公开(公告)号：US20210231057A1

公开(公告)日：2021-07-29

申请号：US17158982

申请日：2021-01-26

Applicant: Airbus Operations SAS

Inventor： Thomas LIVEBARDON ,  Maxime ZEBIAN

IPC: F02C7/24 ,  F02C7/14

Abstract: A turbomachine for an aircraft, comprising a thermoacoustic system associated with a fluid circuit that serves to supply the motor of the turbomachine with fluid. The thermoacoustic system comprises an exchanger which is connected to the fluid circuit and in which there flows a fluid that is to be cooled, an acoustic attenuation structure which is distinct from the exchanger and which forms all or part of a wall of the fan duct, and at least one heat-duct tube comprising a portion that is entirely received in the acoustic structure and a portion with an end that is received in the exchanger, and a single curved elbow with a non-zero angle between the two portions.