BR112012007831A2 - turbina de geometria variável. - Google Patents
turbina de geometria variável.Info
- Publication number
- BR112012007831A2 BR112012007831A2 BR112012007831A BR112012007831A BR112012007831A2 BR 112012007831 A2 BR112012007831 A2 BR 112012007831A2 BR 112012007831 A BR112012007831 A BR 112012007831A BR 112012007831 A BR112012007831 A BR 112012007831A BR 112012007831 A2 BR112012007831 A2 BR 112012007831A2
- Authority
- BR
- Brazil
- Prior art keywords
- turbine
- inlet
- jacket
- variable geometry
- axial extension
- 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
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
-
- 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
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/18—Final actuators arranged in stator parts varying effective number of nozzles or guide conduits, e.g. sequentially operable valves for steam turbines
-
- 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
- F05D2220/40—Application in turbochargers
-
- 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
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
-
- 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
- F05D2250/10—Two-dimensional
- F05D2250/18—Two-dimensional patterned
- F05D2250/182—Two-dimensional patterned crenellated, notched
-
- 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
- F05D2250/60—Structure; Surface texture
- F05D2250/61—Structure; Surface texture corrugated
- F05D2250/611—Structure; Surface texture corrugated undulated
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
- Hydraulic Turbines (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
turbina de geometria variável - de acordo com um primeiro aspecto da presente invenção, é provida uma turbina de geometria variável compreendendo: uma roda de turbina montada para rotação em torno de um eixo geométrico da turbina dentro de um alojamento definido uma entrada anular envolvendo a roda de turbina e definida entre primeira e segunda paredes laterais de entrada, a entrada anular sendo dividida em pelo menos duas porções de entrada axialmente deslocadas; uma camisa cilíndrica axialmente móvel através da entrada anular para variar o tamanho do caminho de fluxo de gás através da entrada; em que a extensão axial da extremidade de avanço da camisa varia de magnitude em torno da circunferência da camisa. a variação na extensão axial define uma pluralidade de recessos e/ou protuberâncias localizada em torno da circunferência da extremidade de avanço da camisa. a camisa, ou a sua extensão axial, é livre de paletas.
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0917513A GB0917513D0 (en) | 2009-10-06 | 2009-10-06 | Axially divided nozzle VG |
GBGB1005680.2A GB201005680D0 (en) | 2010-04-06 | 2010-04-06 | Variable geometry turbine |
GBGB1012488.1A GB201012488D0 (en) | 2010-07-26 | 2010-07-26 | Turbomachine |
PCT/GB2010/001869 WO2011042695A2 (en) | 2009-10-06 | 2010-10-06 | Turbomachine |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112012007831A2 true BR112012007831A2 (pt) | 2016-03-08 |
Family
ID=43857220
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112012007831A BR112012007831A2 (pt) | 2009-10-06 | 2010-10-06 | turbina de geometria variável. |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP2486245A2 (pt) |
CN (1) | CN102667071A (pt) |
BR (1) | BR112012007831A2 (pt) |
IN (1) | IN2012DN02723A (pt) |
WO (1) | WO2011042695A2 (pt) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113710884B (zh) * | 2019-04-19 | 2023-10-20 | 三菱重工发动机和增压器株式会社 | 可变容量涡轮机以及增压器 |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2861774A (en) * | 1950-02-16 | 1958-11-25 | Alfred J Buchi | Inlet control for radial flow turbines |
BE793550A (fr) * | 1971-12-29 | 1973-04-16 | Gen Electric | Pompe centrifuge a diffuseur reglable |
JPH05133238A (ja) * | 1991-11-11 | 1993-05-28 | Mitsubishi Heavy Ind Ltd | 可変容量過給機 |
DE4204019A1 (de) * | 1992-02-12 | 1993-05-27 | Daimler Benz Ag | Gesteuerte abgasturboladerturbine fuer einen verbrennungsmotor |
GB0521354D0 (en) * | 2005-10-20 | 2005-11-30 | Holset Engineering Co | Variable geometry turbine |
EP1957757B1 (en) * | 2005-11-16 | 2013-02-13 | Honeywell International Inc. | Turbocharger having an axially sliding piston cartridge |
-
2010
- 2010-10-06 WO PCT/GB2010/001869 patent/WO2011042695A2/en active Application Filing
- 2010-10-06 EP EP10776114A patent/EP2486245A2/en not_active Withdrawn
- 2010-10-06 BR BR112012007831A patent/BR112012007831A2/pt not_active IP Right Cessation
- 2010-10-06 IN IN2723DEN2012 patent/IN2012DN02723A/en unknown
- 2010-10-06 CN CN2010800553264A patent/CN102667071A/zh active Pending
Also Published As
Publication number | Publication date |
---|---|
EP2486245A2 (en) | 2012-08-15 |
IN2012DN02723A (pt) | 2015-09-11 |
CN102667071A (zh) | 2012-09-12 |
WO2011042695A2 (en) | 2011-04-14 |
WO2011042695A3 (en) | 2011-11-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application fees: dismissal - article 86 of industrial property law |
Free format text: REFERENTE AS 5A E 6A ANUIDADES. |
|
B08K | Lapse as no evidence of payment of the annual fee has been furnished to inpi (acc. art. 87) |
Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2384 DE 13-09-2016 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013. |