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

• Main Author: CHALAUD SEBASTIEN CHRISTOPHE
• Format: Patent
• Language: Chinese; English
• Published: 17.07.2018
• Subjects: 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

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...