ASTM E1556-2003 Standard Specification for Epoxy Resin System for Composite Skin Honeycomb Sandwich Panel Repair《合成革、蜂窝状夹层板修补用环氧树脂系统标准规范》.pdf
《ASTM E1556-2003 Standard Specification for Epoxy Resin System for Composite Skin Honeycomb Sandwich Panel Repair《合成革、蜂窝状夹层板修补用环氧树脂系统标准规范》.pdf》由会员分享,可在线阅读,更多相关《ASTM E1556-2003 Standard Specification for Epoxy Resin System for Composite Skin Honeycomb Sandwich Panel Repair《合成革、蜂窝状夹层板修补用环氧树脂系统标准规范》.pdf(9页珍藏版)》请在麦多课文档分享上搜索。
1、Designation: E 1556 03Standard Specification forEpoxy Resin System for Composite Skin, HoneycombSandwich Panel Repair1This standard is issued under the fixed designation E 1556; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the y
2、ear of last revision. A number in parentheses indicates the year of last reapproval. Asuperscript epsilon (e) indicates an editorial change since the last revision or reapproval.This standard has been approved for use by agencies of the Department of Defense.1. Scope1.1 This specification covers the
3、 requirements for an epoxyresin system intended for the repair of sandwich panels fordurable, rigidwall, relocatable structures. It must be usable in afield environment and shall not require the use of specialequipment such as autoclaves or presses. The epoxy systemcovered by this specification shal
4、l be usable for simultaneousimpregnation of a wet-layup composite skin and bonding ofthat skin to a substrate honeycomb core. The material shallwithstand exposure to temperatures from 54 to 93C (65 to199F) and high relative humidity, and also the combination ofstress, temperature, and relative humid
5、ity that are expected tobe encountered in service.1.2 The values stated in SI units are to be regarded asstandard where only SI units are given or where SI units aregiven first followed by inch-pound units; where inch-poundunits are given first followed by SI units, the inch-pound unitsare to be reg
6、arded as the standard.1.3 The following safety hazards caveat refers only to thetest methods described in this specification. This standard doesnot purport to address all of the safety concerns, if any,associated with its use. It is the responsibility of the user of thisstandard to establish appropr
7、iate safety and health practicesand determine the applicability of regulatory limitations priorto use.2. Referenced Documents2.1 ASTM Standards:C 297 Test Method for Flatwise Tensile Strength of Sand-wich ConstructionsD 792 Test Methods for Density and Specific Gravity (Rela-tive Density) of Plastic
8、s by DisplacementD 2344 Test Method for Strength of Polymer Matrix Com-posite Materials by Short-Beam MethodD 2584 Test Method for Ignition Loss of Cured ReinforcedResinsD 2734 Test Methods for Void Content of Reinforced Plas-ticsD 3165 Test Method for Strength Properties ofAdhesives inShear by Tens
9、ion Loading of Single-Lap-Joint LaminatedAssembliesE 874 Practice forAdhesive Bonding ofAluminum Facingsto Nonmetallic Honeycomb Core for Shelter PanelsE 1091 Specification for Nonmetallic Honeycomb Core forUse in Shelter Panels2.2 Military Specifications:MIL-I-24768 Insulation, Plastic, Laminated,T
10、hermosetting,Glass-Cloth, Epoxy-Resin22.3 Military Standards:MIL-STD-1916 DOD Preferred Methods for Acceptance ofProduct22.4 Commercial StandardsSAE-AMS-C-9084 Cloth, Glass, Finished for Epoxy ResinLaminates33. Physical Requirements3.1 Working Characteristics:3.1.1 ApplicationThe components of the e
11、poxy resin shallbe readily hand-mixed to a smooth consistency suitable forapplication. It shall be uniform and free of lumps. The resincomponents, once mixed, shall not settle out. The epoxymaterial shall be suitable for the wet-layup impregnation ofSAE-AMS-C-9084 glass cloth and for application to
12、corematerials over the temperature range of 16 to 38C (60 to100F) and at relative humidities of 30 to 75 %.3.1.2 Application LifeThe application life of a 200-g kitof the mixed epoxy system shall be at least 60 min when testedin accordance with 3.1.5. The epoxy shall be considered tohave reached the
13、 end of its application life when the viscosityof this 200-g quantity of mixed adhesive exceeds 20 000centipoise.3.1.3 CuringThe epoxy system shall be capable of curingat 23 6 2C (73 6 4F) in 7 days, or for no longer than3hat1This specification is under the jurisdiction of ASTM Committee E06 onPerfo
14、rmance of Buildings and is the direct responsibility of Subcommittee E06.53on Materials and Processes for Durable Rigidwall Relocatable Structures.Current edition approved Oct. 1, 2003. Published October 2003. Originallyapproved in 1993. Last previous edition appoved in 1998 as E 1556 98.2Available
15、from Standardization Documents Order Desk, Bldg. 4 Section D, 700Robbins Ave., Philadelphia, PA 19111-5094, Attn: NPODS.3Available from Society of Automotive Engineers (SAE), 400 CommonwealthDr., Warrendale, PA 15096-0001.1Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Consho
16、hocken, PA 19428-2959, United States.a temperature of 60 to 66C (140 to 151F), with a curingpressure not to exceed 14 psig. In a 236 3C cure, the curingpressure is not required to be maintained after the first 24 h. Ina236 2C cure, the epoxy material shall develop the propertylevels listed in Table
17、1 within the first 24 h of cure (see 7.3.5).In order to meet the requirements of this specification, theproperty levels listed in Tables 2-4 must be achieved with the7-day cure at 23 6 2C (73 6 4F).3.1.4 Storage LifeThe storage life period of the two partsof the epoxy resin system, when stored in ai
18、rtight containers at23C (73F), shall be at least 12 months from the date ofshipment when tested in accordance with 7.3.5.3.1.5 ViscosityThe viscosity of a 200-g kit of the mixedresin system shall be determined at 23 6 2C (73 6 4F) usinga Brookfield viscometer with a No. 3 spindle at 20 rpm. Aviscosi
19、ty curve shall be determined by taking a readingimmediately after mixing, and every 5 min thereafter until theviscosity exceeds 20 000 centipoise.The viscosity immediatelyafter mixing shall not exceed 14 000 centipoise.3.2 Mechanical PropertiesMechanical properties of testspecimens prepared and test
20、ed as specified in Section 7 shallmeet the respective requirements listed in Tables 2-4.3.3 Instruction SheetThe manufacturer shall provide adated, coded, and titled instruction sheet outlining instructionsfor use of the epoxy system in impregnating and bondingSAE-AMS-C-9084 glass composite skins to
21、 honeycomb cores(Specification E 1091, Types I or II). These instructions shallbe supplied by the manufacturer with the test report whenrequesting qualification (see 6.3) and also with each shipmentof epoxy material (see 9.2). The following information shall beincluded:3.3.1 All of the information l
22、isted in 5.3.1-5.3.11.3.3.2 The application life of the mixed epoxy system at 236 2C (73 6 4F) and 38 6 2C (100 6 4F).3.3.3 Mixing instructions shall be stated in detail for theepoxy resin system in the particular container supplied.3.3.4 Application, impregnating, and curing instructions,including
23、the spreading method, thickness range, andtemperature/relative humidity working limitations.3.3.5 Material Safety Data Sheets and necessary safetyprecautions to be observed throughout all operations.3.3.6 Any other pertinent information relative to the use andstorage of the two-part system (resin an
24、d curing agent) package(see 9.2).4. Significance and Use4.1 Epoxy resin systems used in the repair of composite skinsandwich panels for durable, rigidwall, relocatable sheltersmust have a combination of mechanical property levels andenvironmental resistance that will assure long-term durabilityof th
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