JP4974096B2 - 縦溝付き圧縮機流路 - Google Patents
縦溝付き圧縮機流路 Download PDFInfo
- Publication number
- JP4974096B2 JP4974096B2 JP2001039367A JP2001039367A JP4974096B2 JP 4974096 B2 JP4974096 B2 JP 4974096B2 JP 2001039367 A JP2001039367 A JP 2001039367A JP 2001039367 A JP2001039367 A JP 2001039367A JP 4974096 B2 JP4974096 B2 JP 4974096B2
- Authority
- JP
- Japan
- Prior art keywords
- flow path
- adjacent
- compressor
- blade
- wall
- 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
- 230000007423 decrease Effects 0.000 claims description 4
- 230000006835 compression Effects 0.000 description 9
- 238000007906 compression Methods 0.000 description 9
- 238000009792 diffusion process Methods 0.000 description 8
- 239000007789 gas Substances 0.000 description 8
- 238000013461 design Methods 0.000 description 7
- 238000011144 upstream manufacturing Methods 0.000 description 7
- 238000005086 pumping Methods 0.000 description 5
- 239000000567 combustion gas Substances 0.000 description 3
- 239000000446 fuel Substances 0.000 description 3
- 230000002829 reductive effect Effects 0.000 description 3
- 230000007704 transition Effects 0.000 description 3
- 230000035939 shock Effects 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 238000010835 comparative analysis Methods 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000000670 limiting effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000036961 partial effect Effects 0.000 description 1
- 230000001141 propulsive effect Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 230000002441 reversible effect Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 239000013589 supplement Substances 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
- F01D5/12—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
- F01D5/143—Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/68—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
- F04D29/681—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
-
- 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
-
- 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)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/507,408 US6561761B1 (en) | 2000-02-18 | 2000-02-18 | Fluted compressor flowpath |
| US09/507408 | 2000-02-18 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2001271792A JP2001271792A (ja) | 2001-10-05 |
| JP2001271792A5 JP2001271792A5 (enExample) | 2008-04-03 |
| JP4974096B2 true JP4974096B2 (ja) | 2012-07-11 |
Family
ID=24018530
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2001039367A Expired - Fee Related JP4974096B2 (ja) | 2000-02-18 | 2001-02-16 | 縦溝付き圧縮機流路 |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US6561761B1 (enExample) |
| EP (1) | EP1126132A3 (enExample) |
| JP (1) | JP4974096B2 (enExample) |
| BR (1) | BR0100603B1 (enExample) |
| CA (1) | CA2333843C (enExample) |
| PL (1) | PL200265B1 (enExample) |
| RU (1) | RU2232922C2 (enExample) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20190234217A1 (en) * | 2018-02-01 | 2019-08-01 | Honda Motor Co., Ltd. | Fan blade and method for determining shape of fan blade |
Families Citing this family (125)
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| JP2001271602A (ja) * | 2000-03-27 | 2001-10-05 | Honda Motor Co Ltd | ガスタービンエンジン |
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| JP2005155613A (ja) * | 2003-10-31 | 2005-06-16 | Hitachi Ltd | ガスタービン及びガスタービンの製造方法 |
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| US7690890B2 (en) * | 2004-09-24 | 2010-04-06 | Ishikawajima-Harima Heavy Industries Co. Ltd. | Wall configuration of axial-flow machine, and gas turbine engine |
| US7217096B2 (en) * | 2004-12-13 | 2007-05-15 | General Electric Company | Fillet energized turbine stage |
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| US7249933B2 (en) * | 2005-01-10 | 2007-07-31 | General Electric Company | Funnel fillet turbine stage |
| WO2006080055A1 (ja) | 2005-01-26 | 2006-08-03 | Ishikawajima-Harima Heavy Industries Co., Ltd. | ターボファンエンジン |
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| GB0518628D0 (en) * | 2005-09-13 | 2005-10-19 | Rolls Royce Plc | Axial compressor blading |
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| JP4616781B2 (ja) * | 2006-03-16 | 2011-01-19 | 三菱重工業株式会社 | タービン翼列エンドウォール |
| US7874794B2 (en) * | 2006-03-21 | 2011-01-25 | General Electric Company | Blade row for a rotary machine and method of fabricating same |
| US8500399B2 (en) * | 2006-04-25 | 2013-08-06 | Rolls-Royce Corporation | Method and apparatus for enhancing compressor performance |
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| US8366399B2 (en) * | 2006-05-02 | 2013-02-05 | United Technologies Corporation | Blade or vane with a laterally enlarged base |
| US7887297B2 (en) * | 2006-05-02 | 2011-02-15 | United Technologies Corporation | Airfoil array with an endwall protrusion and components of the array |
| US7721526B2 (en) | 2006-06-28 | 2010-05-25 | Ishikawajima-Harima Heavy Industries Co., Ltd. | Turbofan engine |
| JP4911344B2 (ja) | 2006-07-04 | 2012-04-04 | 株式会社Ihi | ターボファンエンジン |
| FR2907519B1 (fr) * | 2006-10-20 | 2011-12-16 | Snecma | Nageoire de plateforme de soufflante |
| US8413709B2 (en) | 2006-12-06 | 2013-04-09 | General Electric Company | Composite core die, methods of manufacture thereof and articles manufactured therefrom |
| US7624787B2 (en) * | 2006-12-06 | 2009-12-01 | General Electric Company | Disposable insert, and use thereof in a method for manufacturing an airfoil |
| US20080135721A1 (en) * | 2006-12-06 | 2008-06-12 | General Electric Company | Casting compositions for manufacturing metal casting and methods of manufacturing thereof |
| US7938168B2 (en) * | 2006-12-06 | 2011-05-10 | General Electric Company | Ceramic cores, methods of manufacture thereof and articles manufactured from the same |
| US7487819B2 (en) * | 2006-12-11 | 2009-02-10 | General Electric Company | Disposable thin wall core die, methods of manufacture thereof and articles manufactured therefrom |
| US8884182B2 (en) | 2006-12-11 | 2014-11-11 | General Electric Company | Method of modifying the end wall contour in a turbine using laser consolidation and the turbines derived therefrom |
| GB0704426D0 (en) * | 2007-03-08 | 2007-04-18 | Rolls Royce Plc | Aerofoil members for a turbomachine |
| JP5283855B2 (ja) * | 2007-03-29 | 2013-09-04 | 株式会社Ihi | ターボ機械の壁、及びターボ機械 |
| DE102007020025A1 (de) * | 2007-04-27 | 2008-10-30 | Honda Motor Co., Ltd. | Form eines Gaskanals in einer Axialströmungs-Gasturbinenmaschine |
| US8313291B2 (en) * | 2007-12-19 | 2012-11-20 | Nuovo Pignone, S.P.A. | Turbine inlet guide vane with scalloped platform and related method |
| FR2926856B1 (fr) * | 2008-01-30 | 2013-03-29 | Snecma | Compresseur de turboreacteur |
| FR2928172B1 (fr) * | 2008-02-28 | 2015-07-17 | Snecma | Aube avec plateforme non axisymetrique lineaire. |
| FR2928174B1 (fr) * | 2008-02-28 | 2011-05-06 | Snecma | Aube avec plateforme non axisymetrique : creux et bosse sur extrados. |
| FR2928173B1 (fr) * | 2008-02-28 | 2015-06-26 | Snecma | Aube avec plateforme 3d comportant un bulbe interaubes. |
| DE102008021053A1 (de) * | 2008-04-26 | 2009-10-29 | Mtu Aero Engines Gmbh | Nachgeformter Strömungspfad einer Axialströmungsmaschine zur Verringerung von Sekundärströmung |
| DE102008031789A1 (de) * | 2008-07-04 | 2010-01-07 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Verfahren und Vorrichtung zur Beeinflussung von Sekundärströmungen bei einer Turbomaschine |
| DE102008060424A1 (de) | 2008-12-04 | 2010-06-10 | Rolls-Royce Deutschland Ltd & Co Kg | Strömungsmaschine mit Seitenwand-Grenzschicht-Barriere |
| US8647067B2 (en) * | 2008-12-09 | 2014-02-11 | General Electric Company | Banked platform turbine blade |
| US8459956B2 (en) * | 2008-12-24 | 2013-06-11 | General Electric Company | Curved platform turbine blade |
| US8231353B2 (en) * | 2008-12-31 | 2012-07-31 | General Electric Company | Methods and apparatus relating to improved turbine blade platform contours |
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| JP5398405B2 (ja) * | 2009-07-30 | 2014-01-29 | 三菱重工業株式会社 | 流路構造及びガスタービン排気ディフューザ |
| US8439643B2 (en) * | 2009-08-20 | 2013-05-14 | General Electric Company | Biformal platform turbine blade |
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2000
- 2000-02-18 US US09/507,408 patent/US6561761B1/en not_active Expired - Lifetime
-
2001
- 2001-02-01 CA CA002333843A patent/CA2333843C/en not_active Expired - Fee Related
- 2001-02-14 PL PL345839A patent/PL200265B1/pl unknown
- 2001-02-16 EP EP01301359A patent/EP1126132A3/en not_active Withdrawn
- 2001-02-16 RU RU2001104477/06A patent/RU2232922C2/ru not_active IP Right Cessation
- 2001-02-16 BR BRPI0100603-7A patent/BR0100603B1/pt not_active IP Right Cessation
- 2001-02-16 JP JP2001039367A patent/JP4974096B2/ja not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20190234217A1 (en) * | 2018-02-01 | 2019-08-01 | Honda Motor Co., Ltd. | Fan blade and method for determining shape of fan blade |
| US10934848B2 (en) * | 2018-02-01 | 2021-03-02 | Honda Motor Co., Ltd. | Fan blade and method for determining shape of fan blade |
Also Published As
| Publication number | Publication date |
|---|---|
| EP1126132A3 (en) | 2003-05-02 |
| EP1126132A2 (en) | 2001-08-22 |
| PL345839A1 (en) | 2001-08-27 |
| RU2232922C2 (ru) | 2004-07-20 |
| BR0100603B1 (pt) | 2010-02-09 |
| JP2001271792A (ja) | 2001-10-05 |
| CA2333843A1 (en) | 2001-08-18 |
| CA2333843C (en) | 2009-09-15 |
| BR0100603A (pt) | 2001-10-09 |
| US6561761B1 (en) | 2003-05-13 |
| PL200265B1 (pl) | 2008-12-31 |
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