System and method for supplying lubrication fluid to at least one member of aircraft propulsion assembly

The invention relates to a system (1, 100, 110) for supplying lubricating oil to members of a turbine engine having one reducer. The power supply system (1, 100) includes: a kinetic pumping device (2)to be connected upstream to an oil tank (3) and rotated at a decorrelated speed of an operation mode...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	CHALAUD SEBASTIEN CHRISTOPHE
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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