FR2960905B1 - METHOD AND SYSTEM FOR CONTROLLING TURBINE ROTOR BLACK SUMP - Google Patents
METHOD AND SYSTEM FOR CONTROLLING TURBINE ROTOR BLACK SUMPInfo
- Publication number
- FR2960905B1 FR2960905B1 FR1054366A FR1054366A FR2960905B1 FR 2960905 B1 FR2960905 B1 FR 2960905B1 FR 1054366 A FR1054366 A FR 1054366A FR 1054366 A FR1054366 A FR 1054366A FR 2960905 B1 FR2960905 B1 FR 2960905B1
- Authority
- FR
- France
- Prior art keywords
- sump
- black
- turbine rotor
- controlling turbine
- controlling
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
- F01D11/20—Actively adjusting tip-clearance
- F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Control Of Turbines (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1054366A FR2960905B1 (en) | 2010-06-03 | 2010-06-03 | METHOD AND SYSTEM FOR CONTROLLING TURBINE ROTOR BLACK SUMP |
BR112012030635A BR112012030635A2 (en) | 2010-06-03 | 2011-06-01 | Method and system for controlling the blade tip clearance of a turbine rotor |
CN201180027544.1A CN103003529B (en) | 2010-06-03 | 2011-06-01 | For controlling the method and system in the gap at the vane tip place of turbine rotor |
RU2012157775/06A RU2566510C2 (en) | 2010-06-03 | 2011-06-01 | Method and system for adjustment of clearance at turbine rotor blade edges |
PCT/FR2011/051261 WO2011151602A1 (en) | 2010-06-03 | 2011-06-01 | Method and system for controlling the clearance at the blade tips of a turbine rotor |
US13/701,700 US20130177414A1 (en) | 2010-06-03 | 2011-06-01 | Method and system for controlling the clearance at the blades tips of a turbine rotor |
CA2801193A CA2801193A1 (en) | 2010-06-03 | 2011-06-01 | Method and system for controlling the clearance at the blade tips of a turbine rotor |
EP11728349.9A EP2576994A1 (en) | 2010-06-03 | 2011-06-01 | Method and system for controlling the clearance at the blade tips of a turbine rotor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1054366A FR2960905B1 (en) | 2010-06-03 | 2010-06-03 | METHOD AND SYSTEM FOR CONTROLLING TURBINE ROTOR BLACK SUMP |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2960905A1 FR2960905A1 (en) | 2011-12-09 |
FR2960905B1 true FR2960905B1 (en) | 2014-05-09 |
Family
ID=43471088
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1054366A Active FR2960905B1 (en) | 2010-06-03 | 2010-06-03 | METHOD AND SYSTEM FOR CONTROLLING TURBINE ROTOR BLACK SUMP |
Country Status (8)
Country | Link |
---|---|
US (1) | US20130177414A1 (en) |
EP (1) | EP2576994A1 (en) |
CN (1) | CN103003529B (en) |
BR (1) | BR112012030635A2 (en) |
CA (1) | CA2801193A1 (en) |
FR (1) | FR2960905B1 (en) |
RU (1) | RU2566510C2 (en) |
WO (1) | WO2011151602A1 (en) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2997443B1 (en) * | 2012-10-31 | 2015-05-15 | Snecma | CONTROL UNIT AND METHOD FOR CONTROLLING THE AUBES TOP SET |
US9266618B2 (en) * | 2013-11-18 | 2016-02-23 | Honeywell International Inc. | Gas turbine engine turbine blade tip active clearance control system and method |
CN104963729A (en) * | 2015-07-09 | 2015-10-07 | 中国航空工业集团公司沈阳发动机设计研究所 | Heavy-duty gas turbine high-vortex tip clearance control structure |
US10138752B2 (en) | 2016-02-25 | 2018-11-27 | General Electric Company | Active HPC clearance control |
US10344614B2 (en) | 2016-04-12 | 2019-07-09 | United Technologies Corporation | Active clearance control for a turbine and case |
GB201819695D0 (en) * | 2018-12-03 | 2019-01-16 | Rolls Royce Plc | Methods and apparatus for controlling at least part of a start-up or re-light process of a gas turbine engine |
GB2584693A (en) * | 2019-06-12 | 2020-12-16 | Rolls Royce Plc | Improving deceleration of a gas turbine |
CN110318823B (en) * | 2019-07-10 | 2022-07-15 | 中国航发沈阳发动机研究所 | Active clearance control method and device |
GB201910008D0 (en) * | 2019-07-12 | 2019-08-28 | Rolls Royce Plc | Gas turbine engine electrical generator |
US11982189B2 (en) | 2021-06-04 | 2024-05-14 | Rtx Corporation | Warm start control of an active clearance control for a gas turbine engine |
US11788425B2 (en) * | 2021-11-05 | 2023-10-17 | General Electric Company | Gas turbine engine with clearance control system |
US11808157B1 (en) * | 2022-07-13 | 2023-11-07 | General Electric Company | Variable flowpath casings for blade tip clearance control |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2006593C1 (en) * | 1991-07-01 | 1994-01-30 | Иван Анатольевич Черняев | Method of control of radial clearance between rotor blade tips and housing of turbomachine of gas-turbine engine |
RU2175410C1 (en) * | 2000-04-18 | 2001-10-27 | Открытое акционерное общество "Авиадвигатель" | Gas-turbine engine compressor |
GB2363864B (en) * | 2000-06-23 | 2004-08-18 | Rolls Royce Plc | A control arrangement |
GB2388407B (en) * | 2002-05-10 | 2005-10-26 | Rolls Royce Plc | Gas turbine blade tip clearance control structure |
US20050109016A1 (en) * | 2003-11-21 | 2005-05-26 | Richard Ullyott | Turbine tip clearance control system |
FR2867224B1 (en) * | 2004-03-04 | 2006-05-19 | Snecma Moteurs | AXIAL AXIS HOLDING DEVICE FOR RING OF A TURBOMACHINE HIGH-PRESSURE TURBINE |
US7597537B2 (en) * | 2005-12-16 | 2009-10-06 | General Electric Company | Thermal control of gas turbine engine rings for active clearance control |
US7431557B2 (en) * | 2006-05-25 | 2008-10-07 | General Electric Company | Compensating for blade tip clearance deterioration in active clearance control |
US7686569B2 (en) * | 2006-12-04 | 2010-03-30 | Siemens Energy, Inc. | Blade clearance system for a turbine engine |
US8126628B2 (en) * | 2007-08-03 | 2012-02-28 | General Electric Company | Aircraft gas turbine engine blade tip clearance control |
US20090053042A1 (en) * | 2007-08-22 | 2009-02-26 | General Electric Company | Method and apparatus for clearance control of turbine blade tip |
-
2010
- 2010-06-03 FR FR1054366A patent/FR2960905B1/en active Active
-
2011
- 2011-06-01 CA CA2801193A patent/CA2801193A1/en not_active Abandoned
- 2011-06-01 CN CN201180027544.1A patent/CN103003529B/en not_active Expired - Fee Related
- 2011-06-01 WO PCT/FR2011/051261 patent/WO2011151602A1/en active Application Filing
- 2011-06-01 RU RU2012157775/06A patent/RU2566510C2/en not_active IP Right Cessation
- 2011-06-01 BR BR112012030635A patent/BR112012030635A2/en not_active IP Right Cessation
- 2011-06-01 EP EP11728349.9A patent/EP2576994A1/en not_active Withdrawn
- 2011-06-01 US US13/701,700 patent/US20130177414A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
RU2566510C2 (en) | 2015-10-27 |
CN103003529B (en) | 2015-09-30 |
US20130177414A1 (en) | 2013-07-11 |
WO2011151602A1 (en) | 2011-12-08 |
CA2801193A1 (en) | 2011-12-08 |
BR112012030635A2 (en) | 2016-08-16 |
CN103003529A (en) | 2013-03-27 |
EP2576994A1 (en) | 2013-04-10 |
RU2012157775A (en) | 2014-07-20 |
FR2960905A1 (en) | 2011-12-09 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 |
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PLFP | Fee payment |
Year of fee payment: 11 |
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PLFP | Fee payment |
Year of fee payment: 12 |
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PLFP | Fee payment |
Year of fee payment: 13 |
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PLFP | Fee payment |
Year of fee payment: 14 |