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本文(SAE AS 27194B-2014 SEAL BONDED ALUMINUM ALLOY 6061-T6 AMS4027 MOLD IN GROOVE NBR RUBBER AMS-P-5315《AMS-P-5315丁腈橡胶槽模制的AMS4027 6061-T6铝合金粘结密封》.pdf)为本站会员(孙刚)主动上传,麦多课文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

SAE AS 27194B-2014 SEAL BONDED ALUMINUM ALLOY 6061-T6 AMS4027 MOLD IN GROOVE NBR RUBBER AMS-P-5315《AMS-P-5315丁腈橡胶槽模制的AMS4027 6061-T6铝合金粘结密封》.pdf

1、 AEROSPACE STANDARD SEAL, BONDED, ALUMINUM ALLOY 6061-T6, AMS4027, MOLD IN GROOVE, NBR RUBBER, AMS-P-5315 AS27194Copyright 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,

2、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 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org ISSUED 2001-03REV

3、ISED 2014-04THIRD ANGLE PROJECTION CUSTODIAN: A-6/A-6C2 REV.B FEDERAL SUPPLY CLASS 5331 AS27194 SHEET 1 OF 6 REV. B PROCUREMENT SPECIFICATION: NONESAE Technical Standards Board Rules provide that: “This report ispublished by SAE toadvance thestate of technicalandengineering sciences. Theuse ofthisre

4、port is entirelyvoluntary, andits applicability and suitability 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. S

5、AE invites yourwrittencomments andsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS27194B RATIONALE THE PURPOSE OF THIS REVISION IS TO REMOVE A CONFLICT IN SEALING SURFACE INSPECTION REQUIREMENTS AND TO CORRECT AN E

6、RROR IN THE TEMPERATURE LIMITS IN THE APPLICATION SECTION. NOTE: DIMENSIONING AND TOLERANCING PER ASME Y14.5 FIGURE 1 - SEAL -12 THRU -32 NOTE: DIMENSIONING AND TOLERANCING PER ASME Y14.5 FIGURE 2 - SEAL -40 THRU -48 AEROSPACE STANDARD AS27194 SHEET 2 OF 6 REV. B SEAL, BONDED, ALUMINUM ALLOY 6061-T6

7、, AMS4027, MOLD IN GROOVE, NBR RUBBER, AMS-P-5315 NOTE: DIMENSIONING AND TOLERANCING PER ASME Y14.5 FIGURE 3 - SEAL -56 THRU -64 NOTE: DIMENSIONING AND TOLERANCING PER ASME Y14.5 FIGURE 4 - ENLARGED SECTION, TYPICAL FOR ALL SIZES AEROSPACE STANDARD AS27194 SHEET 3 OF 6 REV. B SEAL, BONDED, ALUMINUM

8、ALLOY 6061-T6, AMS4027, MOLD IN GROOVE, NBR RUBBER, AMS-P-5315 TABLE 1A - DIMENSIONS IN INCHES TABLE 1B - DIMENSIONS IN MILLIMETERS MS PART NO. NOMINAL TUBE OD REF. A B .38 C D .38 E 0.10 F G H +.25 -.13 J RAD. K RAD. MS27194 -12 3/4 16.99 40.48 41.53 31.75 2.03 24.21 29.36 5.21 5.56 5.56 MS27194 -1

9、2 -16 3/4 16.99 44.45 47.14 38.10 2.03 30.56 33.33 5.21 5.56 5.56 MS27194 -16 1 22.96 44.45 47.14 38.10 2.03 30.56 33.33 5.21 5.56 5.56 MS27194-16 -24 1 22.96 60.33 65.10 53.98 2.03 44.05 46.03 6.76 7.14 7.14 MS27194 -20 1 1/4 28.91 55.56 59.49 46.83 2.03 38.10 42.06 6.76 6.75 6.75 MS27194 -20 -24 1

10、 1/4 28.91 60.33 65.10 53.98 2.03 44.05 46.03 6.76 7.14 7.14 MS27194 -24 1 1/2 34.85 60.33 65.10 53.98 2.03 44.05 46.03 6.76 7.14 7.14 MS27194 -32 2 46.76 76.20 85.32 69.85 2.03 61.12 60.33 8.33 7.94 7.94 MS27194 -40 2 1/2 59.46 101.60 96.83 82.55* 2.29 71.83 8.33 9.53 9.53* MS27194 -48 3 72.16 114.

11、30 109.53 95.25* 2.29 84.14 8.33 15.88 15.88* MS27194 -56 3 1/2 84.86 141.29 123.83 2.29 96.84 8.33 MS27194 -64 4 97.56 155.58 138.13 2.29 109.54 8.33 *SUGGESTED DIMENSIONS FOR “D“ AND “K“ SIZES -40 THROUGH -48. TABLE 2A - TOLERANCES IN INCHES MS PART NO. .WWW .XXX .YYY .ZZZ MS27194 - ALL SIZES .020

12、 .005 .010 .003 TABLE 2B - TOLERANCES IN MILLIMETERS MS PART NO. .WWW .XXX .YYY .ZZZ MS27194 - ALL SIZES 0.51 0.13 0.25 0.08 MS PART NO. NOMINAL TUBE OD REF. A B .015 C D .015 E .004 F G H +.010 -.005 J RAD. K RAD. MS27194 -12 3/4 .669 1.594 1.635 1.250 .080 .953 1.156 .205 .219 .219 MS27194 -12-16

13、3/4 .669 1.750 1.856 1.500 .080 1.203 1.312 .205 .219 .219 MS27194 -16 1 .904 1.750 1.856 1.500 .080 1.203 1.312 .205 .219 .219 MS27194 -16 -24 1 .904 2.375 2.563 2.125 .080 1.734 1.812 .266 .281 .281 MS27194 -20 1 1/4 1.138 2.188 2.342 1.844 .080 1.500 1.656 .266 .266 .266 MS27194 -20 -24 1 1/4 1.1

14、38 2.375 2.563 2.125 .080 1.734 1.812 .266 .281 .281 MS27194 -24 1 1/2 1.372 2.375 2.563 2.125 .080 1.734 1.812 .266 .281 .281 MS27194 -32 2 1.841 3.000 3.359 2.750 .080 2.406 2.375 .328 .313 .313 MS27194 -40 2 1/2 2.341 4.000 3.812 3.250* .090 2.828 .328 .375 .375* MS27194 -48 3 2.841 4.500 4.312 3

15、.750* .090 3.313 .328 .625 .625* MS27194 -56 3 1/2 3.341 5.563 4.875 .090 3.813 .328 MS27194 -64 4 3.841 6.125 5.438 .090 4.313 .328 AEROSPACE STANDARD AS27194 SHEET 4 OF 6 REV. B SEAL, BONDED, ALUMINUM ALLOY 6061-T6, AMS4027, MOLD IN GROOVE, NBR RUBBER, AMS-P-5315 TABLE 3A - FIGURE 4 DIMENSIONS IN

16、INCHES MS PART NO. N MIN P MIN R SEALING SURFACE Ra (MICROINCHES) MS27194 - ALL SIZES .050 .060 .020 63 TABLE 3B - FIGURE 4 DIMENSIONS IN MILLIMETERS MS PART NO. N MIN P MIN R SEALING SURFACE Ra (MICROMETERS) MS27194 - ALL SIZES 1.27 1.52 0.51 1.6 APPLICATION: THESE PRODUCTS HAVE BEEN USED TYPICALLY

17、 AT TEMPERATURES FROM -65 F (-54 C) TO +160 F (+71 C) WHERE RESISTANCE TO FUEL IS REQUIRED. THESE PRODUCTS ARE NOT TO BE USED DIRECTLY ON CFRP COMPOSITE MATERIALS. APPLICABLE REFERENCES: SAE PUBLICATIONS: AVAILABLE FROM SAE INTERNATIONAL, 400 COMMONWEALTH DRIVE, WARRENDALE, PA 15096-0001, TEL: 877-6

18、06-7323 (INSIDE USA AND CANADA) OR 724-776-4970 (OUTSIDE USA), www.sae.org. AMS2817 PACKAGING AND IDENTIFICATION PREFORMED PACKINGS AMS4027 ALUMINUM ALLOY, SHEET AND PLATE 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061; -T6 SHEET, -T651 PLATE) SOLUTION AND PRECIPITATION HEAT TREATED - UNS A96061 AMS-P-5315

19、ACRYLONITRILE-BUTADIENE (NBR) RUBBER FOR FUEL-RESISTANT SEALS 60 TO 70 AS478 IDENTIFICATION MARKING METHODS ARP5316 STORAGE OF ELASTOMER SEALS AND SEAL ASSEMBLIES WHICH INCLUDE AN ELASTOMER ELEMENT PRIOR TO HARDWARE ASSEMBLY AS5752 AEROSPACE - VISUAL INSPECTION STANDARD FOR ELASTOMERIC SEALING ELEME

20、NTS OTHER THAN O-RINGS U.S. GOVERNMENT PUBLICATIONS: AVAILABLE FROM DLA DOCUMENT SERVICES, BUILDING 4/D, 700 ROBBINS AVENUE, PHILADELPHIA, PA 19111-5094, TEL: 215-697-6396, http:/quicksearch.dla.mil/. MIL-A-8625 ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS ASQ PUBLICATIONS: AVAILABLE FROM AMERIC

21、AN SOCIETY FOR QUALITY, 600 NORTH PLANKINTON AVENUE, MILWAUKEE, WI 53203, TEL: 800-248-1946 (UNITED STATES OR CANADA), 001-800-514-1564 (MEXICO) OR +1-414-272-8575 (ALL OTHER LOCATIONS), www.asq.org. ANSI/ASQ Z1.4 SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES AEROSPACE STANDARD AS27194

22、 SHEET 5 OF 6 REV. B SEAL, BONDED, ALUMINUM ALLOY 6061-T6, AMS4027, MOLD IN GROOVE, NBR RUBBER, AMS-P-5315 ASME AND ISO PUBLICATIONS: AVAILABLE FROM AMERICAN NATIONAL STANDARDS INSTITUTE, 25 WEST 43RD STREET, 4TH FLOOR, NEW YORK, NY 10036-8002, TEL: 212-642-4900, www.ansi.org. ASME Y14.5 DIMENSIONIN

23、G AND TOLERANCING ASME Y14.36M SURFACE TEXTURE SYMBOLS ASME B46.1 SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) ISO 4287 GEOMETRICAL PRODUCT SPECIFICATIONS (GPS) - SURFACE TEXTURE: PROFILE METHOD - TERMS, DEFINITIONS AND SURFACE TEXTURE PARAMETERS ISO 3601-1 FLUID POWER SYSTEMS - O-RINGS -

24、PART 1: INSIDE DIAMETERS, CROSS-SECTIONS, TOLERANCES AND DESIGNATION CODES REQUIREMENTS: 1. MATERIALS: a. METAL RETAINER, 6061-T6 ALUMINUM ALLOY SHEET OR 6061-T651 ALUMINUM ALLOY PLATE PER AMS4027, ANODIZED TO MIL-A-8625, TYPE II. b. RUBBER SEAL SHALL CONFORM TO MATERIAL REQUIREMENTS OF SPEC AMS-P-5

25、315. 2. DIMENSIONAL AND VISUAL INSPECTION: a. DIMENSIONAL INSPECTION: THE SAMPLE SIZE SHALL BE IN ACCORDANCE WITH ANSI/ASQ Z1.4 SINGLE SAMPLING PLAN INSPECTION LEVEL II WITH AN AQL 1.0 EXCEPT THAT THE ACCEPTANCE NUMBER SHALL BE ZERO. THE SAMPLE UNIT SHALL BE ONE PLATE. THE PROCEDURES OUTLINED IN ANN

26、EX B OF ISO 3601-1 SHALL BE FOLLOWED FOR DIMENSIONAL INSPECTION OF THE RUBBER SEAL. DIMENSIONAL INSPECTION OF THE METAL RETAINER SHALL INCLUDE ALL DIMENSIONAL REQUIREMENTS LISTED ABOVE. IF THE PURCHASER REQUIRES A DIFFERENT SAMPLING PLAN OR VISUAL INSPECTION CRITERIA, PURCHASER AND MANUFACTURER SHAL

27、L AGREE PRIOR TO TIME OF ORDER. b. VISUAL INSPECTION: PRIOR TO INSPECTION, MOLD FLASH SHALL BE REMOVED FROM THE RUBBER SEALS IN SUCH A MANNER THAT THEY CONFORM TO THE REQUIREMENTS SPECIFIED HEREIN. FOR END OF PROCESS INSPECTION, EACH INDIVIDUAL RUBBER SEAL (100%) SHALL BE MANUALLY INSPECTED ACCORDIN

28、G TO AS5752, TYPE 1 REQUIREMENTS UNDER 2X MAGNIFICATION. THE ENTIRE RUBBER SEAL SURFACE SHALL BE INSPECTED. METAL RETAINERS SHALL BE VISUALLY INSPECTED TO BE FREE FROM GOUGES, SCRATCHES, AND OTHER SURFACE IMPERFECTIONS. SURFACES SHALL BE SMOOTH AND CONTINUOUS. 3. THE MANUFACTURER OF THE PLATES SHALL

29、 BE RESPONSIBLE FOR THE REQUIRED INSPECTIONS. PURCHASER RESERVES THE RIGHT TO SAMPLE AND PERFORM ANY CONFIRMATORY INSPECTION DEEMED NECESSARY TO ENSURE THAT THE PLATES CONFORM TO THE SPECIFIED REQUIREMENTS. 4. LOT ACCEPTANCE: THE REQUIREMENTS ARE LISTED IN AMS-P-5315, EXCEPT HARDNESS SHALL BE 65 5 S

30、HORE M. THE LOT CERTIFICATION REPORT SHALL BE FURNISHED TO THE PURCHASER WHEN THE PRODUCT IS SHIPPED. THE MANUFACTURER OF THE PLATES SHALL BE RESPONSIBLE FOR THE LOT ACCEPTANCE TESTS. PURCHASER RESERVES THE RIGHT TO SAMPLE AND PERFORM ANY CONFIRMATORY INSPECTION DEEMED NECESSARY TO ENSURE THAT THE P

31、LATES CONFORM TO THE SPECIFIED REQUIREMENTS. 5. PART NUMBER: THE PLATE PART NUMBERS ARE DESIGNATED MS27194-XX OR MS27194-XX-XX, WHERE XX OR XX-XX REPRESENTS THE DASH NUMBER. 6. PRODUCT SHALL BE PERMANENTLY IDENTIFIED PER AS478 AS TO MANUFACTURER AND TYPE. 7. PACKAGING SHALL BE IN ACCORDANCE WITH AMS

32、2817 WITH THE FOLLOWING EXCEPTIONS: IF REQUIRED BY PURCHASER: NATIONAL STOCK NUMBER IF REQUIRED BY PURCHASER: SHELF LIFE REQUIREMENTS OF ARP5316 IF REQUIRED BY THE PURCHASER: NUMBER OF PLATES PER PACKAGE AEROSPACE STANDARD AS27194 SHEET 6 OF 6 REV. B SEAL, BONDED, ALUMINUM ALLOY 6061-T6, AMS4027, MO

33、LD IN GROOVE, NBR RUBBER, AMS-P-5315 8. PURCHASE DOCUMENTS SHOULD SPECIFY NOT LESS THAN THE FOLLOWING: PART NUMBER OF PLATE PER AS27194 QUANTITY OF PLATES DESIRED SPECIAL PACKAGING AND LABELING, IF REQUIRED 9. DO NOT USE UNASSIGNED PART NUMBERS. 10. COLOR MARKINGS: a. ON SIZES -12 THRU -48, OUTSIDE

34、EDGE SHALL HAVE AT LEAST 3 NON-PERMANENT RED COLORED MARKINGS MORE THAN 1/4 INCH LONG TO INDICATE TYPE OF SEAL. b. ON SIZES -56 THRU -64, OUTSIDE EDGE SHALL HAVE A NON-PERMANENT RED COLORED MARKING EXTENDING AT LEAST THREE QUARTERS OF THE WAY AROUND THE PART. 11. DIMENSIONS AND PROPERTIES IN INCH UN

35、ITS ARE PRIMARY; DIMENSIONS AND PROPERTIES IN SI UNITS ARE SHOWN AS THE APPROXIMATE EQUIVALENTS OF THE PRIMARY UNITS AND ARE PRESENTED ONLY FOR INFORMATION. 12. TOLERANCES: UNLESS OTHERWISE SPECIFIED, LINEAR DIMENSIONS .005 INCH (0.13 MM), ANGULAR DIMENSIONS .50. 13. SURFACE TEXTURE SHALL BE IN ACCO

36、RDANCE WITH ASME B46.1 FOR MICROINCHES Ra AND ISO 4287 FOR MICROMETERS Ra. SYMBOLS SHALL BE IN ACCORDANCE WITH ASME Y14.36M. UNLESS OTHERWISE SPECIFIED, THE MAXIMUM MACHINED SURFACES SHALL BE 125 MICROINCHES Ra (3.2 MICROMETERS Ra). 14. BREAK ALL EDGES .003 TO .010 INCH (0.08 TO 0.25 MM) UNLESS OTHE

37、RWISE SPECIFIED. 15. SEAL DESIGN MUST PROVIDE 80% MINIMUM OCCUPANCY OF THE GROOVE WHEN ASSEMBLED. NOTES: 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.

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