1、SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirelyvoluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefro
2、m, is the sole responsibility of the user.”SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions.Copyright 2005 SAE InternationalAll rights reserved. No part of this publication may be
3、reproduced, stored in a retrieval system or transmitted, in any form 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-
4、776-0790Email: custsvcsae.orgSAE WEB ADDRESS: http:/www.sae.orgTow or Yarn, Carbon FibersFor Structural CompositesGF 325 (2241) Tensile Strength, 57 (393) Tensile Modulus1. SCOPE:1.1 Form: This specification covers one type of continuous multifilament carbon fibers in the form of a tow or yarn (when
5、 twisted). The weight per unit length of the tow or yarn is governed by the filament count which is identified by the suppliers grade or material designation.1.2 Classification: Carbon tow or yarn, derived from a polyacrylonitrile precursor, with typical 325 ksi (2241 MPa) tensile strength and 57 Ms
6、i (393 GPa) tensile modulus for use in general purpose structural composites requiring moderately high tensile strength and high modulus of elasticity in tension.2. APPLICABLE DOCUMENTS: See AMS 3892.3. TECHNICAL REQUIREMENTS: 3.1 Basic Specification: The complete requirements for procuring the carb
7、on tow or yarn described herein shall consist of this document and the latest issue of the basic specification. 3.2 Storage Life: The product shall be readily strippable from the spool and the filaments spreadable when tested at any time up to six months from date of receipt by purchaser provided it
8、 has been stored at room temperature in the original closed container.AEROSPACE MATERIAL SPECIFICATIONAMS 3892/6AIssued JUL 1984Revised OCT 1992Reaffirmed MAY 2005Superseding AMS 3892/6Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permi
9、tted without license from IHS-,-,-AMS 3892/6A SAE AMS 3892/6A- 2 -3.3 Properties: Shall conform to the requirements shown in Table 1. The requirements of 3.3.1 and 3.3.2 apply to the average of the number of determinations indicated in the basic specification but no individual value shall be less th
10、an 90% of the specified minimum average unless due to an obvious testing problem, in which case a substitute specimen may be tested:4. QUALITY ASSURANCE PROVISIONS: See 3892.5. PREPARATION FOR DELIVERY: See AMS 3892.6. ACKNOWLEDGMENT: See AMS 3892.TABLE 1 - PropertiesParagraph Property Requirement3.
11、3.1 Tensile Strength, minimum 300 ksi (2068 MPa)3.3.2 Tensile Modulus,minimummaximum53.0 Msi (365 GPa)60.5 Msi (417 GPa)3.3.3 Mass per unit length Preproduction Value 5%3.3.4 Finish Content, maximum 2% by weight3.3.5 Density 0.064 to 0.067 pound per cubic inch(1.77 to 1.85 g/cm3)3.3.6 Yarn Twist (wh
12、en applicable),nominalmaximum0.4 turn per inch (15 turns/m)0.8 turn per inch (30 turns/m)Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AMS 3892/6A SAE AMS 3892/6A- 3 -7. REJECTIONS: See AMS 3892.8. NOTES:See AMS 3892.PREPARED UNDER THE JURISDICTION OF AMS COMMITTEE “P”Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
