ASTM D3338 D3338M-2009 Standard Test Method for Estimation of Net Heat of Combustion of Aviation Fuels《航空燃料燃烧净热值的评价的标准试验方法》.pdf

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1、Designation: D 3338/D 3338M 09An American National StandardStandard Test Method forEstimation of Net Heat of Combustion of Aviation Fuels1This standard is issued under the fixed designation D 3338/D 3338M; the number immediately following the designation indicates theyear of original adoption or, in

2、 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.This standard has been approved for use by agencies of the Department of Defense.1. Scope*1.1 T

3、his test method covers the estimation of the net heat ofcombustion (megajoules per kilogram or Btu per pound) ofaviation gasolines and aircraft turbine and jet engine fuels inthe range from 40.19 to 44.73 megajoules per kilogram or17 280 to 19 230 Btu per pound. The precision for estimationof the ne

4、t heat of combustion outside this range has not beendetermined for this test method.1.2 This test method is purely empirical and is applicable toliquid hydrocarbon fuels that conform to the specifications foraviation gasolines or aircraft turbine and jet engine fuels ofgrades Jet A, Jet A-1, Jet B,

5、JP-4, JP-5, JP-7, and JP-8.NOTE 1The experimental data on heat of combustion from which theTest Method D 3338 correlation was devised was obtained by a precisionmethod similar to Test Method D 4809.NOTE 2The estimation of the net heat of combustion of a hydrocar-bon fuel is justifiable only when the

6、 fuel belongs to a well-defined classfor which a relation between heat of combustion and aromatic and sulfurcontents, density, and distillation range of the fuel has been derived fromaccurate experimental measurements on representative samples of thatclass. Even in this case, the possibility that th

7、e estimates may be in errorby large amounts for individual fuels should be recognized. The fuels usedto establish the correlation presented in this method are defined as follows:Fuels:Aviation gasolineGrades 100/130 and 115/145 (1, 2)2Kerosines, alkylates, and special WADC fuels (3)Pure hydrocarbons

8、paraffins, naphthenes, and aromatics (4)Fuels for which data were reported by the Coordinating ResearchCouncil (5).NOTE 3The property ranges used in this correlation are as follows:Aromaticsfrom 0 to 100 mass %API Gravityfrom 25.7 to 81.2APIVolatilityfrom 160 to 540F, average boiling point1.3 The va

9、lues stated in either SI units or inch-pound unitsare to be regarded separately as standard. The values stated ineach system may not be exact equivalents; therefore, eachsystem shall be used independently of the other. Combiningvalues from the two systems may result in non-conformancewith the standa

10、rd.1.3.1 Although the test method permits the calculation ofnet heat of combustion in either SI or inch-pound units, SI unitsare the preferred units.1.3.2 The net heat of combustion can also be estimated ininch-pound units by Test Method D 1405 or in SI units by TestMethod D 4529. Test Method D 1405

11、 requires calculation ofone of four equations dependent on the fuel type with aprecision equivalent to that of this test method. Test MethodD 4529 requires calculation of a single equation for all aviationfuels with a precision equivalent to that of this test method.Unlike Test Method D 1405 and D 4

12、529, Test Method D 3338does not require the use of aniline point.1.4 This standard does not purport to address all of thesafety concerns, if any, associated with its use. It is theresponsibility of the user of this standard to establish appro-priate safety and health practices and determine the appl

13、ica-bility of regulatory limitations prior to use.2. Referenced Documents2.1 ASTM Standards:3D86 Test Method for Distillation of Petroleum Products atAtmospheric PressureD 240 Test Method for Heat of Combustion of LiquidHydrocarbon Fuels by Bomb CalorimeterD 1266 Test Method for Sulfur in Petroleum

14、Products(Lamp Method)D 1298 Test Method for Density, Relative Density (SpecificGravity), or API Gravity of Crude Petroleum and LiquidPetroleum Products by Hydrometer MethodD 1319 Test Method for Hydrocarbon Types in LiquidPetroleum Products by Fluorescent Indicator AdsorptionD 1405 Test Method for E

15、stimation of Net Heat of Com-bustion of Aviation FuelsD 1552 Test Method for Sulfur in Petroleum Products1This test method is under the jurisdiction of ASTM Committee D02 onPetroleum Products and Lubricants and is the direct responsibility of SubcommitteeD02.05 on Properties of Fuels, Petroleum Coke

16、 and Carbon Material.Current edition approved April 15, 2009. Published April 2009. Originallyapproved in 1974. Last previous edition approved in 2008 as D 333808.2The boldface numbers in parentheses refer to a list of references at the end ofthis standard.3For referenced ASTM standards, visit the A

17、STM website, www.astm.org, orcontact ASTM Customer Service at serviceastm.org. For Annual Book of ASTMStandards volume information, refer to the standards Document Summary page onthe ASTM website.1*A Summary of Changes section appears at the end of this standard.Copyright ASTM International, 100 Bar

18、r Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.(High-Temperature Method)D 2622 Test Method for Sulfur in Petroleum Products byWavelength Dispersive X-ray Fluorescence SpectrometryD 2887 Test Method for Boiling Range Distribution ofPetroleum Fractions by Gas Chromatograp

19、hyD 3120 Test Method for Trace Quantities of Sulfur in LightLiquid Petroleum Hydrocarbons by Oxidative Microcou-lometryD 4052 Test Method for Density and Relative Density ofLiquids by Digital Density MeterD 4294 Test Method for Sulfur in Petroleum and PetroleumProducts by Energy Dispersive X-ray Flu

20、orescence Spec-trometryD 4529 Test Method for Estimation of Net Heat of Com-bustion of Aviation FuelsD 4809 Test Method for Heat of Combustion of LiquidHydrocarbon Fuels by Bomb Calorimeter (PrecisionMethod)D 5453 Test Method for Determination of Total Sulfur inLight Hydrocarbons, Spark Ignition Eng

21、ine Fuel, DieselEngine Fuel, and Engine Oil by Ultraviolet FluorescenceD 6379 Test Method for Determination of Aromatic Hydro-carbon Types in Aviation Fuels and PetroleumDistillatesHigh Performance Liquid ChromatographyMethod with Refractive Index Detection2.2 Energy Institute Standard:4IP 436 Test

22、Method for Determination of Aromatic Hydro-carbon Types in Aviation Fuels and PetroleumDistillatesHigh Performance Liquid ChromatographyMethod with Refractive Index Detection3. Terminology3.1 Definitions:3.1.1 gross heat of combustion, Qg (MJ/kg)quantity ofenergy released when a unit mass of fuel is

23、 burned in a constantvolume enclosure, with the products being gaseous, other thanwater, which is condensed to the liquid state.3.1.2 net heat of combustion, Qn (MJ/kg)quantity ofenergy released when a unit mass of fuel is burned at constantpressure, with all of the products, including water, beingg

24、aseous.4. Summary of Test Method4.1 A correlation (6) in inch-pound units has been estab-lished between the net heat of combustion and gravity, aro-matic content, and average volatility of the fuel. This correla-tion was converted to SI units; the relationships are given bythe following equations:Ty

25、pe FuelAll aviation gasolines, aircraft turbine, and jet engine fuelsEquationQp15 16.24G! 2 3.007A! 1 0.01714G 3 V! (1)2 0.2983A 3 G! 1 0.00053A 3 G 3 V! 1 17685or in SI unitsQp25 5528.73 2 92.6499A 1 10.1601T (2)1 0.314169AT/D 1 0.0791707A2 0.00944893T 2 0.000292178AT 1 35.9936where:Qp1= net heat o

26、f combustion, Btu/lb sulfur-free basis,Qp2= net heat of combustion, MJ/kg, sulfur-free basis,A = aromatics, volume %G = gravity, API,V = volatility: boiling point or average of Test MethodD86or D 2887 10 %, 50 %, and 90 % points, F,D = density, kg/m3at 15CT = volatility: boiling point or average of

27、Test MethodD86or D 2887 10 %, 50 %, and 90 % points, C.4.2 To correct for the effect of the sulfur content of the fuelon the net heat of combustion, apply the following equation:Q 5 Qp3 1 2 0.01S1!# 1 CS1! (3)where:Q = net heat of combustion, MJ/kg or Btu/lb, of the fuelcontaining S1weight percent s

28、ulfur,Qp= Qp1inch-pound units or Qp2(SI units),S1= sulfur content of the fuel, mass %, andC = 0.10166 (SI units) or 43.7 (inch-pound units) = aconstant based on the thermochemical data on sulfurcompounds.4.3 The empirical equations for the estimated net heat ofcombustion, sulfur-free basis, were der

29、ived by stepwise linearregression methods using data from 241 fuels, most of whichconform to specifications for aviation gasolines and aircraftturbine or jet engine fuels.5. Significance and Use5.1 This test method is intended for use as a guide in caseswhere experimental determination of heat of co

30、mbustion is notavailable and cannot be made conveniently and where anestimate is considered satisfactory. It is not intended as asubstitute for experimental measurements of heat of combus-tion. Table 1 shows a summary for the range of each variableused in developing the correlation. The mean value a

31、nd anestimate of its distribution about the mean, namely the standarddeviation, is shown. This indicates, for example, that the meandensity for all fuels used in developing the correlation was779.3 kg/m3and that two thirds of the samples had a densitybetween 721.4 and 837.1 kg/m3, that is, plus or m

32、inus onestandard deviation. The correlation is most accurate when thevalues of the variables used are within one standard deviationof the mean, but is useful up to two standard deviations of themean. The use of this correlation may be applicable to otherhydrocarbon distillates and pure hydrocarbons;

33、 however, only4Available from Energy Institute, 61 New Cavendish St., London, WIG 7AR,U.K., http:/www.energyinst.org.uk.TABLE 1 Mean and Standard Deviation of the VariablesVariable MeanStandardDeviationAromatics, volume % 13.5 23.9Density, kg/m3API 779.3 50.0 58.0 13.5Volatility, C F 171.11 340 57.2

34、 103Heat of combustion, MJ/kg Btu/lb 43.421 18 668 0.862 371D 3338/D 3338M 092limited data on non-aviation fuels over the entire range of thevariables were included in the correlation.NOTE 4The procedures for the experimental determination of thegross and net heats of combustion are described in Tes

35、t Methods D 240and D 4809.5.2 The calorimetric methods cited in Note 4 measure grossheat of combustion. However, net heat is used in aircraftcalculations because all combustion products are in the gaseousstate. This calculation method is based on net heat, but acorrection is required for condensed s

36、ulfur compounds.6. Procedure6.1 Determine the aromatic content of the fuel to the nearest0.1 % vol as described in Test Method D 1319.6.1.1 Test Method D 6379 or IP 436 may be used as analternative to Test Method D 1319 for determining fuel aro-matics content for use in this test method.6.1.2 If Tes

37、t Method D 6379 or IP 436 is used, multiply thetotal aromatics content in vol% by 25/26.5 (=0.9434), and usethis corrected value in place of aromatics determined by TestMethod D 1319 in Eq 2.6.2 Determine the density at 15C or the API gravity of thefuel to the nearest 0.1 kg/m3or 0.1 API as describe

38、d in TestMethod D 1298 or in Test Method D 4052.6.3 Determine the 10 %, 50 %, and 90 % boiling points ofthe fuel to the nearest 1C or 1F as described in Test MethodD86. Average these three temperatures to obtain the T value(C) or the V value F used in the equations of 4.1. For a purehydrocarbon, T o

39、r V is the normal boiling point.6.3.1 Test Method D 2887 may be used as an alternative toTest Method D86for determining fuel volatility for use in thistest method. The average of the 10 %, 50 %, and 90 % boilingpoints determined by Test Method D 2887 may be used directlyin place of the corresponding

40、 average determined by TestMethod D86.6.4 Determine the sulfur content of the fuel to the nearest0.02 % sulfur as described in Test Methods D 1266, D 1552,D 2622, D 3120, D 4294,orD 5453, depending upon thevolatility of the sample.7. Calculation and Report7.1 SI Units:7.1.1 Calculate the net heat of

41、 combustion, sulfur-free basis,using Eq 2 of 4.1. Round the value obtained to the nearestone-thousandth.Example:Sample: KerosineDetermined Values:Aromatics, A = 12.5 % volumeDensity, D = 805.0 kg/m3DistillationT105 203C (4)T505 233CT905 245CT 5 203 1 233 1 245!/3 5 227CCalculated Value: A 3 T 5 2837

42、.5 (5)Substituting into Eq 2 in 4.1:Qp25 5528.73 2 92.649912.5! 1 10.1601227! (6)1 0.3141692837.5!#/805.0 1 0.079170712.5!2 0.00944893227! 2 0.0002921782837.5!1 35.9936Qp25 43.411015 5 43.411 MJ/kg, sulfur2free basis (7)7.1.2 Calculate the net heat of combustion corrected for thesulfur content of th

43、e fuel using Eq 3 of 4.2. Round the valueobtained to the nearest one-thousandth.Example: Qp2= 43.411 MJ/kgDetermined Value: Sulfur, S1= 0.10 mass %Substituting into Eq 3 in 4.2:Q 5 43.4111 2 0.010.1!# 1 0.101660.1! (8)Q 5 43.3778 5 43.378 MJ/kg (9)7.2 Inch-Pound Units:7.2.1 Calculate the net heat of

44、 combustion, sulfur-free basis,using Eq 1 in 4.1. Round the value obtained to the nearestinteger.Example:Sample: KerosineDetermined Values:Aromatics, A = 12.5 % volumeGravity, G = 44.2 APIDistillationT105 398F (10)T505 451FT905 473FT 5 398 1 451 1 473!/3 5 440.7FCalculated Values:G 3 V 5 19 478.9 (1

45、1)A 3 G 5 552.5 (12)A 3 G 3 V 5 243486.8 (13)Substituting into Eq 1 in 4.1:Qp15 16.2444.2! 2 3.00712.5! 1 (14)0.0171419 478.9! 2 0.2983552.5! 10.00053243 486.8! 1 17 685Qp15 18 663.3 5 18 663 Btu/lb, sulfur2free basis (15)7.2.2 Calculate the net heat of combustion corrected for thesulfur content of

46、the fuel and round the value obtained to thenearest integer.Example: Qp1= 18 663 Btu/lbDetermined Value: Sulfur, S1= 0.10 mass %Q 5 18 6631 2 0.010.1!# 1 43.70.1! (16)Q 5 18 648.7 5 18 649 Btu/lb (17)8. Report8.1 Report the result from 7.1 to the nearest one-thousandthas net heat of combustion of th

47、e fuel in megajoules perkilogram or from 7.2 to the nearest integer as net heat ofcombustion of the fuel in Btu per pound.D 3338/D 3338M 0938.2 Report whether the result is determined on sulfur-free orsulfur-corrected basis.9. Precision and Bias59.1 The following criteria should be used for judging

48、theacceptability of estimated net heat of combustion results (95 %confidence):9.1.1 RepeatabilityThe difference between successive re-sults obtained by the same operator (using a second set ofmeasured values for aromatics content, density, and distillationdata) on identical test material would, in t

49、he long run, in thenormal and correct use of the test method, exceed the followingvalues (sulfur-free basis) in only one case in twenty.Repeatability 5 0.021 MJ/kg or 9 Btu/lb9.1.2 ReproducibilityThe difference between two singleand independent results obtained by different operators work-ing in different laboratories on identical test material would, inthe long run, exceed the following values in only one case intwenty.Reproducibility 5 0.046 MJ/kg or 20 Btu/lbNOTE