ASTM D3241-2016a
航空涡轮机燃料油热氧化安定性的标准试验方法

Standard Test Method for Thermal Oxidation Stability of Aviation Turbine Fuels

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标准号

ASTM D3241-2016a

发布日期

2016年

实施日期

废止日期

无

中国标准分类号

E31

国际标准分类号

75.160.20

发布单位

US-ASTM

适用范围

5.1x00a0;The test results are indicative of fuel performance during gas turbine operation and can be used to assess the level of deposits that form when liquid fuel contacts a heated surface that is at a specified temperature.

1.1x00a0;This test method covers the procedure for rating the tendencies of gas turbine fuels to deposit decomposition products within the fuel system.

1.2x00a0;The differential pressure values in mm Hg are defined only in terms of this test method.

1.3x00a0;The deposition values stated in SI units shall be regarded as the referee value.

1.4x00a0;The pressure values stated in SI units are to be regarded as standard. The psi comparison is included for operational safety with certain older instruments that cannot report pressure in SI units.

1.5x00a0;No other units of measurement are included in this standard.

1.6x00a0;WARNINGx2014;Mercury has been designated by many regulatory agencies as a hazardous material that can cause central nervous system, kidney and liver damage. Mercury, or its vapor, may be hazardous to health and corrosive to materials. Caution should be taken when handling mercury and mercury containing products. See the applicable product Material Safety Data Sheet (MSDS) for details and EPAx2019;s websitex2014;http://www.epa.gov/mercury/faq.htmx2014;for additional information. Users should be aware that selling mercury and/or mercury containing products into your state or country may be prohibited by law.

1.7x00a0;This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use. For specific warning statements, see 6.1.1, 7.2, 7.2.1, 7.3, 11.1.1, and Annex A5.