BR112014012584A2 - pá de turbomáquina, notadamente para disco com pás monobloco - Google Patents
pá de turbomáquina, notadamente para disco com pás monoblocoInfo
- Publication number
- BR112014012584A2 BR112014012584A2 BR112014012584A BR112014012584A BR112014012584A2 BR 112014012584 A2 BR112014012584 A2 BR 112014012584A2 BR 112014012584 A BR112014012584 A BR 112014012584A BR 112014012584 A BR112014012584 A BR 112014012584A BR 112014012584 A2 BR112014012584 A2 BR 112014012584A2
- Authority
- BR
- Brazil
- Prior art keywords
- blade
- notably
- foot
- disc
- turbocharger
- Prior art date
Links
Classifications
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- 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
- 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
- F04D29/324—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
- F01D5/34—Rotor-blade aggregates of unitary construction, e.g. formed of sheet laminae
-
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/321—Application in turbines in gas turbines for a special turbine stage
- F05D2220/3216—Application in turbines in gas turbines for a special turbine stage for a special compressor stage
-
- 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
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/24—Rotors for turbines
- F05D2240/242—Rotors for turbines of reaction type
-
- 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
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/303—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the leading edge of a rotor blade
-
- 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
- F05D2250/00—Geometry
- F05D2250/70—Shape
- F05D2250/71—Shape curved
-
- 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)
- Ceramic Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
1/1 resumo pá de turbomáquina, notadamente para disco com pás monobloco a invenção se refere a uma pá de turbomáquina, que compreende uma lâmina que se estende axialmente entre um bordo de ataque e um bordo de fuga e radialmente entre um pé e um topo. o bordo de ataque da lâmina apresenta um ângulo de flecha que é positivo e continuamente crescente a partir do pé até uma primeira altura radial de lâmina (h1) situada entre 20 % e 40 % da altura radial total da lâmina medida a partir do pé na direção do topo, e continuamente decrescente a partir dessa primeira altura radial de lâmina até o topo.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1160893 | 2011-11-29 | ||
FR1160893A FR2983234B1 (fr) | 2011-11-29 | 2011-11-29 | Aube pour disque aubage monobloc de turbomachine |
PCT/FR2012/052695 WO2013079851A1 (fr) | 2011-11-29 | 2012-11-22 | Aube de turbomachine notamment pour disque aubage monobloc |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112014012584A2 true BR112014012584A2 (pt) | 2017-06-13 |
BR112014012584B1 BR112014012584B1 (pt) | 2022-01-04 |
Family
ID=47436044
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112014012584-8A BR112014012584B1 (pt) | 2011-11-29 | 2012-11-22 | Pá de turbomáquina, disco com pás monobloco e turbomáquina |
Country Status (9)
Country | Link |
---|---|
US (1) | US9556740B2 (pt) |
EP (1) | EP2785978B1 (pt) |
JP (1) | JP6091517B2 (pt) |
CN (1) | CN103958833B (pt) |
BR (1) | BR112014012584B1 (pt) |
CA (1) | CA2855956C (pt) |
FR (1) | FR2983234B1 (pt) |
RU (1) | RU2607712C1 (pt) |
WO (1) | WO2013079851A1 (pt) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3009588B1 (fr) * | 2013-08-07 | 2018-01-26 | Safran Aircraft Engines | Aube mobile de turbomachine |
FR3010442B1 (fr) | 2013-09-09 | 2015-10-09 | Snecma | Disque aubage monobloc a contraintes reduites en pied d'aube, de preference pour soufflante de turbomachine d'aeronef |
US10495106B2 (en) | 2014-02-19 | 2019-12-03 | United Technologies Corporation | Gas turbine engine airfoil |
EP4279706A3 (en) | 2014-02-19 | 2024-02-28 | RTX Corporation | Turbofan engine with geared architecture and lpc blade airfoils |
EP3108105B1 (en) | 2014-02-19 | 2021-05-12 | Raytheon Technologies Corporation | Gas turbine engine airfoil |
WO2015126774A1 (en) | 2014-02-19 | 2015-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
WO2015175045A2 (en) | 2014-02-19 | 2015-11-19 | United Technologies Corporation | Gas turbine engine airfoil |
EP3108103B1 (en) | 2014-02-19 | 2023-09-27 | Raytheon Technologies Corporation | Fan blade for a gas turbine engine |
WO2015126453A1 (en) | 2014-02-19 | 2015-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
EP3108109B1 (en) | 2014-02-19 | 2023-09-13 | Raytheon Technologies Corporation | Gas turbine engine fan blade |
US10465702B2 (en) * | 2014-02-19 | 2019-11-05 | United Technologies Corporation | Gas turbine engine airfoil |
US10584715B2 (en) | 2014-02-19 | 2020-03-10 | United Technologies Corporation | Gas turbine engine airfoil |
WO2015178974A2 (en) | 2014-02-19 | 2015-11-26 | United Technologies Corporation | Gas turbine engine airfoil |
WO2015126454A1 (en) | 2014-02-19 | 2015-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
US10385866B2 (en) | 2014-02-19 | 2019-08-20 | United Technologies Corporation | Gas turbine engine airfoil |
US9599064B2 (en) | 2014-02-19 | 2017-03-21 | United Technologies Corporation | Gas turbine engine airfoil |
US10557477B2 (en) | 2014-02-19 | 2020-02-11 | United Technologies Corporation | Gas turbine engine airfoil |
WO2015175044A2 (en) | 2014-02-19 | 2015-11-19 | United Technologies Corporation | Gas turbine engine airfoil |
EP3108110B1 (en) | 2014-02-19 | 2020-04-22 | United Technologies Corporation | Gas turbine engine airfoil |
EP4279747A3 (en) | 2014-02-19 | 2024-03-13 | RTX Corporation | Turbofan engine with geared architecture and lpc blades |
EP3108114B1 (en) | 2014-02-19 | 2021-12-08 | Raytheon Technologies Corporation | Gas turbine engine airfoil |
US10443390B2 (en) | 2014-08-27 | 2019-10-15 | Pratt & Whitney Canada Corp. | Rotary airfoil |
US9765795B2 (en) | 2014-08-27 | 2017-09-19 | Pratt & Whitney Canada Corp. | Compressor rotor airfoil |
GB201702382D0 (en) | 2017-02-14 | 2017-03-29 | Rolls Royce Plc | Gas turbine engine fan blade |
GB201702384D0 (en) | 2017-02-14 | 2017-03-29 | Rolls Royce Plc | Gas turbine engine fan blade |
GB201702380D0 (en) * | 2017-02-14 | 2017-03-29 | Rolls Royce Plc | Gas turbine engine fan blade with axial lean |
CN109598081B (zh) * | 2018-12-13 | 2020-11-10 | 西安交通大学 | 基于数据降维及多二维流面的径流式透平气动优化方法 |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5088892A (en) * | 1990-02-07 | 1992-02-18 | United Technologies Corporation | Bowed airfoil for the compression section of a rotary machine |
US5642985A (en) * | 1995-11-17 | 1997-07-01 | United Technologies Corporation | Swept turbomachinery blade |
JPH10103002A (ja) * | 1996-09-30 | 1998-04-21 | Toshiba Corp | 軸流流体機械用翼 |
US6312219B1 (en) * | 1999-11-05 | 2001-11-06 | General Electric Company | Narrow waist vane |
US6331100B1 (en) * | 1999-12-06 | 2001-12-18 | General Electric Company | Doubled bowed compressor airfoil |
US6328533B1 (en) | 1999-12-21 | 2001-12-11 | General Electric Company | Swept barrel airfoil |
US6899526B2 (en) * | 2003-08-05 | 2005-05-31 | General Electric Company | Counterstagger compressor airfoil |
DE102004011607B4 (de) * | 2004-03-10 | 2016-11-24 | MTU Aero Engines AG | Verdichter einer Gasturbine sowie Gasturbine |
JP4863162B2 (ja) * | 2006-05-26 | 2012-01-25 | 株式会社Ihi | ターボファンエンジンのファン動翼 |
FR2908152B1 (fr) * | 2006-11-08 | 2009-02-06 | Snecma Sa | Aube en fleche de turbomachine |
US7967571B2 (en) * | 2006-11-30 | 2011-06-28 | General Electric Company | Advanced booster rotor blade |
US7758306B2 (en) * | 2006-12-22 | 2010-07-20 | General Electric Company | Turbine assembly for a gas turbine engine and method of manufacturing the same |
DE102008055824B4 (de) * | 2007-11-09 | 2016-08-11 | Alstom Technology Ltd. | Dampfturbine |
US8147207B2 (en) * | 2008-09-04 | 2012-04-03 | Siemens Energy, Inc. | Compressor blade having a ratio of leading edge sweep to leading edge dihedral in a range of 1:1 to 3:1 along the radially outer portion |
US8167567B2 (en) | 2008-12-17 | 2012-05-01 | United Technologies Corporation | Gas turbine engine airfoil |
FR2969230B1 (fr) | 2010-12-15 | 2014-11-21 | Snecma | Aube de compresseur a loi d'empilage amelioree |
JP5703750B2 (ja) * | 2010-12-28 | 2015-04-22 | 株式会社Ihi | ファン動翼及びファン |
US8702398B2 (en) * | 2011-03-25 | 2014-04-22 | General Electric Company | High camber compressor rotor blade |
-
2011
- 2011-11-29 FR FR1160893A patent/FR2983234B1/fr active Active
-
2012
- 2012-11-22 JP JP2014543953A patent/JP6091517B2/ja active Active
- 2012-11-22 EP EP12806546.3A patent/EP2785978B1/fr active Active
- 2012-11-22 US US14/361,594 patent/US9556740B2/en active Active
- 2012-11-22 CN CN201280058657.2A patent/CN103958833B/zh active Active
- 2012-11-22 CA CA2855956A patent/CA2855956C/fr active Active
- 2012-11-22 BR BR112014012584-8A patent/BR112014012584B1/pt active IP Right Grant
- 2012-11-22 WO PCT/FR2012/052695 patent/WO2013079851A1/fr active Application Filing
- 2012-11-22 RU RU2014126418A patent/RU2607712C1/ru active
Also Published As
Publication number | Publication date |
---|---|
WO2013079851A1 (fr) | 2013-06-06 |
JP6091517B2 (ja) | 2017-03-08 |
JP2014533809A (ja) | 2014-12-15 |
CN103958833A (zh) | 2014-07-30 |
FR2983234A1 (fr) | 2013-05-31 |
EP2785978A1 (fr) | 2014-10-08 |
BR112014012584B1 (pt) | 2022-01-04 |
CN103958833B (zh) | 2016-03-02 |
EP2785978B1 (fr) | 2016-04-27 |
CA2855956A1 (fr) | 2013-06-06 |
RU2607712C1 (ru) | 2017-01-10 |
US20140341749A1 (en) | 2014-11-20 |
CA2855956C (fr) | 2019-02-12 |
US9556740B2 (en) | 2017-01-31 |
FR2983234B1 (fr) | 2014-01-17 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette] | ||
B350 | Update of information on the portal [chapter 15.35 patent gazette] | ||
B06A | Patent application procedure suspended [chapter 6.1 patent gazette] | ||
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B16A | Patent or certificate of addition of invention granted [chapter 16.1 patent gazette] |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 22/11/2012, OBSERVADAS AS CONDICOES LEGAIS. |