Standard Test Method for Thermal Oxidation Stability of Aviation Turbine Fuels

Importancia y uso:

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.

Subcomité:

D02.J0.03

Referida por:

D7671-21, D6469-24, D7667-21, D1655-25A, D6615-25, D6469-24, D7671-21, D7223-21, D8147-24, D5677-17R23, D7566-25A, D1655-25A, D7667-21, D1655-25A, D4054-25A

Volúmen:

05.01

Número ICS:

75.160.20 (Liquid fuels)

Palabras clave:

differential pressure; fuel decomposition; heater tube deposits; oxidative deposits; thermal stability; turbine fuel ;