Structural casing for an axial turbine engine

Patent metadata

Field	Value
Publication number	US-10907504-B2
Application number	US-201916263958-A
Country	US
Kind code	B2
Filing date	Jan 31, 2019
Priority date	Feb 2, 2018
Publication date	Feb 2, 2021
Grant date	Feb 2, 2021

Abstract

A structural casing for an axial turbine engine includes an outer ring, an inner hub, and a plurality of struts extending radially from the hub to the ring, wherein the ring is made of a plurality of angular segments welded together. The segments extend circumferentially of different angles, some segments being larger angularly than others. The structural casing is adapted to be an intermediate casing between two compressors of a turbine engine.

First claim

We claim:

1. A structural casing for an axial turbomachine, the casing comprising:
an outer ring;
an inner hub; and
a plurality of struts extending radially from the inner hub to the outer ring, the outer ring being made of a plurality of angular segments welded to each other, and each segment of the plurality of angular segments being welded to at least one strut of the plurality of struts;
wherein at least two of the angular segments extend angularly of different angles.

2. The structural casing according to claim 1 , wherein the at least two of the angular segments extend of two respective angles, one of which being at least twice the other one.

3. The structural casing according to claim 1 wherein the plurality of angular segments comprises:
exactly three angular segments, one of which extending angularly over between 80° and 100°.

4. The structural casing according to claim 1 , wherein the plurality of angular segments comprises:
exactly four angular segments, one of which extending angularly over more than 90°.

5. The structural casing according to claim 1 , wherein the plurality of angular segments comprises:
at least five angular segments, the at least five angular segments comprising:
at least three large angular segments, each of them extending angularly over between 80° and 100°; and
at least two small angular segments, each of them extending angularly over between 30° and 60°.

6. The structural casing according to claim 5 , wherein at least one of the at least three large angular segments is arranged angularly between two of the at least two small angular segments.

7. The structural casing according to claim 5 , wherein at least one of the at least three large angular segments is provided with an attachment ring for attaching the casing to a pylon of an aircraft wing.

8. The structural casing according to claim 1 , wherein the plurality of angular segments comprises:
two angular segments made of different material.

9. The structural casing according to claim 1 , wherein each of the struts comprises:
an internal end welded to the inner hub and an external end welded to the outer ring.

10. The structural casing according to claim 1 , wherein at least one fastening flange is provided integral to the angular segments.

11. The structural casing according to claim 1 , wherein the inner hub is made of a plurality of angular parts.

12. The structural casing according to claim 1 , wherein the struts are hollow.

13. A method for manufacturing a structural casing for an axial turbomachine, the structural casing comprising:
an outer ring;
an inner hub; and
a plurality of struts extending radially from the inner hub to the outer ring; the method comprising a welding step wherein a plurality of angular segments are welded to each other to form the outer ring, and each angular segment of the plurality of segments is welded to at least one strut of the plurality of struts;
wherein the inner hub and the struts are a one-piece cast part.

14. The method according to claim 13 , wherein the struts are distributed angularly irregularly.

15. A structural casing for an axial turbomachine, the casing comprising:
an outer ring;
an inner hub; and
a plurality of struts extending radially from the inner hub to the outer ring, wherein the outer ring is made of a plurality of angular segments welded to each other, and welded to the struts, the plurality of angular segments having contact surfaces where the angular segments join each other;
wherein the inner hub is made of a plurality of angular parts, welded to each other, and welded to the struts, the plurality of angular parts having contact surfaces where the angular parts join each other; and
wherein at least one contact surface of one of the angular segments is arranged at a circumferential position that differs from all the contact surfaces of the angular parts.

16. The structural casing according to claim 15 , wherein the inner hub comprises:
an external surface with recesses for receiving the struts.

17. The structural casing according to claim 16 , wherein the external surface is conical.

18. The structural casing according to claim 15 , wherein at least two of the angular segments extend angularly of different angles.

19. The structural casing according to claim 18 , wherein the at least two of the angular segments extend of two respective angles, one of which being at least three times the other one.

20. The structural casing according to claim 18 , wherein the plurality of angular parts comprises:
at least three large angular parts, each large angular part extending angularly over between 80° and 100°; and
at least two small angular parts, each small angular part extending angularly over between 30° and 60°.

Assignees

• Safran Aero Boosters Sa

Inventors

• Bovyn Ludovic
• Englebert Eric
• Peeters Maxime

Classifications

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title

• F01D9/042 Primary

  fixing blades to stators (fixing stator-rings in the casing or to each other F01D25/246) · 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

• F01D25/243

  Flange connections; Bolting arrangements (F01D25/265 takes precedence) · CPC title

• F05D2250/52

  Outlet · CPC title