ASTM D7223-2017 red 6250 Standard Specification for Aviation Certification Turbine Fuel《航空认证涡轮机燃料的标准规格》.pdf

1、Designation: D7223 16aD7223 17 An American National StandardStandard Specification forAviation Certification Turbine Fuel1This standard is issued under the fixed designation D7223; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, th

2、e 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*1.1 This specification covers the use of purchasing agencies in formulating specifications for purchases of avi

3、ation turbine fuelunder contract.1.2 This specification defines one specific type of aviation turbine fuel for civil use in the certification of aircraft. Thespecification can be used as a standard in describing the quality of this aviation fuel from the refinery to the aircraft.1.3 This specificati

4、on does not include the fuels that are commonly used in aviation turbine engines. Those are listed inSpecification D1655.1.4 The aviation turbine fuel defined by this specification may be used in other than turbine engines that are specificallydesigned and certified for this fuel.1.5 The use of EI/I

5、P (Energy Institute/Institute of Petroleum) test methods is permitted. The user of this specification is referredto Specification D1655 (latest revision), Specification for Aviation Turbine Fuels, Paragraph 2, Referenced Documents and Table1, Detailed Requirements of Aviation Turbine Fuels, Column 4

6、, Test Methods, to determine the pairing of the IP test method withthe particular detailed requirement, and to Section 11, Test Methods, to identify jointed standards and referee methods.1.6 The values stated in SI units are to be regarded as standard. No other units of measurement are included in t

7、his standard.1.6.1 ExceptionUnits of pressure are also given in psi.1.7 This international standard was developed in accordance with internationally recognized principles on standardizationestablished in the Decision on Principles for the Development of International Standards, Guides and Recommenda

8、tions issuedby the World Trade Organization Technical Barriers to Trade (TBT) Committee.2. Referenced Documents2.1 ASTM Standards:2D56 Test Method for Flash Point by Tag Closed Cup TesterD86 Test Method for Distillation of Petroleum Products and Liquid Fuels at Atmospheric PressureD130 Test Method f

9、or Corrosiveness to Copper from Petroleum Products by Copper Strip TestD381 Test Method for Gum Content in Fuels by Jet EvaporationD445 Test Method for Kinematic Viscosity of Transparent and Opaque Liquids (and Calculation of Dynamic Viscosity)D1266 Test Method for Sulfur in Petroleum Products (Lamp

10、 Method)D1298 Test Method for Density, Relative Density, or API Gravity of Crude Petroleum and Liquid Petroleum Products byHydrometer MethodD1319 Test Method for Hydrocarbon Types in Liquid Petroleum Products by Fluorescent Indicator AdsorptionD1322 Test Method for Smoke Point of Kerosine and Aviati

11、on Turbine FuelD1655 Specification for Aviation Turbine FuelsD1840 Test Method for Naphthalene Hydrocarbons in Aviation Turbine Fuels by Ultraviolet SpectrophotometryD2386 Test Method for Freezing Point of Aviation FuelsD2622 Test Method for Sulfur in Petroleum Products by Wavelength Dispersive X-ra

12、y Fluorescence SpectrometryD2624 Test Methods for Electrical Conductivity of Aviation and Distillate Fuels1 This specification is under the jurisdiction ofASTM Committee D02 on Petroleum Products, Liquid Fuels, and Lubricants and is the direct responsibility of SubcommitteeD02.J0 on Aviation Fuels.C

13、urrent edition approved July 1, 2016July 1, 2017. Published July 2016July 2017. Originally approved in 2005. Last previous edition approved in 2016 asD7223 16.D7223 16a. DOI: 10.1520/D7223-16A.10.1520/D7223-17.2 For referencedASTM standards, visit theASTM website, www.astm.org, or contactASTM Custom

14、er 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

15、previous 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

16、 Changes section appears at the end of this standardCopyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States1D2887 Test Method for Boiling Range Distribution of Petroleum Fractions by Gas ChromatographyD3227 Test Method for (Thiol Mercaptan) S

17、ulfur in Gasoline, Kerosine, Aviation Turbine, and Distillate Fuels (PotentiometricMethod)D3241 Test Method for Thermal Oxidation Stability of Aviation Turbine FuelsD3242 Test Method for Acidity in Aviation Turbine FuelD3338 Test Method for Estimation of Net Heat of Combustion of Aviation FuelsD3828

18、 Test Methods for Flash Point by Small Scale Closed Cup TesterD3948 Test Method for Determining Water Separation Characteristics of Aviation Turbine Fuels by Portable SeparometerD4052 Test Method for Density, Relative Density, and API Gravity of Liquids by Digital Density MeterD4057 Practice for Man

19、ual Sampling of Petroleum and Petroleum ProductsD4171 Specification for Fuel System Icing InhibitorsD4294 Test Method for Sulfur in Petroleum and Petroleum Products by Energy Dispersive X-ray Fluorescence SpectrometryD4306 Practice for Aviation Fuel Sample Containers for Tests Affected by Trace Cont

20、aminationD4529 Test Method for Estimation of Net Heat of Combustion of Aviation FuelsD4809 Test Method for Heat of Combustion of Liquid Hydrocarbon Fuels by Bomb Calorimeter (Precision Method)D4952 Test Method for Qualitative Analysis for Active Sulfur Species in Fuels and Solvents (Doctor Test)D500

21、1 Test Method for Measurement of Lubricity of Aviation Turbine Fuels by the Ball-on-Cylinder Lubricity Evaluator(BOCLE)D5006 Test Method for Measurement of Fuel System Icing Inhibitors (Ether Type) in Aviation FuelsD5453 Test Method for Determination of Total Sulfur in Light Hydrocarbons, Spark Igni

22、tion Engine Fuel, Diesel Engine Fuel,and Engine Oil by Ultraviolet FluorescenceD5972 Test Method for Freezing Point of Aviation Fuels (Automatic Phase Transition Method)D6378 Test Method for Determination of Vapor Pressure (VPX) of Petroleum Products, Hydrocarbons, and Hydrocarbon-Oxygenate Mixtures

23、 (Triple Expansion Method)D6469D7042 Guide for Microbial Contamination in Fuels and Fuel SystemsTest Method for Dynamic Viscosity and Density ofLiquids by Stabinger Viscometer (and the Calculation of Kinematic Viscosity)E29 Practice for Using Significant Digits in Test Data to Determine Conformance

24、with Specifications2.2 Other Standards:AFRL-RQ-WP-TR-2013-0271 Determination of the Minimum Use Level of Fuel System Icing Inhibitor (FSII) in JP-8 that willProvide Adequate Icing Inhibition and Biostatic Protection for Air Force Aircraft33. General3.1 This specification, unless otherwise provided,

25、prescribes the required properties of aviation certification turbine fuel at thetime and place of delivery.4. Classification4.1 One type of aviation turbine fuel is provided, as follows:4.1.1 Jet C-1A relatively wide boiling range volatile distillate.5. Materials and Manufacture5.1 Aviation turbine

26、fuel, except as otherwise specified in this specification, shall consist of blends of refined hydrocarbons (seeNote 1) derived from conventional sources including crude oil, natural gas liquid condensates, heavy oil, shale oil, and oil sands.The use of jet fuel blends, containing components from oth

27、er sources, is permitted only on a specific, individual basis (see AnnexA1 on fuels from non-conventional sources in Specification D1655).NOTE 1Conventionally refined jet fuel contains trace levels of materials which are not hydrocarbons, including oxygenates, organosulfur, andnitrogeneous compounds

28、.5.1.1 Fuels used in engines and aircraft are ultimately approved by the certifying authority subsequent to formal submission ofevidence to the authority as part of the type certification program for that aircraft and engine model. Additives to be used assupplements to an approved fuel must also be

29、similarly approved on an individual basis (see Specification D1655).5.2 AdditivesMay be added to this aviation turbine fuel in the amount and of the composition specified in the following listof approved material:45.2.1 AntioxidantsIn amounts not to exceed 24.0 mgL active ingredients (not including

30、mass of solvent):5.2.1.1 2,6-ditertiary-butyl phenol.3 Available from Defense Technical Information Center (DTIC), 8725 John J. Kingman Road, Ft. Belvoir, VA 220606218, http:/www.dtic.mil/dtic, accession numberADA595127.4 Supporting data (Guidelines forApproval or Disapproval ofAdditives) have been

31、filed atASTM International Headquarters and may be obtained by requesting ResearchReport RR:D02-1125.D7223 1725.2.1.2 2,6-ditertiary-butyl-4-methyl phenol.5.2.1.3 2,4-dimethyl-6-tertiary-butyl phenol.5.2.1.4 75 % minimum 2,6-ditertiary-butyl phenol, plus 25 % maximum mixed tertiary and tritertiary-b

32、utyl phenols.5.2.1.5 55 % minimum 2,4-dimethyl-6-tertiary-butyl phenol, plus 15 % minimum 2,6-ditertiary-butyl-4-methyl phenol,remainder as monomethyl and dimethyl tertiary-butyl phenols.5.2.1.6 72 % minimum 2,4-dimethyl-6-tertiary-butyl phenol, 28 % maximum monomethyl and dimethyl-tertiary-butyl ph

33、enols.5.2.2 Metal Deactivator Additive (MDA), in amount not to exceed 2.0 mgL (not including mass of solvent) on initial fuelmanufacture at the refinery. Higher initial concentrations are permitted in circumstances where copper contamination is suspectedto occur during distribution. Cumulative conce

34、ntration of MDA when retreating the fuel shall not exceed 5.7 mgL:5.2.2.1 N,N-disalicylidene-1,2-propane diamine.5.2.3 Electrical Conductivity AdditiveStadis 4505 not to exceed 3 mgL.5.2.3.1 When loss of fuel conductivity necessitates retreatment with electrical conductivity additive, the following

35、concentrationlimits apply:At Manufacture:Stadis 450 3 mg L, maxRetreatment:Stadis 450 cumulative total 5 mg L, max5.2.4 Leak Detection AdditiveTracer A (LDTA-A)6 may be added to the fuel in amounts not to exceed 1 mgkg.5.2.5 Other additives are permitted. These include fuel system icing inhibitor an

36、d special purpose additives such as biocides.The quantities and types must be declared by the fuel supplier and agreed to by the purchaser. Only additives approved by theaircraft certifying authority are permitted in the fuel on which an aircraft is operated.5.2.5.1 Biocidal additives are available

37、for controlled usage. Where such an additive is used in the fuel, the approval status ofthe additive and associated conditions must be checked for the specific aircraft and engines to be operated.5.2.5.2 Fuel System Icing Inhibitor:(1) Diethylene Glycol Monomethyl Ether (DIEGME), conforming to the r

38、equirements of Specification D4171, Type III, maybe used in concentrations of 0.10 % to 0.15 % by volume.(2) Test Method D5006 may be used to determine the concentration of DIEGME in aviation fuels.5.3 Guidance material is presented inAppendix X3 of Specification D1655 concerning the need to control

39、 processing additivesin jet fuel production.6. Detailed Requirements6.1 The aviation turbine fuel shall conform to the requirements prescribed in Table 1.6.2 Test results shall not exceed the maximum or be less than the minimum values specified in Table 1. No allowance shall bemade for the precision

40、 of the test methods.To determine conformance to the specification requirement, a test result may be roundedto the same number of significant figures as in Table 1 using Practice E29. Where multiple determinations are made, the averageresult, rounded according to Practice E29, shall be used.6.3 If a

41、ny additives are used, the aviation turbine fuel shall conform to the Table 2 listed requirements.7. Workmanship, Finish, and Appearance7.1 The aviation turbine fuel herein specified shall be visually free of undissolved water, sediment, and suspended matter. Theodor of the fuel shall not be nauseat

42、ing or irritating. No substance of known dangerous toxicity under usual conditions of handlingand use shall be present, except as permitted in this specification.8. Sampling8.1 Because of the importance of proper sampling procedures in establishing fuel quality, use the appropriate procedures inPrac

43、tice D4057 to obtain a representative sample from the batch of fuel for specification compliance testing. This requirement ismet by producing fuel as a discrete batch then testing it for specification compliance. This requirement is not satisfied by averagingonline analysis results.8.2 A number of j

44、et fuel properties including thermal stability, water separation, electrical conductivity, and others are verysensitive to trace contamination that can originate from sample containers. For recommended sample containers refer to PracticeD4306.9. Report9.1 The type and number of reports to ensure con

45、formance with the requirements of this specification shall be mutually agreedupon by the seller and the purchaser of the aviation turbine fuel.5 Stadis 450 is a registered trademark marketed by Innospec Inc., Innospec Manufacturing Park, Oil Sites Road, Ellesmere Port, Cheshire, CH65 4EY, UK.6 Trace

46、r A (LDTA-A) is a registered trademark of Tracer Research Corp., 3755 N. Business Center Dr., Tucson, AZ 85705.D7223 1739.2 A suggested form for reporting inspection data on aviation turbine fuel is given in Specification D1655.10. Test Methods10.1 Determine the requirements enumerated in this speci

47、fication in accordance with the following ASTM test methods.10.1.1 DensityTest Method D1298 or D4052. Test Method D4052 shall be the referee test method.10.1.2 DistillationTest Method D86 or D2887 with the conversion to D86 temperatures given in correlation procedure(Appendix X5) in Test Method D288

48、7.10.1.3 Vapor PressureTest Method D6378. Record absolute vapor pressure (VPx).TABLE 1 Detailed Requirements of Aviation Certification Turbine FuelAProperty Jet C-1 ASTM Test MethodBAcidity, total mg KOH/g max 0.10 D3242Vol fraction of aromatics, cL/L min/max 8 to 25 D1319Mass fraction of mercaptan

49、sulfur,C cg/g max 0.003 D3227Mass fraction of total sulfur, cg/g max 0.30 D1266, D2622, D4294 orD5453Distillation temperature, C (F):Initial boiling point, temperature min/max 70/100 (158/212) D2887, D86D5 % recovered, temperature min/max 80/110 (176/230) D2887, D86D10 % recovered, temperature min/max 90/120 (194/248) D2887, D86D20 % recovered, temperature min/max 105/140 (221/284) D2887, D86D50 % recovered, temperature min/max 150/195 (302/383) D2887, D86D90 % recovered, temperature min/max 215/255 (419/491) D2887, D86DFinal boiling point, temperature min