Transition duct cooling feed tubes

• US 8,151,570 B2
• Filed: 12/06/2007
• Issued: 04/10/2012
• Est. Priority Date: 12/06/2007
• Status: Active Grant

• Current Assignee: Ansaldo Energia Switzerland AG
• Original Assignee: Alstom Technology Ltd. (Alstom SA)
• Inventors: Jennings, Stephen, Stuttaford, Peter, Jorgensen, Stephen W.
• Primary Examiner(s): Rodriguez, William H
• Assistant Examiner(s): Choi, Young
• Application Number:
  US11/951,790
• Publication Number:
  US 20090145099A1
• Time in Patent Office: 1,587 Days
• Field of Search: 607/59, 607/52, 607/54, 607/55, 607/57, 607/58, 607/60
• US Class Current: 60/759
• CPC Class Codes: F01D 25/12 Cooling
• CPC Class Codes: F01D 9/023 Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
• CPC Class Codes: F05D 2260/20 Heat transfer, e.g. cooling
• CPC Class Codes: F05D 2260/201 by impingement of a fluid

Abstract

Embodiments for an apparatus and associated method for providing a cooling fluid to a gas turbine transition duct in order to lower the effective operating temperatures of the transition duct are disclosed. The transition duct has an inner liner and an impingement sleeve positioned radially outward with a passageway formed therebetween. The impingement sleeve has a plurality of openings where a portion of the openings each have a feed tube extending through the opening and into the passageway. The feed tubes are oriented at an angle relative to the impingement sleeve, such that an inlet to the feed tube is directed generally towards an oncoming flow of cooling fluid. The feed tubes direct a portion of the cooling fluid toward the inner liner and into the passageway for cooling of the transition duct.

Claims

1. An assembly of transition ducts for a gas turbine engine, each transition duct comprising:

an inner liner having a first liner end and a second liner end;

an impingement sleeve positioned radially outward of an encompassing the inner liner and having a first sleeve end, a second sleeve end, and a plurality of openings;

a plurality of feed tubes positioned through at least a portion of the plurality of openings, the feed tubes are configured with a tube length, the tube length having a tube inlet and a tube outlet, wherein the feed tubes extend into a passageway formed between the inner liner and the impingement sleeve;

a plurality of retaining devices having at least one extending portion extending outward from the tube inlet of the feed tubes, respectively, wherein the at least one extending portion of the plurality of retaining devices prevents the feed tubes, respectively, from sliding into the passageway, wherein the contact between the at least one extending portion and the impingement sleeve fixedly retain the feed tubes within the impingement sleeve at a plurality of surface angles, respectively, and wherein the plurality of surface angles are generally established by the retaining devices, respectively, to receive oncoming cooling flow; and

a mounting bracket,

wherein the transition ducts are mounted adjacent to each other with gaps therebetween, such that the plurality of feed tubes are positioned to extend into the gaps so as to locally capture additional cooking air for increasing air pressure in the passageway.

2. The transition duct of claim 1, wherein the inner liner further comprises a thermal barrier coating.

3. The transition duct of claim 1, wherein the first liner end and first sleeve end are generally cylindrical and the second liner end and second sleeve end are generally arc-shaped rectangles.

4. The transition duct of claim 3, wherein the passageway varies in cross-sectional area from the second end to the first end.

5. The transition duct of claim 1, wherein a cross-sectional, radially measured, inner diameter of the tube inlet is greater than a cross-sectional, radially measured, inner diameter of the tube outlet.

6. The transition duct of claim 1, wherein the plurality of feed tubes are oriented at an angle relative to the impingement sleeve such that the tube inlet is directed generally towards an oncoming flow of cooling fluid.

7. The transition duct of claim 1, wherein the plurality of feed tubes are permanently fixed to the impingement sleeve of the transition duct.

13. The transition duct of claim 4, wherein the surface angles of the feed tubes with respect to the impingement sleeve vary in degree across the feed tubes in accordance with the variation in cross-sectional area of the passageway.

8. A feed tube for a gas turbine transition duct comprising:

a generally cylindrical portion having a tube inlet and a tube outlet located at opposed ends of a tube length and oriented in parallel-spaced relation, the cylindrical portion is provided with an inner wall, an outer wall, and a thickness therebetween, a cross-sectional, radially measured, inner diameter of the tube inlet is greater than a cross-sectional, radially measured, inner diameter of the tube outlet,

wherein the feed tube is capable of being positioned within an opening of a transition duct outer wall and extending into an atmosphere region between adjacent transition ducts; and

a retaining device having a extending portion extending outward from the tube inlet of the feed tube, respectively, wherein the extending portion of the retaining device prevents the feed tube, respectively, from sliding into the passageway, wherein the contact between the extending portion and the transition duct outer wall fixedly retain the feed tube within the transition duct outer wall at a plurality of surface angles, respectively, and wherein the plurality of surface angles are generally established by the retaining device, respectively, to receive oncoming cooling flow.

9. The feed tube of claim 8, wherein the feed tube is fixed to the transition duct outer wall.

10. The feed tube of claim 9, wherein the feed tube outlet extends into the passageway.

11. The feed tube of claim 8, wherein the retaining device is generally D-shaped.

12. A transition duct of a gas turbine engine, the transition duct comprising:

an inner liner for directing hot combustion gas from a combustor to a turbine;

an impingement sleeve radially encompassing the inner liner to form a passageway, wherein the impingement sleeve is formed with a plurality of openings, and wherein the passageway varies in cross-sectional area from a first end to a second end thereof;

a plurality of feed tubes positioned through at least a portion of the plurality of openings, respectively, the feed tubes configured with a tube length, the tube length having a tube inlet and a tube outlet, wherein the feed tubes extend into a passageway at respective penetration depths, wherein the penetration depths vary in length across the feed tubes in accordance with the variation in cross-sectional area of the passageway; and

a plurality of retaining devices having a extending portion extending outward from the tube inlet of the feed tubes, respectively, wherein the extending portion of the retaining devices prevents the feed tubes, respectively, from sliding into the passageway, wherein the contact between the extending portion and the impingement sleeve fixedly retain the feed tube within the impingement sleeve at a plurality of surface angles, respectively, and wherein the plurality of surface angles are generally established by the retaining device, respectively, to receive oncoming cooling flow.