SAE AS 5192D-2014 FITTING TEE INTERNAL STRAIGHT THREAD PORT《内部直螺纹端口三通管配件》.pdf

上传人:李朗 文档编号:1024774 上传时间:2019-03-21 格式:PDF 页数:5 大小:44.81KB
下载 相关 举报
SAE AS 5192D-2014 FITTING TEE INTERNAL STRAIGHT THREAD PORT《内部直螺纹端口三通管配件》.pdf_第1页
第1页 / 共5页
SAE AS 5192D-2014 FITTING TEE INTERNAL STRAIGHT THREAD PORT《内部直螺纹端口三通管配件》.pdf_第2页
第2页 / 共5页
SAE AS 5192D-2014 FITTING TEE INTERNAL STRAIGHT THREAD PORT《内部直螺纹端口三通管配件》.pdf_第3页
第3页 / 共5页
SAE AS 5192D-2014 FITTING TEE INTERNAL STRAIGHT THREAD PORT《内部直螺纹端口三通管配件》.pdf_第4页
第4页 / 共5页
SAE AS 5192D-2014 FITTING TEE INTERNAL STRAIGHT THREAD PORT《内部直螺纹端口三通管配件》.pdf_第5页
第5页 / 共5页
亲,该文档总共5页,全部预览完了,如果喜欢就下载吧!
资源描述

1、AEROSPACE STANDARD FITTING, TEE, INTERNAL STRAIGHT THREAD PORT AS5192Copyright 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, photocopying, recording, or othe

2、rwise, 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 2000-07REVISED 2014-04THIRD ANGLE PROJECTION CUSTODIAN

3、: G-3/G-3B REV.DFEDERAL SUPPLY CLASS 4730 AS5192SHEET 1 OF 5REV. DPROCUREMENT SPECIFICATION: /4/ AS4875SAE Technical Standards Board Rules provide that: “This report ispublishedby SAE toadvance thestate of technicalandengineeringsciences.The useofthis reportisentirelyvoluntary, andits applicability

4、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 yourwrittencomments andsuggestions.

5、SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS5192DRATIONALE ADDED MATERIAL CODE “D” AND CLARIFIED NOTE /19/. FIGURE 1 - FITTING, TEE MATERIAL USAGE RECOMMENDATIONS /19/AEROSPACE STANDARD AS5192SHEET 2 OF 5REV. DFITTING, TEE,

6、 INTERNAL STRAIGHT THREAD PORT TABLE 1A - DIMENSIONS BASIC NO. AS5192/18/SIZE CODE (NOMINAL TUBESIZE)T THREAD PERAS8879CLASS 3B AB.016 C+.000-.015 DE V W 04 .250 .4375-20 UNJF .787 .688 .397 .040 .483 .735- .753 .050 05 .312 .5000-20 UNJF .787 .750 .459 .040 .452 .735- .753 .050 06 .375 .5625-18 UNJ

7、F .849 .813 .516 .040 .475 .797- .815 .050 08 .500 .7500-16 UNJF 1.037 1.063 .697 .071 .569 1.047-1.065 .050 10 .625 .8750-14 UNJF 1.193 1.188 .815 .071 .638 1.173-1.191 .070 12 .750 1.0625-12 UNJ 1.396 1.438 .991 .077 .730 1.418-1.443 .080 16 1.000 1.3125-12 UNJ 1.568 1.688 1.241 .077 .777 1.668-1.

8、693 .090 20 1.250 1.6250-12 UNJ 1.771 2.000 1.553 .077 .824 1.980-2.005 .110 TABLE 1B - WEIGHTS BASIC NO.AS5192/18/SIZE CODE LB/EAAPPROX REF ALLB/EAAPPROX REF STEELLB/EAAPPROX REF TI04 .0539 .155 .0854 05 .0534 .153 .084506 .0533 .153 .0844 08 .126 .362 .200 10 .170 .488 .269 12 .284 .814 .449 16 .3

9、78 1.09 .599 20 .510 1.47 .780 NOTES: NOTICE THIS DOCUMENT REFERENCES A PART WHICH CONTAINS CADMIUM AS A PLATING MATERIAL. CONSULT LOCAL OFFICIALS IF YOU HAVE QUESTIONS CONCERNING CADMIUMS USE. /1/ MATERIAL: a. DASH AS CODE LETTER - TYPE 4130 STEEL FORGING OR BAR PER AMS6370 OR AMS-S-6758, OR TYPE 4

10、140 STEEL BAR PER AMS6382. /2/ b. CODE LETTER D TYPE 2014-T6 ALUMINUM ALLOY FORGING PER AMS4134 OR 2024-T6 ALUMINUM ALLOY BAR PER AMS4112. /2/ /19/ c. CODE LETTER J - TYPE 304 CORROSION RESISTANT STEEL FORGING OR BAR PER AMS5639. d. CODE LETTER K - TYPE 316 CORROSION RESISTANT STEEL FORGING OR BAR P

11、ER AMS5648. e. CODE LETTER R - TYPE 321 CORROSION RESISTANT STEEL FORGING OR BAR PER AMS5645. f. CODE LETTER S - TYPE 347 CORROSION RESISTANT STEEL FORGING OR BAR PER AMS5646. /19/ AEROSPACE STANDARD AS5192SHEET 3 OF 5REV. DFITTING, TEE, INTERNAL STRAIGHT THREAD PORT g. CODE LETTER T - TYPE 6AL-4V T

12、ITANIUM ALLOY FORGING OR BAR PER AMS4928. /17/ h. CODE LETTER W - TYPE 7075-T73 ALUMINUM ALLOY FORGING PER AMS4141; OR TYPE 7075-T73 ALUMINUM ALLOY BAR PER AMS-QQ-A-225/9; OR TYPE 7075-T7351 ALUMINUM ALLOY BAR PER AMS4124. /2/ /2/ HEAT TREATMENT: a. DASH AS MATERIAL CODE LETTER - SEE HARDNESS REQUIR

13、EMENT PER PROCUREMENT SPECIFICATION. b. MATERIAL CODE LETTER D SEE PROCUREMENT SPECIFICATION. c. MATERIAL CODE LETTER W - SEE PROCUREMENT SPECIFICATION. d. OTHER MATERIAL CODE LETTERS - NONE. 3. FINISH: a. DASH AS MATERIAL CODE LETTER - CADMIUM PLATE PER AMS-QQ-P-416, TYPE II, CLASS 2, DYE BLACK AND

14、 COAT WITH A LIGHT FILM OF OIL PER PROCUREMENT SPECIFICATION. b. MATERIAL CODE LETTER D - ANODIZE PER AMS2472 OR MIL-A-8625, TYPE II, CLASS 2, DYE BLUE, DUPLEX SEAL PER PROCUREMENT SPECIFICATION. c. MATERIAL CODE LETTER J - PASSIVATE PER AMS2700 TYPE 6 OR TYPE 7 OR METHOD 2. d. MATERIAL CODE LETTER

15、K - PASSIVATE PER AMS2700 TYPE 6 OR TYPE 7 OR METHOD 2. e. MATERIAL CODE LETTER R - PASSIVATE PER AMS2700 TYPE 6 OR TYPE 7 OR METHOD 2. f. MATERIAL CODE LETTER S - PASSIVATE PER AMS2700 TYPE 6 OR TYPE 7 OR METHOD 2. g. MATERIAL CODE LETTER T - ANODIZE PER AMS2488 OR FLUORIDE PHOSPHATE CONVERSION COA

16、T PER AMS2486 WITH COLOR PER PROCUREMENT SPECIFICATION. h. MATERIAL CODE LETTER W: 1. ANODIZE PER AMS2472 OR MIL-A-8625, TYPE II, CLASS 2, DYE BROWN, DUPLEX SEAL PER PROCUREMENT SPECIFICATION. 2. W CODE PARTS TO BE COATED WITH HIGH PURITY ALUMINUM ONLY WILL HAVE THE FINISH CODE LETTER “V” PLACED AFT

17、ER THE SIZE CODE IN THE PART NUMBER. THE FINISH WILL BE: COAT WITH HIGH PURITY ALUMINUM PER MIL-DTL-83488, CLASS 3, TYPE II, WITH MAXIMUM COATING THICKNESS OF .0005. GLASS BEAD PEEN PRESSURE SHALL BE 25 PSI MAXIMUM. /4/ PROCUREMENT SPECIFICATION: AS4875 EXCEPT AS SPECIFIED ON THIS STANDARD. PRODUCT

18、SUPPLIED TO THIS SPECIFICATION SHALL BE MANUFACTURED BY AN ACCREDITED MANUFACTURER LISTED IN THE NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM (NADCAP) QUALIFIED MANUFACTURER LIST FOR THIS PRODUCT TYPE. THE QML IS AVAILABLE AT www.eAuditN./5/ IDENTIFICATION AT LOCATION SHOWN: MARK

19、 PER AS478 CLASS C OR D, OR METHOD 7A3, 15A3, OR 15B. a. FOR SIZES 06 AND SMALLER: MANUFACTURERS NAME, CAGE CODE OR TRADEMARK, LETTERS “AS“ AND MATERIAL CODE LETTER. b. FOR SIZES 08 AND LARGER: MANUFACTURERS NAME, CAGE CODE OR TRADEMARK, BASIC PART NUMBER AND MATERIAL CODE LETTER. AEROSPACE STANDARD

20、 AS5192SHEET 4 OF 5REV. DFITTING, TEE, INTERNAL STRAIGHT THREAD PORT 6. INTENDED USE: THIS PART IS DESIGNED FOR USE IN SYSTEMS WITH MAXIMUM OPERATING PRESSURES AS SHOWN IN TABLE 2. TABLE 2 - OPERATING PRESSURES FOR ASSOCIATED MATERIAL SIZE MATERIAL PSI 04-08 ALUMINUM ALLOY 3000 10-16 ALUMINUM ALLO 1

21、50020 ALUMINUM ALLOY 100004-16 STEEL 3000 20 STEEL 150004-16 CORROSION RESISTANT STEEL 3000 20 CORROSION RESISTANT STEEL 150004-16 TITANIUM ALLOY 3000 20 TITANIUM ALLO 15007. THIS STANDARD IS A FUNCTIONAL EQUIVALENT OF AN938 AND IS INTENDED TO BE SUITABLE AS A REPLACEMENT STANDARD. 8. WHEN MACHINED

22、FROM BAR OR OVERSIZED FORGING, THE CENTER BODY DIMENSIONS SHALL CONFORM TO AS1376, TABLE 1. /9/ RADIUS APPLICABLE FOR TITANIUM ALLOY PARTS ONLY. 10. 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

23、 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. 11. INTERP

24、RETATION OF DRAWING PER AS4296. 12. SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M. REQUIREMENTS PER ASME B46.1. UNLESS OTHERWISE SPECIFIED, MACHINED SURFACES TO BE 125 MICROINCHES Ra. FORGED SURFACES MAY BE 250 MICROINCHES Ra. 13. BREAK EDGES .003 TO .015 UNLESS OTHERWISE SPECIFIED. 14. DIMENSIONING AND

25、 TOLERANCING: ASME Y14.5M-1994. 15. DIMENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED, TOLERANCES: LINEAR DIMENSIONS .010, ANGULAR DIMENSIONS 0 DEGREES 30 MINUTES. 16. INVENTORIED PARTS CONFORMING TO THE PREVIOUS “LETTER CHANGE” MAY BE USED TO DEPLETION. /17/ TITANIUM AND CADMIUM SHALL NOT BE USED FO

26、R OXYGEN OR POTABLE WATER SYSTEMS. /18/ EXAMPLE OF PART NUMBER: BASIC PART NUMBER MATERIAL CODE LETTER /1/SIZE CODE, TUBE SIZE IN .062 INCREMENTS THE FINISH CODE LETTER “V” WILL BE PLACED HERE ONLY FOR MATERIAL CODE “W” PARTS THAT ARE TO BE COATED WITH HIGH PURITY ALUMINUM AS5192 W 08 VAEROSPACE STA

27、NDARD AS5192SHEET 5 OF 5REV. DFITTING, TEE, INTERNAL STRAIGHT THREAD PORT /19/ MATERIAL USAGE RECOMMENDATIONS: a. FOR HYDRAULIC APPLICATIONS, IT IS RECOMMENDED THAT CODE “W”, 7075 ALUMINUM ALLOY, BE USED IN LIEU OF CODE “D” MATERIAL BECAUSE 7075 MATERIAL HAS HIGHER STRENGTH PROPERTIES AND SUPERIOR CORROSION RESISTANCE. b. MATERIAL CODE “S”, CORROSION RESISTANT STEEL (TYPE 347), WAS OBSOLETED IN 1987 AND IS ONLY DISPLAYED HERE FOR LEGACY REASONS. USE MATERIAL CODE “R” IN LIEU OF CODE “S”.

展开阅读全文
相关资源
猜你喜欢
相关搜索

当前位置:首页 > 标准规范 > 国际标准 > 其他

copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
备案/许可证编号:苏ICP备17064731号-1