BR0005767A - Estrutura para uma palheta de estator de motor a jato ou turbina a gás - Google Patents
Estrutura para uma palheta de estator de motor a jato ou turbina a gásInfo
- Publication number
- BR0005767A BR0005767A BR0005767-3A BR0005767A BR0005767A BR 0005767 A BR0005767 A BR 0005767A BR 0005767 A BR0005767 A BR 0005767A BR 0005767 A BR0005767 A BR 0005767A
- Authority
- BR
- Brazil
- Prior art keywords
- vanes
- stator
- vane
- structural ring
- gas turbine
- 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
- 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
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
-
- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/005—Sealing means between non relatively rotating elements
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Patente de Invenção:<B>"ESTRUTURA PARA UMA PALHETA DE ESTATOR DE MOTOR A JATO OU TURBINA A GáS"<D>. Um conjunto de estrutura para palhetas de estator incluindo um anel estrutural externo (34), um anel estrutural interno (36), um conjunto de palhetas individuais (22) cada uma conectando o anel estrutural externo(34) e o anel estrutural interno (36), formando plataformas interna e externa com as palhetas (22) vizinhas definindo um conjunto de trajetórias de fluxo, um conjunto de membros de vedação (30, 32, 58, 70) conformado a um conjunto de folgas (60) entre o conjunto de palhetas (22) disposto para vedar a folga (60). Um método para a aplicação de um membro de vedação (30, 32,58, 70) contra as folgas (60) entre uma plataforma formada como resultado do acoplamento entre as palhetas (22) incluindo a fixação de um conjunto de palhetas de estator (22) em uma estrutura interna e a uma estrutura externa, e a vedação de um conjunto de membros de fixação (30, 32, 58, 70) sobre a superfície da parte traseira de uma estrutura de palheta de estator. A natureza discreta de uma palheta individual vedada pelos membros de vedação (30, 32, 58, 70) faz com que o conjunto de estrutura para palhetas de estator a adicione um efeito de amortecimento o qual aumenta a vida sem fadiga da palheta (22), e permite o emprego de material com menor resistência, mais leve e mais barato.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/456,967 US6343912B1 (en) | 1999-12-07 | 1999-12-07 | Gas turbine or jet engine stator vane frame |
Publications (2)
Publication Number | Publication Date |
---|---|
BR0005767A true BR0005767A (pt) | 2001-07-17 |
BR0005767B1 BR0005767B1 (pt) | 2008-11-18 |
Family
ID=23814880
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0005767-3A BR0005767B1 (pt) | 1999-12-07 | 2000-12-07 | conjunto de estrutura para palhetas de estator. |
Country Status (6)
Country | Link |
---|---|
US (1) | US6343912B1 (pt) |
EP (1) | EP1106784B1 (pt) |
JP (1) | JP4737820B2 (pt) |
BR (1) | BR0005767B1 (pt) |
CA (1) | CA2326425C (pt) |
DE (1) | DE60028507T2 (pt) |
Families Citing this family (71)
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---|---|---|---|---|
US6984108B2 (en) * | 2002-02-22 | 2006-01-10 | Drs Power Technology Inc. | Compressor stator vane |
US7651319B2 (en) * | 2002-02-22 | 2010-01-26 | Drs Power Technology Inc. | Compressor stator vane |
US6733237B2 (en) * | 2002-04-02 | 2004-05-11 | Watson Cogeneration Company | Method and apparatus for mounting stator blades in axial flow compressors |
US6969239B2 (en) | 2002-09-30 | 2005-11-29 | General Electric Company | Apparatus and method for damping vibrations between a compressor stator vane and a casing of a gas turbine engine |
US20050172485A1 (en) * | 2004-02-10 | 2005-08-11 | Ramsay Mussen | Method of repair for cast article |
US20050220622A1 (en) * | 2004-03-31 | 2005-10-06 | General Electric Company | Integral covered nozzle with attached overcover |
FR2902843A1 (fr) * | 2006-06-23 | 2007-12-28 | Snecma Sa | Secteur de redresseur de compresseur ou secteur de distributeur de turbomachine |
US7748956B2 (en) * | 2006-12-19 | 2010-07-06 | United Technologies Corporation | Non-stablug stator apparatus and assembly method |
US20090110552A1 (en) * | 2007-10-31 | 2009-04-30 | Anderson Rodger O | Compressor stator vane repair with pin |
EP2075412B1 (fr) * | 2007-12-26 | 2012-02-29 | Techspace Aero | Dispositif de fixation par boulonnage d'aubes à une virole d'étage de stator d'une turbomachine et procédé associé de fixation par boulonnage |
US8511983B2 (en) | 2008-02-19 | 2013-08-20 | United Technologies Corporation | LPC exit guide vane and assembly |
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US8162603B2 (en) * | 2009-01-30 | 2012-04-24 | General Electric Company | Vane frame for a turbomachine and method of minimizing weight thereof |
US8371810B2 (en) * | 2009-03-26 | 2013-02-12 | General Electric Company | Duct member based nozzle for turbine |
EP2339120B1 (fr) * | 2009-12-22 | 2015-07-08 | Techspace Aero S.A. | Étage redresseur de turbomachine et compresseur associé |
US8356975B2 (en) * | 2010-03-23 | 2013-01-22 | United Technologies Corporation | Gas turbine engine with non-axisymmetric surface contoured vane platform |
US9976433B2 (en) | 2010-04-02 | 2018-05-22 | United Technologies Corporation | Gas turbine engine with non-axisymmetric surface contoured rotor blade platform |
FR2961553B1 (fr) * | 2010-06-18 | 2012-08-31 | Snecma | Secteur angulaire de redresseur pour compresseur de turbomachine, redresseur de turbomachine et turbomachine comprenant un tel secteur |
US8966755B2 (en) | 2011-01-20 | 2015-03-03 | United Technologies Corporation | Assembly fixture for a stator vane assembly |
US8966756B2 (en) * | 2011-01-20 | 2015-03-03 | United Technologies Corporation | Gas turbine engine stator vane assembly |
US8951013B2 (en) | 2011-10-24 | 2015-02-10 | United Technologies Corporation | Turbine blade rail damper |
CN103917761B (zh) * | 2011-12-29 | 2017-06-30 | 艾利奥特公司 | 一种燃气涡轮机装置及其进气壳组件的装配方法 |
WO2013180916A1 (en) * | 2012-05-30 | 2013-12-05 | United Technologies Corporation | Assembly fixture for a stator vane assembly |
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US9541006B2 (en) | 2012-12-29 | 2017-01-10 | United Technologies Corporation | Inter-module flow discourager |
US10294819B2 (en) | 2012-12-29 | 2019-05-21 | United Technologies Corporation | Multi-piece heat shield |
US10094389B2 (en) | 2012-12-29 | 2018-10-09 | United Technologies Corporation | Flow diverter to redirect secondary flow |
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US9206742B2 (en) | 2012-12-29 | 2015-12-08 | United Technologies Corporation | Passages to facilitate a secondary flow between components |
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US10472987B2 (en) | 2012-12-29 | 2019-11-12 | United Technologies Corporation | Heat shield for a casing |
US9850780B2 (en) | 2012-12-29 | 2017-12-26 | United Technologies Corporation | Plate for directing flow and film cooling of components |
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WO2014105577A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Scupper channelling in gas turbine modules |
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US10060279B2 (en) | 2012-12-29 | 2018-08-28 | United Technologies Corporation | Seal support disk and assembly |
US10378370B2 (en) | 2012-12-29 | 2019-08-13 | United Technologies Corporation | Mechanical linkage for segmented heat shield |
WO2014105657A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Mount with deflectable tabs |
US9631517B2 (en) | 2012-12-29 | 2017-04-25 | United Technologies Corporation | Multi-piece fairing for monolithic turbine exhaust case |
WO2014105800A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Gas turbine seal assembly and seal support |
US9771818B2 (en) | 2012-12-29 | 2017-09-26 | United Technologies Corporation | Seals for a circumferential stop ring in a turbine exhaust case |
WO2014105604A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Angled cut to direct radiative heat load |
US10329956B2 (en) | 2012-12-29 | 2019-06-25 | United Technologies Corporation | Multi-function boss for a turbine exhaust case |
US9297312B2 (en) | 2012-12-29 | 2016-03-29 | United Technologies Corporation | Circumferentially retained fairing |
EP2938845A4 (en) | 2012-12-29 | 2016-01-13 | United Technologies Corp | TURBINE EXHAUST HOUSING ARCHITECTURE |
WO2014105803A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Gas turbine seal assembly and seal support |
US9347330B2 (en) | 2012-12-29 | 2016-05-24 | United Technologies Corporation | Finger seal |
US10053998B2 (en) | 2012-12-29 | 2018-08-21 | United Technologies Corporation | Multi-purpose gas turbine seal support and assembly |
US9863261B2 (en) | 2012-12-29 | 2018-01-09 | United Technologies Corporation | Component retention with probe |
WO2014143329A2 (en) | 2012-12-29 | 2014-09-18 | United Technologies Corporation | Frame junction cooling holes |
US9828867B2 (en) | 2012-12-29 | 2017-11-28 | United Technologies Corporation | Bumper for seals in a turbine exhaust case |
WO2014105688A1 (en) | 2012-12-31 | 2014-07-03 | United Technologies Corporation | Turbine exhaust case multi-piece frame |
US10054009B2 (en) | 2012-12-31 | 2018-08-21 | United Technologies Corporation | Turbine exhaust case multi-piece frame |
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US10330011B2 (en) | 2013-03-11 | 2019-06-25 | United Technologies Corporation | Bench aft sub-assembly for turbine exhaust case fairing |
US10087766B2 (en) | 2013-03-13 | 2018-10-02 | United Technologies Corporation | Structural guide vane outer diameter K gussets |
FR3008639B1 (fr) * | 2013-07-18 | 2015-08-07 | Snecma | Procede d'assemblage de pieces de turbomachine et ensemble mis en œuvre lors d'un tel procede |
US10344603B2 (en) * | 2013-07-30 | 2019-07-09 | United Technologies Corporation | Gas turbine engine turbine vane ring arrangement |
US9816387B2 (en) | 2014-09-09 | 2017-11-14 | United Technologies Corporation | Attachment faces for clamped turbine stator of a gas turbine engine |
US9810075B2 (en) | 2015-03-20 | 2017-11-07 | United Technologies Corporation | Faceted turbine blade damper-seal |
US9777594B2 (en) | 2015-04-15 | 2017-10-03 | Siemens Energy, Inc. | Energy damping system for gas turbine engine stationary vane |
US10301951B2 (en) | 2016-05-20 | 2019-05-28 | United Technologies Corporation | Turbine vane gusset |
FR3051840B1 (fr) * | 2016-05-31 | 2020-01-10 | Safran Aircraft Engines | Carter intermediaire de turbomachine, equipee d'une piece d'etancheite a interface bras/virole |
US10364748B2 (en) | 2016-08-19 | 2019-07-30 | United Technologies Corporation | Finger seal flow metering |
US20220290573A1 (en) * | 2021-03-09 | 2022-09-15 | Raytheon Technologies Corporation | Chevron grooved mateface seal |
US11674404B2 (en) | 2021-05-04 | 2023-06-13 | Raytheon Technologies Corporation | Seal assembly with seal arc segment |
CN114458628B (zh) * | 2022-04-12 | 2022-06-24 | 广东威灵电机制造有限公司 | 风机及电器设备 |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3752598A (en) * | 1971-11-17 | 1973-08-14 | United Aircraft Corp | Segmented duct seal |
US3892497A (en) * | 1974-05-14 | 1975-07-01 | Westinghouse Electric Corp | Axial flow turbine stationary blade and blade ring locking arrangement |
GB1483532A (en) * | 1974-09-13 | 1977-08-24 | Rolls Royce | Stator structure for a gas turbine engine |
US4422827A (en) * | 1982-02-18 | 1983-12-27 | United Technologies Corporation | Blade root seal |
US4492517A (en) * | 1983-01-06 | 1985-01-08 | General Electric Company | Segmented inlet nozzle for gas turbine, and methods of installation |
JPS60118306A (ja) * | 1983-11-29 | 1985-06-25 | Ishikawajima Harima Heavy Ind Co Ltd | 圧延機 |
US4524980A (en) * | 1983-12-05 | 1985-06-25 | United Technologies Corporation | Intersecting feather seals for interlocking gas turbine vanes |
JPS60118306U (ja) * | 1984-01-20 | 1985-08-10 | 株式会社日立製作所 | 流体機械における静翼部のシ−ル装置 |
US4655682A (en) * | 1985-09-30 | 1987-04-07 | United Technologies Corporation | Compressor stator assembly having a composite inner diameter shroud |
US4749333A (en) * | 1986-05-12 | 1988-06-07 | The United States Of America As Represented By The Secretary Of The Air Force | Vane platform sealing and retention means |
CA2031085A1 (en) * | 1990-01-16 | 1991-07-17 | Michael P. Hagle | Arrangement for sealing gaps between adjacent circumferential segments of turbine nozzles and shrouds |
US5074748A (en) * | 1990-07-30 | 1991-12-24 | General Electric Company | Seal assembly for segmented turbine engine structures |
US5154577A (en) * | 1991-01-17 | 1992-10-13 | General Electric Company | Flexible three-piece seal assembly |
CA2070511C (en) * | 1991-07-22 | 2001-08-21 | Steven Milo Toborg | Turbine nozzle support |
US5380155A (en) * | 1994-03-01 | 1995-01-10 | United Technologies Corporation | Compressor stator assembly |
US5411370A (en) * | 1994-08-01 | 1995-05-02 | United Technologies Corporation | Vibration damping shroud for a turbomachine vane |
US5820338A (en) * | 1997-04-24 | 1998-10-13 | United Technologies Corporation | Fan blade interplatform seal |
US5848874A (en) * | 1997-05-13 | 1998-12-15 | United Technologies Corporation | Gas turbine stator vane assembly |
DE69824925T2 (de) * | 1997-09-17 | 2005-08-25 | Mitsubishi Heavy Industries, Ltd. | Leitschaufelpaar |
-
1999
- 1999-12-07 US US09/456,967 patent/US6343912B1/en not_active Expired - Lifetime
-
2000
- 2000-11-23 CA CA002326425A patent/CA2326425C/en not_active Expired - Fee Related
- 2000-12-06 JP JP2000370805A patent/JP4737820B2/ja not_active Expired - Fee Related
- 2000-12-07 BR BRPI0005767-3A patent/BR0005767B1/pt not_active IP Right Cessation
- 2000-12-07 EP EP00310883A patent/EP1106784B1/en not_active Expired - Lifetime
- 2000-12-07 DE DE60028507T patent/DE60028507T2/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
CA2326425C (en) | 2007-06-12 |
CA2326425A1 (en) | 2001-06-07 |
BR0005767B1 (pt) | 2008-11-18 |
DE60028507T2 (de) | 2007-06-06 |
JP4737820B2 (ja) | 2011-08-03 |
EP1106784A2 (en) | 2001-06-13 |
DE60028507D1 (de) | 2006-07-20 |
EP1106784B1 (en) | 2006-06-07 |
US6343912B1 (en) | 2002-02-05 |
EP1106784A3 (en) | 2003-07-16 |
JP2001207998A (ja) | 2001-08-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
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 07/12/2000, OBSERVADAS AS CONDICOES LEGAIS. |
|
B21F | Lapse acc. art. 78, item iv - on non-payment of the annual fees in time | ||
B24J | Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12) |