JP4272483B2 - 軸方向にカットバックされかつ周方向にスキューされた冷却空気スロットを備えるガスタービンエンジンのディスクリム - Google Patents
軸方向にカットバックされかつ周方向にスキューされた冷却空気スロットを備えるガスタービンエンジンのディスクリム Download PDFInfo
- Publication number
- JP4272483B2 JP4272483B2 JP2003303865A JP2003303865A JP4272483B2 JP 4272483 B2 JP4272483 B2 JP 4272483B2 JP 2003303865 A JP2003303865 A JP 2003303865A JP 2003303865 A JP2003303865 A JP 2003303865A JP 4272483 B2 JP4272483 B2 JP 4272483B2
- Authority
- JP
- Japan
- Prior art keywords
- rim
- cooling air
- wall surface
- center line
- respect
- 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 title claims description 57
- 239000007789 gas Substances 0.000 description 11
- 238000004519 manufacturing process Methods 0.000 description 4
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 239000000567 combustion gas Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
Images
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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
-
- 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
- F01D5/08—Heating, heat-insulating or cooling means
- F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
-
- 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
- F01D5/08—Heating, heat-insulating or cooling means
- F01D5/085—Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor
- F01D5/087—Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor in the radial passages of the rotor disc
-
- 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
- F05D2250/00—Geometry
- F05D2250/70—Shape
-
- 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
- F05D2260/30—Retaining components in desired mutual position
- F05D2260/33—Retaining components in desired mutual position with a bayonet coupling
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/231,420 US6749400B2 (en) | 2002-08-29 | 2002-08-29 | Gas turbine engine disk rim with axially cutback and circumferentially skewed cooling air slots |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2004092644A JP2004092644A (ja) | 2004-03-25 |
| JP2004092644A5 JP2004092644A5 (enExample) | 2006-10-05 |
| JP4272483B2 true JP4272483B2 (ja) | 2009-06-03 |
Family
ID=31495388
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2003303865A Expired - Fee Related JP4272483B2 (ja) | 2002-08-29 | 2003-08-28 | 軸方向にカットバックされかつ周方向にスキューされた冷却空気スロットを備えるガスタービンエンジンのディスクリム |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US6749400B2 (enExample) |
| EP (1) | EP1394358B1 (enExample) |
| JP (1) | JP4272483B2 (enExample) |
| CN (1) | CN100359133C (enExample) |
| DE (1) | DE60318977T2 (enExample) |
Families Citing this family (32)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7192245B2 (en) * | 2004-12-03 | 2007-03-20 | Pratt & Whitney Canada Corp. | Rotor assembly with cooling air deflectors and method |
| DE102005059084A1 (de) * | 2005-12-10 | 2007-06-14 | Mtu Aero Engines Gmbh | Turbomaschine, insbesondere Gasturbine |
| GB2435909A (en) * | 2006-03-07 | 2007-09-12 | Rolls Royce Plc | Turbine blade arrangement |
| FR2918104B1 (fr) * | 2007-06-27 | 2009-10-09 | Snecma Sa | Dispositif de refroidissement des alveoles d'un disque de rotor de turbomachine a double alimentation en air. |
| FR2928406A1 (fr) * | 2008-03-07 | 2009-09-11 | Snecma Sa | Dispositif de retenue axiale d'aubes montees sur un disque de rotor de turbomachine, disque de rotor et flasque de maintien d'un tel dispositif |
| FR2937371B1 (fr) * | 2008-10-20 | 2010-12-10 | Snecma | Ventilation d'une turbine haute-pression dans une turbomachine |
| US8172506B2 (en) * | 2008-11-26 | 2012-05-08 | General Electric Company | Method and system for cooling engine components |
| US8662845B2 (en) | 2011-01-11 | 2014-03-04 | United Technologies Corporation | Multi-function heat shield for a gas turbine engine |
| US8740554B2 (en) | 2011-01-11 | 2014-06-03 | United Technologies Corporation | Cover plate with interstage seal for a gas turbine engine |
| US8840375B2 (en) | 2011-03-21 | 2014-09-23 | United Technologies Corporation | Component lock for a gas turbine engine |
| US9145772B2 (en) | 2012-01-31 | 2015-09-29 | United Technologies Corporation | Compressor disk bleed air scallops |
| US9091173B2 (en) | 2012-05-31 | 2015-07-28 | United Technologies Corporation | Turbine coolant supply system |
| US10119400B2 (en) | 2012-09-28 | 2018-11-06 | United Technologies Corporation | High pressure rotor disk |
| US9228443B2 (en) * | 2012-10-31 | 2016-01-05 | Solar Turbines Incorporated | Turbine rotor assembly |
| US9677407B2 (en) | 2013-01-09 | 2017-06-13 | United Technologies Corporation | Rotor cover plate |
| US10458258B2 (en) * | 2013-01-30 | 2019-10-29 | United Technologies Corporation | Double snapped cover plate for rotor disk |
| US10253642B2 (en) | 2013-09-16 | 2019-04-09 | United Technologies Corporation | Gas turbine engine with disk having periphery with protrusions |
| WO2015069362A2 (en) | 2013-09-17 | 2015-05-14 | United Technologies Corporation | Gas turbine engine with seal having protrusions |
| EP2860351A1 (de) * | 2013-10-10 | 2015-04-15 | Siemens Aktiengesellschaft | Anordnung zum Sichern einer Funktionsstellung einer an einer Läuferscheibe angeordneten Deckplatte relativ zu einer an der Läuferscheibe angeordneten Laufschaufel |
| US10221708B2 (en) * | 2014-12-03 | 2019-03-05 | United Technologies Corporation | Tangential on-board injection vanes |
| US9810087B2 (en) | 2015-06-24 | 2017-11-07 | United Technologies Corporation | Reversible blade rotor seal with protrusions |
| GB201514212D0 (en) * | 2015-08-12 | 2015-09-23 | Rolls Royce Plc | Turbine disc assembly |
| US10612383B2 (en) * | 2016-01-27 | 2020-04-07 | General Electric Company | Compressor aft rotor rim cooling for high OPR (T3) engine |
| FR3064667B1 (fr) * | 2017-03-31 | 2020-05-15 | Safran Aircraft Engines | Dispositif de refroidissement d'un rotor de turbomachine |
| US10280842B2 (en) * | 2017-04-10 | 2019-05-07 | United Technologies Corporation | Nut with air seal |
| US10975714B2 (en) * | 2018-11-22 | 2021-04-13 | Pratt & Whitney Canada Corp. | Rotor assembly with blade sealing tab |
| CN109489957B (zh) * | 2018-12-10 | 2020-12-15 | 中国航发四川燃气涡轮研究院 | 一种用于轮盘试验的带应力分割槽的转接结构 |
| CN111828108B (zh) * | 2020-07-24 | 2023-02-21 | 中国科学院工程热物理研究所 | 一种发动机涡轮盘预旋系统用盖板盘结构 |
| CN112459851B (zh) * | 2020-10-27 | 2021-12-17 | 中船重工龙江广瀚燃气轮机有限公司 | 一种涡轮动叶冷却空气增压装置 |
| CN112302731B (zh) * | 2020-10-27 | 2022-11-18 | 西北工业大学 | 一种用于涡轮盘多排渐缩型圆柱孔状的径向轮缘密封结构 |
| RU208145U1 (ru) * | 2021-06-07 | 2021-12-06 | Публичное Акционерное Общество "Одк-Сатурн" | Узел ротора турбины высокого давления |
| US11795821B1 (en) | 2022-04-08 | 2023-10-24 | Pratt & Whitney Canada Corp. | Rotor having crack mitigator |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2951340A (en) * | 1956-01-03 | 1960-09-06 | Curtiss Wright Corp | Gas turbine with control mechanism for turbine cooling air |
| US3748060A (en) * | 1971-09-14 | 1973-07-24 | Westinghouse Electric Corp | Sideplate for turbine blade |
| US4344738A (en) * | 1979-12-17 | 1982-08-17 | United Technologies Corporation | Rotor disk structure |
| JPH0231355U (enExample) * | 1988-08-19 | 1990-02-27 | ||
| FR2663997B1 (fr) * | 1990-06-27 | 1993-12-24 | Snecma | Dispositif de fixation d'une couronne de revolution sur un disque de turbomachine. |
| US5143512A (en) | 1991-02-28 | 1992-09-01 | General Electric Company | Turbine rotor disk with integral blade cooling air slots and pumping vanes |
| JPH0571305A (ja) * | 1991-03-04 | 1993-03-23 | General Electric Co <Ge> | ロータブレードをロータデイスクに取付けるプラツトホームアセンブリ |
| US5275534A (en) | 1991-10-30 | 1994-01-04 | General Electric Company | Turbine disk forward seal assembly |
| US5333993A (en) * | 1993-03-01 | 1994-08-02 | General Electric Company | Stator seal assembly providing improved clearance control |
| JP3052980B2 (ja) * | 1993-07-13 | 2000-06-19 | 株式会社日立製作所 | 冷媒回収型ガスタービン |
| FR2744761B1 (fr) * | 1996-02-08 | 1998-03-13 | Snecma | Disque labyrinthe avec raidisseur incorpore pour rotor de turbomachine |
| GB9615394D0 (en) * | 1996-07-23 | 1996-09-04 | Rolls Royce Plc | Gas turbine engine rotor disc with cooling fluid passage |
| US5984636A (en) * | 1997-12-17 | 1999-11-16 | Pratt & Whitney Canada Inc. | Cooling arrangement for turbine rotor |
| US5984630A (en) | 1997-12-24 | 1999-11-16 | General Electric Company | Reduced windage high pressure turbine forward outer seal |
| DE59810560D1 (de) * | 1998-11-30 | 2004-02-12 | Alstom Switzerland Ltd | Schaufelkühlung |
| JP2000186502A (ja) * | 1998-12-24 | 2000-07-04 | Hitachi Ltd | ガスタービン |
| US6331097B1 (en) | 1999-09-30 | 2001-12-18 | General Electric Company | Method and apparatus for purging turbine wheel cavities |
-
2002
- 2002-08-29 US US10/231,420 patent/US6749400B2/en not_active Expired - Fee Related
-
2003
- 2003-08-28 JP JP2003303865A patent/JP4272483B2/ja not_active Expired - Fee Related
- 2003-08-29 CN CNB031557066A patent/CN100359133C/zh not_active Expired - Fee Related
- 2003-08-29 DE DE60318977T patent/DE60318977T2/de not_active Expired - Lifetime
- 2003-08-29 EP EP03255403A patent/EP1394358B1/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| DE60318977T2 (de) | 2009-02-05 |
| JP2004092644A (ja) | 2004-03-25 |
| US20040042900A1 (en) | 2004-03-04 |
| EP1394358A2 (en) | 2004-03-03 |
| EP1394358A3 (en) | 2005-11-23 |
| US6749400B2 (en) | 2004-06-15 |
| CN1490496A (zh) | 2004-04-21 |
| CN100359133C (zh) | 2008-01-02 |
| DE60318977D1 (de) | 2008-03-20 |
| EP1394358B1 (en) | 2008-02-06 |
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Legal Events
| Date | Code | Title | Description |
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| A521 | Written amendment |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20060818 |
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| A621 | Written request for application examination |
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| A01 | Written decision to grant a patent or to grant a registration (utility model) |
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| A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20090227 |
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| FPAY | Renewal fee payment (event date is renewal date of database) |
Free format text: PAYMENT UNTIL: 20120306 Year of fee payment: 3 |
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| R150 | Certificate of patent or registration of utility model |
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| LAPS | Cancellation because of no payment of annual fees |