D5/D5A DF-42 integrated exit cone and splash plate
AssigneeSiemens Energy, Inc.
InventorsRichard L. Thackway, Charalambos Polyzopoulos, Jr., James M. Hurney
Life of this patent
Estimating the term…
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.
Claims17
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.
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.
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.
Dependencies are inferred from the claim text.