D5/D5A DF-42 integrated exit cone and splash plate

Patent metadata

Field	Value
Publication number	US-10139108-B2
Application number	US-201514732954-A
Country	US
Kind code	B2
Filing date	Jun 8, 2015
Priority date	Jun 8, 2015
Publication date	Nov 27, 2018
Grant date	Nov 27, 2018

Abstract

A combustor basket assembly for a gas turbine engine that includes a combustor basket having a basket liner including an input end and an output end. An integrated exit cone and splash plate member is affixed to the output end of the basket liner and includes a base portion, an exit cone portion and a splash plate portion. The base portion includes an annular cooling channel that receives a cooling air flow and the exit cone portion and the splash plate portion each include an array of cooling feed holes in fluid communication with the cooling channel. The spacing between the feed holes and the size of the feed holes can be optimized to provide more cooling for hotter regions.

First claim

What is claimed is:

1. A combustor basket assembly for a combustor in a gas turbine engine, said combustor basket assembly comprising a combustor basket including a basket liner having an input end and an output end through which a hot working gas exits the combustor basket, said combustor basket further including a single piece member affixed to the output end of the basket liner, said single piece member including a base portion, a splash plate portion integral with the base portion and an exit cone portion integral with the base portion, where the hot working gas exits the combustor basket through the exit cone portion,
wherein the splash plate portion extends from an aft end of the base portion and the exit cone portion extends at an angle from the aft end of the base portion so as to define an annular channel between the splash plate portion and the exit cone portion,
wherein the base portion includes a cooling air chamber that receives a cooling air flow, the splash plate portion includes a first plurality of cooling air feed holes that are in fluid communication with the cooling air chamber and receive a first portion of cooling air therefrom, and the exit cone portion includes a second plurality of cooling air feed holes that are in fluid communication with the cooling air chamber and receive a second portion of cooling air therefrom, the cooling air flow from the cooling air chamber is split into the first plurality of cooling air feed holes and the second plurality of cooling air feed holes so that the first portion of cooling air and the second portion of cooling air flow in parallel.

2. The combustor basket assembly according to claim 1 , wherein a first spacing between each of the first plurality of cooling air feed holes, a second spacing between each of the second plurality of cooling air feed holes, a first size of each of the first plurality of cooling air feed holes and a second size of each of the second plurality of cooling air feed holes are selected to regulate the amount of cooling air flow split between the first plurality of cooling air feed holes and the second plurality of cooling air feed holes.

3. The combustor basket assembly according to claim 1 , wherein the cooling air chamber is an annular chamber that is circumferentially disposed around the single piece member.

4. The combustor basket assembly according to claim 1 , wherein the single piece member is an annular member where the splash plate portion has a larger diameter than a diameter of the exit cone portion.

5. The combustor basket assembly according to claim 1 , further comprising an annular spring clip mounted to an outer wall of the base portion, the annular spring clip allowing the cooling air flow to the base portion.

6. The combustor basket assembly according to claim 1 , wherein an inner surface and an outer surface of the exit cone portion are coated with a thermal barrier coating.

7. The combustor basket assembly according to claim 1 , wherein an inner surface and an outer surface of the splash plate portion are coated with a thermal barrier coating.

8. The combustor basket assembly according to claim 1 , wherein the single piece member is welded to the output end of the basket liner.

9. An annular single piece member operable to be affixed to an output end of a basket liner associated with a combustor in a gas turbine engine, said annular single piece member comprising a base portion, a splash plate portion integral with the base portion and an exit cone portion integral with the base portion, wherein the base portion includes an annular cooling air chamber that receives a cooling air flow, the splash plate portion includes a first plurality of cooling air feed holes that are in fluid communication with the annular cooling air chamber and receive the cooling air flow therefrom, and the exit cone portion includes a second plurality of cooling air feed holes that are in fluid communication with the annular cooling air chamber and receive the cooling air flow therefrom; and
wherein the splash plate portion extends from an aft end of the base portion and the exit cone portion extends at an angle from the aft end of the base portion so as to define an annular channel between the splash plate portion and the exit cone portion.

10. The annular single piece member according to claim 9 , wherein the splash plate portion has a larger diameter than a diameter the exit cone portion.

11. The annular single piece member according to claim 9 , wherein an inner surface and an outer surface of the exit cone portion are coated with a thermal barrier coating, and an inner surface and an outer surface of the splash plate portion are coated with a thermal barrier coating.

12. A gas turbine engine, comprising:
a shaft provided along a center line of the gas turbine engine;
a compressor section responsive to a working fluid and being operable to compress the working fluid to produce a compressed working fluid;
a combustion section in fluid communication with the compressor section that receives the compressed working fluid, said combustion section including a plurality of combustors that mix the compressed working fluid with a fuel and combust the compressed fluid and fuel mixture to produce a hot working gas, each combustor including a combustor basket assembly in which the combustion occurs, said combustor basket assembly comprising a combustor basket including a basket liner having an input end and an output end through which the hot working gas exits the combustor basket, said combustor basket further including a single piece member affixed to the output end of the basket liner, said single piece member including a base portion, a splash plate portion integral with the base portion and an exit cone portion integral with the base portion, where the hot working gas exits the combustor basket through the exit cone portion, wherein the splash plate portion extends from an aft end of the base portion and the exit cone portion extends at an angle from the aft end of the base portion so as to define an annular channel between the splash plate portion and the exit cone portion; and
a turbine section in fluid communication with the combustion section, said turbine section expanding the hot working gas to produce mechanical power through rotation of the shaft,
wherein the base portion includes a cooling air chamber that receives a cooling air flow, the splash plate portion includes a first plurality of cooling air feed holes that are in fluid communication with the cooling air chamber and receive a first portion of cooling air therefrom, and the exit cone portion includes a second plurality of cooling air feed holes that are in fluid communication with the cooling air chamber and receive a second portion of cooling air therefrom, the cooling air flow from the cooling air chamber is split into the first plurality of cooling air feed holes and the second plurality of cooling air feed holes so that the first portion of cooling air and the second portion of cooling air flow in parallel.

13. The gas turbine engine according to claim 12 , wherein the cooling air chamber is an annular chamber that is circumferentially disposed around the single piece member.

14. The gas turbine engine according to claim 12 , wherein the single piece member is an annular member where the splash plate portion has a larger diameter than a diameter of the exit cone portion.

15. The gas turbine engine according to claim 12 , further comprising an annular spring clip mounted to an outer wall of the base portion, the annular spring clip allowing the cooling air flow to flow to the base port

Assignees

• Siemens Energy Inc

Inventors

• Thackway Richard L
• Polyzopoulos Jr Charalambos
• Hurney James M

Classifications

• F23R3/54

  Reverse-flow combustion chambers · CPC title

• F23R3/06

  Arrangement of apertures along the flame tube · CPC title

• F05B2260/20

  Heat transfer, e.g. cooling · CPC title

• F02C3/145

  the combustion chamber being in the reverse flow-type · CPC title

• F05B2260/203

  by transpiration cooling · CPC title