SAE AMS-STD-401-1999 Sandwich Constructions and Core Materials General Test Methods《夹层结构和芯材料 通用测试方法FSC 5680 应代替1999年9月24日作废的MIL-STD-401B标准》.pdf
《SAE AMS-STD-401-1999 Sandwich Constructions and Core Materials General Test Methods《夹层结构和芯材料 通用测试方法FSC 5680 应代替1999年9月24日作废的MIL-STD-401B标准》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS-STD-401-1999 Sandwich Constructions and Core Materials General Test Methods《夹层结构和芯材料 通用测试方法FSC 5680 应代替1999年9月24日作废的MIL-STD-401B标准》.pdf(34页珍藏版)》请在麦多课文档分享上搜索。
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 1999 Society of Automotive Engineers, Inc.All rights reserved. Printed in U.S.
3、A.QUESTIONS REGARDING THIS DOCUMENT: (724) 772-7121 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 15096-0001AEROSPACE MATERIAL SPECIFICATIONAMS-STD-401Issued JUN 1999Sandwich Constructions and
4、Core Materials;General Test MethodsNOTICEThis document has been taken directly from U.S. Military Specification MIL-STD-401B and contains only minor editorial and format changes required to bring it into conformance with the publishing requirements of SAE technical standards. The initial release of
5、this document is intended to replace MIL-STD-401B. Any part numbers established by the original specification remain unchanged.The original Military Specification was adopted as an SAE standard under the provisions of the SAE Technical Standards Board (TSB) Rules and Regulations (TSB 001) pertaining
6、 to accelerated adoption of government specifications and standards. TSB rules provide for (a) the publication of portions of unrevised government specifications and standards without consensus voting at the SAE Committee level, and (b) the use of the existing government specification or standard fo
7、rmat.Under Department of Defense policies and procedures, any qualification requirements and associated qualified products lists are mandatory for DOD contracts. Any requirement relating to qualified products lists (QPLs) has not been adopted by SAE and is not part of this SAE technical document.AMS
8、-STD-401 SAE AMS-STD-401- 2 -CONTENTSPageParagraph 1. SCOPE 41.1 Scope 42. APPLICABLE DOCUMENTS 42.1 U.S. Government Publications 42.2 ASTM Publications 43. DEFINITIONS 53.1 General 53.1.1 Sandwich 53.1.2 Core 53.1.3 Facing 53.1.4 Flatwise 53.1.5 Edgewise 53.1.6 Isotropic 53.1.7 Orthotropic 53.1.7.1
9、 Orthotropic facing directions 53.1.7.2 Orthotropic core directions 64. GENERAL REQUIREMENTS 64.1 Selection of test samples 64.1.1 Design data 64.1.2 Quality assurance provisions 64.1.2.1 Sampling for the various inspections, examinations and tests 64.2 Test conditions 74.3 Test apparatus 74.4 Repor
10、t of test results 84.5 Designation of units of measurement 85. DETAIL TEST METHODS 85.1 Core Test Methods 85.1.1 Core Density and Specific Gravity 85.1.2 Core Moisture Sorption 95.1.3 Core Thermal Conductivity 105.1.4 Core Compression 105.1.5 Core Shear 125.1.6 Core Tension 155.1.7 Core Water Migrat
11、ion 155.1.8 Core Delamination of Honeycomb Core 165.2 Sandwich test methods 175.2.1 Sandwich Compression 175.2.2 Sandwich Shear 185.2.3 Sandwich Tension 185.2.4 Sandwich Flexure 195.2.5 Sandwich Thermal Conductivity 225.2.6 Sandwich Peel 235.3 Fatigue Tests 255.4 Creep Characteristics 26AMS-STD-401
12、SAE AMS-STD-401- 3 -FIGURESPageFigure 1. Axes notation for sandwich cores. 272. Sketch showing shear specimens attached to loadingplates and plane of action of applied loads. 283. Compression test apparatus showing an adjustable supportingbase and slotted round bars in position on the specimen ends.
13、Deformations are being measured with Martens mirrorcompressometers. 294. Test apparatus for tension flatwise test of core material forsandwich-type constructions showing specimens and fitting forapplying load. 305. Apparatus for conducting flexure test of sandwich construction. 316. Type of apparatu
14、s suitable for making sandwich peel test. 327. Possible modes of failure of sandwich composite under edgewiseloads: General buckling, shear crimping, dimpling of facings,and wrinkling of facings either away from or into the core 338. Apparatus for node strength tests. 34AMS-STD-401 SAE AMS-STD-401-
15、4 -1. SCOPE:1.1 Scope: This standard covers the general requirements and methods for testing sandwich core materials and for testing sandwich construction of the types used primarily in aircraft structures. This standard does not include test methods applicable only to a specific product; such test
16、methods are included in the detailed specifications for the product.2. APPLICABLE DOCUMENTS 1/: The following publications, of the issue in effect on date of invitation for bids or request for proposal, form a part of this specification to the extent specified herein.2.1 U.S. Government Publications
17、: Available from DODSSP, Subscription Services Desk, Building 4D, 700 Robbins Avenue, Philadelphia, PA 19111-5094.MIL-STD-105 Sampling Procedures and Tables for Inspection by Attributes2.2 ASTM Publications: Available from ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959.ASTM C 177 Meth
18、od of Test for Thermal Conductivity of Materials by Means of the Guarded Hot PlateASTM C 236 Method of Test for Thermal Conductance and Transmittance of Built-up Sections by Means of the Guarded Hot BoxASTM C 271 Method of Test for Density of Core Materials for Structural Sandwich ConstructionsASTM
19、C 272 Method of Test for Water Absorption of Core Materials for Structural Sandwich ConstructionsASTM C 273 Method of Shear Test in Flatwise Plane of Flat Sandwich Constructions or Sandwich CoresASTM C 297 Methods for Tension Test of Flat Sandwich Constructions in Flatwise Plane1/ Designations of co
20、mparable test methods of the American Society for Testing and Materials (ASTM) are given, where they exist, for reference information. The methods specified herein are similar in techniques and procedures to the ASTM methods but are frequently more restricted in scope to include tests specifically a
21、pplicable to sandwich constructions for aircraft.AMS-STD-401 SAE AMS-STD-401- 5 -2.2 (Continued):ASTM C 363 Method of Test for Delamination Strength of Honeycomb Type Core MaterialASTM C 364 Method of Test for Edgewise Compressive Strength of Flat Sandwich ConstructionsASTM C 365 Method of Test for
22、Flatwise Compressive Strength of Sandwich CoresASTM C 393 Method of Flexure Test of Flat Sandwich ConstructionsASTM C 394 Method of Test for Shear Fatigue of Sandwich Core MaterialsASTM D 1781 Method for Climbing Drum Peel Test for Adhesives3. DEFINITIONS: 3.1 General: The following terms are used t
23、hroughout this standard and their interpretation shall be construed in accordance with the following definitions.3.1.1 Sandwich: A laminar construction, consisting of thin facings bonded to a relatively thick lightweight core, resulting in a rigid and lightweight panel. In this standard, bonded mean
24、s “joined by welding, brazing or adhesive.”3.1.2 Core: A lightweight natural, synthetic, or fabricated material bonded between the facings of sandwich construction in order to separate the facings and to support them against buckling under stress.3.1.3 Facing: One of the two outer layers which have
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