Granted Patent B2

US 12,404,780 · App. 18/425,993 · Granted Sep 2, 2025

Inventors: Jocelyn Bisson (Québec, CA); Jagdeep Singh Jhinger (Québec, CA); Guy Lefebvre (Québec, CA)

Assignee: PRATT & WHITNEY CANADA CORP.

F01D21/045F01D25/243F02C7/00

Abstract

Claims (22)

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

a main body portion, the main body portion having an outer periphery and an inner periphery and a forward end and an aft end each extending between the outer periphery and the inner periphery, the main body portion having a center axis and also including an outer containment zone and an inner containment zone, the inner containment zone is integrally formed with the outer containment zone in order to provide a single unitary structure and the inner containment zone being radially inward from the outer containment zone, the inner containment zone extending radially outward from the inner periphery and having a plurality of ribs, each of the plurality of ribs extending continuously from the forward end and the aft end and each of the plurality of ribs being substantially parallel to the center axis, wherein the plurality of ribs are each separated by an opening extending into the inner periphery, the opening does not extend to the outer periphery or the forward end or the aft end and each of the plurality of ribs have opposing surfaces that are anularly offset in the same direction with respect to the inner periphery of the containment ring and to a plane extending radially from the center axis.

2. The containment ring as in claim 1 , wherein the plurality of ribs are equally spaced from each other.

3. The containment ring as in claim 1 , further comprising a flange portion secured to the main body portion.

4. The containment ring as in claim 3 , wherein the flange portion is secured to the main body portion via a plurality of tabs.

5. The containment ring as in claim 1 , wherein the main body portion is circular in shape.

6. The containment ring as in claim 1 , wherein the opening extends from the inner periphery and has a scalloped shape.

7. The containment ring as in claim 1 , wherein the opening has an inner surface that is furthest from the inner periphery at a central portion of the opening and a depth of the opening from the inner periphery gradually decreases as it extends from the central portion towards the forward end or the aft end.

8. The containment ring as in claim 7 , wherein the opening has a curved bottom surface that extends from the central portion towards the forward end and the aft end of the main body portion.

9. The containment ring as in claim 1 , wherein an axial length of the inner periphery from the forward end to the aft end is greater than an axial length of the outer periphery from the forward end to the aft end.

10. The containment ring as in claim 1 , wherein the main body portion has a trapezoidal shape in its cross section.

11. The containment ring as in claim 1 , wherein the forward end and the aft end are angled surfaces that extend towards each other from the inner periphery.

12. A turbine casing assembly, comprising:

an outer structural case; and

a containment ring, comprising: a main body portion, the main body portion having an outer periphery and an inner periphery and a forward end and an aft end each extending between the outer periphery and the inner periphery, the main body portion having a center axis and also including an outer containment zone and an inner containment zone, the inner containment zone is integrally formed with the outer containment zone in order to provide a single unitary structure and the inner containment zone being radially inward from the outer containment zone, the inner containment zone extending radially outward from the inner periphery and having a plurality of ribs, each of the plurality of ribs extending continuously from the forward end and the aft end and each of the plurality of ribs being substantially parallel to the center axis, wherein the plurality of ribs are each separated by an opening extending into the inner periphery, the opening does not extend to the outer periphery or the forward end or the aft end and each of the plurality of ribs have opposing surfaces that are angularly offset in the same direction with respect to the inner periphery of the containment ring and to a plane extending radially from the center axis.

13. 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 main body portion, the main body portion having an outer periphery and an inner periphery and a forward end and an aft end each extending between the outer periphery and the inner periphery, the main body portion having a center axis and also including an outer containment zone and an inner containment zone, the inner containment zone is integrally formed with the outer containment zone in order to provide a single unitary structure and the inner containment zone is radially inward from the outer containment zone, the inner containment zone extending radially outward from the inner periphery and having a plurality of ribs, each of the plurality of ribs extending continuously from the forward end and the aft end and each of the plurality of ribs being substantially parallel to the center axis, wherein the plurality of ribs are each separated by an opening extending into the inner periphery, the opening does not extend to the outer periphery or the forward end or the aft end and each of the plurality of ribs have opposing surfaces that are angularly offset in the same direction with respect to the inner periphery of the containment ring and to a plane extending radially from the center axis.

Assignments (1)

Continuity (1)

References Cited (27)