BRPI0418861A - estrutura de montante em um dispositivo de turbina ou compressor e método para montar a estrutura - Google Patents
estrutura de montante em um dispositivo de turbina ou compressor e método para montar a estruturaInfo
- Publication number
- BRPI0418861A BRPI0418861A BRPI0418861-6A BRPI0418861A BRPI0418861A BR PI0418861 A BRPI0418861 A BR PI0418861A BR PI0418861 A BRPI0418861 A BR PI0418861A BR PI0418861 A BRPI0418861 A BR PI0418861A
- Authority
- BR
- Brazil
- Prior art keywords
- inner ring
- struts
- support structure
- cross sectional
- sectional dimensions
- 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
- F01D9/06—Fluid supply conduits to nozzles or the like
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
- F01D25/162—Bearing supports
-
- 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
- F05D2230/00—Manufacture
- F05D2230/10—Manufacture by removing material
- F05D2230/11—Manufacture by removing material by electrochemical methods
-
- 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
- F05D2230/00—Manufacture
- F05D2230/10—Manufacture by removing material
- F05D2230/12—Manufacture by removing material by spark erosion methods
-
- 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
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/21—Manufacture essentially without removing material by casting
-
- 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
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
-
- 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
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
- F05D2230/61—Assembly methods using limited numbers of standard modules which can be adapted by machining
-
- 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
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
- Y10T29/49323—Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
ESTRUTURA DE MONTANTE EM UM DISPOSITIVO DE TURBINA OU COMPRESSOR E MéTODO PARA MONTAR A ESTRUTURA. A presente invenção se refere a uma estrutura de sustentação e a um método para montar uma estrutura de sustentação em um motor de turbina ou de compressor para suportar de forma giratória um membro de rotor (2) em um membro de estator (1). A estrutura de sustentação inclui um anel interno, um anel externo e um pluralidade de montantes (15) que se estendem em direção radial entre o anel interno e o anel externo. O anel interno apresenta porções integradas ou solidárias que se projetam na direção dos montantes e que formam as conexões de extremidade dos montantes. As porções de conexão de extremidade integradas (19) do anel interno estão juntas com o anel produzido a partir de uma liga de metal que apresenta inicialmente dimensões de seção transversal sobre-dimensionadas em relação às dimensões de seção transversal do montante correspondente, seguidas de uma usinagem de pelo menos uma superfície lateral para remover o material. A finalidade é conseguir dimensões e posição final para conformar-se às dimensões de seção transversal e a posição correta de cada montante correspondente (15).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/SE2004/000824 WO2005116405A1 (en) | 2004-05-27 | 2004-05-27 | A support structure in a turbine or compressor device and a method for assembling the structure |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0418861A true BRPI0418861A (pt) | 2007-11-20 |
Family
ID=35450943
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0418861-6A BRPI0418861A (pt) | 2004-05-27 | 2004-05-27 | estrutura de montante em um dispositivo de turbina ou compressor e método para montar a estrutura |
Country Status (8)
Country | Link |
---|---|
US (1) | US7544040B2 (pt) |
EP (1) | EP1753938B1 (pt) |
JP (1) | JP4489808B2 (pt) |
AT (1) | ATE390542T1 (pt) |
BR (1) | BRPI0418861A (pt) |
DE (1) | DE602004012781T2 (pt) |
ES (1) | ES2305774T3 (pt) |
WO (1) | WO2005116405A1 (pt) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2010071499A1 (en) * | 2008-12-19 | 2010-06-24 | Volvo Aero Corporation | Spoke for a stator component, stator component and method for manufacturing a stator component |
US8430627B2 (en) * | 2009-10-29 | 2013-04-30 | Alstom Technology Ltd | Gas turbine exhaust strut refurbishment |
WO2011075013A1 (en) * | 2009-12-17 | 2011-06-23 | Volvo Aero Corporation | Arrangement and method for closed flow cooling of a gas turbine engine component |
US9765648B2 (en) | 2011-12-08 | 2017-09-19 | Gkn Aerospace Sweden Ab | Gas turbine engine component |
US9803551B2 (en) | 2011-12-20 | 2017-10-31 | Gkn Aerospace Sweden Ab | Method for manufacturing of a gas turbine engine component |
JP5946542B2 (ja) | 2011-12-22 | 2016-07-06 | ゲーコーエヌ エアロスペース スウェーデン アーベー | ガスタービンエンジンコンポーネント |
EP2795071B1 (en) | 2011-12-23 | 2017-02-01 | GKN Aerospace Sweden AB | Gas turbine engine component |
JP5946543B2 (ja) | 2011-12-23 | 2016-07-06 | ゲーコーエヌ エアロスペース スウェーデン アーベー | ガスタービンエンジンの支持構造物 |
US9797312B2 (en) * | 2012-05-02 | 2017-10-24 | Gkn Aerospace Sweden Ab | Supporting structure for a gas turbine engine |
CA3013015C (en) * | 2012-06-15 | 2020-06-02 | United Technologies Corporation | High durability turbine exhaust case |
WO2014007685A1 (en) * | 2012-07-03 | 2014-01-09 | Gkn Aerospace Sweden Ab | Supporting structure for a gas turbine engine |
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 |
US20150044046A1 (en) * | 2013-08-07 | 2015-02-12 | Yevgeniy Shteyman | Manufacturing method for strut shield collar of gas turbine exhaust diffuser |
US9556746B2 (en) | 2013-10-08 | 2017-01-31 | Pratt & Whitney Canada Corp. | Integrated strut and turbine vane nozzle arrangement |
WO2015130425A2 (en) * | 2014-02-03 | 2015-09-03 | United Technologies Corporation | Gas turbine engine cooling fluid composite tube |
US9702267B2 (en) | 2014-10-15 | 2017-07-11 | Pratt & Whitney Canada Corp. | Engine structure assembly procedure |
US10655482B2 (en) * | 2015-02-05 | 2020-05-19 | Rolls-Royce Corporation | Vane assemblies for gas turbine engines |
US9909434B2 (en) | 2015-07-24 | 2018-03-06 | Pratt & Whitney Canada Corp. | Integrated strut-vane nozzle (ISV) with uneven vane axial chords |
JP6546481B2 (ja) * | 2015-08-31 | 2019-07-17 | 川崎重工業株式会社 | 排気ディフューザ |
US10385868B2 (en) * | 2016-07-05 | 2019-08-20 | General Electric Company | Strut assembly for an aircraft engine |
US10443451B2 (en) | 2016-07-18 | 2019-10-15 | Pratt & Whitney Canada Corp. | Shroud housing supported by vane segments |
DE102016217320A1 (de) * | 2016-09-12 | 2018-03-15 | Siemens Aktiengesellschaft | Gasturbine mit getrennter Kühlung für Turbine und Abgasgehäuse |
GB201707103D0 (en) | 2017-05-04 | 2017-06-21 | Rolls Royce Plc | Vane arrangement for a gas turbine engine |
GB201707101D0 (en) * | 2017-05-04 | 2017-06-21 | Rolls Royce Plc | Vane arrangement for a gas turbine engine |
CN107524523B (zh) * | 2017-08-17 | 2020-06-02 | 中国科学院工程热物理研究所 | 一种轻质传力支板结构及具有该支板结构的机匣 |
US11242762B2 (en) * | 2019-11-21 | 2022-02-08 | Raytheon Technologies Corporation | Vane with collar |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2463340A (en) * | 1945-02-22 | 1949-03-01 | Wiberg Oscar Anton | Axial flow turbine blade structure |
US4883216A (en) * | 1988-03-28 | 1989-11-28 | General Electric Company | Method for bonding an article projection |
US5056738A (en) * | 1989-09-07 | 1991-10-15 | General Electric Company | Damper assembly for a strut in a jet propulsion engine |
JPH05321694A (ja) * | 1992-05-26 | 1993-12-07 | Ishikawajima Harima Heavy Ind Co Ltd | ベアリングフレームの製造方法 |
US5284011A (en) * | 1992-12-14 | 1994-02-08 | General Electric Company | Damped turbine engine frame |
US5865364A (en) * | 1996-12-24 | 1999-02-02 | United Technologies Corporation | Process for linear friction welding |
US6045325A (en) * | 1997-12-18 | 2000-04-04 | United Technologies Corporation | Apparatus for minimizing inlet airflow turbulence in a gas turbine engine |
DE19922012C1 (de) * | 1999-05-12 | 2000-10-19 | Mtu Muenchen Gmbh | Verfahren zur Fertigung angepaßter, strömungstechnischer Oberflächen |
US6619916B1 (en) * | 2002-02-28 | 2003-09-16 | General Electric Company | Methods and apparatus for varying gas turbine engine inlet air flow |
-
2004
- 2004-05-27 WO PCT/SE2004/000824 patent/WO2005116405A1/en not_active Application Discontinuation
- 2004-05-27 EP EP04735153A patent/EP1753938B1/en not_active Expired - Lifetime
- 2004-05-27 DE DE602004012781T patent/DE602004012781T2/de not_active Expired - Lifetime
- 2004-05-27 AT AT04735153T patent/ATE390542T1/de not_active IP Right Cessation
- 2004-05-27 BR BRPI0418861-6A patent/BRPI0418861A/pt active Search and Examination
- 2004-05-27 JP JP2007514968A patent/JP4489808B2/ja not_active Expired - Fee Related
- 2004-05-27 ES ES04735153T patent/ES2305774T3/es not_active Expired - Lifetime
-
2006
- 2006-10-21 US US11/551,707 patent/US7544040B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
ATE390542T1 (de) | 2008-04-15 |
US7544040B2 (en) | 2009-06-09 |
US20070140845A1 (en) | 2007-06-21 |
WO2005116405A1 (en) | 2005-12-08 |
ES2305774T3 (es) | 2008-11-01 |
DE602004012781T2 (de) | 2009-04-16 |
EP1753938A1 (en) | 2007-02-21 |
JP2008500488A (ja) | 2008-01-10 |
EP1753938B1 (en) | 2008-03-26 |
DE602004012781D1 (de) | 2008-05-08 |
JP4489808B2 (ja) | 2010-06-23 |
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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 A 3A ANUIDADES |
|
B08H | Application fees: decision cancelled [chapter 8.8 patent gazette] |
Free format text: REFERENTE AO DESPACHO 8.6 DA RPI 2082 DE 30/11/2010. |
|
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B11D | Dismissal acc. art. 38, par 2 of ipl - failure to pay fee after grant in time |