"NON-FLAME-OUT TEST FOR THE COMBUSTION CHAMBER OF A TURBINE ENGINE"

The invention relates in a method for the ground control of the proper operation of an aeronautical turbine engine for a plane. Accordingly, the lest comprises carrying out, on the operating turbine engine and from a predetermined speed, a quick reduction in the fuel flow according to a programmed d...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	PHILIPPE ROGER COURTIE, HUBERT PASCAL VERDIER, PHILIPPE ETCHEPARE
Format:	Patent
Sprache:	eng
Schlagworte:	MEASURING PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
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Beschreibung
Zusammenfassung:	The invention relates in a method for the ground control of the proper operation of an aeronautical turbine engine for a plane. Accordingly, the lest comprises carrying out, on the operating turbine engine and from a predetermined speed, a quick reduction in the fuel flow according to a programmed decrease in order to evaluate the flame-oul resistance of the combustion chamber of said turbine engine during a quick inflight deceleration manoeuver of the speed thereof.