BRPI0603516A - pá de guia de entrada, método para projetar uma pá de guia de entrada, e, aba para uma pá de guia de entrada - Google Patents
pá de guia de entrada, método para projetar uma pá de guia de entrada, e, aba para uma pá de guia de entradaInfo
- Publication number
- BRPI0603516A BRPI0603516A BRPI0603516-7A BRPI0603516A BRPI0603516A BR PI0603516 A BRPI0603516 A BR PI0603516A BR PI0603516 A BRPI0603516 A BR PI0603516A BR PI0603516 A BRPI0603516 A BR PI0603516A
- Authority
- BR
- Brazil
- Prior art keywords
- flap
- guide paddle
- entrance guide
- tab
- designing
- 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
- F01D5/148—Blades with variable camber, e.g. by ejection of fluid
-
- 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
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/30—Vanes
-
- 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
- F04D29/18—Rotors
- F04D29/22—Rotors specially for centrifugal pumps
- F04D29/24—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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
-
- 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
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S415/00—Rotary kinetic fluid motors or pumps
- Y10S415/914—Device to control boundary layer
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Air-Flow Control Members (AREA)
- Superstructure Of Vehicle (AREA)
Abstract
Pá DE GUIA DE ENTRADA, MéTODO PARA PROJETAR UMA Pá DE GUIA DE ENTRADA, E, ABA PARA UMA Pá DE GUIA DE ENTRADA Um pá de guia de entrada proporciona um fluxo de ar suave aperfeiçoado e evita separação de fluxo sob altos ângulos de incidência. A pá de guia de entrada inclui um esteio tendo superfícies laterais opostas que são continuamente curvadas para proporcionar uma distribuição de velocidade controlada na bonda de fuga do esteio. A pá de guia de entrada adicionalmente inclui uma aba tendo uma borda de ataque alinhada por trás da borda de fuga do esteio. Geralmente, o esteio e a aba são construídos conjuntamente para que ar de baixo momento no intervalo entre o esteio e a aba seja ativado e arrastado na camada limite da aba. O fluxo de ar proveniente do intervalo permanecerá apenso à aba para aperfeiçoar o fluxo proveniente da aba.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/258,608 US7549839B2 (en) | 2005-10-25 | 2005-10-25 | Variable geometry inlet guide vane |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0603516A true BRPI0603516A (pt) | 2007-08-14 |
Family
ID=36972756
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0603516-7A BRPI0603516A (pt) | 2005-10-25 | 2006-08-23 | pá de guia de entrada, método para projetar uma pá de guia de entrada, e, aba para uma pá de guia de entrada |
Country Status (11)
Country | Link |
---|---|
US (1) | US7549839B2 (pt) |
EP (3) | EP2460977B1 (pt) |
JP (1) | JP2007120494A (pt) |
KR (1) | KR20070044765A (pt) |
CN (1) | CN1955441A (pt) |
AU (1) | AU2006230736A1 (pt) |
BR (1) | BRPI0603516A (pt) |
CA (1) | CA2555074A1 (pt) |
IL (1) | IL177592A0 (pt) |
RU (1) | RU2006130698A (pt) |
SG (1) | SG131832A1 (pt) |
Families Citing this family (54)
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JP5029396B2 (ja) * | 2008-02-06 | 2012-09-19 | 株式会社Ihi | インレットガイドベーン及びターボ圧縮機並びに冷凍機 |
US9353765B2 (en) * | 2008-02-20 | 2016-05-31 | Trane International Inc. | Centrifugal compressor assembly and method |
US8349104B2 (en) * | 2008-07-21 | 2013-01-08 | United Technologies Corporation | Method and assembly for validating bond line |
DE102008049358A1 (de) * | 2008-09-29 | 2010-04-01 | Mtu Aero Engines Gmbh | Axiale Strömungsmaschine mit asymmetrischem Verdichtereintrittsleitgitter |
JP2010112298A (ja) * | 2008-11-07 | 2010-05-20 | Ihi Corp | ターボファンエンジン |
US9249736B2 (en) * | 2008-12-29 | 2016-02-02 | United Technologies Corporation | Inlet guide vanes and gas turbine engine systems involving such vanes |
AU2010310532B2 (en) | 2009-10-23 | 2015-07-23 | Dresser-Rand Company | Energy conversion system with duplex radial flow turbine |
US8534990B2 (en) * | 2009-11-11 | 2013-09-17 | Hamilton Sundstrand Corporation | Inlet guide vane drive system with spring preload on mechanical linkage |
US20110232291A1 (en) * | 2010-03-26 | 2011-09-29 | General Electric Company | System and method for an exhaust diffuser |
CN101967996A (zh) * | 2010-11-03 | 2011-02-09 | 上海理工大学 | 可调导叶 |
US20140064955A1 (en) * | 2011-09-14 | 2014-03-06 | General Electric Company | Guide vane assembly for a gas turbine engine |
US9068460B2 (en) | 2012-03-30 | 2015-06-30 | United Technologies Corporation | Integrated inlet vane and strut |
US10221707B2 (en) | 2013-03-07 | 2019-03-05 | Pratt & Whitney Canada Corp. | Integrated strut-vane |
US9835038B2 (en) | 2013-08-07 | 2017-12-05 | Pratt & Whitney Canada Corp. | Integrated strut and vane arrangements |
US9494053B2 (en) | 2013-09-23 | 2016-11-15 | Siemens Aktiengesellschaft | Diffuser with strut-induced vortex mixing |
US9556746B2 (en) | 2013-10-08 | 2017-01-31 | Pratt & Whitney Canada Corp. | Integrated strut and turbine vane nozzle arrangement |
US9656760B2 (en) | 2013-11-07 | 2017-05-23 | Sikorsky Aircraft Corporation | Variable geometry helicopter engine inlet |
US10094223B2 (en) | 2014-03-13 | 2018-10-09 | Pratt & Whitney Canada Corp. | Integrated strut and IGV configuration |
CN105443162B (zh) * | 2014-09-26 | 2017-04-19 | 中航商用航空发动机有限责任公司 | 发动机过渡段以及航空发动机 |
GB201419951D0 (en) * | 2014-11-10 | 2014-12-24 | Rolls Royce Plc | A guide vane |
CN105715585B (zh) * | 2014-12-05 | 2019-06-28 | 上海电气集团股份有限公司 | 可变几何出口导叶 |
EP3250830B1 (en) | 2015-01-28 | 2022-06-01 | Nuovo Pignone Tecnologie - S.r.l. | Device for controlling the flow in a turbomachine, turbomachine and method |
US10151325B2 (en) | 2015-04-08 | 2018-12-11 | General Electric Company | Gas turbine diffuser strut including a trailing edge flap and methods of assembling the same |
US9909434B2 (en) | 2015-07-24 | 2018-03-06 | Pratt & Whitney Canada Corp. | Integrated strut-vane nozzle (ISV) with uneven vane axial chords |
US9915149B2 (en) | 2015-08-27 | 2018-03-13 | Rolls-Royce North American Technologies Inc. | System and method for a fluidic barrier on the low pressure side of a fan blade |
US10125622B2 (en) | 2015-08-27 | 2018-11-13 | Rolls-Royce North American Technologies Inc. | Splayed inlet guide vanes |
US20170057649A1 (en) | 2015-08-27 | 2017-03-02 | Edward C. Rice | Integrated aircraft propulsion system |
US10267159B2 (en) | 2015-08-27 | 2019-04-23 | Rolls-Royce North America Technologies Inc. | System and method for creating a fluidic barrier with vortices from the upstream splitter |
US9976514B2 (en) | 2015-08-27 | 2018-05-22 | Rolls-Royce North American Technologies, Inc. | Propulsive force vectoring |
US10233869B2 (en) | 2015-08-27 | 2019-03-19 | Rolls Royce North American Technologies Inc. | System and method for creating a fluidic barrier from the leading edge of a fan blade |
US10267160B2 (en) | 2015-08-27 | 2019-04-23 | Rolls-Royce North American Technologies Inc. | Methods of creating fluidic barriers in turbine engines |
US10280872B2 (en) | 2015-08-27 | 2019-05-07 | Rolls-Royce North American Technologies Inc. | System and method for a fluidic barrier from the upstream splitter |
US10718221B2 (en) | 2015-08-27 | 2020-07-21 | Rolls Royce North American Technologies Inc. | Morphing vane |
CN106050318B (zh) * | 2016-05-30 | 2018-01-05 | 西安交通大学 | 一种适应大变工况范围的柔性静叶装置 |
US10443451B2 (en) | 2016-07-18 | 2019-10-15 | Pratt & Whitney Canada Corp. | Shroud housing supported by vane segments |
US10233782B2 (en) * | 2016-08-03 | 2019-03-19 | Solar Turbines Incorporated | Turbine assembly and method for flow control |
CN107725482A (zh) * | 2016-08-10 | 2018-02-23 | 上海电气燃气轮机有限公司 | 改善压气机变工况性能的分段调节出口导叶及其调节机构 |
US10253779B2 (en) * | 2016-08-11 | 2019-04-09 | General Electric Company | Inlet guide vane assembly for reducing airflow swirl distortion of an aircraft aft fan |
US20190078450A1 (en) * | 2017-09-08 | 2019-03-14 | United Technologies Corporation | Inlet guide vane having a varied trailing edge geometry |
CN107420349B (zh) * | 2017-09-14 | 2019-03-01 | 西安交通大学 | 一种预旋条件下低流动损失的离心压缩机进口导叶结构的设计方法 |
CN109159902B (zh) * | 2018-08-23 | 2020-08-21 | 金湖县农副产品营销协会 | 一种无人机发动机进气口引流机构 |
US10794200B2 (en) * | 2018-09-14 | 2020-10-06 | United Technologies Corporation | Integral half vane, ringcase, and id shroud |
US10781707B2 (en) * | 2018-09-14 | 2020-09-22 | United Technologies Corporation | Integral half vane, ringcase, and id shroud |
CN109058159B (zh) * | 2018-09-21 | 2024-07-23 | 特灵空调系统(中国)有限公司 | 风机和空调系统 |
US10815802B2 (en) * | 2018-12-17 | 2020-10-27 | Raytheon Technologies Corporation | Variable vane assemblies configured for non-axisymmetric actuation |
CN110296525A (zh) * | 2019-06-21 | 2019-10-01 | 珠海格力电器股份有限公司 | 具有降低噪音效果的导风叶片及其控制方法、空调机组 |
US10851705B1 (en) | 2019-07-12 | 2020-12-01 | Gm Global Technology Operations, Llc | Variable inlet guide vane system for a turbocharger used in a motor vehicle |
BE1027876B1 (fr) * | 2019-12-18 | 2021-07-26 | Safran Aero Boosters Sa | Module pour turbomachine |
CN111022189B (zh) * | 2019-12-24 | 2022-11-01 | 哈尔滨工程大学 | 一种输水槽带导流管的进气滤清装置惯性级叶片 |
TWI775377B (zh) * | 2021-04-06 | 2022-08-21 | 宏碁股份有限公司 | 散熱風扇 |
CN113819487B (zh) * | 2021-08-17 | 2024-09-20 | 南京航空航天大学 | 进气余旋角度和温度分布耦合的瞬态可调畸变发生装置 |
US11873738B2 (en) | 2021-12-23 | 2024-01-16 | General Electric Company | Integrated stator-fan frame assembly |
CN114526126B (zh) * | 2022-04-24 | 2022-07-26 | 中国航发四川燃气涡轮研究院 | 一种可消除旋转凸台的进口可变弯度导叶结构 |
CN115717604B (zh) * | 2022-09-28 | 2023-06-13 | 广东顺威精密塑料股份有限公司 | 一种带襟叶的后向离心风轮及其叶片叶型设计方法 |
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US2396811A (en) * | 1943-12-10 | 1946-03-19 | James E Bathras | Airplane propeller |
US3442493A (en) * | 1965-10-22 | 1969-05-06 | Gen Electric | Articulated airfoil vanes |
US4618313A (en) * | 1980-02-06 | 1986-10-21 | Cofimco S.R.L. | Axial propeller with increased effective displacement of air whose blades are not twisted |
US4542868A (en) * | 1983-06-06 | 1985-09-24 | Lockheed Corporation | Trailing edge device for an airfoil |
FR2607188B1 (fr) * | 1986-11-26 | 1991-02-08 | Snecma | Carter d'entree de turbomachine a bras rayonnants |
US4856962A (en) * | 1988-02-24 | 1989-08-15 | United Technologies Corporation | Variable inlet guide vane |
DE69420603T2 (de) * | 1993-03-13 | 1999-12-30 | Gkn Westland Helicopters Ltd., Yeovil | Drehbare Blätter |
US6045325A (en) * | 1997-12-18 | 2000-04-04 | United Technologies Corporation | Apparatus for minimizing inlet airflow turbulence in a gas turbine engine |
GB2339244B (en) * | 1998-06-19 | 2002-12-18 | Rolls Royce Plc | A variable camber vane |
ATE491634T1 (de) * | 1999-12-31 | 2011-01-15 | Deutsch Zentr Luft & Raumfahrt | Flügelprofil mit leistungs-steigernder hinterkante |
US6619916B1 (en) * | 2002-02-28 | 2003-09-16 | General Electric Company | Methods and apparatus for varying gas turbine engine inlet air flow |
FR2857699B1 (fr) * | 2003-07-17 | 2007-06-29 | Snecma Moteurs | Dispositif de degivrage pour aube de roue directrice d'entree de turbomachine, aube dotee d'un tel dispositif de degivrage, et moteur d'aeronef equipe de telles aubes |
-
2005
- 2005-10-25 US US11/258,608 patent/US7549839B2/en active Active
-
2006
- 2006-08-02 CA CA002555074A patent/CA2555074A1/en not_active Abandoned
- 2006-08-16 EP EP12157163.2A patent/EP2460977B1/en active Active
- 2006-08-16 EP EP12157167.3A patent/EP2460978B1/en active Active
- 2006-08-16 EP EP06254284A patent/EP1780378B1/en active Active
- 2006-08-21 IL IL177592A patent/IL177592A0/en unknown
- 2006-08-23 SG SG200605790-5A patent/SG131832A1/en unknown
- 2006-08-23 BR BRPI0603516-7A patent/BRPI0603516A/pt not_active IP Right Cessation
- 2006-08-24 KR KR1020060080160A patent/KR20070044765A/ko active IP Right Grant
- 2006-08-25 CN CNA2006101216441A patent/CN1955441A/zh active Pending
- 2006-08-25 RU RU2006130698/06A patent/RU2006130698A/ru unknown
- 2006-08-25 JP JP2006228521A patent/JP2007120494A/ja active Pending
- 2006-10-20 AU AU2006230736A patent/AU2006230736A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
EP1780378A2 (en) | 2007-05-02 |
CN1955441A (zh) | 2007-05-02 |
EP2460978A1 (en) | 2012-06-06 |
US7549839B2 (en) | 2009-06-23 |
RU2006130698A (ru) | 2008-02-27 |
EP1780378A3 (en) | 2010-10-13 |
CA2555074A1 (en) | 2007-04-25 |
IL177592A0 (en) | 2006-12-10 |
EP2460977A1 (en) | 2012-06-06 |
EP2460978B1 (en) | 2016-01-20 |
JP2007120494A (ja) | 2007-05-17 |
KR20070044765A (ko) | 2007-04-30 |
AU2006230736A1 (en) | 2007-05-10 |
SG131832A1 (en) | 2007-05-28 |
EP1780378B1 (en) | 2012-03-28 |
EP2460977B1 (en) | 2016-01-20 |
US20070092372A1 (en) | 2007-04-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] |
Free format text: REFERENTE AS 3A, 4A E 5A ANUIDADES. |
|
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |
Free format text: REFERENTE AO DESPACHO 8.6 PUBLICADO NA RPI 2160 DE 29/05/2012. |