SAE AMS 3832C-1994 Roving Type S-2 Glass Epoxy Resin Impregnated《粗纱类型》.pdf
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1、SAE-AMS3832ADOPTION NOTICESAE-AMS3832, “GLASS ROVING, TYPE S-2, EPOXY RESIN IMPREGNATED“,was adopted on 29-JUL-80 for use by the Department of Defense(DoD). Proposed changes by DoD activities must be submitted tothe DoD Adopting Activity: Commander, Naval Air Warfare Center,Aircraft Division, Code 4
2、14100B120-3, Highway 547, Lakehurst, NJ08733-5100. Copies of this document may be purchased from theSociety of Automotive Engineers 400 Commonwealth DriveWarrendale, Pennsylvania, United States, 15096-0001. http:/www.sae.org/_Custodians: Adopting Activity:Navy - ASArmy - MRNavy - ASAir Force - 11Rev
3、iewer Activities:DLA - GSAREA CMPSDISTRIBUTION STATEMENT A: Approved for public release; distributionis unlimited.COPYRIGHT SAE International (Society of Automotive Engineers, Inc)Licensed by Information Handling ServicesCopyright SAE International Provided by IHS under license with SAENot for Resal
4、eNo reproduction or networking permitted without license from IHS-,-The Engineering SocietyFor Advancing MobilityLand Sea Air and Space AEROSPACEMATERIALAMS 3832CINTERNATIONAL400 Commonwealth Drive, Warrendale, PA 15096-0001SPECIFICATION Issued NOV 1970Revised MAY 1994Superseding AMS 3832BSubmitted
5、for recognition as an American National StandardROVING, TYPE “S-2“ GLASSEpoxy Resin Impregnated1. SCOPE:1.1 Form:This specification covers continuous, multiple-strand, roving of Type “S-2“glass impregnated with a heat-curable epoxy resin matrix and processed to a“B“ stage condition.1.2 Application:T
6、his roving has been used typically for filament winding of rocket motorcases, pressure vessels,aircraft, and related structures, but usage is notlimited to such applications.1.3 Safety - Hazardous Materials:While the materials, methods, applications, and processes described orreferenced in this spec
7、ification may involve the use of hazardous materials,this specification does not address the hazards which may be involved in suchuse. It is the sole responsibility of the user to ensure familiarity withthe safe and proper use of any hazardous materials and to take necessaryprecautionary measures to
8、 ensure the health and safety of all personnelinvolved.2. APPLICABLE DOCUMENTS:The following publications form a part of this specification to the extentspecified herein. The applicable issue of referenced publications shall bethe issue in effect on the date of the purchase order.SAE Technical Stand
9、ards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineeringsciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringementarising therefrom, is the sole respo
10、nsibility 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 writtencomments and suggestions.Copyright 1994 Society of Automotive Engineers, Inc.All rights reserved. Printed in U.S.A.COPYRIGHT SAE Inter
11、national (Society of Automotive Engineers, Inc)Licensed by Information Handling ServicesCopyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-AMS 3832C SAE AMS 3832C2.1 ASTM Publications:Available from ASTM,
12、 1916 Race Street, Philadelphia, PA 19103-1187.ASTM D 2290 Apparent Tensile Strength of Ring or Tubular Plastics andReinforced Plastics by Split Disk MethodASTM D 2291 Fabrication of Ring Test Specimens for Glass-Resin CompositesASTM D 2343 Tensile Properties of Glass Fiber Strands, Yarns, and Rovin
13、gsUsed in Reinforced PlasticsASTM D 2344 Apparent Interlaminar Shear Strength of Parallel FiberComposites by Short Beam MethodASTM D 2410 Finish Content of Woven Glass Fabric, Cleaned andAfter-Finished with Chrome Complexes, for Plastic Laminates2.2 U.S. Government Publications:Available from DODSSP
14、, Subscription Services Desk, Building 4D, 700 RobbinsAvenue, Philadelphia, PA 19111-5094.MIL-STD-2073-1 DOD Materiel, Procedures for Development and Application ofPackaging Requirements3. TECHNICAL REQUIREMENTS:3.1 Material:3.1.1 Roving: Shall be “20 End“ Type “S-2“ Glass, treated immediforming wit
15、h a suitable high-strength finish.3.1.2 Splices: No splices or knots shall be introduced during thimpregnation process.ately aftere resin3.1.3 Resin: Shall be a low-pressure, epoxy laminating resin modified asnecessary to meet the requirements of 3.2.3.1.4 Shelf Life: The impregnated roving shall ha
16、ve a shelf life of not lessthan three months from date of impregnation when packaged in vapor-proof,heat-sealed bags and stored at not higher than -18 C (0 F).3.1.5 Cure: Product shall become fully processed by filament winding undertension of 12 to 15 pounds force (53.4 to 66.7 N) and curing, using
17、temperature ranges and times recommended by the manufacturer; however,curing time, exclusive of the post cure, shall not exceed five hours.3.2 Properties:The product shall conform to the requirements of 3.2.1 and 3.2.2; tests shallbe performed on the product supplied and in accordance with specified
18、 testmethods, insofar as practicable.-2-COPYRIGHT SAE International (Society of Automotive Engineers, Inc)Licensed by Information Handling ServicesCopyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-AMS 38
19、32CSAEAMS 3832C3.2.1 Uncured Properties:Shall be as shown in Table 1.TABLE 1 - Uncured PropertiesParagraph PropertyRequirementTest Method3.2.1.1Resin Solids17 to 23% by weight4.5.1(Volatile Free)3.2.1.2Volatiles, max3% by weight4.5.13.2.1.3Gel Time1 to 4 minutes4.5.23.2.1.4Resin Flow8 to 17% by weig
20、ht4.5.33.2.1.5Filament Diameter0.00035 to 0.00050 inch(8.9 to 1O.2m)-3.2.1.6Weight0.560to 0.640 gram per yard-(0.61 to 0.70 g/m)3.2.1.7Tensile Strength,525 ksiASTM D 2343min(3620 MPa)TABLE 2- Cured PropertiesParagraph Property3.2.2.1Tensile Strength, min(Determined on specimensconforming to ASTM D 2
21、343)3.2.2.2Horizontal Shear Strength, min(Determined on specimensconforming to ASTM D 2291,Type C.)Requirement380 ksi(2620 MPa)8.0 ksi(55.2 MPa)Test MethodASTM D 2290ASTM D 23443.2.2 As Cured:Specimens fabricated in accordance with ASTM D 2291 from “B“stage impregnated roving and cured as in 3.1.5 s
22、hall have the propertiesshown in Table 2, determined at 23 C 1 (73 2).3.3 Quality:The product, as received by purchaser,shall be uniform in quality andcondition and free from foreign materials and from imperfections detrimentalto usage of the product.-3-COPYRIGHT SAE International (Society of Automo
23、tive Engineers, Inc)Licensed by Information Handling ServicesCopyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-AMS 3832C SAE AMS 3832C4. QUALITY ASSURANCE PROVISIONS:4.1 Responsibility for Inspection:(R)
24、The manufacturer of the product shall supply all samples for manufacturerstests and shall be responsible for performing all required tests. Purchaserreserves the right to sample and to perform any confirmatory testing deemednecessary to ensure that the product conforms to the requirements of thisspe
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