Rotating airfoil component of a turbomachine
US-8967957-B2 · Mar 3, 2015 · US
US9702261B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9702261-B2 |
| Application number | US-201314098997-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 6, 2013 |
| Priority date | Dec 6, 2013 |
| Publication date | Jul 11, 2017 |
| Grant date | Jul 11, 2017 |
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A steam turbine is provided. The steam turbine includes a housing and a steam inlet coupled in flow communication to the housing which is configured to discharge a first steam flow within the housing. A stator is coupled to the housing and includes plurality of vanes. A rotor is coupled to the housing and located within the stator, wherein the rotor and the stator are configured to form a first flow path there between and in flow communication with the first steam flow. The rotor includes a plurality of blades coupled to the rotor, at least one root of the plurality of blades has a first side, a second side and a passageway coupled in flow communication to the first side and the second side. The passageway is configured to define a second flow path in flow communication with the first flow path and to discharge a second steam flow within the at least one root. The at least one root of the plurality of blades includes an angel wing in flow communication with the passageway and configured to seal the passageway from the first flow path.
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What is claimed is: 1. A steam turbine comprising: a housing; a steam inlet coupled in flow communication to said housing and configured to discharge a first steam flow within said housing; a stator coupled to said housing and comprising a plurality of vanes; and a rotor coupled to said housing and located within said stator, said rotor and said stator define a first flow path therebetween and in flow communication with the first steam flow, said rotor comprising at least an upstream stage and an adjacent downstream stage, wherein the upstream and downstream directions are defined by the first steam flow, each of said upstream and downstream stages comprising a plurality of blades coupled to said rotor, at least one root of said plurality of blades of said downstream stage comprising a first side, a second side and a passageway extending through said root in flow communication with said first side and said second side, said passageway is configured to receive a portion of the first steam flow from said first flow path at said second side and to discharge the portion of the first steam flow from said first side, said at least one root of said plurality of blades of said downstream stage comprises a first angel wing extending upstream from said first side, at least one root of said plurality of turbine blades of said upstream stage comprises a second angel wing extending downstream and adjacent to said first angel wing, said first and second angel wings configured to cooperate to seal the discharged portion of the first steam flow from said first flow path. 2. The steam turbine of claim 1 , wherein the discharged portion of the first steam flow comprises a temperature that is different than said first steam flow. 3. The steam turbine of claim 1 , wherein said steam inlet is coupled in flow communication with said first flow path and located within said housing. 4. The steam turbine of claim 1 , further comprising another steam inlet coupled in flow communication to said first flow path and located external to said housing. 5. The steam turbine of claim 1 , further comprising another steam inlet coupled in flow communication to at least one vane of said plurality of vanes. 6. The steam turbine of claim 5 , wherein at least one said vane comprises a first end, a second end and a radial flow path coupled in flow communication to said first end and said second end, said first end is coupled in flow communication to said steam inlet and said second end is coupled in flow communication to said first flow path. 7. The steam turbine of claim 1 , wherein said first flow path and said passageway are coupled in flow communication in a negative root reaction configuration. 8. The steam turbine of claim 1 , wherein said rotor comprises a third flow path coupled in flow communication to said passageway configured to receive a portion of the first steam flow. 9. The steam turbine of claim 1 , wherein said rotor comprises a third flow path coupled in flow communication to said passageway configured to receive a portion of the first steam flow and a packing head coupled in flow communication to said third flow path. 10. The steam turbine of claim 1 , wherein said housing comprises a high pressure multi-stage arrangement. 11. The steam turbine of claim 1 , wherein at least one of said roots comprises an axial dovetail configuration. 12. A rotor assembly coupled to a housing and located within a stator of a steam turbine, said rotor assembly comprising: a rotor coupled to the housing and comprising a first flow path, said rotor further comprising at least an upstream stage and an adjacent downstream stage, wherein the upstream and downstream directions are defined by a first steam flow; a plurality of blades coupled to each of said upstream and downstream stages of said rotor, at least one root of said plurality of blades of said downstream stage comprising a first side, a second side and a passageway extending through said root in flow communication with said first side and said second side, said passageway is configured to receive a portion of the first steam flow from the first flow path at said second side and to discharge the portion of the first steam flow from said first side, said at least one root of said plurality of blades of said downstream stage further comprises a first angel wing extending upstream from said first side, at least one root of said plurality of turbine blades of said upstream stage comprises a second angel wing extending downstream and adjacent to said first angel wing, said first and second angel wings configured to cooperate to seal the discharged portion of the first steam flow from said first flow path; and a seal assembly coupled to said rotor and in flow communication with said passageway. 13. The rotor assembly of claim 12 , further comprising a steam inlet coupled in flow communication to said first flow path and located within said housing. 14. The rotor assembly of claim 13 , further comprising another steam inlet coupled in flow communication to said first flow path and located external to said housing. 15. The rotor assembly of claim 13 , further comprising another steam inlet coupled in flow communication to at least one vane of a plurality of vanes. 16. The rotor assembly of claim 12 , wherein said at least one of said roots comprises an axial dovetail configuration. 17. The rotor assembly of claim 12 , wherein said seal assembly comprises a third flow path in flow communication with said passageway. 18. A method of assembling a steam turbine, said method comprising: coupling a stator to a housing; coupling a steam inlet in flow communication to the housing; and coupling a rotor to the housing and within the stator such that a first flow path is defined within the housing and in flow communication with the steam inlet, the rotor comprises at least an upstream stage and an adjacent downstream stage, wherein the upstream and downstream directions are defined by a first steam flow, each of said upstream and downstream stages including a plurality of blades coupled to the rotor, at least one root of the plurality of blades of the downstream stage including a first side, a second side and a passageway extending through the root in flow communication with the first side and the second side, the passageway is configured to receive a portion of the first steam flow from the first flow path at the second side and to discharge the portion of the first steam flow from the first side, the at least one root of the plurality of blades of the downstream stage includes a first angel wing extending upstream from the first side, at least one root of the plurality of turbine blades of the upstream stage includes a second angel wing extending downstream and adjacent to the first angel wing, the first and second angel wings configured to cooperate to seal the discharged portion of the first steam flow from the first flow path. 19. The method of claim 18 , further comprising coupling a seal assembly to the rotor and in flow communication with the passageway. 20. The method of claim 18 , wherein coupling the steam inlet comprises coupling the steam inlet in flow communication to the stator.
with stationary working-fluid guiding means and bladed or like rotor, {e.g. multi-bladed impulse steam turbines}(F01D1/24 takes precedence; without stationary working-fluid guiding means F01D1/18) · CPC title
using sealing fluid, e.g. steam · CPC title
for sealing space between stator blade and rotor · CPC title
Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles · CPC title
Seals · CPC title
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