Exhaust housing hub for a turbomachine

Patent metadata

Field	Value
Publication number	US-9970320-B2
Application number	US-201314439998-A
Country	US
Kind code	B2
Filing date	Oct 22, 2013
Priority date	Oct 31, 2012
Publication date	May 15, 2018
Grant date	May 15, 2018

Abstract

An exhaust housing hub of a turbomachine, including a connecting wall and an inner channel wall, the connecting wall connecting the inner channel wall to inner attachment flanges, wherein a radial section of the connecting wall is curved and can be formed, as required, as a single component with the inner channel wall, the hub also including a series of ribs extending radially between the connecting wall and the inner channel wall.

First claim

The invention claimed is:

1. A hub of an exhaust housing of a turbomachine, said hub comprising:
inner attachment flanges intended to be attached to a bearing support;
an annular connecting wall; and
an annular inner channel wall,
wherein the annular connecting wall connects the annular inner channel wall to the inner attachment flanges,
wherein a radial section of the annular connecting wall includes, from the inner attachment flanges to the annular inner channel wall:
a first portion, straight, extending radially in the direction downstream of the hub; and
a second portion with a curved shape, the concavity whereof is oriented upstream of the hub, and
wherein the radial section of the annular connecting wall is curved from the first portion to a junction between the annular connecting wall and the annular inner channel wall,
wherein a series of ribs extends radially between the second portion of the annular connecting wall and the annular inner channel wall.

2. The hub according to claim 1 , wherein the annular connecting wall, the annular inner channel wall, and the inner attachment flanges are formed integrally.

3. The hub according to claim 1 , wherein the curvature of the radial section of the annular connecting wall has no inflection point.

4. The hub according to claim 1 , wherein the annular connecting wall has a concavity oriented upstream of the housing.

5. The hub according to claim 1 , wherein an upstream end of the annular connecting wall, located at the junction between the annular connecting wall and the annular inner channel wall has a tangent parallel to the annular inner channel wall.

6. The hub according to claim 1 , further including a thickness at the intersection between the annular inner channel wall and the annular connecting wall.

7. The hub according to claim 6 , wherein the thickness extends at a right angle with a radial leading edge of the first portions of arms.

8. The hub according to claim 1 , wherein the hub further comprises a first portions of arms, extending from the annular inner channel wall and formed integrally therewith, and intended to be attached to a second portions of arms complementary to the housing.

9. The hub according to claim 1 , further including an annular ridge extending radially from the annular inner channel wall downstream of the series of ribs.

10. The hub according to claim 1 , wherein the radial section of the annular connecting wall further includes a third portion with a curved shape, the concavity whereof is oriented upstream of the hub, a downstream end of the third portion of the radial section of the annular connecting wall is connected to the second portion of the radial section of the annular connecting wall, and an upstream end of the third portion of the radial section of the annular connecting wall is located at the junction between the annular connecting wall and the annular inner channel wall,
wherein the second portion of the radial section of the annular connecting wall and the third portion of the radial section of the annular connecting wall form a concave portion of the annular connecting wall, and
wherein a radius of the second portion of the radial section of the annular connecting wall is greater than a radius of the third portion of the radial section of the annular connecting wall.

11. An exhaust housing for a turbomachine, having a principal direction extending along a longitudinal axis and including
a hub according to claim 1 , centered on the longitudinal axis,
an external frame coaxial with the hub, and
a set of arms connecting the annular inner channel wall to the outer frame.

12. A turbomachine, comprising: an exhaust housing including
a hub, centered on a longitudinal axis of the turbomachine, the hub comprising:
inner attachment flanges intended to be attached to a bearing support;
an annular connecting wall; and
an annular inner channel wall,
wherein the annular connecting wall connects the annular inner channel wall to the inner attachment flanges,
wherein a radial section of the annular connecting wall includes, from the inner attachment flanges to the annular inner channel wall:
a first portion, straight, extending radially in the direction downstream of the hub; and
a second portion with a curved shape, the concavity whereof is oriented upstream of the hub, and
wherein the radial section of the annular connecting wall is curved from the first portion to a junction between the annular connecting wall and the annular inner channel wall,
wherein a series of ribs extends radially between the second portion of the annular connecting wall and the annular inner channel wall;
an external frame coaxial with the hub; and
a set of arms connecting the annular inner channel wall to the outer frame.

Assignees

• Snecma

Inventors

• De Sousa Mario Cesar
• Noel Frederic
• Pommier Nicolas
• Renon Olivier

Classifications

• F01D25/28

  Supporting or mounting arrangements, e.g. for turbine casing · CPC title

• F01D25/243

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

• F01D25/162 Primary

  Bearing supports · CPC title

• F01D9/04

  forming ring or sector · CPC title