ASTM D7566-2017a red 2500 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格》.pdf
《ASTM D7566-2017a red 2500 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格》.pdf》由会员分享,可在线阅读,更多相关《ASTM D7566-2017a red 2500 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格》.pdf(44页珍藏版)》请在麦多课文档分享上搜索。
1、Designation: D7566 17D7566 17a 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 U.S. Department of Defense.1. Scope*1.1
3、This 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 requirement
4、s of Table 1 of this specification (D7566),meets the requirements of Specification D1655 and shall be regarded as Specification D1655 turbine fuel. Duplicate testing is notnecessary; the same data may be used for both D7566 and D1655 compliance. Once the fuel is released to this specification(D7566)
5、 the unique requirements of this specification are no longer applicable: any recertification shall be done in accordance withTable 1 of Specification D1655.1.2.2 Field blending of synthesized paraffinic kerosine (SPK) blendstocks, as described in Annex A1 (FT SPK), Annex A2(HEFA SPK), Annex A3 (SIP)
6、, synthesized paraffinic kerosine plus aromatics (SPK/A) as described in Annex A4, or Annex A5(ATJ) with D1655 fuel (which may on the whole or in part have originated as D7566 fuel) shall be considered batch originationin which case all of the requirements ofTable 1 of this specification (D7566) app
7、ly and shall be evaluated. Short form conformancetest programs commonly used to ensure transportation quality are not sufficient. The fuel shall be regarded as D1655 turbine fuelafter certification and release as described in 1.2.1.1.2.3 Once a fuel is redesignated as D1655 aviation turbine fuel, it
8、 can be handled in the same fashion as the equivalent refinedD1655 aviation turbine fuel.1.3 This specification defines the minimum property requirements for aviation turbine fuel that contain synthesizedhydrocarbons and lists acceptable additives for use in civil operated engines and aircrafts. Spe
9、cification D7566 is directed at civilapplications, and maintained as such, but may be adopted for military, government, or other specialized uses.1.4 This specification can be used as a standard in describing the quality of aviation turbine fuel from production to the aircraft.However, this specific
10、ation does not define the quality assurance testing and procedures necessary to ensure that fuel in thedistribution system continues to comply with this specification after batch certification. Such procedures are defined elsewhere, forexample in ICAO 9977, EI/JIG Standard 1530, JIG 1, JIG 2, API 15
11、43, API 1595, and ATA-103.1.5 This specification does not include all fuels satisfactory for aviation turbine engines. Certain equipment or conditions of usemay permit a wider, or require a narrower, range of characteristics than is shown by this specification.1.6 While aviation turbine fuels define
12、d by Table 1 of this specification can be used in applications other than aviation turbineengines, requirements for such other applications have not been considered in the development of this specification.1.7 Synthetic blending components, synthetic fuels, and blends of synthetic fuels with convent
13、ional petroleum-derived fuels inthis specification have been evaluated and approved in accordance with the principles established in Practice D4054.1.8 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard.1.9 This standard does not
14、 purport 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 safety, health, and healthenvironmental practices and determine theapplicability of regulatory limitations prior to use.1 This specifi
15、cation is under the jurisdiction ofASTM Committee D02 on Petroleum Products, Liquid Fuels, and Lubricants and is the direct responsibility of SubcommitteeD02.J0.06 on Emerging Turbine Fuels.Current edition approved May 1, 2017Oct. 1, 2017. Published July 2017October 2017. Originally approved in 2009
16、. Last previous edition approved in 20162017 asD7566 16b.D7566 17. DOI: 10.1520/D7566-17.10.1520/D7566-17A.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 previous version. Becauseit may not be tec
17、hnically 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 Changes section appears at the end of thi
18、s standardCopyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States11.10 This international standard was developed in accordance with internationally recognized principles on standardizationestablished in the Decision on Principles for the Deve
19、lopment of International Standards, Guides and Recommendations 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 a
20、nd Liquid Fuels at Atmospheric PressureD93 Test Methods for Flash Point by Pensky-Martens Closed Cup TesterD129 Test Method for Sulfur in Petroleum Products (General High Pressure Decomposition Device Method)D130 Test Method for Corrosiveness to Copper from Petroleum Products by Copper Strip TestD15
21、6 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 Vapor Pressure of Petroleum Products (Reid Method)D381 Test Method for Gum Content in Fuels by Jet Evaporation
22、D445 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 Method for Density, Relative Density, or API Gravity of Crude Petroleum and Liquid Petroleum Products byHydromet
23、er 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 Test Method for Estimation of Net Heat of Combustion of Aviation FuelsD1655 Specification for Aviation Turbine
24、 FuelsD1840 Test Method for Naphthalene Hydrocarbons in Aviation Turbine Fuels by Ultraviolet SpectrophotometryD2276 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 Distil
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