ASTM D7566-2016b red 6591 Standard Specification for Aviation Turbine Fuel Containing Synthesized Hydrocarbons《含合成碳氢化合物的航空涡轮机燃料的标准规格》.pdf
《ASTM D7566-2016b red 6591 Standard Specification for Aviation Turbine Fuel Containing Synthesized Hydrocarbons《含合成碳氢化合物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 D7566-2016b red 6591 Standard Specification for Aviation Turbine Fuel Containing Synthesized Hydrocarbons《含合成碳氢化合物的航空涡轮机燃料的标准规格》.pdf(43页珍藏版)》请在麦多课文档分享上搜索。
1、Designation: D7566 16aD7566 16b 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 th
2、e 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 requiremen
4、ts 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5、) the unique requirements of this specification are no longer applicable: any recertification shall be done in accordance withTable 1 of Specification D1655.1.2.2 Field blending of synthesized paraffinic kerosine (SPK) blendstocks,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(HEFASPK), AnnexA3 (SIP),
6、 synthesized paraffinic kerosine plus aromatics (SPK/A), or AnnexA5 (ATJ) as described in AnnexA4 with D1655 fuel (which may on the whole or in part have originated as D7566 fuel) shall be considered batch origination inwhich case all of the requirements of Table 1 of this specification (D7566) appl
7、y 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 specific types of the minimum property requirements for aviation turbine fuel that containsynthesized hydrocarbons for civil use in the operation and certification of aircraftand li
9、sts acceptable additives for use in civiloperated engines and aircrafts. Specification D7566 and describes fuels found satisfactory for the operation of aircraft and engines.The specification is intended to be used as a standard in describing the quality of aviation turbine fuels and synthetic blend
10、ingcomponents 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.is directed at civil applications, and maintained as such, but may be adopted for military,government, or other specialized use
11、s.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 specification does not define the quality assurance testing and procedures necessary to ensure that fuel in thedistribution system continues to comply w
12、ith this specification after batch certification. Such procedures are defined elsewhere, forexample in ICAO 9977, EI/JIG Standard 1530, JIG 1, JIG 2, API 1543, API 1595, and ATA-103.1.5 This specification does not include all fuels satisfactory for aviation turbine engines. Certain equipment or cond
13、itions of usemay permit a wider, or require a narrower, range of characteristics than is shown by this specification.1.6 While aviation turbine fuels defined by Table 1 of this specification can be used in applications other than aviation turbineengines, requirements for such other applications have
14、 not been considered in the development of this specification.1.7 Synthetic blending components, synthetic fuels, and blends of synthetic fuels with conventional petroleum-derived fuels inthis specification have been evaluated and approved in accordance with the principles established in Practice D4
15、054.1.8 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard.1 This specification is under the jurisdiction ofASTM Committee D02 on Petroleum Products, Liquid Fuels, and Lubricants and is the direct responsibility of SubcommitteeD0
16、2.J0.06 on Emerging Turbine Fuels.Current edition approved June 1, 2016July 1, 2016. Published August 2016. Originally approved in 2009. Last previous edition approved in 2016 asD7566 16.D7566 16a. DOI: 10.1520/D7566-16A.10.1520/D7566-16B.This document is not an ASTM standard and is intended only to
17、 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 current versionof
18、 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 States11.9 This standard does not purport to addres
19、s all of the safety concerns, if any, associated with its use. It is the responsibilityof the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatorylimitations prior to use.2. Referenced Documents2.1 ASTM Standards:2D56 Test Method fo
20、r Flash Point by Tag Closed Cup TesterD86 Test Method for Distillation of Petroleum Products and 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 Metho
21、d)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 Vapor Pressure o
22、f 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 Method for Density
23、, 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 Test Method for
24、Estimation of Net Heat of Combustion of Aviation FuelsD1655 Specification for Aviation Turbine 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 Metho
- 1.请仔细阅读文档,确保文档完整性,对于不预览、不比对内容而直接下载带来的问题本站不予受理。
- 2.下载的文档,不会出现我们的网址水印。
- 3、该文档所得收入(下载+内容+预览)归上传者、原创作者;如果您是本文档原作者,请点此认领!既往收益都归您。
下载文档到电脑,查找使用更方便
5000 积分 0人已下载
下载 | 加入VIP,交流精品资源 |
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- ASTMD75662016BRED6591STANDARDSPECIFICATIONFORAVIATIONTURBINEFUELCONTAININGSYNTHESIZEDHYDROCARBONS 合成

链接地址:http://www.mydoc123.com/p-525832.html