1、SAETechnicalStandardsBoardRulesprovidethat:“ThisreportispublishedbySAEtoadvancethestateoftechnicalandengineeringsciences.Theuseofthisreportisentirelyvoluntary,anditsapplicabilityandsuitabilityforanyparticularuse,includinganypatentinfringementarisingtherefrom,isthesoleresponsibilityoftheuser.”SAErevi
2、ewseachtechnicalreportatleasteveryfiveyearsatwhichtimeitmaybereaffirmed,revised,orcancelled.SAEinvitesyourwrittencommentsandsuggestions.SHEET 1 OF 4AS101THIRD ANGLE PROJECTIONAEROSPACE STANDARDAS101ISSUED1992-07REAFFIRMED2004-07CROSS ASSEMBLY,RETAINED NUT,SHORT FLARELESSCUSTODIAN: SAE G-3/G-3B PROCU
3、REMENT SPECIFICATION: /4/ MIL-F-18280FEDERAL SUPPLY CLASS 4730FIGURE 1 - CROSS ASSEMBLYFIGURE 2 - INSTALLATION, RETAINED NUT AND RETAINING WIRECopyright 2004 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form
4、 or by any means, electronic, 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: 724-776-4970 (outside USA) Fax: 724-776-0790 Email: custsvcsae.org SAE WEB ADDRESS: http:/www.sae.or
5、g Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-CROSS ASSEMBLY,RETAINED NUT,SHORT FLARELESSAEROSPACE STANDARD AS101SHEET 2 OF 4AS101TABLE 1 - DIMENSIONS AND WEIGHTSNOTES:/1/ MATERIAL: a. CODE LETTER
6、T: 1. BODY: TYPE 6AL-4V TITANIUM ALLOY PER AMS 49282. NUT: CODE LETTER T OF AS4702 REFERENCE (TYPE 6AL-4V TITANIUM ALLOY)3. WIRE: PER AS4701 REFERENCE (CLASS 302 OR 305 CORROSION RESISTANT STEEL)b. CODE LETTER V: 1. BODY: TYPE 15-5PH CORROSION RESISTANT STEEL PER AMS 56592. NUT: CODE LETTER V OF AS4
7、702 REFERENCE (TYPE 15-5PH CORROSION RESISTANT STEEL)3. WIRE: PER AS4701 REFERENCE (CLASS 302 OR 305 CORROSION RESISTANT STEEL)c. CODE LETTER W: 1. BODY: TYPE 7075-T73 ALUMINUM ALLOY FORGING PER AMS 4141 OR TYPE 7075-T7351 ALUMINUM ALLOY BAR PER AMS 41242. NUT: CODE LETTER W OF AS4702 REFERENCE (TYP
8、E 7075-T73 ALUMINUM ALLOY)3. WIRE: PER AS4701 REFERENCE (CLASS 302 OR 305 CORROSION RESISTANT STEEL)2. HEAT TREAT:a. MATERIAL CODE LETTER T: 1. BODY, NUT, AND WIRE: NONEb. MATERIAL CODE LETTER V: 1. BODY: HEAT TREAT TO CONDITION H-1075 PER AMS 2759/32. NUT: MATERIAL CODE LETTER V OF AS4702 REFERENCE
9、 (HEAT TREAT TO CONDITION H-1075)3. WIRE: NONEc. MATERIAL CODE LETTER W: 1. BODY, NUT, AND WIRE: NONE/3/ FINISH: a. MATERIAL CODE LETTER T: 1. BODY: FLUORIDE PHOSPHATE CONVERSION COAT PER AMS 24862. NUT: CODE LETTER T OF AS4702 OR AS1790 WITH SUFFIX N REFERENCE (FLUORIDE PHOSPHATE CONVERSION COAT AN
10、D COAT WITH DRY LUBRICANT ON ID)3. WIRE: PER AS4701 OR AS1791 REFERENCE (PASSIVATE AND COAT WITH DRY LUBRICANT)Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-CROSS ASSEMBLY,RETAINED NUT,SHORT FLARELES
11、SAEROSPACE STANDARD AS101SHEET 3 OF 4AS101/3/ (Continued):b. MATERIAL CODE LETTER V:1. BODYa. V CODE PARTS TO BE PASSIVATED ONLY WILL HAVE NO FINISH CODE LETTER AFTER THE PART NUMBER. THE FINISH WILL BE: PASSIVATE PER QQ-P-35, TYPE II OR VIII.b. V CODE PARTS TO BE CADMIUM PLATED ONLY WILL HAVE THE F
12、INISH CODE LETTER “P” AFTER THE SIZE CODE IN THE PART NUMBER. THE FINISH WILL BE: CADMIUM PLATE PER QQ-P-416, TYPE II, CLASS 2.2. NUT: CODE LETTER V OF AS4702 OR AS1790 REFERENCEa. NO FINISH CODE LETTER AT END OF PART NUMBER: PASSIVATE AND COAT WITH DRY FILM LUBRICANT ON IDb. FINISH CODE LETTER P AT
13、 END OF PART NUMBER: CADMIUM PLATE3. WIRE: PER AS4701 OR AS1791 REFERENCE (PASSIVATE AND COAT WITH DRY LUBRICANT)c. MATERIAL CODE LETTER W: 1. BODY: ANODIZE PER AMS 2472 DYED BROWN, SIMILAR TO COLOR 10080 OF FED-STD-5952. NUT: CODE LETTER W OF AS4702 OR AS1790 WITH SUFFIX N REFERENCE (ANODIZE DYED B
14、ROWN AND COAT WITH DRY LUBRICANT)3. WIRE: PER AS4701 OR AS1791 REFERENCE. FINISH CODE LETTER P AT END OF PART NUMBER (CADMIUM PLATE)/4/ PROCUREMENT SPECIFICATION: MIL-F-18280 EXCEPT AS SPECIFIED ON THIS STANDARD. THIS PART SHALL BE QUALIFIED TO THE PROCUREMENT SPECIFICATION AS APPLICABLE IN A COMPLE
15、TE ASSEMBLY. USERS OF THIS STANDARD ARE ADVISED TO CONTROL SOURCE APPROVAL(S) BY STANDARD PAGE SUPPLEMENT OR SIMILAR MEANS./5/ IDENTIFICATION AT LOCATION SHOWN: MARK PER AS478 CLASS C OR D OR METHOD 7A3, 15A3, OR 15B. MANUFACTURERS NAME, TRADEMARK OR CAGE CODE, BASIC PART NUMBER AND MATERIAL CODE LE
16、TTER.6. THIS PART IS DESIGNED FOR USE IN SYSTEMS WITH OPERATING PRESSURES AS FOLLOWS:a. SIZES -20 AND -24 TITANIUM ALLOY AND CORROSION RESISTANT STEEL AT 3000 psib. SIZES -20 AND -24 ALUMINUM ALLOY AT 600 psi7. WHEN MACHINED FROM BAR OR OVERSIZED FORGINGS THE CENTER BODY SECTION SHALL CONFORM TO AS1
17、376, TABLE 10./8/ RADIUS APPLICABLE FOR TITANIUM PARTS ONLY./9/ ASSEMBLE AS4702 RETAINED NUT TO FITTING BODY WITH AS4701 RETAINING WIRE AS SHOWN IN FIGURE 2. THE NUT SHALL BE FREE TO ROTATE AFTER ASSEMBLY./10/ THIS IS A NONREDUCER FITTING. ALL PORTS OF ANY GIVEN PART WILL BE THE SAME SIZE. FOR REDUC
18、ERS USE AS103.11. INTERPRETATION OF DRAWING PER ARP4296.12. SURFACE TEXTURE: SYMBOLS PER ANSI Y14.36; REQUIREMENTS PER ANSI/ASME B46.1. UNLESS OTHERWISE SPECIFIED, MACHINED SURFACES TO BE 125 in Ra.13. BREAK EDGES .003 TO .015 UNLESS OTHERWISE SPECIFIED.14. DIMENSIONING AND TOLERANCING: ANSI Y14.5M.
19、15. DIMENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED, TOLERANCES: LINEAR DIMENSIONS .010, ANGULAR DIMENSIONS 5 .Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-CROSS ASSEMBLY,RETAINED NUT,SHORT FLARELESSAEROSPACE STANDARD AS101SHEET 4 OF 4AS101/16/ EXAMPLE OF PART NUMBER:Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-
