SAE AS 14154B-2007 Circuit Breaker - Aircraft Trip-Free Push-Pull 3 Phase 1 Thru 20 Amp Type 1《航空器用I型电流1～20A三相推挽式自动短路断路器》.pdf

1、 AEROSPACE STANDARD CIRCUIT BREAKER - AIRCRAFT, TRIP-FREE, PUSH-PULL, 3 PHASE, 1 THRU 20 AMP, TYPE 1 AS14154 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, mech

2、anical, 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 1997-08REVISED 20

3、07-02 THIRD ANGLE PROJECTION CUSTODIAN: SAE AE-8/AE-8B1 REV. B FEDERAL SUPPLY CLASS5925 AS14154 SHEET 1 OF 3 REV.B PROCUREMENT SPECIFICATION: AS58091SAE TechnicalStandards Board Rules provide that: “This report is published by SAE toadvance thestate of technical andengineering sciences. Theuse of th

4、isreportis entirely voluntary, andits applicabilityandsuitability forany particularuse,including any patent infringement arising therefrom, is thesole responsibility oftheuser.” SAE reviews each technical report at least every five yearsat which time it may be reaffirmed, revised, orcancelled.SAE in

5、vites yourwritten commentsandsuggestions.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 MILITARY. THE REQUIREMENTS FO

6、R 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 Provided by IHS under lic

7、ense with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD CIRCUIT BREAKER - AIRCRAFT, TRIP-FREE, PUSH-PULL, 3 PHASE, 1 THRU 20 AMP, TYPE 1 AS14154 REV. B AS14154 SHEET 2 OF 3 REV.B TABLE 2 - ELECTRICAL AND MECHANICAL CHARACTERISTICS ENDURANCE

8、CYCLES OPERATING FORCE MAX (LB) RESISTIVE INDUCTIVE DASH NUMBER NOMINAL AMPERAGE RATING (A) VOLT DROP MAX (V) WEIGHT MAX (LB) PULLOUT RESET AC DC AC DC MECH. NO. LOAD 1 1 1.10 .15 18 12 5000 1/ NONE 2500 1/ NONE 5000 2 2 .75 .15 18 12 5000 1/ NONE 2500 1/ NONE 5000 2 2-1/2 .70 .15 18 12 5000 1/ NONE

9、 2500 1/ NONE 5000 3 3 .55 .15 18 12 5000 1/ NONE 2500 1/ NONE 5000 4 4 .45 .15 18 12 5000 1/ NONE 2500 1/ NONE 5000 5 5 .35 .15 18 12 5000 1/ NONE 2500 1/ NONE 5000 7 7-1/2 .30 .15 18 12 5000 1/ NONE 2500 1/ NONE 5000 10 10 .28 .15 18 12 5000 1/ NONE 2500 1/ NONE 5000 15 15 .28 .15 18 12 5000 1/ NO

10、NE 2500 1/ NONE 5000 20 20 .25 .15 18 12 5000 1/ NONE 2500 1/ NONE 5000 1/ 115/200 VOLT 400 HZ SYSTEM, TESTED AT 120 5 VOLTS 380 TO 400 HZ TABLE 3 - DETAIL CALIBRATION REQUIREMENTS +25 C -55 C +71 C % RATED CURRENT % RATED CURRENT % RATED CURRENT NOMINAL AMPERAGE RATING (A) 110 145 200 500 1000 110

11、165 200 500 1000 100 145 200 500 1000 -1 -2 -2 -3 -4 -5 -7 -10 -15 -20 MUSTHOLD- 1HOURMIN. 1/ 2/ MUST TRIP - 1HOUR MAX. 1/ 2/ 4 TO 203/ 0.4 TO2.0 3/ 0.10TO 0.533/ MUSTHOLD- 1HOURMIN. 2/ MUST TRIP - 1HOUR MAX. 2/ 6 TO 403/ 0.55TO 3.5 3/ 0.15TO 0.803/ MUSTHOLD- 1HOURMIN. 2/ MUST TRIP - 1HOUR MAX. 2/ 3

12、 TO 203/ 0.33TO 1.7 3/ 0.08TO .40 3/ 1/ ONE PHASE AT SPECIFIED LOAD AND OTHER PHASES CARRYING RATED LOAD. 2/ BALANCED THREE PHASE LOAD. 3/ SINGLE PHASE LOAD ONLY. TRIP TIME IN SECONDS. TABLE 4 - INTERRUPTING CAPACITY REQUIREMENTS - AMPERES TEST DESIGNATION PER AS58091 A B G H NOMINAL AMPERAGE RATING

13、 (A) 10 30 10 30 C D E F 10 30 10 30 -1 (*) (*) (*) (*) (*) (*) (*) (*) 2000 1200 2000 1200 -2 (*) (*) (*) (*) (*) (*) (*) (*) 2000 1200 2000 1200 -2 (*) (*) (*) (*) (*) (*) (*) (*) 2000 1200 2000 1200 -3 (*) (*) (*) (*) (*) (*) (*) (*) 2000 1200 2000 1200 -4 (*) (*) (*) (*) (*) (*) (*) (*) 2000 120

14、0 2000 1200 -5 (*) (*) (*) (*) (*) (*) (*) (*) 2000 1200 2000 1200 -7 (*) (*) (*) (*) (*) (*) (*) (*) 2000 1200 2000 1200 -10 (*) (*) (*) (*) (*) (*) (*) (*) 2000 1200 2000 1200 -15 (*) (*) (*) (*) (*) (*) (*) (*) 2000 1200 2000 1200 -20 (*) (*) (*) (*) (*) (*) (*) (*) 2000 1200 2000 1200 * NOT APPL

15、ICABLE Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD CIRCUIT BREAKER - AIRCRAFT, TRIP-FREE, PUSH-PULL, 3 PHASE, 1 THRU 20 AMP, TYPE 1 AS14154 REV. B AS14154 SHEET 3 OF 3 REV.B TA

16、BLE 5 - ENVIRONMENTAL PERFORMANCE 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 PADS: IF INCLUDED, VIBRATION STABIL

17、IZING PADS SHALL BE SILICON RUBBER 9235 OR EQUIVALENT AND SHALL BE 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. D

18、EPARTMENT 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. DIMENSIONS ARE IN INCHES. 2. UNLESS OTHERWISE SPECIFIED, TOLERANCES: DECIMALS .031. 3. VOLTAGE RATING 115V L-N 400 HZ NOMINAL OR 200V L-L 400

19、HZ NOMINAL. 4. IN THE EVENT OF A CONFLICT BETWEEN THE TEXT OF THIS STANDARD AND THE REFERENCES CITED HEREIN, THE TEXT OF THE STANDARD SHALL TAKE PRECEDENCE. 5. THE CHANGE BAR ( l ) LOCATED IN THE LEFT MARGIN IS FOR THE CONVENIENCE OF THE USER IN LOCATING AREAS WHERE TECHNICAL CHANGES, NOT EDITORIAL

20、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. MAXIMUM OPERATING ALTITUDE - FT 70,000 OPERATING AMBIENT TEMPERATURE RANGE -55 TO +71 C VIBRATION - IN ACCORDANCE WITH AS58091 SINE - REQUIRED HIGH LEVEL SINE (OPTIONAL) SHOCK 50G, MIL-STD-202, METHOD 213 TEST CONDITION G Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-