GB2445895A - First stage turbine airfoil - Google Patents
First stage turbine airfoilInfo
- Publication number
- GB2445895A GB2445895A GB0807796A GB0807796A GB2445895A GB 2445895 A GB2445895 A GB 2445895A GB 0807796 A GB0807796 A GB 0807796A GB 0807796 A GB0807796 A GB 0807796A GB 2445895 A GB2445895 A GB 2445895A
- Authority
- GB
- United Kingdom
- Prior art keywords
- stage turbine
- external surface
- turbine airfoil
- airfoil
- streamwise
- 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.)
- Granted
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
-
- 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
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/047—Nozzle boxes
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Architecture (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
The present invention provides an airfoil for a first stage turbine blade having an external surface with first and second sides. The external surface extends spanwise between a hub and a tip and streamwise between a leading edge and a trailing edge of the airfoil. The external surface includes a contour substantially defined by Table 1 as listed in the specification.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US75503305P | 2005-12-29 | 2005-12-29 | |
| PCT/IB2006/004082 WO2008035135A2 (en) | 2005-12-29 | 2006-12-21 | First stage turbine airfoil |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| GB0807796D0 GB0807796D0 (en) | 2008-06-04 |
| GB2445895A true GB2445895A (en) | 2008-07-23 |
| GB2445895B GB2445895B (en) | 2011-06-22 |
Family
ID=39523307
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB0807796A Expired - Fee Related GB2445895B (en) | 2005-12-29 | 2006-12-21 | First stage turbine airfoil |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB2445895B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US12509988B2 (en) | 2024-06-14 | 2025-12-30 | Pratt & Whitney Canada Corp. | Turbine engine airfoil |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1560683A (en) * | 1972-11-28 | 1980-02-06 | Rolls Royce | Turbine blade |
| US6749396B2 (en) * | 2002-06-17 | 2004-06-15 | General Electric Company | Failsafe film cooled wall |
-
2006
- 2006-12-21 GB GB0807796A patent/GB2445895B/en not_active Expired - Fee Related
Non-Patent Citations (1)
| Title |
|---|
| Not yet advised * |
Also Published As
| Publication number | Publication date |
|---|---|
| GB2445895B (en) | 2011-06-22 |
| GB0807796D0 (en) | 2008-06-04 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB2448087A (en) | Second Stage Turbine Airfoil | |
| GB2445894A (en) | Third stage turbine airfoil | |
| WO2008035135A3 (en) | First stage turbine airfoil | |
| GB2448085B (en) | Airfoil for a third stage nozzle guide vane | |
| GB2445896A (en) | Turbine nozzle blade airfoil geometry | |
| WO2007085912A3 (en) | Airfoil for a first stage nozzle guide vane | |
| EP2025777A3 (en) | Low transit thermal stress turbine engine components | |
| GB2413599B (en) | Turbine airfoil trailing edge repair and methods therefor | |
| WO2012134833A3 (en) | High camber compressor rotor blade | |
| ATE490913T1 (en) | AERODYNAMIC FLAP OF AN AIRCRAFT HAVING A DEVICE AFFECTING THE FLAP VOLTAGE | |
| CA2580105C (en) | Hp turbine vane airfoil profile | |
| EP1754859A3 (en) | Methods and apparatus for reducing vibrations induced to airfoils | |
| AU2003299548A1 (en) | Slotted aircraft wing | |
| DK201170603A (en) | Noise reducer for rotor blade in wind turbine | |
| WO2010124914A3 (en) | Wind turbine rotor blade | |
| WO2013130181A3 (en) | Low loss airfoil platform trailing edge | |
| WO2009112775A3 (en) | Blade with non-axisymmetric platform | |
| EP2484869A3 (en) | Strut airfoil design for low solidity exhaust gas diffuser | |
| TW200714794A (en) | Turbine vane construction | |
| PL1524431T3 (en) | Wind turbine blade with trailing edge flaps | |
| DK201370046A (en) | Wind turbine rotor blade assembly with root extension panel and method of assembly | |
| EP1693552A3 (en) | A turbine blade | |
| SG134213A1 (en) | Microcircuit cooling with an aspect ratio of unity | |
| CA2640697A1 (en) | Axial-flow fluid machine blade | |
| EP2050926A3 (en) | Method for restoring airfoil contour on integrally bladed rotors |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 732E | Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977) |
Free format text: REGISTERED BETWEEN 20150305 AND 20150311 |
|
| PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20181221 |