A method is provided for treating a fuel system 22 of a turbine engine 24. During this method, a treatment system 20 is connected to the turbine engine. Preservation fluid is drawn out of the fuel system using the treatment system. I - rI I I E on to I I I u I I ~- - to U, I 4~kD I C-' E-ao
De-Preserving a Fuel System of a Turbine Engine
02.02.2023
Patent
Elektronische Ressource
Englisch
IPC: | F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT ENDURANCE TEST (CONTAMINATED FUEL)
SAE Technical Papers | 1981