JPH11294103A5 - - Google Patents
Info
- Publication number
- JPH11294103A5 JPH11294103A5 JP1999042005A JP4200599A JPH11294103A5 JP H11294103 A5 JPH11294103 A5 JP H11294103A5 JP 1999042005 A JP1999042005 A JP 1999042005A JP 4200599 A JP4200599 A JP 4200599A JP H11294103 A5 JPH11294103 A5 JP H11294103A5
- Authority
- JP
- Japan
- Prior art keywords
- guide vane
- cover band
- housing
- ring
- vane 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.)
- Granted
Links
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19807247:3 | 1998-02-20 | ||
| DE19807247A DE19807247C2 (de) | 1998-02-20 | 1998-02-20 | Strömungsmaschine mit Rotor und Stator |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JPH11294103A JPH11294103A (ja) | 1999-10-26 |
| JPH11294103A5 true JPH11294103A5 (enExample) | 2006-03-09 |
| JP4230040B2 JP4230040B2 (ja) | 2009-02-25 |
Family
ID=7858458
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP04200599A Expired - Fee Related JP4230040B2 (ja) | 1998-02-20 | 1999-02-19 | ロータとステータを備えた流体機械 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US6139263A (enExample) |
| EP (1) | EP0937864B1 (enExample) |
| JP (1) | JP4230040B2 (enExample) |
| DE (2) | DE19807247C2 (enExample) |
Families Citing this family (33)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| IT1318103B1 (it) * | 2000-07-03 | 2003-07-23 | Nuovo Pignone Spa | Sistema di connessione tra un ugello di bassa pressione ed untransition duct in una turbina a gas |
| DE10037837C2 (de) * | 2000-08-03 | 2002-08-01 | Mtu Aero Engines Gmbh | Aufhängung |
| JP2002129901A (ja) * | 2000-10-30 | 2002-05-09 | Ishikawajima Harima Heavy Ind Co Ltd | チップシュラウド構造 |
| DE10064272A1 (de) * | 2000-12-22 | 2002-07-04 | Alstom Switzerland Ltd | Turbinenschaufel für eine Gasturbine |
| DE10122464C1 (de) * | 2001-05-09 | 2002-03-07 | Mtu Aero Engines Gmbh | Mantelring |
| US7059821B2 (en) * | 2003-05-07 | 2006-06-13 | General Electric Company | Method and apparatus to facilitate sealing within turbines |
| DE10359730A1 (de) | 2003-12-19 | 2005-07-14 | Mtu Aero Engines Gmbh | Turbomaschine, insbesondere Gasturbine |
| DE102004016222A1 (de) * | 2004-03-26 | 2005-10-06 | Rolls-Royce Deutschland Ltd & Co Kg | Anordnung zur selbsttätigen Laufspalteinstellung bei einer zwei- oder mehrstufigen Turbine |
| GB2448116B (en) * | 2007-04-05 | 2009-05-27 | Rolls Royce Plc | Means for cooling a bearing assembly |
| US8090456B2 (en) * | 2008-11-03 | 2012-01-03 | United Technologies Corporation | System and method for design and control of engineering systems utilizing component-level dynamic mathematical model |
| DE102009037620A1 (de) | 2009-08-14 | 2011-02-17 | Mtu Aero Engines Gmbh | Strömungsmaschine |
| US8315741B2 (en) * | 2009-09-02 | 2012-11-20 | United Technologies Corporation | High fidelity integrated heat transfer and clearance in component-level dynamic turbine system control |
| US8668434B2 (en) * | 2009-09-02 | 2014-03-11 | United Technologies Corporation | Robust flow parameter model for component-level dynamic turbine system control |
| DE102009042029A1 (de) * | 2009-09-17 | 2011-03-24 | Mtu Aero Engines Gmbh | Schaufelkranz für eine Strömungsmaschine |
| DE102009052314A1 (de) | 2009-11-07 | 2011-05-12 | Mtu Aero Engines Gmbh | Dichtanordnung für eine Gasturbine und eine derartige Gasturbine |
| US20110255959A1 (en) * | 2010-04-15 | 2011-10-20 | General Electric Company | Turbine alignment control system and method |
| ES2793725T3 (es) | 2010-11-16 | 2020-11-16 | Mtu Aero Engines Gmbh | Conjunto de paletas del rotor para una turbina |
| DE102011083814A1 (de) | 2011-09-30 | 2013-04-04 | Mtu Aero Engines Gmbh | Segmentiertes Bauteil |
| ES2700788T3 (es) | 2012-04-04 | 2019-02-19 | MTU Aero Engines AG | Sistema de sellado para una turbomáquina |
| EP2647796A1 (de) | 2012-04-04 | 2013-10-09 | MTU Aero Engines GmbH | Dichtungssystem für eine Strömungsmaschine |
| ES2552474T3 (es) | 2012-04-04 | 2015-11-30 | Mtu Aero Engines Gmbh | Método para la fabricación de un revestimiento |
| KR101480089B1 (ko) * | 2012-05-10 | 2015-01-08 | 이병화 | 목재용 앵커 볼트 |
| EP2719869A1 (de) | 2012-10-12 | 2014-04-16 | MTU Aero Engines GmbH | Axiale Abdichtung in einer Gehäusestruktur für eine Strömungsmaschine |
| ES2679343T3 (es) * | 2013-04-24 | 2018-08-24 | MTU Aero Engines AG | Junta de estanqueidad deslizante |
| CN103482219B (zh) * | 2013-09-16 | 2016-06-01 | 沈阳黎明航空发动机(集团)有限责任公司 | 一种燃气轮机运输过程中对转子进行轴、径向定位方法 |
| DE102014209057A1 (de) * | 2014-05-14 | 2015-11-19 | MTU Aero Engines AG | Gasturbinengehäuseanordnung |
| US10975721B2 (en) * | 2016-01-12 | 2021-04-13 | Pratt & Whitney Canada Corp. | Cooled containment case using internal plenum |
| IT201900014736A1 (it) | 2019-08-13 | 2021-02-13 | Ge Avio Srl | Elementi di tenuta integrali per pale trattenute in un rotore a tamburo esterno anulare girevole in una turbomacchina. |
| IT201900014739A1 (it) | 2019-08-13 | 2021-02-13 | Ge Avio Srl | Elementi di trattenimento delle pale per turbomacchine. |
| IT201900014724A1 (it) | 2019-08-13 | 2021-02-13 | Ge Avio Srl | Elementi di trattenimento delle pale per turbomacchine. |
| CN115387906B (zh) * | 2022-05-12 | 2024-04-16 | 中国航发四川燃气涡轮研究院 | 低进口轮毂比发动机的进气承力框架连接结构及装配方法 |
| US12529322B1 (en) * | 2024-11-08 | 2026-01-20 | Pratt & Whitney Canada Corp. | Gas turbine engine stator vane stage |
| CN119914562B (zh) * | 2024-12-30 | 2025-11-21 | 北京航空航天大学 | 一种机匣结构及航空发动机 |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2968467A (en) * | 1956-11-14 | 1961-01-17 | Orenda Engines Ltd | Connecting means, especially for securing annular stator elements between supports whose positions are fixed |
| GB1158238A (en) * | 1968-06-27 | 1969-07-16 | Rolls Royce | Blade Assembly for a Fluid Flow Machine. |
| US3542483A (en) * | 1968-07-17 | 1970-11-24 | Westinghouse Electric Corp | Turbine stator structure |
| GB1387866A (en) * | 1972-06-21 | 1975-03-19 | Rolls Royce | Aerofoil members for gas turbine engines |
| GB1605310A (en) * | 1975-05-30 | 1989-02-01 | Rolls Royce | Nozzle guide vane structure |
| DE2745130C2 (de) | 1977-10-07 | 1980-01-03 | Mtu Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen | Dichtungseinrichtung für die freien Schaufelenden von Axialturbinen |
| DE3336420A1 (de) * | 1982-10-06 | 1984-04-12 | Rolls-Royce Ltd., London | Mechanismus zur verhinderung eines ueberdrehens des turbinenrotors eines gasturbinentriebwerks im falle eines wellenbruches |
| US4679400A (en) * | 1983-12-15 | 1987-07-14 | General Electric Company | Variable turbine vane support |
| DE3540943A1 (de) | 1985-11-19 | 1987-05-21 | Mtu Muenchen Gmbh | Gasturbinenstrahltriebwerk in mehr-wellen-zweistrom-bauweise |
-
1998
- 1998-02-20 DE DE19807247A patent/DE19807247C2/de not_active Expired - Fee Related
-
1999
- 1999-02-18 EP EP99103156A patent/EP0937864B1/de not_active Expired - Lifetime
- 1999-02-18 DE DE59906550T patent/DE59906550D1/de not_active Expired - Lifetime
- 1999-02-19 US US09/252,752 patent/US6139263A/en not_active Expired - Lifetime
- 1999-02-19 JP JP04200599A patent/JP4230040B2/ja not_active Expired - Fee Related
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JPH11294103A5 (enExample) | ||
| JP4230040B2 (ja) | ロータとステータを備えた流体機械 | |
| US7824152B2 (en) | Multivane segment mounting arrangement for a gas turbine | |
| EP2279364B1 (en) | Non-contact seal for a gas turbine engine | |
| US4981415A (en) | Support for oil film dampers | |
| EP2665897B1 (en) | Seal with stacked sealing elements | |
| US6155040A (en) | Gas turbine | |
| US8388310B1 (en) | Turbine disc sealing assembly | |
| JP2680651B2 (ja) | ターボマシンのロータ用ブレード間のシール | |
| CN101146980A (zh) | 涡轮机的导流盘和叶片 | |
| JP5728501B2 (ja) | タービンエンジンのための、突起を有する、柔軟性のある後部ベアリングマウント | |
| JP6072930B2 (ja) | アンダーラップ端部を有するベリーシール | |
| JPH0921301A (ja) | ロータ | |
| US8235656B2 (en) | Catenary turbine seal systems | |
| US4813848A (en) | Turbine rotor disk and blade assembly | |
| JPS6411801B2 (enExample) | ||
| EP1705341B1 (en) | Variable stator vane mounting ring segment | |
| US12196102B2 (en) | Rotor with a balancing flange, rotor assembly with at least one rotor, and turbomachine with at least one rotor or with a rotor assembly | |
| CN103195513B (zh) | 涡轮机组件和用于支撑涡轮机部件的方法 | |
| EP2787257B1 (en) | Fluid transfer seal assemblies, fluid transfer systems, and methods for transferring process fluid between stationary and rotating components using the same | |
| JP5235996B2 (ja) | 軸流流体機械におけるロータ | |
| EP3933233B1 (en) | Non-contact seal assembly with multiple axially spaced spring elements | |
| JPH05113136A (ja) | セラミツクガスタービン | |
| US8870531B2 (en) | Turbomachine rotor having blades of composite material provided with metal labyrinth teeth | |
| GB2432638A (en) | A fluid bearing arrangement |