Method for manufacturing a turbomachine exhaust casing from segments welded together

Patent metadata

Field	Value
Publication number	US-11261756-B2
Application number	US-201716304110-A
Country	US
Kind code	B2
Filing date	May 22, 2017
Priority date	May 26, 2016
Publication date	Mar 1, 2022
Grant date	Mar 1, 2022

Abstract

A method for manufacturing a casing, for example, an exhaust casing, for a turbomachine. The method generally includes: (a) producing casing sectors, each casing sector having a hub sector, a ferrule sector, and at least one arm linking the hub and ferrule sectors, (b) arranging the casing sectors adjacently and circumferentially, such that each hub sector has longitudinal edges facing longitudinal edges of adjacent hub sectors, (c) welding the longitudinal edges facing the hub sectors, and (d) adding and welding at least a second part of the ferrule to the casing sectors.

First claim

The invention claimed is:

1. A method for manufacturing an casing ( 10 ′) for a turbomachine, the casing having an inner hub and an outer annular ferrule extending around the inner hub about an axis of rotation, the ferrule rigidly linked to the hub by arms and configured to define, with the inner hub, an annular flow path for a gas stream the method comprising:
(a) producing casing sectors, wherein each casing sector comprises a hub sector , a first ferrule sector, and at least one arm linking the hub and ferrule sectors;
(b) arranging the casing sectors adjacently and circumferentially with respect to the axis, such that each hub sector has longitudinal edges ( 34 ) facing longitudinal edges of adjacent hub sectors;
c) welding the longitudinal edges facing the hub sectors, wherein, in step (b), at least some of the first ferrule sectors have longitudinal edges at a circumferential distance of longitudinal edges of first adjacent ferrule sectors; and
(d) adding and welding second ferrule sectors between the longitudinal edges at a distance from the first ferrule sectors.

2. The method of claim 1 , wherein, in step (b), at least some of the first ferrule sectors have longitudinal edges facing longitudinal edges of first adjacent ferrule sectors, and, in step (c), the longitudinal edges facing the first ferrule sectors are welded.

3. The method of claim 1 , wherein at least some of the first ferrule sectors, some of the second ferrule sectors, or some of the first and second ferrule sectors are formed form one single part with a tread.

4. The method of claim 1 , wherein at least some of the casing sectors have first ferrule sectors having a circumferential extent less than that of the corresponding hub sectors.

5. The method of claim 1 , wherein the number of casing sectors is equal to the number of arms.

6. The method of claim 1 , wherein the casing sectors are manufactured by casting.

7. The method of claim 1 , wherein the inner hub comprises: a first substantially cylindrical annular wall linked at an axial end to a second substantially frustoconical annular wall; and stiffeners extending between the lower surfaces of the first and second annular walls, the stiffeners extending substantially to the right of radially inner ends of the arms, wherein each hub sector comprises at least one stiffener.

Assignees

• Safran Aircraft Engines

Inventors

• Debray Benoit Argémiro Matthieu
• Fouquet Dominique Michel
• Ghosarossian-Prillieux Grégory
• Sevi Guillaume
• Sultana Patrick
• Vieillefond Guy

Classifications

• B23K15/0093

  characterised by the properties of the materials to be welded · CPC title

• B23K31/02 Primary

  relating to soldering or welding · CPC title

• F01D25/24 Primary

  Casings (modified for heating or cooling F01D25/14); Casing parts, e.g. diaphragms, casing fastenings (casings for rotary machines or engines in general F16M {; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045}) · CPC title

• F05D2230/60

  Assembly methods · CPC title

• B23K15/006

  of rectilinear seams · CPC title