ASTM E1556-2008 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的标准规范》.pdf
《ASTM E1556-2008 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的标准规范》.pdf》由会员分享,可在线阅读,更多相关《ASTM E1556-2008 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的标准规范》.pdf(9页珍藏版)》请在麦多课文档分享上搜索。
1、Designation: E 1556 08Standard 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 () 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 shall
4、 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 humidi
5、ty 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 rega
6、rded 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 appropri
7、ate safety and health practicesand determine the applicability of regulatory limitations priorto use.2. Referenced Documents2.1 ASTM Standards:2C 297/C 297M Test Method for Flatwise Tensile Strengthof Sandwich ConstructionsD 792 Test Methods for Density and Specific Gravity (Rela-tive Density) of Pl
8、astics by DisplacementD 2344/D 2344M Test Method for Short-Beam Strength ofPolymer Matrix Composite Materials and Their LaminatesD 2584 Test Method for Ignition Loss of Cured ReinforcedResinsD 2734 Test Methods for Void Content of Reinforced Plas-ticsE 874 Practice forAdhesive Bonding ofAluminum Fac
9、ingsto Nonmetallic Honeycomb Core for Shelter PanelsD 3165 Test Method for Strength Properties ofAdhesives inShear by Tension Loading of Single-Lap-Joint LaminatedAssembliesE 1091 Specification for Nonmetallic Honeycomb Core forUse in Shelter Panels2.2 Military Specifications:3MIL-I-24768 Insulation
10、, Plastic, Laminated,Thermosetting,Glass-Cloth, Epoxy-Resin2.3 Military Standards:3MIL-STD-129 Military Marking for Shipping and StorageMIL-STD-1916 DOD Preferred Methods for Acceptance ofProduct2.4 Commercial Standards:4SAE-AMS-C-9084 Cloth, Glass, Finished for Epoxy ResinLaminates3. Physical Requi
11、rements3.1 Working Characteristics:3.1.1 ApplicationThe components of the epoxy 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
12、wet-layup impregnation ofSAE-AMS-C-9084 glass cloth and for application to 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 teste
13、din accordance with 3.1.5. The epoxy shall be considered to1This specification is under the jurisdiction of ASTM Committee E06 onPerformance of Buildings and is the direct responsibility of Subcommittee E06.53on Materials and Processes for Durable Rigidwall Relocatable Structures.Current edition app
14、roved Nov. 1, 2008. Published December 2008. Originallyapproved in 1993. Last previous edition approved in 2003 as E 1556 03.2For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Customer Service at serviceastm.org. For Annual Book of ASTMStandards volume information,
15、refer to the standards Document Summary page onthe ASTM website.3Available from Standardization Documents Order Desk, DODSSP, Bldg. 4,Section D, 700 Robbins Ave., Philadelphia, PA 19111-5098, http:/www.dodssp.daps.mil.4Available from Society of Automotive Engineers (SAE), 400 CommonwealthDr., Warren
16、dale, PA 15096-0001, http:/www.sae.org.1Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.have reached the end of its application life when the viscosityof this 200-g quantity of mixed adhesive exceeds 20 000centipoise.3.1.3 CuringThe e
17、poxy system shall be capable of curingat 23 6 2C (73 6 4F) in 7 days, or for no longer than3hata 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
18、material shall develop the propertylevels listed in Table 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
19、 the two partsof the epoxy resin system, when stored in airtight 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 Broo
20、kfield viscometer with a No. 3 spindle at 20 rpm. Aviscosity 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 Properti
21、esMechanical properties of testspecimens prepared and tested 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 impre
22、gnating and bondingSAE-AMS-C-9084 glass composite skins to 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 i
23、nformation shall beincluded:3.3.1 All of the information listed 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 App
24、lication, impregnating, and curing instructions,including 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 relat
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