Patent · US2011168482A1 · A1 · US
Vane type silencers in elbow for gas turbine
- (11) Publication number
- US2011168482A1
- (21) Application number
- US-68416110-A
- (22) Filing date
- 2010-01-08
- (30) Priority date
- 2010-01-08
- (43) Publication date
- 2011-07-14
- (52) CPC
- F02C Gas-turbine plants; air intakes for jet-propulsion plants; controlling fuel supply in air-breathing jet-propulsion plants: 7/045
- F01D Non-positive displacement machines or engines, e.g. steam turbines: 25/30
- F05D Indexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants: 2240/126, 2260/96
- (73) Assignee
- MERCHANT LAXMIKANT; VENUGOPAL DINESH SETTY; PRABHAKARAN RAJESH SARASWATHI
- (54) Title
- Vane type silencers in elbow for gas turbine
- (57) Abstract
A silencer for a gas turbine includes a first duct portion; a second duct portion connected to the first duct portion, the first and second duct portions forming an elbow region at the connection; and a plurality of elbow shaped vanes provided in the elbow region. The plurality of elbow shaped vanes have equal lengths and are spaced equally apart.
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Claims (1)
- A silencer for a gas turbine, comprising: a first duct portion; a second duct portion connected to the first duct portion, the first and second duct portions forming an elbow region at the connection, the elbow region having an inlet plane and an outlet plane that are perpendicular to one another; and a plurality of elbow shaped vanes provided in the elbow region, wherein the elbow region has a first flow path region having a cross section corresponding to a cross section of the first duct portion at the connection, a second flow path region defined by the plurality of elbow shaped vanes that have equal lengths and are spaced equally apart, and a third flow path region having a cross section corresponding to a cross section of the second duct portion at the connection. 2. A silencer according to claim 1, wherein the first duct portion comprises an inlet and a transition region between the inlet and the plurality of elbow shaped vanes, and a cross section of the transition region increases from the inlet towards the connection. 3. A silencer according to claim 2, wherein the first duct portion comprises a portion of constant cross section between the transition region and the inlet plane. 4. A silencer according to claim 2, wherein the inlet comprises a circular duct, a rectangular duct, or a square duct. 5 - 6. (canceled) 7. A silencer according to claim 1, wherein the second duct portion comprises an exhaust chimney and a transition region between the plurality of elbow shaped vanes, and a cross section of the transition region decreases from the outlet plane to the exhaust chimney. 8. A silencer according to claim 7, wherein the exhaust chimney comprises a circular duct, a rectangular duct, or a square duct. 9 - 10. (canceled) 11. A silencer according to claim 1, wherein each elbow shaped silencer vane extends an equal distance into the first duct portion and the second duct portion. 12. A silencer according to claim 1, wherein the plurality of elbow shaped vanes are supported by a corresponding plurality of slots in a side wall of the elbow region. 13. A silencer according to claim 1, wherein the first duct portion is disposed substantially horizontally and the second duct portion is disposed substantially vertically and the plurality of elbow shaped vanes provided in the elbow region attenuate a sound of a flow as it turns from horizontal to vertical. 14. A silencer according to claim 1, wherein the plurality of elbow shaped vanes are parallel to each other. 15. A silencer according to claim 14, wherein each elbow shaped vane extends in a direction transverse to a direction of a flow of exhaust gas in the the first and second duct portions. 16. A silencer according to claim 14, wherein each elbow shaped vane extends in a direction parallel to a flow of exhaust gas in the direction of a the first and second duct portions. 17. A silencer according to claim 1, wherein each elbow shaped vane comprises at least one sheet and sound attenuating material. 18. A silencer according to claim 17, wherein the at least one sheet is perforated. 19. A silencer for a gas turbine, comprising: a first duct portion; a second duct portion connected to the first duct portion, the first and second duct portions forming an elbow region at the connection; and a plurality of L shaped shaped baffles provided in the elbow region in a direction parallel to a direction of flow of exhaust gas in the silencer, wherein the plurality of L-shaped baffles have equal lengths and are spaced equally apart. 20. A silencer according to claim 19, wherein the first duct portion comprises a first section having a first cross section, a second duct portion having a second cross section that is larger than the first cross section, and a transition portion from the first duct portion to the second duct portion, and the plurality of parallel L-shaped baffles extend for an entire length of the second duct portion. 21. A silencer for a gas turbine, comprising: a first duct portion; a second duct portion provided at an angle to the first duct portion, the first and second duct portions forming an elbow region at an intersection of the first and second duct portions, the elbow region having an inlet plane and an outlet plane that are not parallel to each other; and a plurality of elbow shaped vanes provided in the elbow region, wherein the plurality of elbow shaped vanes have equal lengths and are spaced equally apart. 22. A silencer according to claim 21, wherein the inlet and outlet planes are perpendicular to each other. 23. A silencer according to claim 21, wherein the plurality of vanes extend in a direction traverse to a direction of a flow of exhaust gas in the first and second duct portions. 24. A silencer according to claim 21, wherein the plurality of elbow shaped vanes are supported by a corresponding plurality of slots in a side wall of the elbow region.
Citations (45)
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- US2003072648A1
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Record as JSON
{
"publication_number": "US2011168482A1",
"country": "US",
"kind": "A1",
"title": "Vane type silencers in elbow for gas turbine",
"abstract": "A silencer for a gas turbine includes a first duct portion; a second duct portion connected to the first duct portion, the first and second duct portions forming an elbow region at the connection; and a plurality of elbow shaped vanes provided in the elbow region. The plurality of elbow shaped vanes have equal lengths and are spaced equally apart.",
"claims": [
"1. A silencer for a gas turbine, comprising: a first duct portion; a second duct portion connected to the first duct portion, the first and second duct portions forming an elbow region at the connection, the elbow region having an inlet plane and an outlet plane that are perpendicular to one another; and a plurality of elbow shaped vanes provided in the elbow region, wherein the elbow region has a first flow path region having a cross section corresponding to a cross section of the first duct portion at the connection, a second flow path region defined by the plurality of elbow shaped vanes that have equal lengths and are spaced equally apart, and a third flow path region having a cross section corresponding to a cross section of the second duct portion at the connection. 2. A silencer according to claim 1, wherein the first duct portion comprises an inlet and a transition region between the inlet and the plurality of elbow shaped vanes, and a cross section of the transition region increases from the inlet towards the connection. 3. A silencer according to claim 2, wherein the first duct portion comprises a portion of constant cross section between the transition region and the inlet plane. 4. A silencer according to claim 2, wherein the inlet comprises a circular duct, a rectangular duct, or a square duct. 5 - 6. (canceled) 7. A silencer according to claim 1, wherein the second duct portion comprises an exhaust chimney and a transition region between the plurality of elbow shaped vanes, and a cross section of the transition region decreases from the outlet plane to the exhaust chimney. 8. A silencer according to claim 7, wherein the exhaust chimney comprises a circular duct, a rectangular duct, or a square duct. 9 - 10. (canceled) 11. A silencer according to claim 1, wherein each elbow shaped silencer vane extends an equal distance into the first duct portion and the second duct portion. 12. A silencer according to claim 1, wherein the plurality of elbow shaped vanes are supported by a corresponding plurality of slots in a side wall of the elbow region. 13. A silencer according to claim 1, wherein the first duct portion is disposed substantially horizontally and the second duct portion is disposed substantially vertically and the plurality of elbow shaped vanes provided in the elbow region attenuate a sound of a flow as it turns from horizontal to vertical. 14. A silencer according to claim 1, wherein the plurality of elbow shaped vanes are parallel to each other. 15. A silencer according to claim 14, wherein each elbow shaped vane extends in a direction transverse to a direction of a flow of exhaust gas in the the first and second duct portions. 16. A silencer according to claim 14, wherein each elbow shaped vane extends in a direction parallel to a flow of exhaust gas in the direction of a the first and second duct portions. 17. A silencer according to claim 1, wherein each elbow shaped vane comprises at least one sheet and sound attenuating material. 18. A silencer according to claim 17, wherein the at least one sheet is perforated. 19. A silencer for a gas turbine, comprising: a first duct portion; a second duct portion connected to the first duct portion, the first and second duct portions forming an elbow region at the connection; and a plurality of L shaped shaped baffles provided in the elbow region in a direction parallel to a direction of flow of exhaust gas in the silencer, wherein the plurality of L-shaped baffles have equal lengths and are spaced equally apart. 20. A silencer according to claim 19, wherein the first duct portion comprises a first section having a first cross section, a second duct portion having a second cross section that is larger than the first cross section, and a transition portion from the first duct portion to the second duct portion, and the plurality of parallel L-shaped baffles extend for an entire length of the second duct portion. 21. A silencer for a gas turbine, comprising: a first duct portion; a second duct portion provided at an angle to the first duct portion, the first and second duct portions forming an elbow region at an intersection of the first and second duct portions, the elbow region having an inlet plane and an outlet plane that are not parallel to each other; and a plurality of elbow shaped vanes provided in the elbow region, wherein the plurality of elbow shaped vanes have equal lengths and are spaced equally apart. 22. A silencer according to claim 21, wherein the inlet and outlet planes are perpendicular to each other. 23. A silencer according to claim 21, wherein the plurality of vanes extend in a direction traverse to a direction of a flow of exhaust gas in the first and second duct portions. 24. A silencer according to claim 21, wherein the plurality of elbow shaped vanes are supported by a corresponding plurality of slots in a side wall of the elbow region."
],
"cpc": [
"F02C 7/045",
"F01D 25/30",
"F05D 2240/126",
"F05D 2260/96"
],
"assignees": [
"MERCHANT LAXMIKANT",
"VENUGOPAL DINESH SETTY",
"PRABHAKARAN RAJESH SARASWATHI"
],
"filing_date": "2010-01-08",
"publication_date": "2011-07-14",
"priority_date": "2010-01-08",
"application_number": "US-68416110-A",
"family_id": "44257658",
"citations": [
"US2002084138A1",
"US2003072648A1",
"US2004103667A1",
"US2004238271A1",
"US2874627A",
"US3011584A",
"US3174581A",
"US3187835A",
"US3511336A",
"US3698509A",
"US3704762A",
"US3709319A",
"US3715009A",
"US3739872A",
"US3762498A",
"US4050237A",
"US4105089A",
"US4131432A",
"US4180141A",
"US4371054A",
"US4537277A",
"US4581048A",
"US4738585A",
"US4753319A",
"US5355074A",
"US5495754A",
"US5713196A",
"US5715672A",
"US5809770A",
"US6260658B1",
"US6290266B1",
"US6397759B1",
"US6520286B1",
"US6537490B2",
"US6640926B2",
"US6668540B2",
"US6725912B1",
"US6748734B1",
"US6802690B2",
"US6851514B2",
"US7048500B2",
"US7051534B2",
"US7104749B2",
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]
}
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