1、 AEROSPACE STANDARD FUSE, LIMITER TYPE ENCLOSED LINK, 1 - 60 AMPERE AS5372/1Copyright 2015 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, photocopying, recording,
2、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 2015-06THIRD ANGLE PROJECTION CUSTODIAN: AE-8/A
3、E-8B FEDERAL SUPPLY CLASS 5920AS5372/1 SHEET 1 OF 4 PROCUREMENT SPECIFICATION: AS5372SAE Technical Standards Board Rules provide that: “This report ispublished by SAE toadvance thestate of technicalandengineering sciences. Theuse ofthisreport is entirelyvoluntary, andits applicability and suitabilit
4、y forany particularuse,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 yourwrittencomments andsuggestions. SAE values your
5、 input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS5372/1 RATIONALE THIS DETAIL SPECIFICATION SHEET IS WRITTEN TO PERMIT THE CANCELLATION AND SUPERSESSION OF MIL-DTL-5372/1 WITH THIS DOCUMENT. NOTICE THE COMPLETE REQUIREMENTS FOR PROCURING THE P
6、RODUCT DESCRIBED HEREIN SHALL CONSIST OF THIS DOCUMENT AND THE LATEST ISSUE OF AS5372. FIGURE 1 - FUSE CONFIGURATION AND DIMENSIONS AEROSPACE STANDARD AS5372/1 SHEET 2 OF 4 FUSE, LIMITER TYPE ENCLOSED LINK, 1 - 60 AMPERE TABLE 1 - FIGURE 1 DIMENSIONS A B C D E F NOMINAL G H J .66 (16.8) .56 (14.2) .
7、80 (20.3) .70 (17.8) 1.42 (36.1) 1.32 (33.5).21 (5.3) .11 (2.8) .11 (2.8) .01 (0.3) .03 (0.8) .99 (25.1) .89 (22.6) .19 (4.8) .09 (2.3) .130 (3.30) .120 (3.05) TABLE 1A - FIGURE 1 DIMENSIONS (CONTINUED) K L M N P .73 (18.5) .71 (18.0) .55 (14.0) .45 (11.4) 1.35 (34.3) 1.25 (31.8)2.16 (54.9) 2.06 (52
8、3) .14 (3.6) .04 (1.0) TABLE 2 - AMPERE RATING DASH NUMBER M5372/1- CURRENT RATING (AMPERES) 01 1 02 2 03 3 05 5 10 10 15 15 20 20 25 25 30 30 35 35 40 40 50 50 60 60 TABLE 3 - TERMINAL STRENGTH DIRECTION OF FORCE RATING TO 30 AMPERES ABOVE 30 AMPERES FORCE IN POUNDS (MINIMUM) TO EDGE OF BLADE 10 2
9、5 TO FLAT SIDE OF BLADE 5 10 TO END OF BLADE (INTO FUSE) 30 40 AEROSPACE STANDARD AS5372/1 SHEET 3 OF 4 FUSE, LIMITER TYPE ENCLOSED LINK, 1 - 60 AMPERE FIGURE 2 - FUSING CURRENT VERSUS ELEMENT MELT TIME (20 TO 60 AMPERE) FIGURE 3 - FUSING CURRENT VERSUS ELEMENT MELT TIME (1 TO 15 AMPERE) AEROSPACE S
10、TANDARD AS5372/1 SHEET 4 OF 4 FUSE, LIMITER TYPE ENCLOSED LINK, 1 - 60 AMPERE REQUIREMENTS: ALL REQUIREMENTS SHALL CONSIST OF THIS DOCUMENT AND THE LATEST ISSUE OF AS5372. 1. DESIGN: THE FUSE SHALL BE DESIGNED IN ACCORDANCE WITH FIGURES 1 THROUGH 3 AND TABLES 1 AND 2. DIMENSIONS ARE IN INCHES AND AP
11、PLY AFTER PLATING. METRIC EQUIVALENTS ARE GIVEN FOR INFORMATION PURPOSES ONLY AND ARE BASED ON 1 INCH = 25.4 MM. 2. MATERIALS: BODY - GLASS FILLED MELAMINE IN ACCORDANCE WITH ASTM D5948, TYPE MMI-5 (WHITE). BLADES - COPPER IN ACCORDANCE WITH ASTM B152/B152M, TYPE ETA WITH SILVER PLATE. 3. WEIGHT: .0
12、65 POUNDS MAXIMUM. 4. TERMINAL STRENGTH: WITH THE BODY OF THE FUSE FIRMLY CLAMPED, THE FORCES IN TABLE 3 SHALL BE APPLIED TO BOTH TERMINALS. 5. PART NUMBER: SEE EXAMPLE BELOW: EXAMPLE: M5372 /1 - 01 BASIC PART NUMBER SPECIFICATION SHEET DASH NUMBER (SEE TABLE 2) APPLICATION NOTE: 1. THIS FUSE IS NOT
13、 RECOMMENDED FOR NEW DESIGN. USAGE IS RECOMMENDED FOR REPLACEMENT PURPOSES ONLY. SPECIFICATION NOTE: 1. A 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, INCLUDING TECHNICAL REVISIONS. CHANGE BARS AND (R) ARE NOT USED IN ORIGINAL PUBLICATIONS NOR IN DOCUMENTS THAT CONTAIN EDITORIAL CHANGES ONLY.
