PL2414641T3 - Wirnik osiowej maszyny wirnikowej z tarczą uszczelniającą - Google Patents
Wirnik osiowej maszyny wirnikowej z tarczą uszczelniającąInfo
- Publication number
- PL2414641T3 PL2414641T3 PL10715749T PL10715749T PL2414641T3 PL 2414641 T3 PL2414641 T3 PL 2414641T3 PL 10715749 T PL10715749 T PL 10715749T PL 10715749 T PL10715749 T PL 10715749T PL 2414641 T3 PL2414641 T3 PL 2414641T3
- Authority
- PL
- Poland
- Prior art keywords
- sealing disc
- engine rotor
- turbo engine
- axial turbo
- axial
- 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
- F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
-
- 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
- F01D11/006—Sealing the gap between rotor blades or blades and rotor
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP09004781A EP2239419A1 (de) | 2009-03-31 | 2009-03-31 | Axialturbomaschinenrotor mit Dichtscheibe |
PCT/EP2010/054001 WO2010112422A1 (de) | 2009-03-31 | 2010-03-26 | Axialturbomaschinenrotor mit dichtscheibe |
EP10715749.7A EP2414641B1 (de) | 2009-03-31 | 2010-03-26 | Axialturbomaschinenrotor mit dichtscheibe |
Publications (1)
Publication Number | Publication Date |
---|---|
PL2414641T3 true PL2414641T3 (pl) | 2013-12-31 |
Family
ID=41258149
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL10715749T PL2414641T3 (pl) | 2009-03-31 | 2010-03-26 | Wirnik osiowej maszyny wirnikowej z tarczą uszczelniającą |
Country Status (7)
Country | Link |
---|---|
US (1) | US8920121B2 (pl) |
EP (2) | EP2239419A1 (pl) |
JP (1) | JP5324700B2 (pl) |
CN (1) | CN102378850B (pl) |
ES (1) | ES2426156T3 (pl) |
PL (1) | PL2414641T3 (pl) |
WO (1) | WO2010112422A1 (pl) |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2982635B1 (fr) * | 2011-11-15 | 2013-11-15 | Snecma | Roue a aubes pour une turbomachine |
US9181810B2 (en) * | 2012-04-16 | 2015-11-10 | General Electric Company | System and method for covering a blade mounting region of turbine blades |
WO2014137435A2 (en) | 2013-03-05 | 2014-09-12 | Rolls-Royce North American Technologies, Inc. | Turbine segmented cover plate retention method |
FR3011032B1 (fr) * | 2013-09-25 | 2017-12-29 | Snecma | Ensemble rotatif pour turbomachine |
EP2863019B1 (de) * | 2013-10-18 | 2017-03-29 | Siemens Aktiengesellschaft | Dichtungsanordnung |
EP2957725A1 (de) | 2014-06-16 | 2015-12-23 | Siemens Aktiengesellschaft | Rotor mit Dichtblechen |
GB201508040D0 (en) * | 2015-05-12 | 2015-06-24 | Rolls Royce Plc | A bladed rotor for a gas turbine engine |
JP6613611B2 (ja) * | 2015-05-15 | 2019-12-04 | 株式会社Ihi | タービンブレード取付構造 |
US12037926B2 (en) | 2016-02-05 | 2024-07-16 | Siemens Energy Global GmbH & Co. KG | Rotor comprising a rotor component arranged between two rotor discs |
DE102016107315A1 (de) * | 2016-04-20 | 2017-10-26 | Rolls-Royce Deutschland Ltd & Co Kg | Rotor mit Überhang an Laufschaufeln für ein Sicherungselement |
KR101850922B1 (ko) | 2016-10-07 | 2018-04-20 | 두산중공업 주식회사 | 가스터빈용 연소 덕트 조립체 |
GB2560159B (en) | 2017-02-23 | 2019-12-25 | Advanced Risc Mach Ltd | Widening arithmetic in a data processing apparatus |
EP3438410B1 (en) | 2017-08-01 | 2021-09-29 | General Electric Company | Sealing system for a rotary machine |
CN110005637B (zh) * | 2018-01-04 | 2021-03-26 | 中国航发商用航空发动机有限责任公司 | 轴流式航空发动机转子 |
EP3564489A1 (de) | 2018-05-03 | 2019-11-06 | Siemens Aktiengesellschaft | Rotor mit fliehkraft-optimierten kontaktflächen |
JP7092938B2 (ja) * | 2018-08-02 | 2022-06-28 | シーメンス エナジー グローバル ゲゼルシャフト ミット ベシュレンクテル ハフツング ウント コンパニー コマンディートゲゼルシャフト | 2つのロータディスクの間にロータ組立要素を配置したロータ |
US11093580B2 (en) | 2018-10-31 | 2021-08-17 | Advanced Micro Devices, Inc. | Matrix multiplier with submatrix sequencing |
DE102018218944A1 (de) * | 2018-11-07 | 2020-05-07 | Siemens Aktiengesellschaft | Rotor mit Abdichtung zwischen Laufschaufeln |
DE102018218942A1 (de) * | 2018-11-07 | 2020-05-07 | Siemens Aktiengesellschaft | Rotor mit Abdichtung zwischen Laufschaufeln |
JP7394979B2 (ja) * | 2019-10-18 | 2023-12-08 | シーメンス エナジー グローバル ゲゼルシャフト ミット ベシュレンクテル ハフツング ウント コンパニー コマンディートゲゼルシャフト | 2つのロータディスクの間に配置されたロータコンポーネントを有するロータ |
US11168615B1 (en) * | 2020-08-25 | 2021-11-09 | Raytheon Technologies Corporation | Double ring axial sealing design |
CN117897551A (zh) * | 2021-08-24 | 2024-04-16 | 西门子能源全球有限两合公司 | 转子和具有转子的流体机械 |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2095763A (en) * | 1980-12-29 | 1982-10-06 | Rolls Royce | Enhancing turbine blade coolant seal force |
JPS5896105A (ja) * | 1981-12-03 | 1983-06-08 | Hitachi Ltd | スペ−サ先端空気漏洩防止ロ−タ |
US4523890A (en) * | 1983-10-19 | 1985-06-18 | General Motors Corporation | End seal for turbine blade base |
GB8705216D0 (en) * | 1987-03-06 | 1987-04-08 | Rolls Royce Plc | Rotor assembly |
FR2700807B1 (fr) * | 1993-01-27 | 1995-03-03 | Snecma | Système de rétention et d'étanchéité d'aubes engagées dans des brochages axiaux d'un disque de rotor. |
US5622475A (en) * | 1994-08-30 | 1997-04-22 | General Electric Company | Double rabbet rotor blade retention assembly |
GB2332024B (en) * | 1997-12-03 | 2000-12-13 | Rolls Royce Plc | Rotary assembly |
JP3631898B2 (ja) | 1998-03-03 | 2005-03-23 | 三菱重工業株式会社 | ガスタービンにおける分割環の冷却構造 |
JPH11257015A (ja) * | 1998-03-17 | 1999-09-21 | Mitsubishi Heavy Ind Ltd | ガスタービンにおけるディスクのシール構造 |
US6146091A (en) * | 1998-03-03 | 2000-11-14 | Mitsubishi Heavy Industries, Ltd. | Gas turbine cooling structure |
GB0307043D0 (en) * | 2003-03-26 | 2003-04-30 | Rolls Royce Plc | A method of and structure for enabling cooling of the engaging firtree features of a turbine disk and associated blades |
US7238008B2 (en) * | 2004-05-28 | 2007-07-03 | General Electric Company | Turbine blade retainer seal |
EP1922471A1 (de) | 2005-09-07 | 2008-05-21 | Siemens Aktiengesellschaft | Anordnung zur axialsicherung von laufschaufeln in einem rotor sowie verwendung |
-
2009
- 2009-03-31 EP EP09004781A patent/EP2239419A1/de not_active Withdrawn
-
2010
- 2010-03-26 EP EP10715749.7A patent/EP2414641B1/de not_active Not-in-force
- 2010-03-26 JP JP2012502600A patent/JP5324700B2/ja not_active Expired - Fee Related
- 2010-03-26 CN CN201080014725.6A patent/CN102378850B/zh not_active Expired - Fee Related
- 2010-03-26 WO PCT/EP2010/054001 patent/WO2010112422A1/de active Application Filing
- 2010-03-26 PL PL10715749T patent/PL2414641T3/pl unknown
- 2010-03-26 ES ES10715749T patent/ES2426156T3/es active Active
- 2010-03-26 US US13/260,585 patent/US8920121B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
WO2010112422A1 (de) | 2010-10-07 |
EP2414641B1 (de) | 2013-07-03 |
JP5324700B2 (ja) | 2013-10-23 |
CN102378850A (zh) | 2012-03-14 |
JP2012522169A (ja) | 2012-09-20 |
ES2426156T3 (es) | 2013-10-21 |
US8920121B2 (en) | 2014-12-30 |
EP2414641A1 (de) | 2012-02-08 |
CN102378850B (zh) | 2014-07-16 |
US20120034087A1 (en) | 2012-02-09 |
EP2239419A1 (de) | 2010-10-13 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
PL2414641T3 (pl) | Wirnik osiowej maszyny wirnikowej z tarczą uszczelniającą | |
PL2426315T3 (pl) | Odcinek wirnika do wirnika maszyny wirnikowej | |
GB0903423D0 (en) | Variable drive gas turbine engine | |
PL2494152T3 (pl) | Sprzęgła i związana z nimi linia rotorów maszyny wirowej | |
GB201011854D0 (en) | Vane assembly for an axial flow turbine | |
GB201015028D0 (en) | Gas turbine engine | |
GB0809759D0 (en) | Gas turbine engine | |
EP2256297B8 (en) | Gas turbine vane with improved cooling | |
GB2469447B (en) | Gas turbine engine casing assembly | |
EP2592228A4 (en) | TURBINE DAWN AND MOTOR COMPONENT | |
PL2478198T3 (pl) | Silnik turbinowy z łopatkami równoległymi | |
EP2519437A4 (en) | COMPONENT GAS TURBINE ENGINE COMPONENT | |
EP2630366A4 (en) | Turbine rotor assembly | |
GB0903935D0 (en) | Gas turbine engine | |
GB201015029D0 (en) | Gas turbine engine | |
EP2519714A4 (en) | GAS TURBINE MOTOR AND ASSEMBLY AND DISASSEMBLY OF A SKIN MOTOR RUNNER | |
EP2549121A4 (en) | Gas turbine engine | |
PL2325980T3 (pl) | Tarcza wirnikowa i sposób montażu | |
GB2462245B (en) | Gas turbine engine arrangement | |
EP2551492A4 (en) | TRUNKING STRUCTURE FOR TURBINE ROTOR | |
EP2447473A4 (en) | Turbine rotor | |
GB201002642D0 (en) | Engine for thrust and or shaft output | |
EP2525063A4 (en) | Seal structure and gas turbine engine provided therewith | |
GB201007215D0 (en) | Gas turbine engine | |
EP2494154A4 (en) | GAS TURBINE ENGINE COMPONENT |