公开(公告)号：US12188362B2

公开(公告)日：2025-01-07

申请号：US18457134

申请日：2023-08-28

Applicant: Airbus Operations SAS

Inventor： Christian Flemin

IPC: B64D29/00 ,  F01D25/12 ,  B64D33/02 ,  B64D33/08

Abstract: An aircraft engine nacelle in which the inner fixed structure has a heat exchanger which is filled with a two-phase heat transfer fluid and which comprises a tube forming a loop with front, rear, lower and upper strands, and also a first complementary strand between the central zones of the front strand and of the upper strand, a second complementary strand between the central zones of the front strand and of the lower strand, a third complementary strand between the central zones of the rear strand and of the upper strand, and a fourth complementary strand between the central zones of the rear strand and of the lower strand.