JP4737820B2 - ガスタービン又はジェットエンジンのステータ翼フレーム - Google Patents
ガスタービン又はジェットエンジンのステータ翼フレーム Download PDFInfo
- Publication number
- JP4737820B2 JP4737820B2 JP2000370805A JP2000370805A JP4737820B2 JP 4737820 B2 JP4737820 B2 JP 4737820B2 JP 2000370805 A JP2000370805 A JP 2000370805A JP 2000370805 A JP2000370805 A JP 2000370805A JP 4737820 B2 JP4737820 B2 JP 4737820B2
- Authority
- JP
- Japan
- Prior art keywords
- structural ring
- frame assembly
- stator blade
- series
- ring
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 238000007789 sealing Methods 0.000 claims description 5
- 239000000565 sealant Substances 0.000 claims description 4
- 239000000853 adhesive Substances 0.000 claims description 3
- 230000001070 adhesive effect Effects 0.000 claims description 3
- 238000013016 damping Methods 0.000 description 11
- 239000000463 material Substances 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 125000006850 spacer group Chemical group 0.000 description 2
- 238000004073 vulcanization Methods 0.000 description 2
- 239000004820 Pressure-sensitive adhesive Substances 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 239000011324 bead Substances 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
Images
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)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/456967 | 1999-12-07 | ||
| US09/456,967 US6343912B1 (en) | 1999-12-07 | 1999-12-07 | Gas turbine or jet engine stator vane frame |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2001207998A JP2001207998A (ja) | 2001-08-03 |
| JP2001207998A5 JP2001207998A5 (enExample) | 2008-01-31 |
| JP4737820B2 true JP4737820B2 (ja) | 2011-08-03 |
Family
ID=23814880
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2000370805A Expired - Fee Related JP4737820B2 (ja) | 1999-12-07 | 2000-12-06 | ガスタービン又はジェットエンジンのステータ翼フレーム |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US6343912B1 (enExample) |
| EP (1) | EP1106784B1 (enExample) |
| JP (1) | JP4737820B2 (enExample) |
| BR (1) | BR0005767B1 (enExample) |
| CA (1) | CA2326425C (enExample) |
| DE (1) | DE60028507T2 (enExample) |
Families Citing this family (71)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7651319B2 (en) * | 2002-02-22 | 2010-01-26 | Drs Power Technology Inc. | Compressor stator vane |
| US6984108B2 (en) * | 2002-02-22 | 2006-01-10 | 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 |
| EP2199544B1 (fr) * | 2008-12-22 | 2016-03-30 | Techspace Aero S.A. | Architecture de redresseur |
| 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 |
| JP6141871B2 (ja) * | 2011-12-29 | 2017-06-07 | エリオット・カンパニー | 高温気体膨張装置の入口ケーシング組立体及び方法 |
| WO2013180916A1 (en) * | 2012-05-30 | 2013-12-05 | United Technologies Corporation | Assembly fixture for a stator vane assembly |
| US11035238B2 (en) | 2012-06-19 | 2021-06-15 | Raytheon Technologies Corporation | Airfoil including adhesively bonded shroud |
| US10309235B2 (en) * | 2012-08-27 | 2019-06-04 | United Technologies Corporation | Shiplap cantilevered stator |
| US9366149B2 (en) * | 2012-09-21 | 2016-06-14 | United Technologies Corporation | Multi-stage high pressure compressor case |
| US20140169979A1 (en) * | 2012-12-14 | 2014-06-19 | United Technologies Corporation | Gas turbine engine fan blade platform seal |
| WO2014105512A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Mechanical linkage for segmented heat shield |
| WO2014105599A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Heat shield for cooling a strut |
| US9347330B2 (en) | 2012-12-29 | 2016-05-24 | United Technologies Corporation | Finger seal |
| WO2014105803A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Gas turbine seal assembly and seal support |
| US10240532B2 (en) | 2012-12-29 | 2019-03-26 | United Technologies Corporation | Frame junction cooling holes |
| US10053998B2 (en) | 2012-12-29 | 2018-08-21 | United Technologies Corporation | Multi-purpose gas turbine seal support and assembly |
| WO2014105800A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Gas turbine seal assembly and seal support |
| WO2014105496A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Flow diverter element and assembly |
| EP2938834A1 (en) | 2012-12-29 | 2015-11-04 | United Technologies Corporation | Bumper for seals in a turbine exhaust case |
| WO2014105826A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Seal support disk and assembly |
| US9297312B2 (en) | 2012-12-29 | 2016-03-29 | United Technologies Corporation | Circumferentially retained fairing |
| US9903224B2 (en) | 2012-12-29 | 2018-02-27 | United Technologies Corporation | Scupper channelling in gas turbine modules |
| WO2014137444A2 (en) | 2012-12-29 | 2014-09-12 | United Technologies Corporation | Multi-ply finger seal |
| US10472987B2 (en) | 2012-12-29 | 2019-11-12 | United Technologies Corporation | Heat shield for a casing |
| GB2524211B (en) | 2012-12-29 | 2021-05-26 | United Technologies Corp | Turbine frame assembly and method of designing turbine frame assembly |
| WO2014105657A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Mount with deflectable tabs |
| WO2014105619A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Multi-function boss for a turbine exhaust case |
| US9631517B2 (en) | 2012-12-29 | 2017-04-25 | United Technologies Corporation | Multi-piece fairing for monolithic turbine exhaust case |
| US9206742B2 (en) | 2012-12-29 | 2015-12-08 | United Technologies Corporation | Passages to facilitate a secondary flow between components |
| US9850780B2 (en) | 2012-12-29 | 2017-12-26 | United Technologies Corporation | Plate for directing flow and film cooling of components |
| US9863261B2 (en) | 2012-12-29 | 2018-01-09 | United Technologies Corporation | Component retention with probe |
| US10094389B2 (en) | 2012-12-29 | 2018-10-09 | United Technologies Corporation | Flow diverter to redirect secondary flow |
| US9541006B2 (en) | 2012-12-29 | 2017-01-10 | United Technologies Corporation | Inter-module flow discourager |
| US10006306B2 (en) | 2012-12-29 | 2018-06-26 | United Technologies Corporation | Turbine exhaust case architecture |
| US9771818B2 (en) | 2012-12-29 | 2017-09-26 | United Technologies Corporation | Seals for a circumferential stop ring in a turbine exhaust case |
| US9562478B2 (en) | 2012-12-29 | 2017-02-07 | United Technologies Corporation | Inter-module finger seal |
| US10240481B2 (en) | 2012-12-29 | 2019-03-26 | United Technologies Corporation | Angled cut to direct radiative heat load |
| US10294819B2 (en) | 2012-12-29 | 2019-05-21 | United Technologies Corporation | Multi-piece heat shield |
| WO2014105688A1 (en) | 2012-12-31 | 2014-07-03 | United Technologies Corporation | Turbine exhaust case multi-piece frame |
| WO2014105682A1 (en) | 2012-12-31 | 2014-07-03 | United Technologies Corporation | Turbine exhaust case multi-piece frame |
| GB2524443B (en) | 2012-12-31 | 2020-02-12 | United Technologies Corp | Turbine exhaust case multi-piece frame |
| WO2014197037A2 (en) | 2013-03-11 | 2014-12-11 | 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 |
| EP3027855B1 (en) * | 2013-07-30 | 2020-09-09 | United Technologies Corporation | Gas turbine engine with a 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 |
| US12098643B2 (en) * | 2021-03-09 | 2024-09-24 | Rtx 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 DE DE60028507T patent/DE60028507T2/de not_active Expired - Lifetime
- 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
Also Published As
| Publication number | Publication date |
|---|---|
| EP1106784A2 (en) | 2001-06-13 |
| EP1106784B1 (en) | 2006-06-07 |
| EP1106784A3 (en) | 2003-07-16 |
| US6343912B1 (en) | 2002-02-05 |
| BR0005767B1 (pt) | 2008-11-18 |
| CA2326425C (en) | 2007-06-12 |
| JP2001207998A (ja) | 2001-08-03 |
| DE60028507D1 (de) | 2006-07-20 |
| CA2326425A1 (en) | 2001-06-07 |
| DE60028507T2 (de) | 2007-06-06 |
| BR0005767A (pt) | 2001-07-17 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP4737820B2 (ja) | ガスタービン又はジェットエンジンのステータ翼フレーム | |
| CA2689179C (en) | Stator assembly for a gas turbine engine | |
| US6764276B2 (en) | Guide vane assembly | |
| US4832568A (en) | Turbomachine airfoil mounting assembly | |
| JP6232446B2 (ja) | タービン排気ケースのマルチピース型フレーム | |
| US7114917B2 (en) | Vane assembly for a gas turbine engine | |
| US9359901B2 (en) | Aerofoil assembly | |
| CN1318736C (zh) | 具有热适应性的阻碍密封装置 | |
| US5380155A (en) | Compressor stator assembly | |
| EP2867503B1 (en) | Fairing assembly | |
| US20010033793A1 (en) | Turbine engine damper | |
| US20030206799A1 (en) | Casing section | |
| EP2938860B1 (en) | Turbine exhaust case multi-piece frame | |
| GB2313161A (en) | Turbine casing comprising axially connected rings with integral stator vanes. | |
| GB2115883A (en) | Turbomachine airfoil mounting assembly | |
| JPH02238102A (ja) | ガスタービンエンジンの振動減衰翼列 | |
| US10047625B2 (en) | Fan blade root integrated sealing solution | |
| US11905839B2 (en) | Attachment of an acoustic shroud to a housing shell for an aircraft turbine engine | |
| JP2009508031A (ja) | グロメットを有するベーンアッセンブリ |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A521 | Written amendment |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20071205 |
|
| A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20071205 |
|
| RD02 | Notification of acceptance of power of attorney |
Free format text: JAPANESE INTERMEDIATE CODE: A7422 Effective date: 20100126 |
|
| RD04 | Notification of resignation of power of attorney |
Free format text: JAPANESE INTERMEDIATE CODE: A7424 Effective date: 20100126 |
|
| A977 | Report on retrieval |
Free format text: JAPANESE INTERMEDIATE CODE: A971007 Effective date: 20100730 |
|
| A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20101012 |
|
| A521 | Written amendment |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20110112 |
|
| A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 20110405 |
|
| A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20110426 |
|
| R150 | Certificate of patent or registration of utility model |
Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
| FPAY | Renewal fee payment (event date is renewal date of database) |
Free format text: PAYMENT UNTIL: 20140513 Year of fee payment: 3 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| LAPS | Cancellation because of no payment of annual fees |