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Standard Test Method for Thermal Oxidation Stability of Aviation Turbine Fuels (Includes all amendments And changes 12/19/2014).
Automaticky přeložený název:
Standardní zkušební metoda pro teplotní oxidační stability leteckých turbín paliv
NORMA vydána dne 1.5.2014
Označení normy: ASTM D3241-14e1
Poznámka: NEPLATNÁ
Datum vydání normy: 1.5.2014
Kód zboží: NS-22997
Počet stran: 21
Přibližná hmotnost: 63 g (0.14 liber)
Země: Americká technická norma
Kategorie: Technické normy ASTM
Keywords:
differential pressure, fuel decomposition, oxidative deposits, test filter deposits, thermal stability, turbine fuel, ICS Number Code 75.160.20 (Liquid fuels)
Significance and Use | ||||||||||||||
5.1 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. |
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1. Scope | ||||||||||||||
1.1 This test method covers the procedure for rating the tendencies of gas turbine fuels to deposit decomposition products within the fuel system. 1.2 The differential pressure values in mm Hg are defined only in terms of this test method. 1.3 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard. 1.4 1.5 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. |
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2. Referenced Documents | ||||||||||||||
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