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本文(ASTM D4054-2014 Standard Practice for Qualification and Approval of New Aviation Turbine Fuels and Fuel Additives《鉴定和认证新的航空涡轮燃料和燃料添加剂的标准实践规程》.pdf)为本站会员(boatfragile160)主动上传,麦多课文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

ASTM D4054-2014 Standard Practice for Qualification and Approval of New Aviation Turbine Fuels and Fuel Additives《鉴定和认证新的航空涡轮燃料和燃料添加剂的标准实践规程》.pdf

1、Designation: D4054 09D4054 14 An American National StandardStandard Practice forQualification and Approval of New Aviation Turbine Fuelsand Fuel Additives1This standard is issued under the fixed designation D4054; the number immediately following the designation indicates the year oforiginal adoptio

2、n or, in the case of revision, the year 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.1. Scope Scope*1.1 This practice covers and provides a framework for the qualification

3、and approval of new fuels and new fuel additives foruse in commercial and military aviation gas turbine engines. The practice was developed as a guide by the aviation gas-turbineengine Original Equipment Manufacturers (OEMs) with ASTM International member support. The OEMs are solely responsiblefor

4、approval of a fuel or additive in their respective engines and airframes. For the purpose of this guide, “approval” means“permission to use;” it is not an endorsement of any kind. Standards organizations such as ASTM International (SubcommitteeD02.J0), United Kingdom Ministry of Defence, and the U.S

5、. military list only those fuels and additives that are mutually acceptableto all OEMs. ASTM International and OEM participation in the evaluation or approval procedure does not constitute anendorsement of the fuel or additive.1.2 The OEMs will consider a new fuel or additive based on an established

6、 need or benefit attributed to its use. Upon OEMand regulatory authority approval, the fuel or fuel additive may be listed in fuel specifications such as Pratt General Electric Aviation (GE) Specification No. D50TF2; and Rolls Royce (RR) engine manuals.Subsequent to OEM approval and industry (ASTM)

7、review and ballot, the fuel or fuel additive may be listed in fuel specificationssuch as Specification D1655, Defence Standard 91-91, United States Air Force MIL-DTL-83133, and the United States NavyMIL-DTL-5624. This qualification and approval process has been coordinated with airworthiness and cer

8、tification groups withineach company, the Federal Aviation Administration (FAA), and the European Aviation Safety Agency (EASA).1.3 Units of measure throughout this practice are stated in International System of Units (SI) unless the test method specifiesnon-SI units.1.4 This standard does not purpo

9、rt to 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:2A240/A

10、240M Specification for Chromium and Chromium-Nickel Stainless Steel Plate, Sheet, and Strip for Pressure Vessels andfor General ApplicationsB36/B36M Specification for Brass Plate, Sheet, Strip, And Rolled BarB93/B93M Specification for Magnesium Alloys in Ingot Form for Sand Castings, Permanent Mold

11、Castings, and Die CastingsD56 Test Method for Flash Point by Tag Closed Cup TesterD86 Test Method for Distillation of Petroleum Products at Atmospheric PressureD257 Test Methods for DC Resistance or Conductance of Insulating MaterialsD395 Test Methods for Rubber PropertyCompression SetD412 Test Meth

12、ods for Vulcanized Rubber and Thermoplastic ElastomersTensionD445 Test Method for Kinematic Viscosity of Transparent and Opaque Liquids (and Calculation of Dynamic Viscosity)D471 Test Method for Rubber PropertyEffect of LiquidsD790 Test Methods for Flexural Properties of Unreinforced and Reinforced

13、Plastics and Electrical Insulating Materials1 This practice is under the jurisdiction of ASTM Committee D02 on Petroleum Products, Liquid Fuels, and Lubricants and is the direct responsibility of SubcommitteeD02.03D02.J0.04 on Elemental AnalysisAdditives and Electrical Properties.Current edition app

14、roved Jan. 15, 2012Dec. 1, 2014. Published April 2010February 2015. Originally approved in 1981. Last previous edition approved in 20032009 asD405493(2003).D4054 09. DOI:10.1520/D405409.DOI:10.1520/D4054-14.2 For referencedASTM standards, visit theASTM website, www.astm.org, or contactASTM Customer

15、Service at serviceastm.org. For Annual Book of ASTM Standardsvolume information, refer to the standards Document Summary page on the ASTM website.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 pre

16、vious version. Becauseit may not be technically possible to adequately depict all changes accurately, 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.*A Summary of Ch

17、anges section appears at the end of this standardCopyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States1D924 Test Method for Dissipation Factor (or Power Factor) and Relative Permittivity (Dielectric Constant) of ElectricalInsulating Liquids

18、D1002 Test Method for Apparent Shear Strength of Single-Lap-Joint Adhesively Bonded Metal Specimens by Tension Loading(Metal-to-Metal)D1319 Test Method for Hydrocarbon Types in Liquid Petroleum Products by Fluorescent Indicator AdsorptionD1331 Test Methods for Surface and Interfacial Tension of Solu

19、tions of Paints, Solvents, Solutions of Surface-Active Agents,and Related MaterialsD1414 Test Methods for Rubber O-RingsD1655 Specification for Aviation Turbine FuelsD2240 Test Method for Rubber PropertyDurometer HardnessD2386 Test Method for Freezing Point of Aviation FuelsD2425 Test Method for Hyd

20、rocarbon Types in Middle Distillates by Mass SpectrometryD2624 Test Methods for Electrical Conductivity of Aviation and Distillate FuelsD2717 Test Method for Thermal Conductivity of LiquidsD2887 Test Method for Boiling Range Distribution of Petroleum Fractions by Gas ChromatographyD3241 Test Method

21、for Thermal Oxidation Stability of Aviation Turbine FuelsD3242 Test Method for Acidity in Aviation Turbine FuelD3359 Test Methods for Measuring Adhesion by Tape TestD3363 Test Method for Film Hardness by Pencil TestD3701 Test Method for Hydrogen Content of Aviation Turbine Fuels by Low Resolution Nu

22、clear Magnetic ResonanceSpectrometryD3703 Test Method for Hydroperoxide Number of Aviation Turbine Fuels, Gasoline and Diesel FuelsD3828 Test Methods for Flash Point by Small Scale Closed Cup TesterD3948 Test Method for Determining Water Separation Characteristics of Aviation Turbine Fuels by Portab

23、le SeparometerD4052 Test Method for Density, Relative Density, and API Gravity of Liquids by Digital Density MeterD4066 Classification System for Nylon Injection and Extrusion Materials (PA)D4629 Test Method for Trace Nitrogen in Liquid Petroleum Hydrocarbons by Syringe/Inlet Oxidative Combustion an

24、dChemiluminescence DetectionD5001 Test Method for Measurement of Lubricity of Aviation Turbine Fuels by the Ball-on-Cylinder Lubricity Evaluator(BOCLE)D5291 Test Methods for Instrumental Determination of Carbon, Hydrogen, and Nitrogen in Petroleum Products and LubricantsD5304 Test Method for Assessi

25、ng Middle Distillate Fuel Storage Stability by Oxygen OverpressureD5363 Specification for Anaerobic Single-Component Adhesives (AN)D5972 Test Method for Freezing Point of Aviation Fuels (Automatic Phase Transition Method)D6304 Test Method for Determination of Water in Petroleum Products, Lubricating

26、 Oils, and Additives by Coulometric KarlFischer TitrationD6378 Test Method for Determination of Vapor Pressure (VPX) of Petroleum Products, Hydrocarbons, and Hydrocarbon-Oxygenate Mixtures (Triple Expansion Method)D6379 Test Method for Determination of Aromatic Hydrocarbon Types in Aviation Fuels an

27、d Petroleum DistillatesHighPerformance Liquid Chromatography Method with Refractive Index DetectionD6732 Test Method for Determination of Copper in Jet Fuels by Graphite Furnace Atomic Absorption SpectrometryD6793 Test Method for Determination of Isothermal Secant and Tangent Bulk ModulusD7111 Test

28、Method for Determination of Trace Elements in Middle Distillate Fuels by Inductively Coupled Plasma AtomicEmission Spectrometry (ICP-AES)D7566 Specification for Aviation Turbine Fuel Containing Synthesized HydrocarbonsE411 Test Method for Trace Quantities of Carbonyl Compounds with 2,4-Dinitrophenyl

29、hydrazineE659 Test Method for Autoignition Temperature of Liquid ChemicalsE681 Test Method for Concentration Limits of Flammability of Chemicals (Vapors and Gases)E1269 Test Method for Determining Specific Heat Capacity by Differential Scanning Calorimetry2.2 Federal Specifications:3FED-STD-791 Test

30、ing Method of Lubricants, Liquid Fuels, and Related Products2.3 Department of Defense Specifications:3DOD-L-85645 Lubricant, Dry Film, Molecular BondedMIL-A-8625 Anodic Coatings for Aluminum and Aluminum AlloysMIL-C-83019 Coating, Polyurethane, for Protection of Integral Fuel Tank Sealing Compound3

31、Copies of these documents are available from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia PA 1911-5094 or online athttp:/assist.daps.dla.mil/quicksearch/D4054 142MIL-DTL-5541 Chemical Conversion Coatings on Aluminum and Aluminum AlloysMIL-DTL-5624 Turbine Fu

32、el, Aviation, Grades JP-4 and JP-5MIL-DTL-24441 Paint, Epoxy-Polyamide, General Specification forMIL-PRF-25017 Inhibitor, Corrosion/Lubricity Improver, Fuel SolubleMIL-DTL-25988 Rubber, Fluorosilicone Elastomer, Oil- and Fuel-Resistant, Sheets, Strips, Molded Parts, and Extruded ShapesMIL-DTL-26521

33、Hose Assembly, Nonmetallic, Fuel, Collapsible, Low Temperature with Non-Reusable CouplingsMIL-DTL-83054 Baffle and Inerting Material, Aircraft Fuel TankMIL-DTL-83133 Turbine Fuel, Aviation, Kerosene Type, JP-8 (NATO F-34), NATO F-35, and JP-8+100 (NATO F-37)MIL-H-4495 Hose Assembly, Rubber, Aerial R

34、efuelingMIL-H-17902 Hose, End Fittings and Hose Assemblies, Synthetic Rubber, Aircraft FuelsMIL-HDBK-510-1 Aerospace Fuels CertificationMIL-P-25732 Packing, Preformed, Petroleum Hydraulic Fluid Resistant, Limited Service at 275F (135C)MIL-PRF-370 Hose and Hose Assemblies, Nonmetallic: Elastomeric, L

35、iquid FuelMIL-PRF-6855 Rubber, Synthetic, Sheets, Strips, Molded or Extruded Shapes, General Specification forMIL-PRF-8516 Sealing Compound, Synthetic Rubber, Electric Connectors and Electric Systems, Chemically CuredMIL-PRF-46010 Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting, NATO Code S-

36、1738MIL-PRF-81298 Dye, Liquid for the Detection of Leaks in Aircraft Fuel SystemsMIL-PRF-81733 Sealing and Coating Compound, Corrosion InhibitiveMIL-PRF-87260 Foam Material, Explosion Suppression, Inherently Electrostatically Conductive, for Aircraft Fuel TanksMIL-R-46082 Retaining Compounds, Single

37、 Component, AnaerobicMIL-S-85334 Sealing Compound, Noncuring, Low Consistency, Silicone, Groove Injection, for Integral Fuel TanksMIL-DTL-5578 Tanks, Fuel, Aircraft, Self-SealingMMM-A-132 Adhesives, Heat Resistant, Airframe Structural, Metal to MetalQPL-25017 Qualified Products List for MIL-PRF-2501

38、7 (Inhibitor, Corrosion/Lubricity Improver, Fuel Soluble)2.4 SAE International:4SAE-AMS-2410 Plating, Silver Nickel Strike, High BakeSAE-AMS-2427 Aluminum Coating, Ion Vapor DepositionSAE-AMS-3215 Acrylonitrile Butadiene (NBR) Rubber Aromatic Fuel Resistant 6575SAE-AMS-3265 Sealing Compound, Polysul

39、fide (T) Rubber, Fuel Resistant, Non-chromated Corrosion Inhibiting forIntermittent Use to 360 F (182 C)SAE-AMS-3276 Sealing Compound, Integral Fuel Tanks and General Purpose, Intermittent Use to 360 F (182 C)SAE-AMS-3277 Sealing Compound, Polythioether Rubber Fast Curing Integral Fuel Tanks And Gen

40、eral Purpose, IntermittentUse to 400 F (204 C)SAE-AMS-3278 Sealing and Coating Compound: Polyurethane (PUR) Fuel Resistant High Tensile Strength/Elongation forIntegral Fuel Tanks/Fuel Cavities/General PurposSAE-AMS-3279 Sealing Compound, Sprayable, for Integral Fuel Tanks and Fuel Cell Cavities, for

41、 Intermittent Use to 350 F(177 C)SAE-AMS-3281 Sealing Compound, Polysulfide (T) Synthetic Rubber for Integral Fuel Tank and Fuel Cell Cavities LowDensity for Intermittent Use to 360 F (182 C)SAE-AMS-3283 Sealing Compound, Polysulfide Non-Curing, Groove Injection Temperature and Fuel ResistantSAE-AMS

42、-3361 Silicone Potting Compound, Elastomeric, Two-Part, General Purpose, 150 to 400 Poise (15 to 40 Pas)ViscositySAE-AMS-3375 Adhesive/Sealant, Fluorosilicone, Aromatic Fuel Resistant, One-Part Room Temperature VulcanizingSAE-AMS-3376 Sealing Compound, Non-Curing, Groove Injection Temperature and Fu

43、el ResistantSAE-AMS-4017 Aluminum Alloy Sheet and Plate, 2.5Mg 0.25Cr (5052H34) Strain-Hardened, Half-Hard, and StabilizedSAE-AMS-4027 AluminumAlloy, Sheet and Plate 1.0Mg 0.60Si 0.28Cu 0.20Cr (6061; T6 Sheet, T651 Plate) Solutionand Precipitation Heat TreatedSAE-AMS-4029 AluminumAlloy Sheet and Pla

44、te 4.5Cu 0.85SI 0.80Mn 0.50Mg (2014; T6 Sheet, T651 Plate) Solutionand Precipitation Heat TreatedSAE-AMS-4037 AluminumAlloy, Sheet and Plate 4.4Cu 1.5Mg 0.60 Mn (2024; T3 Flat Sheet, T351 Plate) Solution HeatTreatedSAE-AMS-4107 Aluminum Alloy, Die Forgings (7050T74) Solution Heat Treated and Overage

45、dSAE-AMS-4260 Aluminum Alloy, Investment Castings 7.0Si 0.32Mg (356.0T6) Solution and Precipitation Heat TreatedSAE-AMS-4750 Solder, TinLead 45Sn 55PbSAE-AMS-4751 TinLead Eutectic 63Sn 37PbSAE-AMS-4901 Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 70.0 ksi (485 MPa)4 Available from SA

46、E International, 400 Commonwealth Dr., Warrendale, Pennsylvania 15096, http:/www.sae.org/servlets/indexD4054 143SAE-AMS-4915 Titanium Alloy Sheet, Strip, and Plate 8Al 1V IMo Single AnnealedSAE-AMS-5330 Steel Castings, Investment, 0.80Cr 1.8Ni 0.35Mo (0.380.46C) (SAE 4340 Modified) AnnealedSAE-AMS-5

47、338 Steel, Investment Castings 0.95Cr 0.20Mo (0.350.45C) (SAE 4140 Mod) Normalized or Normalized andTemperedSAE-AMS-5504 Steel, Corrosion and HeatResistant, Sheet, Strip, and Plate 12.5Cr (SAE 51410) AnnealedSAE-AMS-5525 Steel, Corrosion and Heat Resistant, Sheet, Strip, and Plate 15Cr 25.5Ni 1.2Mo

48、2.1Ti 0.006B 0.30V1800 F (982 C) Solution Heat TreatedSAE-AMS-5604 Steel, Corrosion Resistant, Sheet, Strip, and Plate 16.5Cr 4.0Ni 4.0Cu 0.30 Solution Heat Treated,Precipitation HardenableSAE-AMS-5613 Steel, Corrosion and Heat Resistant, Bars, Wire, Forgings, Tubing, and Rings 12.5Cr (SAE 51410) An

49、nealedSAE-AMS-5643 Steel, Corrosion Resistant, Bars, Wire, Forgings, Tubing, and Rings 16Cr 4.0Ni 0.30Cb 4.0Cu SolutionHeat Treated, Precipitation HardenableSAE-AMS-5688 Steel, CorrosionResistant, Wire 18Cr9.0Ni (SAE 30302) Spring TemperSAE-AMS-5737 Steel, Corrosion and HeatResistant, Bars, Wire, Forgings, and Tubing 15Cr 25.5Ni 1.2Mo 2.1Ti 0.006B 0.30V Consumable Electrode Melted, 1650 F (899 C) Solution and Precipitation Heat TreatedSAE-AMS-6277 Steel Bars, Forgings, and

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