SAE AMS 3828C-1993 Glass Roving Epoxy Resin Preimpregnated Type E Glass《环氧树脂预浸渍的E类玻璃粗纱》.pdf
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1、SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and enginee ring sciences. The use of this report is entirelyvoluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefr
2、om, 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 invit es your written comments and suggestions.Copyright 1998 Society of Automotive Engineers, Inc.All rights reserved. Printed in U.
3、S.A.QUESTIONS REGARDING THIS DOCUMENT: (724) 772-7154 FAX: (724) 776-0243TO PLACE A DOCUMENT ORDER: (724) 776-4970 FAX: (724) 776-0790SAE WEB ADDRESS: http:/www.sae.org400 Commonwealth Drive, Warrendale, PA 15096-0001AEROS PACE MATERIAL SPECIFIC ATIONSubmitted for recognition as an American National
4、 StandardAMS 3828CIssued NOV 1968 Revised OCT 1993Reaffirmed SEP 1998Superseding AMS 3828BGlass Roving, Epoxy Resin PreimpregnatedType E Glass1. SCOPE:1.1 Form: This specification covers glass roving impregnated with epoxy resin, the resin being partially processed to a “B“ stage condition.1.2 Appli
5、cation: This roving has been used typically in high strength filament-wound structures for aircraft, missiles, and related structures, but usage is not limited to such applications.1.3 Safety - Hazardous Materials: While the materials, methods, applications, and processes described or referenced in
6、this specification may involve the use of hazardous materials, this specification does not address the hazards which may be involved in such use. It is the sole responsibility of the user to ensure familiarity with the safe and proper use of any hazardous materials and to take necessary precautionar
7、y measures to ensure the health and safety of all personnel involved.2. APPLICABLE DOCUMENTS: The following publications form a part of this specification to the extent specified herein. The latest issue of SAE publications shall apply. The applicable issue of other publications shall be the issue i
8、n effect on the date of the purchase order.2.1 SAE Publications: Available from SAE, 400 Commonwealth Drive, Warrendale, PA15096-0001.AMS 2825 Material Safety Data SheetsCopyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without li
9、cense from IHS-,-,-AMS 3828C SAE AMS 3828C- 2 -2.2 ASTM Publications: Available from ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959.ASTM D 2290 Apparent Tensile Strength of Ring or Tubular Plastics and Reinforced Plastics by Split Disk MethodASTM D 2343 Tensile Properties of Glass Fib
10、er Strands, Yarns, and Rovings Used in Reinforced PlasticsASTM D 2344 Apparent Interlaminar Shear Strength of Parallel Fiber Composites by Short Beam MethodASTM D 2584 Ignition Loss of Cured Reinforced Resins2.3 U.S. Government Publications: Available from DODSSP, Subscription Services Desk, Buildin
11、g 4D, 700 Robbins Avenue, Philadelphia, PA 19111-5094.MIL-C-9084 Cloth, Glass, Finished for Resin LaminatesMIL-R-9300 Resin, Epoxy, Low Pressure LaminatingMIL-R-60346 Roving, Glass, Fibrous (For Prepreg Tape and Roving, Filament Winding, and Pultrusion Applications)MIL-STD-2073-1 DoD Materiel, Proce
12、dures for Development and Application of Packaging Requirements3. TECHNICAL REQUIREMENTS: 3.1 Material: Shall be glass roving conforming to MIL-R-60346, Type II, Class ECG 135-140, impregnated with epoxy resin formulated to meet MIL-R-9300, TypeI, Class 1, the resin being processed to “B“ stage cond
13、ition.3.1.1 Splices: No splices or knots shall be introduced during the impregnation process except as shall have been previously agreed upon by purchaser and vendor.3.1.2 Shelf Life: When packaged in vapor-proof, heat-sealed bags, the preimpregnated roving shall have a shelf life of not less than t
14、hree weeks when stored at not higher than 4 C (39 F), and not less than three months when stored at not higher than -18 C (0 F).3.1.3 Cure: Roving shall be fully cured by filament winding under 12 to 15 psi (83 to 103 kPa) tension and curing for one hour at 95 C 15 (203 F 27) plus two hours at 175 C
15、 15 (347 F 27), or as recommended by the manufacturer.Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AMS 3828C SAE AMS 3828C- 3 -3.2 Properties: Roving shall conform to requirements shown in Table 1
16、; tests shall be performed on the product supplied and in accordance with specified test methods, insofar as practicable.3.3 Quality: Roving, as received by purchaser, shall be uniform in quality and condition and free from foreign materials and from imperfections detrimental to usage of the roving.
17、4. QUALITY ASSURANCE PROVISIONS: 4.1 Responsibility for Inspection: The manufacturer of roving shall supply all samples for required tests and shall be responsible for performing all required tests. Purchaser reserves the right to sample and to perform any confirmatory testing deemed necessary to en
18、sure that the roving conforms to the requirements of this specification.4.2 Classification of Tests: 4.2.1 Acceptance Tests: Tests for volatile matter (3.2.1.1), resin flow (3.2.1.4), and cured hoop tensile strength (3.2.2.1) are acceptance tests and shall be performed on each lot.TABLE 1 - Properti
19、esParagraph Property Requirement Test Method3.2.1 As Received (Uncured):3.2.1.1 Volatile Content, by weight 0.5 to 2.5% 4.5.13.2.1.2 Ignition Loss, by weight 17 to 23% ASTM D 25843.2.1.3 Gel Time 1.0 to 3.5 minutes 4.5.23.2.1.4 Resin Flow, by weight 8 to 17% 4.5.33.2.1.5 Tensile Strength, Impregnate
20、dStrand, min300 ksi(2068 MPa)ASTM D 23433.2.2 As Cured: Specimens, cured as in 3.1.3, shall have the following properties, determined at 23 C 1 (73 F 2):3.2.2.1 Hoop Tensile Strength(NOL Ring), min190 ksi(1310 MPa)ASTM D 22903.2.2.2 Interlaminar Shear Strength, min 6000 psi(41.4 MPa)ASTM D 2344Copyr
21、ight SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AMS 3828C SAE AMS 3828C- 4 -4.2.2 Preproduction Tests: Tests for all technical requirements are preproduction tests and shall be performed prior to or on th
22、e first shipment of roving by the manufacturer, when a change in ingredients and/or processing requires reapproval as in 4.4.2, and when purchaser deems confirmatory testing to be required.4.2.2.1 For direct U.S. Military procurement, substantiating test data and, when requested, preproduction test
23、material shall be submitted to the cognizant agency as directed by the procuring activity, contracting officer, or request for procurement.4.3 Sampling and Testing: Shall be as follows:4.3.1 For Acceptance Tests: Sufficient roving shall be taken at random from each lot to perform all required tests.
24、 The number of determinations for each requirement shall be as specified in the applicable test procedure or, if not specified therein, not less than three.4.3.1.1 A lot shall be all product from the same batches or lots of roving and resin produced in one continuous run and presented for manufactur
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