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Standard Test Method for Freezing Point of Aviation Fuels (Includes all amendments And changes 1/22/2019).
Automaticky přeložený název:
Standardní zkušební metoda pro bod tuhnutí paliv letectví
NORMA vydána dne 1.6.2015
Označení normy: ASTM D2386-15e1
Poznámka: NEPLATNÁ
Datum vydání normy: 1.6.2015
Kód zboží: NS-612377
Počet stran: 5
Přibližná hmotnost: 15 g (0.03 liber)
Země: Americká technická norma
Kategorie: Technické normy ASTM
Keywords:
aviation gasoline, aviation turbine fuels, crystallization point, determination, freezing point, low temperature tests, manual method, petroleum products, physical tests,, ICS Number Code 75.160.20 (Liquid fuels)
Significance and Use | ||||||||||||||||
4.1 The freezing point of an aviation fuel is the lowest temperature at which the fuel remains free of solid hydrocarbon crystals that can restrict the flow of fuel through filters if present in the fuel system of the aircraft. The temperature of the fuel in the aircraft tank normally falls during flight depending on aircraft speed, altitude, and flight duration. The freezing point of the fuel must always be lower than the minimum operational tank temperature. 4.2 Freezing point is a requirement in Specifications D910 and D1655. |
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1. Scope | ||||||||||||||||
1.1 This test method covers the determination of the temperature below which solid hydrocarbon crystals may form in aviation turbine fuels and aviation gasoline. Note 1: The interlaboratory program that generated the
precisions for this test method did not include aviation
gasoline.
1.2 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard. 1.3 1.4 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 5.4, Section 6, and 8.3. |
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2. Referenced Documents | ||||||||||||||||
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