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1、AEROSPACE STANDARD CIRCUIT BREAKER - AIRCRAFT, TRIP-FREE, PUSH-PULL 3 PHASE, 1 THRU 35 AMP, TYPE 1 AS14153 Copyright 2007 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, mechan
2、ical, 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: 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org ISSUED 1997-08 REVISED 200
3、7-02 THIRD ANGLE PROJECTION CUSTODIAN: SAE AE-8/AE-8B1 REV. B FEDERAL SUPPLY CLASS 5925 AS14153 SHEET1 OF 3 REV. B PROCUREMENT SPECIFICATION AS58091 SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use
4、of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, o
5、r cancelled. SAE invites your written comments and suggestions. RATIONALE CORRECT ERRORS AND UPDATE SPECIFICATIONS PRIOR TO AND FROM THE ORIGINAL CONVERSION FROM NAVAIR CONTROL TO SAE CONTROL AND INCLUDE ADDITIONAL CHANGES REQUESTED BY NAVAIR TO REFLECT REQUIREMENTS THAT ARE BEING USED IN THE MILITA
6、RY. THE REQUIREMENTS FOR ACQUIRING THE PRODUCT(S) DESCRIBED HEREIN SHALL CONSIST OF THIS SPECIFICATION SHEET AND THE ISSUE OF THE FOLLOWING SPECIFICATION LISTED IN THAT ISSUE OF THE DODISS SPECIFIED IN THE SOLICITATION: SAE AS58091. FIGURE 1 - TRIP-FREE CIRCUIT BREAKER Copyright SAE International Pr
7、ovided by IHS under license with SAELicensee=Defense Contract Mgmt Command/5935922100 Not for Resale, 05/23/2007 22:52:42 MDTNo reproduction or networking permitted without license from IHS -,-,- AEROSPACE STANDARD CIRCUIT BREAKER - AIRCRAFT, TRIP-FREE, PUSH-PULL 3 PHASE, 1 THRU 35 AMP, TYPE 1 AS141
8、53REV. B AS14153 SHEET2 OF 3 REV. B TABLE 1 - ELECTRICAL AND MECHANICAL CHARACTERISTICS ENDURANCE CYCLES OPERATING FORCE MAX. LB RESISTIVE INDUCTIVE DASH NO. NOMINAL AMPERE RATING VOLT DROP MAX. WEIGHT MAX. LB PULLOUT RESET AC DC AC DC MECH. NO LOAD 1 1 1.10 15 15 20 20 25 25 30 30 35 35 .250 .25181
9、25000 1/ NONE2500 1/ NONE5000 1/ 115/200 VOLT 400 HZ SYSTEM. TESTED AT 120 5 VOLTS 380 TO 400 HZ. TABLE 2 - DETAIL CALIBRATION REQUIREMENTS +25 C -55 C +71 C % OF RATED CURRENT % OF RATED CURRENT % OF RATED CURRENT NOMINAL AMPERE RATING 110 145 200 500 1000 110 165 200 500 1000 100 145 200 500 1000
10、1 15 20 25 30 35 MUST HOLD 1 HOUR MIN. 2/ MUST TRIP 1 HOUR MAX. 2/ 4 TO 20 3/ 0.4 TO 2.0 3/ 0.10 TO 0.53 3/ MUST HOLD 1 HOUR MIN. 2/ MUST TRIP 1 HOUR MAX. 2/ 6 TO 40 3/ 0.55 TO 3.5 3/ 0.15 TO 60 3/ MUST HOLD 1 HOUR MIN. 2/ MUST TRIP 1 HOUR MAX. 2/ 3 TO 20 3/ 0.33 TO 1.7 3/ 0.06 TO 0.40 3/ 1/ ONE PHA
11、SE AT SPECIFIED LOAD AND OTHER PHASES CARRYING RATED LOAD. 2/ BALANCED THREE PHASE LOAD. 3/ SINGLE PHASE LOAD ONLY, TRIP TIME IN SECONDS. TABLE 3 - INTERRUPTING CAPACITY REQUIREMENTS - AMPERES TEST DESIGNATION PER AS58091 A B G H NOMINAL AMPERE RATING 1 3 13 C D E F 1 3 1 3 1 15 20 25 30 35 (*) (*)
12、(*)(*)(*)(*)(*)(*)2000120020001200 (*) NOT APPLICABLE. Copyright SAE International Provided by IHS under license with SAELicensee=Defense Contract Mgmt Command/5935922100 Not for Resale, 05/23/2007 22:52:42 MDTNo reproduction or networking permitted without license from IHS -,-,- AEROSPACE STANDARD
13、CIRCUIT BREAKER - AIRCRAFT, TRIP-FREE, PUSH-PULL 3 PHASE, 1 THRU 35 AMP, TYPE 1 AS14153REV. B AS14153 SHEET3 OF 3 REV. B TABLE 4 - ENVIRONMENTAL PERFORMANCE MAXIMUM OPERATING ALTITUDE - FT 70,000 OPERATING AMBIENT TEMPERATURE RANGE -55 TO +71 C VIBRATION - IN ACCORDANCE WITH AS58091 SINE - REQUIRED
14、SHOCK 50G, MIL-STD-202, METHOD 213, TEST G REQUIREMENTS: 1. THE PART NUMBERS FOR CIRCUIT BREAKERS IN ACCORDANCE WITH THIS SPECIFICATION SHALL CONFORM TO THE EXAMPLE BELOW. WHEN A DESIGNATOR IS NOT APPLICABLE IT SHALL BE OMITTED FROM THE PART NUMBER. 2.OPTIONAL STABILIZING PAD: IF INCLUDED, VIBRATION
15、 STABILIZING PADS SHALL BE SILICON RUBBER 9235. OR EQUIVALENT LOCATED OVER THE PHASE A AND C PLUGGED BUSHING HOLES AND ATTACHED WITH A SILICON ADHESIVE. QUALIFICATION: QUALIFICATION IS REQUIRED FOR U.S. GOVERNMENT PROCUREMENT. THE QUALIFIED PRODUCTS LIST (QPL) QUALIFICATION ACTIVITY FOR U.S. DEPARTM
16、ENT OF DEFENSE PROCUREMENT PURPOSES, NAVAL AIR SYSTEMS COMMAND (CODE 4.4.5.3), 22229 ELMER ROAD, BUILDING 2360, PATUXENT RIVER, MD 20670-1900. NOTES: 1. SURFACE TEXTURE SHALL BE IN ACCORDANCE WITH ANSI B46.1. 2. DIMENSIONS ARE IN INCHES. UNLESS OTHERWISE SPECIFIED, TOLERANCES: DECIMALS .031. 3. VOLT
17、AGE RATING: 115 V 400 HZ NOMINAL L-N OR 200 V 400 HZ NOMINAL L-L. 4. THE CHANGE BAR ( l ) LOCATED IN THE LEFT MARGIN IS FOR THE CONVENIENCE OF THE USER IN LOCATING AREAS WHERE TECHNICAL REVISIONS, NOT EDITORIAL CHANGES, HAVE BEEN MADE TO THE PREVIOUS ISSUE OF THIS DOCUMENT. AN (R) SYMBOL TO THE LEFT OF THE DOCUMENT TITLE INDICATES A COMPLETE REVISION OF THE DOCUMENT. Copyright SAE International Provided by IHS under license with SAELicensee=Defense Contract Mgmt Command/5935922100 Not for Resale, 05/23/2007 22:52:42 MDTNo reproduction or networking permitted without license from IHS -,-,-