ASTM D7566-2013 red 6250 Standard Specification for Aviation Turbine Fuel Containing Synthesized Hydrocarbons《含有合成烃类的航空涡轮机燃料的标准规范》.pdf
《ASTM D7566-2013 red 6250 Standard Specification for Aviation Turbine Fuel Containing Synthesized Hydrocarbons《含有合成烃类的航空涡轮机燃料的标准规范》.pdf》由会员分享,可在线阅读,更多相关《ASTM D7566-2013 red 6250 Standard Specification for Aviation Turbine Fuel Containing Synthesized Hydrocarbons《含有合成烃类的航空涡轮机燃料的标准规范》.pdf(30页珍藏版)》请在麦多课文档分享上搜索。
1、Designation: D7566 12aD7566 13 An American National StandardStandard Specification forAviation Turbine Fuel Containing SynthesizedHydrocarbons1This standard is issued under the fixed designation D7566; the number immediately following the designation indicates the year oforiginal adoption or, in the
2、 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.This standard has been approved for use by agencies of the Department of Defense.1. Scope*1.1 This
3、specification covers the manufacture of aviation turbine fuel that consists of conventional and synthetic blendingcomponents.1.2 This specification applies only at the point of batch origination, as follows:1.2.1 Aviation turbine fuel manufactured, certified, and released to all the requirements of
4、Table 1of 1 of this specification(D7566), meets the requirements of Specification D1655 and shall be regarded as Specification D1655 turbine fuel. Duplicatetesting is not necessary; the same data may be used for both D7566 and D1655 compliance. Once the fuel is released to thisspecification (D7566)
5、the unique requirements of this specification are no longer applicable: any recertification shall be done inaccordance with Table 1 of Specification D1655.1.2.2 Field blending of synthesized paraffinic kerosine (SPK) blendstocks, as described in Annex A1 (FT SPK) or Annex A2(HEFA SPK) with D1655 fue
6、l (which may on the whole or in part have originated as D7566 fuel) shall be considered batchorigination in which case all of the requirements of Table 1 of this specification (D7566) apply and shall be evaluated. Short formconformance test programs commonly used to ensure transportation quality are
7、 not sufficient. The fuel shall be regarded as D1655turbine fuel after certification and release as described in 1.2.1.1.2.3 Once a fuel is redesignated as D1655 aviation turbine fuel, it can be handled in the same fashion as the equivalent refinedD1655 aviation turbine fuel.1.3 This specification d
8、efines specific types of aviation turbine fuel that contain synthesized hydrocarbons for civil use in theoperation and certification of aircraft and describes fuels found satisfactory for the operation of aircraft and engines. Thespecification is intended to be used as a standard in describing the q
9、uality of aviation turbine fuels and synthetic blendingcomponents at the place of manufacture but can be used to describe the quality of aviation turbine fuels for contractual transferat all points in the distribution system.1.4 This specification does not include all fuels satisfactory for aviation
10、 turbine engines. Certain equipment or conditions of usemay permit a wider, or require a narrower, range of characteristics than is shown by this specification.1.5 While aviation turbine fuels defined by Table 1 of this specification can be used in applications other than aviation turbineengines, re
11、quirements for such other applications have not been considered in the development of this specification.1.6 Synthetic blending components, synthetic fuels, and blends of synthetic fuels with conventional petroleum-derived fuels inthis specification have been evaluated and approved in accordance wit
12、h the principles established in Practice D4054.1.7 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard.1.8 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibi
13、lityof the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatorylimitations prior to use.1 This specification is under the jurisdiction of ASTM Committee D02 on Petroleum Products and Lubricants and is the direct responsibility of Su
14、bcommittee D02.J0.06on Emerging Turbine Fuels.Current edition approved Nov. 1, 2012May 1, 2013. Published February 2013June 2013. Originally approved in 2009. Last previous edition approved in 2012 asD756612.12a. DOI: 10.1520/D7566-12A.10.1520/D7566-13.This document is not an ASTM standard and is in
15、tended 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, ASTM recommends that users consult prior editions as appropriate. In all cases only the cur
16、rent versionof the standard as published by ASTM is to be considered the official document.*A Summary of Changes section appears at the end of this standardCopyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States12. Referenced Documents2.1 AST
17、M Standards:2D56 Test Method for Flash Point by Tag Closed Cup TesterD86 Test Method for Distillation of Petroleum Products at Atmospheric PressureD93 Test Methods for Flash Point by Pensky-Martens Closed Cup TesterD129 Test Method for Sulfur in Petroleum Products (General High Pressure Decompositio
18、n Device Method)D130 Test Method for Corrosiveness to Copper from Petroleum Products by Copper Strip TestD156 Test Method for Saybolt Color of Petroleum Products (Saybolt Chromometer Method)D240 Test Method for Heat of Combustion of Liquid Hydrocarbon Fuels by Bomb CalorimeterD323 Test Method for Va
19、por Pressure of Petroleum Products (Reid Method)D381 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 Method)D1298 Test Meth
20、od 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 Aviation Turbine FuelD1405 Te
21、st Method for Estimation of Net Heat of Combustion of Aviation FuelsD1655 Specification for Aviation Turbine FuelsD1740 Test Method for Luminometer Numbers of Aviation Turbine Fuels (Withdrawn 2006)3D1840 Test Method for Naphthalene Hydrocarbons in Aviation Turbine Fuels by Ultraviolet Spectrophotom
22、etryD2276 Test Method for Particulate Contaminant in Aviation Fuel by Line SamplingD2386 Test Method for Freezing Point of Aviation FuelsD2425 Test Method for Hydrocarbon Types in Middle Distillates by Mass SpectrometryD2622 Test Method for Sulfur in Petroleum Products by Wavelength Dispersive X-ray
23、 Fluorescence SpectrometryD2624 Test Methods for Electrical Conductivity of Aviation and Distillate FuelsD2887 Test Method for Boiling Range Distribution of Petroleum Fractions by Gas ChromatographyD2892 Test Method for Distillation of Crude Petroleum (15-Theoretical Plate Column)D3227 Test Method f
24、or (Thiol Mercaptan) Sulfur in Gasoline, Kerosine, Aviation Turbine, and Distillate Fuels (PotentiometricMethod)D3240 Test Method for Undissolved Water In Aviation Turbine FuelsD3241 Test Method for Thermal Oxidation Stability of Aviation Turbine FuelsD3242 Test Method for Acidity in Aviation Turbin
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