IP Library Granted Patent US 7,891,165
Granted Patent B2
US 7,891,165 · App. 12/139,089 · Granted Feb 22, 2011

Exhaust casing hub comprising stress-distributing ribs

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Quick Facts
Patent No.
US 7,891,165
App. No.
12/139,089
Granted
Feb 22, 2011
Kind
B2
Abstract

An exhaust casing hub includes a hub center, and an upstream flange and a downstream flange arranged on either side of the hub center. Each flange is terminated by a rim. A plurality of cuffs are arranged on the hub center so as to form an angle from the tangent toward the radial direction of 10° to 80° , preferably 15° to 75°. At least one rib is formed at the base of each cuff below a critical stress region in the cuff. The rib is joined to the downstream flange by a downstream end and to the upstream flange by an upstream end.

Claims (33)

1. An equipped hub of an exhaust casing comprising:

a hub center;

an upstream flange disposed on an upstream side of the hub center;

a downstream flange disposed on a downstream side of the hub center; and

a plurality of cuffs extending radially from the hub center and arranged circumferentially around the hub center,

wherein at least one rib is provided at an exterior of a base of each cuff so as to surround the cuff below a maximum stress location in the cuff, said rib being joined to the downstream flange at a downstream end of the rib and to the upstream flange at an upstream end of the rib.

2. The equipped hub as claimed in claim 1 , further comprising an upstream rib joined to the upstream flange and a downstream rib joined to the downstream flange.

3. The equipped hub as claimed in claim 1 , wherein a first end of the cuff directly connects with the upstream flange and the downstream flange, and a second end of the cuff directly connects with a circular part so as to form a circular shroud.

4. The equipped hub as claimed in claim 1 , wherein each cuff arranged on the hub center is disposed at an angle of 10° to 80° between a tangent of the hub center and a radial direction of the hub center.

5. The equipped hub as claimed in claim 4 , wherein the angle of each cuff is 15° to 75°.

6. An exhaust casing comprising:

an equipped hub comprising a plurality of cuffs and a shroud surrounding the hub;

arms disposed at an angle of 10° to 80° between a tangent of the hub and a radial direction of the hub, said arms being welded between the shroud and each cuff,

wherein the hub is in accordance with claim 1 .

7. A turbine which comprises an exhaust casing as claimed in claim 6 .

8. A turbomachine which comprises an exhaust casing as claimed in claim 6 .

9. The exhaust casing as claimed in claim 6 , wherein the angle of the arms is 15° to 75°.

10. The equipped hub as claimed in claim 1 , wherein the equipped hub is disposed downstream of a low pressure turbine.

11. The exhaust casing as claimed in claim 1 , wherein the at least one rib provided at the exterior of the base of each cuff entirely surrounds the cuff.

12. An equipped hub of an exhaust casing comprising:

a hub center;

an upstream flange disposed on an upstream side of the hub center;

a downstream flange disposed on a downstream side of the hub center; and

a plurality of cuffs arranged circumferentially around the hub center,

wherein at least one rib is provided at an exterior of a base of each cuff below a maximum stress location in the cuff, said rib being joined to the downstream flange at a downstream end of the rib and to the upstream flange at an upstream end of the rib, and

wherein the rib is joined to the flange via a fillet, and the fillet directly contacts an inner face of the upstream flange.

13. An equipped hub of an exhaust casing comprising:

a hub center;

an upstream flange disposed on an upstream side of the hub center;

a downstream flange disposed on a downstream side of the hub center; and

a plurality of cuffs arranged circumferentially around the hub center,

wherein at least one rib is provided at an exterior of a base of each cuff below a maximum stress location in the cuff, said rib being joined to the downstream flange at a downstream end of the rib and to the upstream flange at an upstream end of the rib, and

wherein the rib is joined to the flange via a fillet, and the fillet directly contacts an inner face of the downstream flange.

Assignments (2)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →