AIRCRAFT ENGINE FUEL CIRCUIT VALVE SLIDE

The present invention relates to a slide (22) for a fuel circuit valve (20) of an aircraft engine extending along a longitudinal axis (23), and comprising a narrowed intermediate portion (32) extending between two cylindrical end portions (29, 31), a first end portion (29) being separated from the n...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	PORA LOIC, CEBILLE CHRISTOPHE, BERNARD CLEMENT
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	ACTUATING-FLOATS BLASTING COCKS DEVICES FOR VENTING OR AERATING ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MECHANICAL ENGINEERING TAPS THERMAL INSULATION IN GENERAL VALVES WEAPONS
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