ASTM D7465 D7465M-2015 red 5040 Standard Specification for Ethylene Propylene Diene Terpolymer (EPDM) Sheet Used In Geomembrane Applications《土工膜用片状乙烯-丙烯-二烯三元共聚物 (EPDM) 的标准规格》.pdf

上传人:周芸 文档编号:525554 上传时间:2018-12-04 格式:PDF 页数:7 大小:81.97KB
下载 相关 举报
ASTM D7465 D7465M-2015 red 5040 Standard Specification for Ethylene Propylene Diene Terpolymer (EPDM) Sheet Used In Geomembrane Applications《土工膜用片状乙烯-丙烯-二烯三元共聚物 (EPDM) 的标准规格》.pdf_第1页
第1页 / 共7页
ASTM D7465 D7465M-2015 red 5040 Standard Specification for Ethylene Propylene Diene Terpolymer (EPDM) Sheet Used In Geomembrane Applications《土工膜用片状乙烯-丙烯-二烯三元共聚物 (EPDM) 的标准规格》.pdf_第2页
第2页 / 共7页
ASTM D7465 D7465M-2015 red 5040 Standard Specification for Ethylene Propylene Diene Terpolymer (EPDM) Sheet Used In Geomembrane Applications《土工膜用片状乙烯-丙烯-二烯三元共聚物 (EPDM) 的标准规格》.pdf_第3页
第3页 / 共7页
ASTM D7465 D7465M-2015 red 5040 Standard Specification for Ethylene Propylene Diene Terpolymer (EPDM) Sheet Used In Geomembrane Applications《土工膜用片状乙烯-丙烯-二烯三元共聚物 (EPDM) 的标准规格》.pdf_第4页
第4页 / 共7页
ASTM D7465 D7465M-2015 red 5040 Standard Specification for Ethylene Propylene Diene Terpolymer (EPDM) Sheet Used In Geomembrane Applications《土工膜用片状乙烯-丙烯-二烯三元共聚物 (EPDM) 的标准规格》.pdf_第5页
第5页 / 共7页
亲,该文档总共7页,到这儿已超出免费预览范围,如果喜欢就下载吧!
资源描述

1、Designation: D7465 08D7465/D7465M 15Standard Specification forEthylene Propylene Diene Terpolymer (EPDM) Sheet Used InGeomembrane Applications1This standard is issued under the fixed designation D7465;D7465/D7465M; the number immediately following the designation indicatesthe year of original adopti

2、on or, in the case of revision, the year of last revision. A number in parentheses indicates the year of lastreapproval. A superscript epsilon () indicates an editorial change since the last revision or reapproval.1. Scope1.1 This specification covers flexible sheet made from ethylene propylene dien

3、e terpolymer (EPDM) geomembrane intended foruse in geotechnical and geoenvironmental applications. The tests and property limits used to characterize the sheet are values toensure minimum quality for the intended use. The vulcanized rubber sheet may be non-reinforced, fabric or scrim reinforcedreinf

4、orced.1.2 In place geomembrane design criteria, such as field seaming strength, and material compatibility, among others, are factorsthat must be considered but are beyond the scope of this specification.1.3 The values stated in either SI units or inch-pound units are to be regarded separately as th

5、e standard. The values stated inparentheses are for information only. each system may not be exact equivalents; therefore, each system shall be used independentlyof the other. Combining values from the two systems may result in non-conformance with the standard.1.4 This standard does not purport to

6、address all of the safety concerns, if any, associated with its use. It is the responsibilityof the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatorylimitations prior to use.2. Referenced Documents2.1 ASTM Standards:2D412 Test Me

7、thods for Vulcanized Rubber and Thermoplastic ElastomersTensionD471 Test Method for Rubber PropertyEffect of LiquidsD518 Test Method for Rubber DeteriorationSurface Cracking (Withdrawn 2007)3D573 Test Method for RubberDeterioration in an Air OvenD624 Test Method for Tear Strength of Conventional Vul

8、canized Rubber and Thermoplastic ElastomersD751 Test Methods for Coated FabricsD1149 Test Methods for Rubber DeteriorationCracking in an Ozone Controlled EnvironmentD1204 Test Method for Linear Dimensional Changes of Nonrigid Thermoplastic Sheeting or Film at Elevated TemperatureD1418 Practice for R

9、ubber and Rubber LaticesNomenclatureD2137 Test Methods for Rubber PropertyBrittleness Point of Flexible Polymers and Coated FabricsD4439 Terminology for GeosyntheticsD4833D4833/D4833M Test Method for Index Puncture Resistance of Geomembranes and Related ProductsD5884 Test Method for Determining Tear

10、ing Strength of Internally Reinforced GeomembranesD7004D7004/D7004M Test Method for Grab Tensile Properties of Reinforced GeomembranesD7635/D7635M Test Method for Measurement of Thickness of Coatings Over Fabric ReinforcementG151 Practice for Exposing Nonmetallic Materials in Accelerated Test Device

11、s that Use Laboratory Light SourcesG155 Practice for Operating Xenon Arc Light Apparatus for Exposure of Non-Metallic Materials3. Terminology3.1 Definitions:3.1.1 For definitions of other geosynthetic terms used in this guide, refer to Terminology D4439.1 This specification is under the jurisdiction

12、 of ASTM Committee D35 on Geosynthetics and is the direct responsibility of Subcommittee D35.10 on Geomembranes.Current edition approved July 1, 2008May 1, 2015. Published October 2008May 2015. Originally approved in 2008. Last previous edition approved in 2008 as D746508.DOI: 10.1520/D7465-08.10.15

13、20/D7465_D7465M-15.2 For referencedASTM standards, visit theASTM website, www.astm.org, or contactASTM Customer Service at serviceastm.org. For Annual Book of ASTM Standardsvolume information, refer to the standards Document Summary page on the ASTM website.3 The last approved version of this histor

14、ical standard is referenced on www.astm.org.This document is not an ASTM standard and is intended only to provide the user of an ASTM standard an indication of what changes have been made to the previous version. Becauseit may not be technically possible to adequately depict all changes accurately,

15、ASTM recommends that users consult prior editions as appropriate. In all cases only the current versionof the standard as published by ASTM is to be considered the official document.Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States13.1.

16、2 composite, nfactory laminated non-woven geotextile and EPDM.3.1.3 EPDM, nterpolymer of ethylene, propylene, and diene with the residual unsaturated portion of the diene in the sidechain. D14183.1.3 composite, nfactory laminated non-woven geotextile and EPDM.4. Classification4.1 Types describe the

17、sheet construction:4.1.1 Type INon-reinforced.4.1.2 Type IIScrim (or fabric) internally reinforced.5. Materials and Manufacture5.1 The sheet shall be formulated from EPDM polymers and other compounding ingredients. EPDM shall be the principalpolymer used in the sheet and shall be greater than 95 % o

18、f the total polymer content.5.2 To make seams and repairs, the sheet shall be capable of being bonded watertight to itself and the supplier or fabricator shallrecommend suitable methods.6. Physical Properties and Requirements6.1 The sheet shall conform to the physical requirements prescribed in Tabl

19、e 1.6.2 The tolerance for time conditions (aging, weathering, and so forth) is 615 min or 61 % of the period; whichever is greater,unless otherwise specified.6.3 Tolerances for temperature shall be 62 C (64 F).62C 64F.7. Dimensions7.1 The width and length of the sheet shall be agreed upon between th

20、e purchaser and the supplier.7.1.1 The width and length tolerance shall be +3 %, -0 %.7.2 The thickness tolerance shall be +15 %, -10 % of the thickness agreed upon between the purchaser and supplier, but in nocase shall the thickness be less than the minimum listed in Table 1.8. Workmanship, Finish

21、, and Appearance8.1 The sheet, including the full width of factory seams if present, shall be fully adhered, watertight, and visibly free of pinholes,particles of foreign matter, undispersed raw material or other manufacturing defects that might affect serviceability. If the numberof irregularities

22、in the form of pockmarks (see Note 1Note 1) ) appear excessive on the sheet (or portion thereof), then its rejectionshall be negotiated between involved parties.NOTE 1Pockmarks are oblong depressions, cavities or craters on the surface of the sheet that have an approximate surface dimension of 3.2 b

23、y 1.6mm 1/8 by 116 in., and have a maximum depth approaching one half of the sheet thickness.8.2 Edges of the sheets shall be straight and flat so that they may be seamed to one another without fishmouthing.NOTE 1Pockmarks are oblong depressions, cavities or craters on the surface of the sheet that

24、have an approximate surface dimension of 3.2 by 1.6mm (1/8 by 1/16 in.), and have a maximum depth approaching one half of the sheet thickness.9. Test Methods9.1 DimensionsTest Methods D751, after permitting the sheet to relax at 2323 6 2C (73.473.4 6 4F)4F for 1 hourh6 15 min.9.2 Thickness, Sheet Ov

25、erallFrom across the full width of the unbuffed sheet, take three samples, 300 by 300 mm (11 by 1ft).ft. Measure the thickness of each corner. Refer to Test MethodMethods D412 for Type I sheet and Test MethodMethods D751for Type II sheet.9.3 Thickness of Coating Over Scrim (Reinforcing Fabric)Optica

26、l Methodsee Annex A1Annex A1. .9.4 Breaking StrengthTest Methods D751, Grab Method.9.5 Tensile StrengthTest Methods D412, Die C.9.6 Puncture ResistanceTest Method D4833D4833/D4833M.9.7 Elongation, UltimateTest Methods D412, Die C.9.8 Elongation at Fabric Break, UltimateTest MethodMethods D751, Grab

27、Method, 50 mm (2 in.)2 in. per minute jawseparation rate.9.9 Tensile SetTest Methods D412, Method A, Die C, 50 % elongation.D7465/D7465M 152TABLE 1 Physical Requirements for EPDM SheetType ASTM I IIThickness, min, mm (in.):Sheet-overall D412 Type 1 1.016 (0.040) 1.016 (0.040)Coating over scrim or fa

28、bric D7004 Type 11 . 0.38 (0.015)Breaking Strength, min, N (lbf) D7004 Grab Method . 400 (90)Tensile strength, min, MPa (psi) D412 Die C 9.0 (1305) .Puncture Resistance N (lbs) Min. D4833 133 (30) 270 (60)Elongation, ultimate, min % D412 Die C 300 250AElongation fabric break, ultimate, D7004, Grabmi

29、n, % Method, 50 mmMachine direction (2 in.)per15Cross direction minute jawseparation rate15Tensile set, max D412 Method A, Die C 10 .Tear resistance, min, kN/m (lbf/in.) D624 Die C 26.27 (150) .Tearing strength, min, N (lbf) D7004, B-Tongue . 45 (10Brittleness point, max C (F) D2137 45 (49) 45 (49)O

30、zone resistance, no cracks D1149 pass passHeat aging: D573Breaking strength, min, N (lbf) D7004 356 (80)Tensile strength, min, mPa (psi) D412 Method A, Die C 8.3 (1205) .Elongation, ultimate, min, % D412 Die C 200 200ATear resistance, min, kN/m (lbf/in) D624 Die C 21.9 (125) .Linear dimensional chan

31、ge, maz, % D1204 1 1Water absorption, max, mass, % D471 8,2 8, 2AAccelerated Weathering: G151 and G155Visual inspection D518 pass passPRFSE, min, % 30 .Elongation, ultimate, min, % 200 .TABLE 1 Physical Requirements for EPDM SheetProperty ASTM Nominal SheetThicknessType I Type IIThickness, min, mm i

32、n.:Sheet-overall D412 1.14 0.0451.52 0.060D751 1.14 0.0451.52 0.060Coating over scrim or fabric D7635/D7635M 1.14 0.0451.52 0.060. 0.38 0.0150.59 0.022Breaking Strength, min, N lbf D7004/D7004M Grab Method 1.14 0.0451.52 0.060. 400 90400 90Tensile strength, min, MPa psi D412 Die C 1.14 0.0451.52 0.0

33、609.0 13059.0 1305.Puncture Resistance N lbs Min. D4833/D4833M 1.14 0.0451.52 0.060133 30178 40270 60350 80Elongation, ultimate, min % D412 Die C 1.14 0.0451.52 0.060300300250A250AElongation fabric break, ultimate, min, %D7004/D7004M, Grab Method,50 mm 2 in. per minutejaw separation rateMachine dire

34、ction 1.14 0.0451.52 0.0601515Cross direction 1.14 0.0451.52 0.0601515Tensile set, max D412 Method A, Die C 1.14 0.0451.52 0.0601010.Tear resistance, min, kN/m lbf/in. D624 Die C 1.14 0.0451.52 0.06026.27 15040.28 230.Tearing strength, min, N lbf D5884 1.14 0.0451.52 0.060. 580 130750 170Brittleness

35、 point, max C F D2137 1.14 0.0451.52 0.06045 4945 4945 4945 49Ozone resistance, no cracks D1149 1.14 0.0451.52 0.060passpasspasspassHeat Aging: D573Breaking strength, min, N lbf D7004/D7004M 1.14 0.0451.52 0.060356 80888 200Tensile strength, min, MPa psi D412 Method A, Die C 1.14 0.0451.52 0.0608.3

36、12058.3 1205.Elongation, ultimate, min, % D412 Die C 1.14 0.0451.52 0.060200200200A200AD7465/D7465M 1539.10 Tear ResistanceTest Method D624, Die C.9.11 Tearing StrengthTest Methods D751, B-Tongue Tear.9.12 Brittleness PointTest Methods D2137.9.13 Ozone ResistanceTest MethodMethods D1149, Terminology

37、 D4439. Inspect at 7 magnification on specimens exposedto 100 mPa (11 105 psi)psi ozone in air at 4040 6 2C (104104 6 4F).4F. Elongate Type I specimens 50 % for 1666 1.66 hourh exposure. And Type II specimens must be wrapped around a 75 mm (3 in.)3 in. diameter mandrel for 166 6 1.66hourh exposure.

38、The required specimen width is 25 mm (1 in.).1 in.9.14 Heat AgingTest Method D573. Age sheet at 116116 6 2C (240240 6 4F)4F for 670 6 6.7 h . h. Specimens arethen cut from the aged sheet for testing of breaking strength, tensile strength, elongation and tear resistance.9.15 Linear Dimensional Change

39、Test Method D1204.9.16 Water AbsorptionTest Method D471, at 7070 6 2C (158158 6 4F)4F for 166 6 1.66 h.9.17 Laboratory Accelerated WeatheringAccelerated weathering tests shall be performed in accordance with Practices G151and G155. These tests are performed on the intact sheet with the weathering si

40、de facing the lamps. Mount specimens for exposureunder no strain. After exposure the specimens shall be removed and inspected immediately for cracks and crazing at 10 % strainin the bent loop configuration in accordance with Test Method D518 under 7 magnifications. A specimen is rated “pass” if nocr

41、acks or crazing are observed. In addition, for Type I sheet, determine tensile strength and ultimate elongation after exposure tolaboratory accelerated weathering. Calculate the specimen percent retained fractional strain energy (PRFSE):PRFSE5 Tensile Strength3Elongation! agedTensile Strength3Elonga

42、tion! original 31009.18 Tbe Xenon-Arc exposure devices shall be operated in accordance with Practices G151 and G155 and the followingcondtions:Filter type: Daylight FilterIrradiance: 0.35 to 0.70 W/(m2. nm) at 340 nm: 0.02 W/(m2. nm) maximum0.02 W/(m2. nm) maximum allowed fluctuationallowed fluctuat

43、ion(42 to 84 W/m2at 300 to 400 nm: 2 W/m2 maximum allowed fluctuation)2 W/m2 maximum allowed fluctuation)Cycle: 690 min 15 min light, 30 min light plus watersprayplus water sprayUninsulated black panel 80 C 2.5 C maximum allowedUninsulated black paneltemp:80 2.5C maximum allowed fluctuation176 4F ma

44、ximum allowed fluctuationtemp: fluctuation ( 176 F 4 F maximumallowed fluctuation)Chamber air temperature 50 C 2 C maximum allowedChamber air temperature(if controlled)50 2C maximum allowed fluctuation(if controlled) fluctuationRelative humidity: 50 %; 5% maximum allowedRelative humidity: 50 %; 5 %

45、maximum allowed fluctuationfluctuationProperty ASTM Nominal SheetThicknessType I Type IITear resistance, min, kN/m lbf/in. D624 Die C 1.14 0.0451.52 0.06021.9 12537.3 213.Linear dimensional change, max, % D1204 1.14 0.0451.52 0.0601111Water absorption, max, mass, % D471 1.14 0.0451.52 0.0608, 28, 28

46、, 2A8, 2ALaboratory Accelerated Weathering: G151 and G155Visual Inspection D518 1.14 0.0451.52 0.060No cracksNo cracksNo cracksNo cracksPRFSE, min, % 1.14 0.0451.52 0.0603030.Elongation, ultimate, min, % 1.14 0.0451.52 0.060200200.A Specimens to be prepared from coating rubber compound, vulcanized i

47、n a similar method to the reinforced products.D7465/D7465M 154Spray Water: Deionized: refer to Practice G155,Section 6.6.1for temperatureof the waterSpray water: Deionized: refer to Practice G155,Section 6.6.1for temperatureof the waterSpecimen Every 315 KJ(m2.nm) at 340 nmSpecimen repositioning(if

48、required):Every 315 kJ (m2.nm) at 340 nm(37.8 MJ/m2 at 300 to 400 nm)repositioning (37.8 MJ/m2 at 300 to 400 nm)(if required):Exposure duration: 5040 KJ(m2.nm) at 340 nmExposure duration: 5040 kJ (m2.nm) at 340 nm(604.8 MJ/m2 at 300 to 400 nm).10. Inspection and Special Testing10.1 The manufacturer shall inspect and test production to ensure compliance of the product with this specification.11. Rejection and Resubmittal11.1 Failure to conform to any one of the requirements prescribed in this specification shall constitute grounds for rejection.Rejection sh

展开阅读全文
相关资源
猜你喜欢
  • AECMA PREN 2867-1992 Aerospace Series Nuts Anchor Self-Locking Floating One Lug with Counterbore in Heat Resisting Steel MoS2 Lubricated Classification  1 110 MPa (at Ambient Tempe.pdf AECMA PREN 2867-1992 Aerospace Series Nuts Anchor Self-Locking Floating One Lug with Counterbore in Heat Resisting Steel MoS2 Lubricated Classification 1 110 MPa (at Ambient Tempe.pdf
  • AECMA PREN 2868-1993 Aerospace Series Nuts Hexagonal Slotted Castellated Normal Height Normal Across Flats in Heat Resisting Steel Silver Plated Classification  1 100 MPa (at Ambie.pdf AECMA PREN 2868-1993 Aerospace Series Nuts Hexagonal Slotted Castellated Normal Height Normal Across Flats in Heat Resisting Steel Silver Plated Classification 1 100 MPa (at Ambie.pdf
  • AECMA PREN 2869-1993 Aerospace Series Nuts Hexagonal Slotted Castellated Normal Height Normal Across Flats in Heat Resisting Steel Passivated Classification  1 100 MPa (at Ambient .pdf AECMA PREN 2869-1993 Aerospace Series Nuts Hexagonal Slotted Castellated Normal Height Normal Across Flats in Heat Resisting Steel Passivated Classification 1 100 MPa (at Ambient .pdf
  • AECMA PREN 2870-1990 Aerospace Series Bolts Bihexagonal Normal Head Close Tolerance Normal Shank Short Thread in Titanium Alloy Anodized MoS2 Lubricated Classification 1100 MPa (at.pdf AECMA PREN 2870-1990 Aerospace Series Bolts Bihexagonal Normal Head Close Tolerance Normal Shank Short Thread in Titanium Alloy Anodized MoS2 Lubricated Classification 1100 MPa (at.pdf
  • AECMA PREN 2874-1992 Aerospace Series Bolts Large Bihexagonal Head Close Tolerance Normal Shank Medium Length Thread in Nickel Alloy Passivated Classification  1 550 MPa (at Ambien.pdf AECMA PREN 2874-1992 Aerospace Series Bolts Large Bihexagonal Head Close Tolerance Normal Shank Medium Length Thread in Nickel Alloy Passivated Classification 1 550 MPa (at Ambien.pdf
  • AECMA PREN 2876-1995 Aerospace Series Nuts Hexagon Plain Reduced Height Normal Across Flats in Aluminium Alloy Anodized Classification  450 MPa (at Ambient Temperature) 120 Degrees.pdf AECMA PREN 2876-1995 Aerospace Series Nuts Hexagon Plain Reduced Height Normal Across Flats in Aluminium Alloy Anodized Classification 450 MPa (at Ambient Temperature) 120 Degrees.pdf
  • AECMA PREN 2878-1998 Aerospace Series Nuts Anchor Self-Locking Air Resistant Sealing Floating Two Lug With Counterbore in Alloy Steel Cadmium Plated MoS2 Lubricated Classification .pdf AECMA PREN 2878-1998 Aerospace Series Nuts Anchor Self-Locking Air Resistant Sealing Floating Two Lug With Counterbore in Alloy Steel Cadmium Plated MoS2 Lubricated Classification .pdf
  • AECMA PREN 2879-1998 Aerospace Series Nuts Anchor Self-Locking Fuel Resistant Sealing Floating Two Lug With Counterbore in Corrosion Resisting Steel Passivated MoS2 Lubricated Clas.pdf AECMA PREN 2879-1998 Aerospace Series Nuts Anchor Self-Locking Fuel Resistant Sealing Floating Two Lug With Counterbore in Corrosion Resisting Steel Passivated MoS2 Lubricated Clas.pdf
  • AECMA PREN 2880-1998 Aerospace Series Nuts Anchor Self-Locking Fuel Resistant Sealing Floating Two Lug With Counterbore in Alloy Steel Cadmium Plated MoS2 Lubricated Classification.pdf AECMA PREN 2880-1998 Aerospace Series Nuts Anchor Self-Locking Fuel Resistant Sealing Floating Two Lug With Counterbore in Alloy Steel Cadmium Plated MoS2 Lubricated Classification.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > ASTM

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1