ASTM D1655-2010 Standard Specification for Aviation Turbine Fuels《航空涡轮机燃料的标准规范》.pdf

1、Designation: D1655 10An American National StandardStandard Specification forAviation Turbine Fuels1This standard is issued under the fixed designation D1655; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year of last revision

2、. 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. Scope*1.1 This specification covers the use of purchasing a

3、genciesin formulating specifications for purchases of aviation turbinefuel under contract.1.2 This specification defines specific types of aviationturbine fuel for civil use in the operation and certification ofaircraft and describes fuels found satisfactory for the operationof aircraft and engines.

4、 The specification can be used as astandard in describing the quality of aviation turbine fuels fromthe refinery to the aircraft.1.3 This specification does not include all fuels satisfactoryfor aviation turbine engines. Certain equipment or conditionsof use may permit a wider, or require a narrower

5、, range ofcharacteristics than is shown by this specification.1.4 Aviation turbine fuels defined by this specification maybe used in other than turbine engines that are specificallydesigned and certified for this fuel.1.5 This specification no longer includes wide-cut aviationturbine fuel (Jet B). F

6、AA has issued a Special AirworthinessInformation Bulletin which now approves the use of Specifi-cation D6615 to replace Specification D1655 as the specifica-tion for Jet B and refers users to this standard for reference.1.6 The values stated in SI units are to be regarded asstandard. No other units

7、of measurement are included in thisstandard.2. Referenced Documents2.1 ASTM Standards:2D56 Test Method for Flash Point by Tag Closed Cup TesterD86 Test Method for Distillation of Petroleum Products atAtmospheric PressureD93 Test Methods for Flash Point by Pensky-MartensClosed Cup TesterD129 Test Met

8、hod for Sulfur in Petroleum Products (Gen-eral Bomb Method)D130 Test Method for Corrosiveness to Copper from Pe-troleum Products by Copper Strip TestD156 Test Method for Saybolt Color of Petroleum Products(Saybolt Chromometer Method)D240 Test Method for Heat of Combustion of LiquidHydrocarbon Fuels

9、by Bomb CalorimeterD323 Test Method for Vapor Pressure of Petroleum Prod-ucts (Reid Method)D381 Test Method for Gum Content in Fuels by Jet Evapo-rationD445 Test Method for Kinematic Viscosity of Transparentand Opaque Liquids (and Calculation of Dynamic Viscos-ity)D1266 Test Method for Sulfur in Pet

10、roleum Products(Lamp Method)D1298 Test Method for Density, Relative Density (SpecificGravity), or API Gravity of Crude Petroleum and LiquidPetroleum Products by Hydrometer MethodD1319 Test Method for Hydrocarbon Types in LiquidPetroleum Products by Fluorescent Indicator AdsorptionD1322 Test Method f

11、or Smoke Point of Kerosine andAviation Turbine FuelD1405 Test Method for Estimation of Net Heat of Combus-tion of Aviation FuelsD1660 Method of Test for Thermal Stability of AviationTurbine Fuels3D1840 Test Method for Naphthalene Hydrocarbons inAvia-tion Turbine Fuels by Ultraviolet Spectrophotometr

12、yD2276 Test Method for Particulate Contaminant inAviationFuel by Line SamplingD2386 Test Method for Freezing Point of Aviation FuelsD2622 Test Method for Sulfur in Petroleum Products byWavelength Dispersive X-ray Fluorescence SpectrometryD2624 Test Methods for Electrical Conductivity ofAviationand D

13、istillate FuelsD2887 Test Method for Boiling Range Distribution ofPetroleum Fractions by Gas ChromatographyD2892 Test Method for Distillation of Crude Petroleum1This specification is under the jurisdiction of ASTM Committee D02 onPetroleum Products and Lubricants and is the direct responsibility of

14、SubcommitteeD02.J0.01 on Jet Fuel Specifications.Current edition approved July 1, 2010. Published August 2010. Originallyapproved in 1959. Last previous edition approved in 2009 as D165509a. DOI:10.1520/D1655-10.2For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Cus

15、tomer Service at serviceastm.org. For Annual Book of ASTMStandards volume information, refer to the standards Document Summary page onthe ASTM website.3Withdrawn. The last approved version of this historical standard is referencedon www.astm.org.1*A Summary of Changes section appears at the end of t

16、his standard.Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.(15-Theoretical Plate Column)D3120 Test Method for Trace Quantities of Sulfur in LightLiquid Petroleum Hydrocarbons by Oxidative Microcou-lometryD3227 Test Method for (Thiol

17、 Mercaptan) Sulfur in Gaso-line, Kerosine, Aviation Turbine, and Distillate Fuels(Potentiometric Method)D3240 Test Method for Undissolved Water In AviationTurbine FuelsD3241 Test Method for Thermal Oxidation Stability ofAviation Turbine FuelsD3242 Test Method for Acidity in Aviation Turbine FuelD333

18、8 Test Method for Estimation of Net Heat of Combus-tion of Aviation FuelsD3343 Test Method for Estimation of Hydrogen Content ofAviation FuelsD3701 Test Method for Hydrogen Content of AviationTurbine Fuels by Low Resolution Nuclear Magnetic Reso-nance SpectrometryD3828 Test Methods for Flash Point b

19、y Small Scale ClosedCup TesterD3948 Test Method for Determining Water SeparationCharacteristics of Aviation Turbine Fuels by PortableSeparometerD4052 Test Method for Density, Relative Density, and APIGravity of Liquids by Digital Density MeterD4057 Practice for Manual Sampling of Petroleum andPetrol

20、eum ProductsD4171 Specification for Fuel System Icing InhibitorsD4176 Test Method for Free Water and Particulate Con-tamination in Distillate Fuels (Visual Inspection Proce-dures)D4294 Test Method for Sulfur in Petroleum and PetroleumProducts by Energy Dispersive X-ray Fluorescence Spec-trometryD430

21、6 Practice for Aviation Fuel Sample Containers forTests Affected by Trace ContaminationD4529 Test Method for Estimation of Net Heat of Combus-tion of Aviation FuelsD4809 Test Method for Heat of Combustion of LiquidHydrocarbon Fuels by Bomb Calorimeter (PrecisionMethod)D4865 Guide for Generation and

22、Dissipation of StaticElectricity in Petroleum Fuel SystemsD4952 Test Method for Qualitative Analysis for ActiveSulfur Species in Fuels and Solvents (Doctor Test)D4953 Test Method for Vapor Pressure of Gasoline andGasoline-Oxygenate Blends (Dry Method)D5001 Test Method for Measurement of Lubricity of

23、 Avia-tion Turbine Fuels by the Ball-on-Cylinder LubricityEvaluator (BOCLE)D5006 Test Method for Measurement of Fuel System IcingInhibitors (Ether Type) in Aviation FuelsD5190 Test Method for Vapor Pressure of Petroleum Prod-ucts (Automatic Method)D5191 Test Method for Vapor Pressure of Petroleum Pr

24、od-ucts (Mini Method)D5452 Test Method for Particulate Contamination in Avia-tion Fuels by Laboratory FiltrationD5453 Test Method for Determination of Total Sulfur inLight Hydrocarbons, Spark Ignition Engine Fuel, DieselEngine Fuel, and Engine Oil by Ultraviolet FluorescenceD5972 Test Method for Fre

25、ezing Point of Aviation Fuels(Automatic Phase Transition Method)D6045 Test Method for Color of Petroleum Products by theAutomatic Tristimulus MethodD6379 Test Method for Determination of Aromatic Hydro-carbon Types in Aviation Fuels and PetroleumDistillatesHigh Performance Liquid ChromatographyMetho

26、d with Refractive Index DetectionD6469 Guide for Microbial Contamination in Fuels andFuel SystemsD6615 Specification for Jet B Wide-Cut Aviation TurbineFuelD6751 Specification for Biodiesel Fuel Blend Stock (B100)for Middle Distillate FuelsD7153 Test Method for Freezing Point of Aviation Fuels(Autom

27、atic Laser Method)D7154 Test Method for Freezing Point of Aviation Fuels(Automatic Fiber Optical Method)D7566 Specification for Aviation Turbine Fuel ContainingSynthesized HydrocarbonsE29 Practice for Using Significant Digits in Test Data toDetermine Conformance with Specifications2.2 Energy Institu

28、te Standards:4IP 225 Copper Content of Aviation Turbine FuelIP 227 Silver Corrosion of Aviation Turbine FuelIP 540 Determination of the existent gum content of avia-tion turbine fuel Jet evaporation methodIP 585 Determination of fatty acid methyl esters (FAME),derived from bio-diesel fuel, in aviati

29、on turbine fuel GC-MS with selective ion monitoring/scan detectionmethod2.3 ANSI Standard:5ANSI 863 Report of Test Results2.4 Other Standards:Defence Standard (Def Stan) 91-91 Turbine Fuel, AviationKerosine Type, Jet A-16IATA Guidance Material on Microbiological Contaminationin Aircraft Fuel Tanks R

30、ef. No: 9680-027EN14214 Automotive fuels - Fatty acid methyl esters(FAME) for diesel engines - Requirements and testmethods84Available from Energy Institute, 61 New Cavendish St., London, WIG 7AR,U.K., http:/www.energyinst.org.uk.5Available from American National Standards Institute (ANSI), 25 W. 43

31、rd St.,4th Floor, New York, NY 10036.6Available from Procurement Executive DFS (Air), Ministry of Defence, St.Giles Court 1, St. Giles High St., London WC2H 8LD.7Available from International Air Transport Association (IATA), (Head Office)800 Place Victoria, PO Box 113, Montreal, H4Z 1M1, Quebec, Can

32、ada. www.iata-.8Available from European Committee for Standardization (CEN), 36 rue deStassart, B-1050, Brussels, Belgium, http:/www.cenorm.be.D1655 1023. General3.1 This specification, unless otherwise provided, prescribesthe required properties of aviation turbine fuel at the time andplace of deli

33、very.4. Classification4.1 Two types of aviation turbine fuels are provided, asfollows:4.1.1 Jet A and Jet A-1Relatively high flash point distil-lates of the kerosine type.4.2 Jet A and Jet A-1 represent two grades of kerosine fuelthat differ in freezing point. Other grades would be suitablyidentifie

34、d.4.3 This specification previously cited the requirements forJet B. Requirements for Jet B fuel now appear in SpecificationD6615.5. Materials and Manufacture5.1 Aviation turbine fuel is a complex mixture predomi-nantly composed of hydrocarbons and varies depending oncrude source and manufacturing p

35、rocess. Consequently, it isimpossible to define the exact composition of Jet A/A-1. Thisspecification has therefore evolved primarily as a performancespecification rather than a compositional specification. It isacknowledged that this largely relies on accumulated experi-ence; therefore the specific

36、ation limits aviation turbine fuels tothose made from conventional sources or by specificallyapproved processes.5.1.1 Aviation turbine fuel, except as otherwise specified inthis specification, shall consist predominantly of refined hydro-carbons (see Note 1) derived from conventional sourcesincludin

37、g crude oil, natural gas liquid condensates, heavy oil,shale oil, and oil sands. The use of jet fuel blends containingcomponents from other sources is permitted only in accordancewith Annex A1.NOTE 1Conventionally refined jet fuel contains trace levels of mate-rials that are not hydrocarbons, includ

38、ing oxygenates, organosulfur, andnitrogenous compounds.5.1.2 Fuels used in certified engines and aircraft are ulti-mately approved by the certifying authority subsequent toformal submission of evidence to the authority as part of thetype certification program for that aircraft and engine model.Addit

39、ives to be used as supplements to an approved fuel mustalso be similarly approved on an individual basis (see X1.2.4and X1.15.1).5.2 AdditivesMay be added to each type of aviationturbine fuel in the amount and of the composition specified inTable 2 or the following list of approved material:5.2.1 Ot

40、her additives are permitted under 5.1 and 7.1. Theseinclude fuel performance enhancing additives and fuel handingand maintenance additives as found under Table 2. Thequantities and types must be declared by the fuel supplier andagreed to by the purchaser. Only additives approved by theaircraft certi

41、fying authority are permitted in the fuel on whichan aircraft is operated.5.2.1.1 Biocidal additives are available for controlled usage.Where such an additive is used in the fuel, the approval statusof the additive and associated conditions must be checked forthe specific aircraft and engines to be

42、operated.5.2.1.2 Fuel System Icing Inhibitor:(1) Diethylene Glycol Monomethyl Ether (DiEGME), con-forming to the requirements of Specification D4171, Type III,may be used in concentrations of 0.10 to 0.15 volume %.(2) Test Method D5006 may be used to determine theconcentration of DiEGME in aviation

43、fuels.5.3 Incidental MaterialsIncidental materials are chemi-cals and compositions that can occur in turbine fuels as a resultof production, processing, distribution, or storage. Table 3 listsspecific materials that have an agreed limit. SpecificationD1655 does not require that each batch of fuel be

44、 analyzed forincidental materials. Further guidance concerning these mate-rials is presented in X1.16.5.4 Guidance material is presented in Appendix X2 con-cerning the need to control processing additives in jet fuelproduction.6. Detailed Requirements6.1 The aviation turbine fuel shall conform to th

45、e require-ments prescribed in Table 1.6.2 Test results shall not exceed the maximum or be lessthan the minimum values specified in Table 1. No allowanceshall be made for the precision of the test methods. Todetermine conformance to the specification requirement, a testresult may be rounded to the sa

46、me number of significant figuresas in Table 1 using Practice E29. Where multiple determina-tions are made, the average result, rounded in accordance withPractice E29, shall be used.7. Workmanship, Finish and Appearance7.1 The aviation turbine fuel specified in this specificationshall be visually fre

47、e of undissolved water, sediment, andsuspended matter. The odor of the fuel shall not be nauseatingor irritating. If the fuel has an odor similar to that of “rottenegg,” please refer to X1.12.5 for further discussion. Nosubstance of known dangerous toxicity under usual conditionsof handling and use

48、shall be present, except as permitted in thisspecification.8. Sampling8.1 Because of the importance of proper sampling proce-dures in establishing fuel quality, use the appropriate proce-dures in Practice D4057 to obtain a representative sample fromthe batch of fuel for specification compliance test

49、ing. Thisrequirement is met by producing fuel as a discrete batch thentesting it for specification compliance. This requirement is notsatisfied by averaging online analysis results.8.2 A number of jet fuel properties, including thermalstability, water separation, electrical conductivity, and others,are very sensitive to trace contamination, which can originatefrom sample containers. For recommended sample containers,refer to Practice D4306.D1655 103TABLE 1 Detailed Requirements of Aviation Turbine FuelsAProperty Jet A or Jet A-1 ASTM Test MethodBCOMPOSITIONAcidi