30 10 10 0.28 15 15 0.25 20 20 0.25 .090 .75-5 1.2-8 1/ 5,000 1/ 2,500 10,000 1/ 115/200 VOLT 400 HZ SYSTEM, TESTED AT 120 5 VOLTS 380-420 HZ. TABLE 2 - DETAIL CALIBRATION REQUIREMENTS OVERLOA
9、D TRIP TIME IN SECS AT PERCENT RATED CURRENT 25 C AMBIENT EFFECT ON CALIBRATION AT PERCENT RATED CURRENT +25 C +71 C -55 C NOMINAL AMPERAGE RATING (A) 200% 500% 1000% 115% 138% 90% 138% 115% 165% 1 1- 2 2- 3 4 5 7- 10 15 20 1.5 TO 40 0.15 TO 3.0 0.35 TO 0.80 MUST HOLD - 1 HOURMIN MUST TRIP - 1 HOUR
10、MAX MUST HOLD - 1 HOURMIN MUST TRIP - 1 HOUR MAX MUST HOLD - 1 HOURMIN MUST TRIP - 1 HOUR MAX AMBIENT TOLERANCE 2 C TABLE 3 - INTERRUPTING CAPACITY (AMPERES) REQUIREMENTS TEST DESIGNATION PER AS5692 NOMINAL AMPERAGE RATING (A) A B C 1 3500 3500 1- 2 2- 2800 2800 3 4 5 7- 10 15 2500 2500 20 2000 2000
11、 (a) 1,500 (b) 750 AEROSPACE STANDARD AS5692/2 SHEET 3 OF 4 ARC FAULT CIRCUIT BREAKER - AIRCRAFT, TRIP FREE, 1-20 AMP, TYPE I TABLE 4 - ENVIRONMENTAL PERFORMANCE MAX. OPERATING ALTITUDE 70,000 FEET OPERATING AMBIENT TEMPERATURE RANGE (-)55 C (+)71 C VIBRATION IN ACCORDANCE WITH AS5692 SINE - REQUIRE
12、D HIGH SINE - (OPTIONAL) RANDOM - (OPTIONAL) SHOCK 50 G, MIL-STD-202, METHOD 213, CONDITION A ACCELERATION 10 G REQUIREMENTS: 1. THE TOP SURFACE OF THE AFCB (IN LOCATION SPECIFIED IN DRAWING) SHALL PROVIDE A GROUNDING SURFACE WHICH MUST MEET THE REQUIREMENTS OF DISSIMILAR METALS (MIL-STD-889) WHEN G
13、ROUNDED TO A BARE ALUMINUM PANEL. THE TOP SURFACE AND THE CIRCUMFERENCE AROUND THE BASE OF THE BUSHING SHALL CARRY THE CURRENT TO OPERATE THE OPENING OF THE AFCB. 2. REVERSE INSTALLATION CRITERIA NUMBER 1, PER PARAGRAPH 4.7.26 OF AS5692, SHALL BE MET TO DEMONSTRATE FULL FUNCTIONALITY IN THE CASE OF
14、REVERSE INSTALLATION. 3. AS A RESULT OF A THERMAL OR ARC FAULT TRIP THE WHITE INDICATOR SHALL BE DISPLAYED. 4. THERE SHALL BE NO REQUIREMENTS FOR ARC FAULT FUNCTION COORDINATION. 5. IF AN AFCB INCLUDES SOFTWARE, THE MANUFACTURERS PART NUMBER MARKING SHALL IDENTIFY THE SOFTWARE PART NUMBER AND REVISI
15、ON. 6. THE PART NUMBERS FOR CIRCUIT BREAKERS IN ACCORDANCE WITH THIS SPECIFICATION SHALL CONFORM TO THE EXAMPLE BELOW. AS5692 / 2 D5VLEXTRA LENGTH PUSHBUTTON (OPTION)HIGH VIBRATION CAPABILITY (OPTION)AMPERAGE RATINGRANDOM VIBRATION LEVEL (OPTION)BASIC PART NUMBERWHEN A DESIGNATOR IS NOT APPLICABLE I
16、T SHALL BE OMITTED FROM THE PART NUMBER. QUALIFICATION: QUALIFICATION IS REQUIRED FOR U.S. GOVERNMENT PROCUREMENT. THE QUALIFIED PRODUCT LIST (QPL) QUALIFICATION ACTIVITY FOR U.S. DEPARTMENT OF DEFENSE PROCUREMENT PURPOSES IS THE NAVAL AIR SYSTEMS COMMAND (CODE 4.4.5.3) 22229 ELMER ROAD, BUILDING 23
17、60, PATUXENT RIVER, MD 20670-1900. NOTES: 1. VOLTAGE RATING 115V 400 HZ NOMINAL. 2. DIMENSIONS ARE IN INCHES. UNLESS OTHERWISE SPECIFIED, TOLERANCES: DECIMALS .031. 3. IN THE EVENT OF A CONFLICT BETWEEN THE TEXT OF THIS STANDARD AND THE REFERENCES CITED HEREIN, THE TEXT OF THE STANDARD SHALL TAKE PR
18、ECEDENCE. 4. IN THE TABLES, ALL NUMERICAL AMPERAGE VALUES LISTED AS PERCENTAGES ARE EXPRESSED IN PERCENT OF RATED CURRENT. AEROSPACE STANDARD AS5692/2 SHEET 4 OF 4 ARC FAULT CIRCUIT BREAKER - AIRCRAFT, TRIP FREE, 1-20 AMP, TYPE I 5. AS5692/2 CIRCUIT BREAKERS MAY BE SUPPLIED WITH A ROUND KEYTAB OF .093 INCH .005 INCH DIAMETER. 6. TERMINAL ANGLE AND RELATED DIMENSIONS SHALL BE MEASURED FROM THE ELECTRICAL MATING SURFACE OF THE TERMINAL TO THE CENTER LINE OF THE BUSHING.
