CA2007633C - Clearance control for the turbine of a gas turbine engine - Google Patents
Clearance control for the turbine of a gas turbine engine Download PDFInfo
- Publication number
- CA2007633C CA2007633C CA002007633A CA2007633A CA2007633C CA 2007633 C CA2007633 C CA 2007633C CA 002007633 A CA002007633 A CA 002007633A CA 2007633 A CA2007633 A CA 2007633A CA 2007633 C CA2007633 C CA 2007633C
- Authority
- CA
- Canada
- Prior art keywords
- turbine
- air
- blade
- tip
- section
- 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.)
- Expired - Fee Related
Links
- 238000001816 cooling Methods 0.000 claims abstract description 52
- 238000007599 discharging Methods 0.000 claims abstract description 9
- 230000003071 parasitic effect Effects 0.000 claims description 9
- 230000008901 benefit Effects 0.000 description 4
- 230000009471 action Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000005086 pumping Methods 0.000 description 2
- WYTGDNHDOZPMIW-RCBQFDQVSA-N alstonine Natural products C1=CC2=C3C=CC=CC3=NC2=C2N1C[C@H]1[C@H](C)OC=C(C(=O)OC)[C@H]1C2 WYTGDNHDOZPMIW-RCBQFDQVSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000002826 coolant Substances 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 210000003141 lower extremity Anatomy 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
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
- 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
- F01D11/10—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using sealing fluid, e.g. steam
-
- 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
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/20—Specially-shaped blade tips to seal space between tips and stator
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/202—Heat transfer, e.g. cooling by film cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/232—Heat transfer, e.g. cooling characterized by the cooling medium
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (11)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US07/236,094 US5667359A (en) | 1988-08-24 | 1988-08-24 | Clearance control for the turbine of a gas turbine engine |
| GB9400380A GB2315818B (en) | 1988-07-29 | 1990-01-09 | Clearence control for the turbine of a gas turbine engine |
| GB9000456A GB2319567B (en) | 1988-07-29 | 1990-01-09 | Clearance control for the turbine of a gas turbine engine |
| AU48813/90A AU684038B1 (en) | 1988-07-29 | 1990-01-12 | Clearance control for the turbine of a gas turbine engine |
| SE9000113D SE9000113L (sv) | 1988-07-29 | 1990-01-12 | Spelstyrning för turbinen vid en gasturbinmotor |
| SE9000113A SE470600B (sv) | 1988-07-29 | 1990-01-12 | Spelstyrning för turbinen vid en gasturbinmotor |
| CA002007633A CA2007633C (en) | 1988-07-29 | 1990-01-12 | Clearance control for the turbine of a gas turbine engine |
| IT04756490A IT1283979B1 (it) | 1988-07-29 | 1990-01-24 | Perfezionamento nelle turbine a flusso assiale |
| DE4003802A DE4003802C2 (de) | 1988-08-24 | 1990-02-08 | Minimale Leckströmung zwischen Schaufelspitze und gegenüberliegender Gehäusewand |
| NL9000541A NL194700C (nl) | 1988-08-24 | 1990-03-09 | Axiale stromingsturbine voor een gasturbinemotor. |
| JP02800007A JP3040158B2 (ja) | 1988-08-24 | 1990-03-16 | ガスタービンエンジン用軸流タービン |
Applications Claiming Priority (10)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US07/226,094 US4921166A (en) | 1987-07-31 | 1988-07-29 | Hot water circulating system |
| GB9400380A GB2315818B (en) | 1988-07-29 | 1990-01-09 | Clearence control for the turbine of a gas turbine engine |
| GB9000456A GB2319567B (en) | 1988-07-29 | 1990-01-09 | Clearance control for the turbine of a gas turbine engine |
| AU48813/90A AU684038B1 (en) | 1988-07-29 | 1990-01-12 | Clearance control for the turbine of a gas turbine engine |
| SE9000113A SE470600B (sv) | 1988-07-29 | 1990-01-12 | Spelstyrning för turbinen vid en gasturbinmotor |
| CA002007633A CA2007633C (en) | 1988-07-29 | 1990-01-12 | Clearance control for the turbine of a gas turbine engine |
| IT04756490A IT1283979B1 (it) | 1988-07-29 | 1990-01-24 | Perfezionamento nelle turbine a flusso assiale |
| DE4003802A DE4003802C2 (de) | 1988-08-24 | 1990-02-08 | Minimale Leckströmung zwischen Schaufelspitze und gegenüberliegender Gehäusewand |
| NL9000541A NL194700C (nl) | 1988-08-24 | 1990-03-09 | Axiale stromingsturbine voor een gasturbinemotor. |
| JP02800007A JP3040158B2 (ja) | 1988-08-24 | 1990-03-16 | ガスタービンエンジン用軸流タービン |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2007633A1 CA2007633A1 (en) | 1997-06-06 |
| CA2007633C true CA2007633C (en) | 2000-03-14 |
Family
ID=27578965
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002007633A Expired - Fee Related CA2007633C (en) | 1988-07-29 | 1990-01-12 | Clearance control for the turbine of a gas turbine engine |
Country Status (4)
| Country | Link |
|---|---|
| AU (1) | AU684038B1 (en:Method) |
| CA (1) | CA2007633C (en:Method) |
| IT (1) | IT1283979B1 (en:Method) |
| SE (2) | SE9000113L (en:Method) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9039346B2 (en) | 2011-10-17 | 2015-05-26 | General Electric Company | Rotor support thermal control system |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4390320A (en) * | 1980-05-01 | 1983-06-28 | General Electric Company | Tip cap for a rotor blade and method of replacement |
-
1990
- 1990-01-12 AU AU48813/90A patent/AU684038B1/en not_active Ceased
- 1990-01-12 CA CA002007633A patent/CA2007633C/en not_active Expired - Fee Related
- 1990-01-12 SE SE9000113D patent/SE9000113L/xx not_active Application Discontinuation
- 1990-01-12 SE SE9000113A patent/SE470600B/sv not_active IP Right Cessation
- 1990-01-24 IT IT04756490A patent/IT1283979B1/it active IP Right Grant
Also Published As
| Publication number | Publication date |
|---|---|
| AU684038B1 (en) | 1997-12-04 |
| IT9047564A0 (en:Method) | 1990-01-24 |
| SE9000113D0 (sv) | 1990-01-12 |
| IT1283979B1 (it) | 1998-05-07 |
| SE470600B (sv) | 1998-09-14 |
| SE9000113L (sv) | 1998-05-03 |
| CA2007633A1 (en) | 1997-06-06 |
| IT9047564A1 (it) | 1991-07-24 |
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| JP2001164904A (ja) | ターボ機械の冷却式流体反動要素 | |
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| JPS6119804B2 (en:Method) | ||
| US6357999B1 (en) | Gas turbine engine internal air system | |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| MKLA | Lapsed |