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US 2023/0272912 A1Published application
Combustor dome-deflector and liner having flexible connections
AssigneeGeneral Electric Company
InventorsRavindra Shankar Ganiger, Hiranya Nath, Sripathi Mohan, Girish Kamath Cannanore
Life of this patent
Estimating the term…
Abstract
A combustor for a gas turbine includes a dome, and a deflector connected to the dome to define a baffle cavity therebetween, the deflector having a deflector cold side adjacent to the baffle cavity and a deflector hot side adjacent to a combustion chamber. At least one dome-deflector connecting member connects the dome and the deflector to each other. The dome-deflector connecting member forms a flexible joint between the dome and the deflector.
Claims18
A combustor for a gas turbine, the combustor comprising:
- a dome;
- a deflector connected to the dome to define a baffle cavity therebetween, the deflector having a deflector cold side adjacent to the baffle cavity and a deflector hot side adjacent to a combustion chamber;
- and
- at least one dome-deflector connecting member connecting the dome and the deflector to each other,
- wherein the at least one dome-deflector connecting member comprises a bolted joint including a bolt having a bolt head and a shank, the bolt head engaging the deflector on the deflector hot side, and
- wherein the shank comprises a hollow cylindrical shank portion, the hollow cylindrical shank portion being unthreaded and defining a hollow cavity within the shank, a helical serration formed through the hollow cylindrical shank portion along a length of the hollow cylindrical shank portion so as to define a heli-coil shank portion, the heli-coil shank portion being arranged between the dome and the deflector, the helical serration defining an airflow path for providing a flow of cooling airflow from the baffle cavity through the helical serration to the hollow cavity, and the bolt head having a cooling passage extending therethrough and in fluid communication with the hollow cavity.
3 more elements
2-4. (canceled)
A combustor for a gas turbine, the combustor comprising:
- a dome;
- a deflector connected to the dome to define a baffle cavity therebetween, the deflector having a deflector cold side adjacent to the baffle cavity and a deflector hot side adjacent to a combustion chamber;
- and
- at least one dome-deflector connecting member connecting the dome and the deflector to each other,
- wherein the at least one dome-deflector connecting member comprises at least one coupler connected to the dome at a first end of the coupler and connected to the deflector at a second end of the coupler, and
- wherein the at least one coupler includes a hollow cylindrical middle section between the first end of the coupler and the second end of the coupler, the hollow cylindrical middle section being unthreaded and defining a hollow cavity within the at least one coupler, a helical serration formed through the hollow cylindrical middle section along a length of the hollow cylindrical middle section so as to define a heli-coil structure, and
- wherein the hollow cavity is in fluid communication with the baffle cavity via the helical serration.
4 more elements
(canceled)
A combustor for a gas turbine, the combustor comprising:
- a dome;
- a deflector connected to the dome to define a baffle cavity therebetween, the deflector having a deflector cold side adjacent to the baffle cavity and a deflector hot side adjacent to a combustion chamber;
- and
- at least one dome-deflector connecting member connecting the dome and the deflector to each other,
- wherein the at least one dome-deflector connecting member includes a ripple-shaped washer having a center opening therethrough, and having a radially outer flange, the deflector includes a stud extending from the deflector cold side, the stud extending through the center opening, and the radially outer flange of the ripple-shaped washer engaging a cold side of the dome, and
- wherein the ripple-shaped washer includes cooling openings therethrough for providing an impingement cooling airflow to impinge against the deflector cold side.
3 more elements
(canceled)
A combustor for a gas turbine, the combustor comprising:
- a dome;
- a deflector connected to the dome to define a baffle cavity therebetween, the deflector having a deflector cold side adjacent to the baffle cavity and a deflector hot side adjacent to a combustion chamber;
- and
- at least one dome-deflector connecting member connecting the dome and the deflector to each other,
- wherein the at least one dome-deflector connecting member includes a first ripple-shaped washer having a first washer center opening therethrough, and having a first washer radially outer flange, a second ripple-shaped washer having a second washer center opening therethrough, and having a second washer radially outer flange, the deflector includes a stud extending from the deflector cold side, the stud extending through the first washer center opening and through the second washer center opening, the first washer radially outer flange engaging with a cold side of the dome, and the first ripple-shaped washer extending through a dome opening and into the baffle cavity, and the second washer radially outer flange engaging with a hot side of the dome, and the second ripple-shaped washer engaging with the cold side of the deflector, and
- wherein the first ripple-shaped washer includes cooling openings therethrough for providing a cooling airflow to a cold side of the second ripple-shaped washer, and the second ripple-shaped washer includes cooling openings therethrough for providing an impingement cooling airflow to impinge against the cold side of the deflector.
3 more elements
(canceled)
A combustor for a gas turbine, the combustor comprising:
- a dome;
- a deflector connected to the dome to define a baffle cavity therebetween, the deflector having a deflector cold side adjacent to the baffle cavity and a deflector hot side adjacent to a combustion chamber;
- and
- at least one dome-deflector connecting member connecting the dome and the deflector to each other,
- wherein the at least one dome-deflector connecting member includes (a) a first ripple-shaped washer having a first washer center opening therethrough, and having a first washer radially outer flange, and (b) a second ripple-shaped washer having a stud extending from a center of the second ripple-shaped flexible washer, and having a second washer radially outer flange, the second ripple-shaped washer being joined to the deflector, the stud extending through the first washer center opening, the second washer radially outer flange engaging with a hot side of the dome, and the first washer radially outer flange engaging with a cold side of dome, and
- wherein the first ripple-shaped washer includes cooling openings therethrough for providing a cooling airflow to a cold side of the second ripple-shaped washer, and the second ripple-shaped washer includes cooling openings therethrough for providing an impingement cooling airflow to impinge against the cold side of the deflector.
3 more elements
(canceled)
A combustor for a gas turbine, the combustor comprising:
- a dome;
- a deflector connected to the dome to define a baffle cavity therebetween, the deflector having a deflector cold side adjacent to the baffle cavity and a deflector hot side adjacent to a combustion chamber;
- at least one dome-deflector connecting member connecting the dome and the deflector to each other;
- and
- a combustor liner including a combustor liner shell and a combustor liner panel connected to the combustor liner shell to define a baffle cavity therebetween, the combustor liner panel being connected to the combustor liner shell via at least one shell-to-panel connecting member at a joint, the at least one shell-to-panel connecting member forming a joint between the combustor liner shell and the combustor liner panel,
- wherein the at least one shell-to-panel connecting member includes (a) a first ripple-shaped washer having a first washer center opening therethrough, and having a first washer radially outer flange, and (b) a second ripple-shaped washer having a stud extending from a center of the second ripple-shaped washer, and having a second washer radially outer flange, the second ripple-shaped washer being joined to the combustor liner panel, the stud extending through the first washer center opening, the second washer radially outer flange engaging with a hot side of the combustor liner shell, and the first washer radially outer flange engaging with a cold side of combustor liner shell, and
- wherein the first ripple-shaped washer includes cooling openings therethrough for providing a cooling airflow to a cold side of the second ripple-shaped washer, and the second ripple-shaped washer includes cooling openings therethrough for providing an impingement cooling airflow to impinge against the cold side of the combustor liner panel.
4 more elements
Dependencies are inferred from the claim text.