Granted Patent B2

US 12,398,661 · App. 18/426,019 · Granted Aug 26, 2025

Inventors: Jocelyn Bisson (Saint-Basile-le-Grand, CA); Guy Lefebvre (St-Bruno, CA)

Assignee: PRATT & WHITNEY CANADA CORP.

F01D25/243F02C7/00

Abstract

Claims (37)

1. A containment ring assembly for a turbine casing assembly, comprising:

a first inner containment ring, the first inner containment ring having a thickened main body portion, the thickened main body portion having a forward end and an aft end;

a second inner containment ring, the second inner containment ring having a thickened main body portion, the thickened main body portion having a forward end and an aft end;

an outer containment ring, the outer containment ring having a thickened main body portion, the thickened main body portion having a forward end and an aft end, the thickened main body portion of the outer containment ring being at least partially located between the aft end of the thickened main body portion of the first inner containment ring and the forward end of the thickened main body portion of the second inner containment ring, the first inner containment ring and the second inner containment ring being radially inward from the outer containment ring, wherein a radial space is located between the outer containment ring and the first inner containment ring and the second inner containment ring, the radial space allowing the first inner containment ring and the second inner containment ring to deform freely with regard to the outer containment ring.

2. The containment ring assembly as in claim 1 , wherein the first inner containment ring is secured to the second inner containment ring by a first plurality of frangible tab members.

3. The containment ring assembly as in claim 2 , wherein the outer containment ring is secured to the first inner containment ring by a second plurality of frangible tab members.

4. The containment ring assembly as in claim 3 , wherein the outer containment ring is secured to the second inner containment ring by a third plurality of frangible tab members.

5. The containment ring assembly as in claim 4 , wherein the second inner containment ring is secured to a flange portion by a fourth plurality of frangible tab members.

6. The containment ring assembly as in claim 5 , wherein each of the first, second, third and fourth plurality of frangible tab members are separated from each other by one of a plurality of openings.

7. The containment ring assembly as in claim 1 , wherein the first inner containment ring defines a first stage containment zone and the outer containment ring defines a second stage containment zone and the second inner containment ring defines a third stage containment zone.

8. The containment ring assembly as in claim 7 , wherein the first inner containment ring is secured to the second inner containment ring by a first plurality of frangible tab members.

9. The containment ring assembly as in claim 8 , wherein the outer containment ring is secured to the first inner containment ring by a second plurality of frangible tab members.

10. The containment ring assembly as in claim 9 , wherein the outer containment ring is secured to the second inner containment ring by a third plurality of frangible tab members.

11. A turbine casing assembly, comprising:

an outer structural case; and

a containment ring, comprising:

a first inner containment ring, the first inner containment ring having a thickened main body portion, the thickened main body portion having a forward end and an aft end;

a second inner containment ring, the second inner containment ring having a thickened main body portion, the thickened main body portion having a forward end and an aft end;

an outer containment ring, the outer containment ring having a thickened main body portion, the thickened main body portion having a forward end and an aft end, the thickened main body portion of the outer containment ring being at least partially located between the aft end of the thickened main body portion of the first inner containment ring and the forward end of the thickened main body portion of the second inner containment ring, the first inner containment ring and the second inner containment ring being radially inward from the outer containment ring, wherein a radial space is located between the outer containment ring and the first inner containment ring and the second inner containment ring, the radial space allowing deformation of the first inner containment ring and the second inner containment ring to deform freely with regard to the outer containment ring.

12. The turbine casing assembly as in claim 11 , wherein the first inner containment ring is secured to the second inner containment ring by a first plurality of frangible tab members.

13. The turbine casing assembly as in claim 12 , wherein the outer containment ring is secured to the first inner containment ring by a second plurality of frangible tab members.

14. The turbine casing assembly as in claim 13 , wherein the outer containment ring is secured to the second inner containment ring by a third plurality of frangible tab members.

15. The turbine casing assembly as in claim 14 , wherein the second inner containment ring is secured to a flange portion by a fourth plurality of frangible tab members and the flange portion is secured to the outer structural case.

16. The turbine casing assembly as in claim 15 , wherein each of the first, second, third and fourth plurality of frangible tab members are separated from each other by one of a plurality of openings.

17. The turbine casing assembly as in claim 11 , wherein the first inner containment ring defines a first stage containment zone and the outer containment ring defines a second stage containment zone and the second inner containment ring defines a third stage containment zone.

18. The turbine casing assembly as in claim 17 , wherein the first inner containment ring is secured to the second inner containment ring by a first plurality of frangible tab members.

19. The turbine casing assembly as in claim 18 , wherein the outer containment ring is secured to the first inner containment ring by a second plurality of frangible tab members.

20. A gas turbine engine, comprising:

a compressor section;

a combustor;

a turbine section; and

a turbine casing assembly, comprising:

an outer structural case; and

a containment ring, comprising:

a first inner containment ring, the first inner containment ring having a thickened main body portion, the thickened main body portion having a forward end and an aft end;

a second inner containment ring, the second inner containment ring having a thickened main body portion, the thickened main body portion having a forward end and an aft end;

an outer containment ring, the outer containment ring having a thickened main body portion, the thickened main body portion having a forward end and an aft end, the thickened main body portion of the outer containment ring being at least partially located between the aft end of the thickened main body portion of the first inner containment ring and the forward end of the thickened main body portion of the second inner containment ring, the first inner containment ring and the second inner containment ring being radially inward from the outer containment ring, wherein a radial space is located between the outer containment ring and the first inner containment ring and the second inner containment ring, the radial space allowing deformation of the first inner containment ring and the second inner containment ring to deform freely with regard to the outer containment ring, the first inner containment ring being aligned with a first stage rotor of the turbine section, the outer containment ring being aligned with a second stage rotor of the turbine section, and the second inner containment ring being aligned with a third stage rotor of the turbine section.

Assignments (1)

Continuity (1)

References Cited (23)