IT1320722B1 - Metodo per il posizionamento di schiere di stadi di una turbina,particolarmente per motori aeronautici. - Google Patents
Metodo per il posizionamento di schiere di stadi di una turbina,particolarmente per motori aeronautici.Info
- Publication number
- IT1320722B1 IT1320722B1 IT2000TO001001A ITTO20001001A IT1320722B1 IT 1320722 B1 IT1320722 B1 IT 1320722B1 IT 2000TO001001 A IT2000TO001001 A IT 2000TO001001A IT TO20001001 A ITTO20001001 A IT TO20001001A IT 1320722 B1 IT1320722 B1 IT 1320722B1
- Authority
- IT
- Italy
- Prior art keywords
- array
- turbine
- positioning
- aircraft engines
- blades
- Prior art date
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
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
- F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
-
- 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)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Jigs For Machine Tools (AREA)
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT2000TO001001A IT1320722B1 (it) | 2000-10-23 | 2000-10-23 | Metodo per il posizionamento di schiere di stadi di una turbina,particolarmente per motori aeronautici. |
AT01114848T ATE277276T1 (de) | 2000-10-23 | 2001-06-28 | Turbinenschaufelanordnung |
EP01114848A EP1201877B1 (en) | 2000-10-23 | 2001-06-28 | Method of positioning turbine stage arrays |
DE60105737T DE60105737T2 (de) | 2000-10-23 | 2001-06-28 | Turbinenschaufelanordnung |
CA002352432A CA2352432C (en) | 2000-10-23 | 2001-07-05 | Method of positioning turbine stage arrays, particularly for aircraft engines |
US09/908,762 US6527503B2 (en) | 2000-10-23 | 2001-07-19 | Method of positioning turbine stage arrays, particularly for aircraft engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT2000TO001001A IT1320722B1 (it) | 2000-10-23 | 2000-10-23 | Metodo per il posizionamento di schiere di stadi di una turbina,particolarmente per motori aeronautici. |
Publications (3)
Publication Number | Publication Date |
---|---|
ITTO20001001A0 ITTO20001001A0 (it) | 2000-10-23 |
ITTO20001001A1 ITTO20001001A1 (it) | 2002-04-23 |
IT1320722B1 true IT1320722B1 (it) | 2003-12-10 |
Family
ID=11458153
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT2000TO001001A IT1320722B1 (it) | 2000-10-23 | 2000-10-23 | Metodo per il posizionamento di schiere di stadi di una turbina,particolarmente per motori aeronautici. |
Country Status (6)
Country | Link |
---|---|
US (1) | US6527503B2 (it) |
EP (1) | EP1201877B1 (it) |
AT (1) | ATE277276T1 (it) |
CA (1) | CA2352432C (it) |
DE (1) | DE60105737T2 (it) |
IT (1) | IT1320722B1 (it) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2310307T3 (es) | 2005-05-10 | 2009-01-01 | Mtu Aero Engines Gmbh | Procedimiento para la optimizacion de la corriente en motores de turbopropulsion de varias fases. |
DE102005048982A1 (de) | 2005-10-13 | 2007-04-19 | Mtu Aero Engines Gmbh | Vorrichtung und Verfahren zum axialen Verschieben eines Turbinenrotors |
US8540490B2 (en) * | 2008-06-20 | 2013-09-24 | General Electric Company | Noise reduction in a turbomachine, and a related method thereof |
JP5374199B2 (ja) * | 2009-03-19 | 2013-12-25 | 三菱重工業株式会社 | ガスタービン |
US10287987B2 (en) | 2010-07-19 | 2019-05-14 | United Technologies Corporation | Noise reducing vane |
US8684684B2 (en) * | 2010-08-31 | 2014-04-01 | General Electric Company | Turbine assembly with end-wall-contoured airfoils and preferenttial clocking |
US20130081402A1 (en) * | 2011-10-03 | 2013-04-04 | General Electric Company | Turbomachine having a gas flow aeromechanic system and method |
US8899975B2 (en) | 2011-11-04 | 2014-12-02 | General Electric Company | Combustor having wake air injection |
US9267687B2 (en) | 2011-11-04 | 2016-02-23 | General Electric Company | Combustion system having a venturi for reducing wakes in an airflow |
US20130209216A1 (en) * | 2012-02-09 | 2013-08-15 | General Electric Company | Turbomachine including flow improvement system |
US9500085B2 (en) * | 2012-07-23 | 2016-11-22 | General Electric Company | Method for modifying gas turbine performance |
US9322553B2 (en) | 2013-05-08 | 2016-04-26 | General Electric Company | Wake manipulating structure for a turbine system |
US9739201B2 (en) | 2013-05-08 | 2017-08-22 | General Electric Company | Wake reducing structure for a turbine system and method of reducing wake |
US9435221B2 (en) * | 2013-08-09 | 2016-09-06 | General Electric Company | Turbomachine airfoil positioning |
EP2918777B1 (en) * | 2014-03-11 | 2016-10-26 | United Technologies Corporation | Method for optimizing a vane to reduce noise |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4968216A (en) * | 1984-10-12 | 1990-11-06 | The Boeing Company | Two-stage fluid driven turbine |
US5486091A (en) * | 1994-04-19 | 1996-01-23 | United Technologies Corporation | Gas turbine airfoil clocking |
US6174129B1 (en) * | 1999-01-07 | 2001-01-16 | Siemens Westinghouse Power Corporation | Turbine vane clocking mechanism and method of assembling a turbine having such a mechanism |
US6402458B1 (en) * | 2000-08-16 | 2002-06-11 | General Electric Company | Clock turbine airfoil cooling |
-
2000
- 2000-10-23 IT IT2000TO001001A patent/IT1320722B1/it active
-
2001
- 2001-06-28 EP EP01114848A patent/EP1201877B1/en not_active Expired - Lifetime
- 2001-06-28 AT AT01114848T patent/ATE277276T1/de not_active IP Right Cessation
- 2001-06-28 DE DE60105737T patent/DE60105737T2/de not_active Expired - Lifetime
- 2001-07-05 CA CA002352432A patent/CA2352432C/en not_active Expired - Fee Related
- 2001-07-19 US US09/908,762 patent/US6527503B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
ITTO20001001A1 (it) | 2002-04-23 |
EP1201877A3 (en) | 2002-09-18 |
EP1201877B1 (en) | 2004-09-22 |
US6527503B2 (en) | 2003-03-04 |
EP1201877A2 (en) | 2002-05-02 |
ITTO20001001A0 (it) | 2000-10-23 |
US20020048510A1 (en) | 2002-04-25 |
ATE277276T1 (de) | 2004-10-15 |
DE60105737T2 (de) | 2005-11-10 |
CA2352432C (en) | 2009-02-17 |
DE60105737D1 (de) | 2004-10-28 |
CA2352432A1 (en) | 2002-04-23 |
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