公开(公告)号：US20220025816A1

公开(公告)日：2022-01-27

申请号：US17492783

申请日：2021-10-04

Applicant: Safran Nacelles

Inventor： Julien CORBIN ,  David PEREIRA ,  Vincent PEYRON ,  Jean-Nicolas BOUCHOUT ,  Caroline DANG ,  Nicolas CHOUQUET

IPC: F02C7/18 ,  F02C9/00

Abstract: A cooling system for cooling an aircraft turbojet engine includes a first heat-exchanger for exchanging heat between a heat-transfer fluid and a lubricant of the turbojet engine, a second heat-exchanger for exchanging heat between the heat-transfer fluid and air, and a circulation duct for circulating heat-transfer fluid in a closed circuit. The cooling system further includes at least one regulating device for regulating the heat drawn from the lubricant, controlled by a control module of the regulating device that is configured to receive information according to the various flight phases.