公开(公告)号：US10316688B2

公开(公告)日：2019-06-11

申请号：US15112952

申请日：2015-01-20

Applicant: SAFRAN AIRCRAFT ENGINES

Inventor： Abdelkader Benyahia ,  Jean-Michel Boiteux ,  Maxime Delabriere ,  Matthieu Fiack ,  Eddy Stephane Joel Fontanel ,  Alberto Martin Matos ,  Helene Orsi ,  Philippe Rembry ,  Olivier Renon ,  Giuliana Elisa Rossi

IPC: F01D17/10 ,  F02C9/18

Abstract: A turbomachine including an exhaust housing, including a plurality of arms, the space separating the arms defining openings in which there circulates a primary air flow of the turbomachine, at least one conduit, a) configured to collect a compressed air flow at one of the ends of same, b) the other end of the conduit being connected to at least one opening of the exhaust housing, so as to insert the collected air flow into the primary air flow, the collected air flow having, when inserted into the opening, a Mach number less than or equal to 0.5.