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 400 (2758) Tensile Strength, 33 (228) 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 400 ksi (2758 MPa) tensile strength and 33 Ms
6、i (228 GPa) tensile modulus for use in general purpose structural composites requiring high tensile strength and moderate modulus of elasticity in tension.2. APPLICABLE DOCUMENTS: See AMS 3892.3. TECHNICAL REQUIREMENTS: 3.1 Basic Specification: The complete requirements for procuring the carbon tow
7、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 has be
8、en stored at room temperature in the original closed container.AEROSPACE MATERIAL SPECIFICATIONAMS 3892/1BIssued NOV 1972Revised OCT 1992Reaffirmed MAY 2005Superseding AMS 3892/1ACopyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted w
9、ithout license from IHS-,-,-AMS 3892/1B SAE AMS 3892/1B- 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 than 90%
10、 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.TABLE 1 - PropertiesParagraph Property Requirement3.3.1 Tensile Strength, minimum 380 ksi
11、(2620 MPa)3.3.2 Tensile Modulusminimummaximum32 Msi (221 GPa)36 Msi (248 GPa)3.3.3 Ultimate Elongationminimum1.1%3.3.4 Mass per unit length Preproduction Value 5%3.3.5 Finish Content, maximum 2% by weight3.3.6 Density 0.061 to 0.066 pound per cubic inch(1.69 to 1.83 g/cm3)3.3.7 Yarn Twist (when appl
12、icable),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 3892/1B SAE AMS 3892/1B- 3 -6. ACKNOWLEDGMENT: See AMS 3892.7. 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-,-,-
