公开(公告)号：US20220186681A1

公开(公告)日：2022-06-16

申请号：US17653245

申请日：2022-03-02

Applicant: SAFRAN AIRCRAFT ENGINES

Inventor： Samuel Louis-Marie BERNARD

IPC: F02K1/04

Abstract: An aircraft turbine engine module, including a degassing tube and an ejection cone. The tube and the cone are engageable together by structures which cause them to be centered when engaged together. Also provided is a locating and adjusting tool for assembling the module.

公开(公告)号：US20180313268A1

公开(公告)日：2018-11-01

申请号：US15769060

申请日：2016-10-25

Applicant: SAFRAN AIRCRAFT ENGINES

Inventor： Samuel Louis-Marie BERNARD

IPC: F02C7/06 ,  F02K1/04

CPC classification number: F02C7/06 ,  F02K1/04 ,  F05D2260/30 ,  F05D2260/605 ,  F05D2260/608 ,  F05D2260/609

Abstract: The invention relates to an aircraft turbine engine module (10), comprising a degassing tube (14) and an ejection cone (12). The tube end the cone comprise centring means engaging together. The invention also relates to a locating and adjusting tool for assembling said module.