DE69936176D1 - Berstschutzring für Turbinen - Google Patents
Berstschutzring für TurbinenInfo
- Publication number
- DE69936176D1 DE69936176D1 DE69936176T DE69936176T DE69936176D1 DE 69936176 D1 DE69936176 D1 DE 69936176D1 DE 69936176 T DE69936176 T DE 69936176T DE 69936176 T DE69936176 T DE 69936176T DE 69936176 D1 DE69936176 D1 DE 69936176D1
- Authority
- DE
- Germany
- Prior art keywords
- turbines
- bursting ring
- bursting
- 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 - Lifetime
Links
- 230000009172 bursting Effects 0.000 title 1
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
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
- F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
-
- 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
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
- F01D11/127—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with a deformable or crushable structure, e.g. honeycomb
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US191659 | 1998-11-13 | ||
US09/191,659 US6120242A (en) | 1998-11-13 | 1998-11-13 | Blade containing turbine shroud |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69936176D1 true DE69936176D1 (de) | 2007-07-12 |
DE69936176T2 DE69936176T2 (de) | 2008-01-17 |
Family
ID=22706390
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69936176T Expired - Lifetime DE69936176T2 (de) | 1998-11-13 | 1999-10-26 | Berstschutzring für Turbinen |
Country Status (4)
Country | Link |
---|---|
US (2) | US6120242A (de) |
EP (1) | EP1001140B1 (de) |
JP (1) | JP4495283B2 (de) |
DE (1) | DE69936176T2 (de) |
Families Citing this family (48)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6341938B1 (en) * | 2000-03-10 | 2002-01-29 | General Electric Company | Methods and apparatus for minimizing thermal gradients within turbine shrouds |
US6547522B2 (en) * | 2001-06-18 | 2003-04-15 | General Electric Company | Spring-backed abradable seal for turbomachinery |
DE10259963B4 (de) * | 2002-12-20 | 2010-04-01 | Mtu Aero Engines Gmbh | Wabendichtung |
US6893217B2 (en) * | 2002-12-20 | 2005-05-17 | General Electric Company | Methods and apparatus for assembling gas turbine nozzles |
US6892931B2 (en) * | 2002-12-27 | 2005-05-17 | General Electric Company | Methods for replacing portions of turbine shroud supports |
US7094029B2 (en) * | 2003-05-06 | 2006-08-22 | General Electric Company | Methods and apparatus for controlling gas turbine engine rotor tip clearances |
GB2407343B (en) * | 2003-10-22 | 2006-04-19 | Rolls Royce Plc | An acoustic liner for a gas turbine engine casing |
GB2418957B (en) * | 2003-10-22 | 2006-07-05 | Rolls Royce Plc | A liner for a gas turbine engine casing |
US7334984B1 (en) | 2003-12-24 | 2008-02-26 | Heico Corporation | Turbine shroud assembly with enhanced blade containment capabilities |
DE102004010236A1 (de) * | 2004-03-03 | 2005-09-15 | Mtu Aero Engines Gmbh | Ringstruktur in Metallbauweise |
GB0408825D0 (en) * | 2004-04-20 | 2004-05-26 | Rolls Royce Plc | A rotor blade containment assembly for a gas turbine engine |
US7147429B2 (en) * | 2004-09-16 | 2006-12-12 | General Electric Company | Turbine assembly and turbine shroud therefor |
GB2429043B (en) * | 2005-08-13 | 2008-02-13 | Rolls Royce Plc | Clip |
FR2899274B1 (fr) * | 2006-03-30 | 2012-08-17 | Snecma | Dispositif de fixation de secteurs d'anneau autour d'une roue de turbine d'une turbomachine |
GB2459646B (en) * | 2008-04-28 | 2011-03-30 | Rolls Royce Plc | A fan assembly |
US8608424B2 (en) * | 2009-10-09 | 2013-12-17 | General Electric Company | Contoured honeycomb seal for a turbomachine |
FR2961848B1 (fr) * | 2010-06-29 | 2012-07-13 | Snecma | Etage de turbine |
US8511971B2 (en) | 2010-07-23 | 2013-08-20 | Hamilton Sundstrand Corporation | One-piece compressor and turbine containment system |
GB201020143D0 (en) | 2010-11-29 | 2011-01-12 | Rolls Royce Plc | A gas turbine engine blade containment arrangement |
US9121301B2 (en) * | 2012-03-20 | 2015-09-01 | General Electric Company | Thermal isolation apparatus |
US9574455B2 (en) * | 2012-07-16 | 2017-02-21 | United Technologies Corporation | Blade outer air seal with cooling features |
US9506367B2 (en) * | 2012-07-20 | 2016-11-29 | United Technologies Corporation | Blade outer air seal having inward pointing extension |
US20140064969A1 (en) * | 2012-08-29 | 2014-03-06 | Dmitriy A. Romanov | Blade outer air seal |
US9238977B2 (en) | 2012-11-21 | 2016-01-19 | General Electric Company | Turbine shroud mounting and sealing arrangement |
US9651059B2 (en) | 2012-12-27 | 2017-05-16 | United Technologies Corporation | Adhesive pattern for fan case conformable liner |
US10024191B2 (en) | 2013-03-11 | 2018-07-17 | Rolls-Royce Corporation | Fan track liner designed to yield next to fan case hook |
US20140271142A1 (en) | 2013-03-14 | 2014-09-18 | General Electric Company | Turbine Shroud with Spline Seal |
JP6184173B2 (ja) | 2013-05-29 | 2017-08-23 | 三菱日立パワーシステムズ株式会社 | ガスタービン |
DE102013210602A1 (de) * | 2013-06-07 | 2014-12-11 | MTU Aero Engines AG | Turbinengehäuse mit Verstärkungselementen im Containmentbereich |
ES2570969T3 (es) * | 2013-07-12 | 2016-05-23 | MTU Aero Engines AG | Grado de turbina de gas |
CN103422913A (zh) * | 2013-08-29 | 2013-12-04 | 哈尔滨工程大学 | 一种带有蜂窝状内壁机匣的涡轮 |
US10408080B2 (en) | 2013-10-07 | 2019-09-10 | United Technologies Corporation | Tailored thermal control system for gas turbine engine blade outer air seal array |
EP2881545B1 (de) * | 2013-12-04 | 2017-05-31 | MTU Aero Engines GmbH | Dichtelement, Dichteinrichtung und Strömungsmaschine |
EP2902592B1 (de) * | 2014-01-31 | 2017-04-12 | Rolls-Royce plc | Gasturbinenantrieb |
EP3153671A1 (de) | 2015-10-08 | 2017-04-12 | MTU Aero Engines GmbH | Schutzvorrichtung für eine strömungsmaschine |
US10197069B2 (en) | 2015-11-20 | 2019-02-05 | United Technologies Corporation | Outer airseal for gas turbine engine |
US11421627B2 (en) * | 2017-02-22 | 2022-08-23 | General Electric Company | Aircraft and direct drive engine under wing installation |
US10487684B2 (en) | 2017-03-31 | 2019-11-26 | The Boeing Company | Gas turbine engine fan blade containment systems |
US10550718B2 (en) | 2017-03-31 | 2020-02-04 | The Boeing Company | Gas turbine engine fan blade containment systems |
US10753222B2 (en) | 2017-09-11 | 2020-08-25 | Raytheon Technologies Corporation | Gas turbine engine blade outer air seal |
FR3072713B1 (fr) * | 2017-10-23 | 2021-09-10 | Safran Aircraft Engines | Secteur d'anneau de turbine pour turbomachine d'aeronef |
US10883377B2 (en) * | 2017-10-27 | 2021-01-05 | Rolls-Royce North American Technolgies Inc. | System and method of controlling tip clearance in a shroud assembly for a bladed disc |
US20200011203A1 (en) * | 2018-07-06 | 2020-01-09 | General Electric Company | Blade containment structure |
US10724403B2 (en) * | 2018-07-16 | 2020-07-28 | Raytheon Technologies Corporation | Fan case assembly for gas turbine engine |
US11319833B2 (en) | 2020-04-24 | 2022-05-03 | General Electric Company | Fan case with crack-arresting backsheet structure and removable containment cartridge |
US11674396B2 (en) | 2021-07-30 | 2023-06-13 | General Electric Company | Cooling air delivery assembly |
US11674405B2 (en) | 2021-08-30 | 2023-06-13 | General Electric Company | Abradable insert with lattice structure |
US20230399981A1 (en) * | 2022-06-09 | 2023-12-14 | Pratt & Whitney Canada Corp. | Containment assembly for an aircraft engine |
Family Cites Families (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1223925A (fr) * | 1959-05-12 | 1960-06-21 | Gen Electric | Dispositif de limitation de vitesse pour les turbines |
US3928963A (en) * | 1974-11-04 | 1975-12-30 | Gen Motors Corp | Cast in place gas turbine containment ring and method of manufacture |
US4009568A (en) * | 1975-10-30 | 1977-03-01 | General Motors Corporation | Turbine support structure |
US4053254A (en) * | 1976-03-26 | 1977-10-11 | United Technologies Corporation | Turbine case cooling system |
US4127357A (en) * | 1977-06-24 | 1978-11-28 | General Electric Company | Variable shroud for a turbomachine |
DE2907748A1 (de) * | 1979-02-28 | 1980-09-04 | Motoren Turbinen Union | Einrichtung zur minimierung und konstanthaltung der bei axialturbinen vorhandenen schaufelspitzenspiele, insbesondere fuer gasturbinentriebwerke |
GB2087979B (en) * | 1980-11-22 | 1984-02-22 | Rolls Royce | Gas turbine engine blade tip seal |
US4417848A (en) * | 1982-02-01 | 1983-11-29 | United Technologies Corporation | Containment shell for a fan section of a gas turbine engine |
US4566700A (en) * | 1982-08-09 | 1986-01-28 | United Technologies Corporation | Abrasive/abradable gas path seal system |
US4784569A (en) * | 1986-01-10 | 1988-11-15 | General Electric Company | Shroud means for turbine rotor blade tip clearance control |
JP2624661B2 (ja) * | 1987-01-07 | 1997-06-25 | 株式会社日立製作所 | ガスタービンエンジンのシール装置 |
US4867639A (en) * | 1987-09-22 | 1989-09-19 | Allied-Signal Inc. | Abradable shroud coating |
US4856963A (en) * | 1988-03-23 | 1989-08-15 | United Technologies Corporation | Stator assembly for an axial flow rotary machine |
FR2635562B1 (fr) * | 1988-08-18 | 1993-12-24 | Snecma | Anneau de stator de turbine associe a un support de liaison au carter de turbine |
JPH02298604A (ja) * | 1989-05-11 | 1990-12-11 | Toshiba Corp | 軸流々体機械の翼端漏洩防止装置 |
IE67360B1 (en) * | 1990-09-25 | 1996-03-20 | United Technologies Corp | Apparatus and method for a stator assembly of a rotary machine |
US5160248A (en) * | 1991-02-25 | 1992-11-03 | General Electric Company | Fan case liner for a gas turbine engine with improved foreign body impact resistance |
US5201846A (en) * | 1991-11-29 | 1993-04-13 | General Electric Company | Low-pressure turbine heat shield |
DE4331060C1 (de) * | 1993-09-13 | 1994-06-30 | Gruenzweig & Hartmann Montage | Wärmedämmanordnung |
US5423659A (en) * | 1994-04-28 | 1995-06-13 | United Technologies Corporation | Shroud segment having a cut-back retaining hook |
US5431532A (en) * | 1994-05-20 | 1995-07-11 | General Electric Company | Blade containment system |
FR2728619B1 (fr) * | 1994-12-21 | 1997-01-24 | Hispano Suiza Sa | Bouclier de protection d'une turbomachine |
US5474417A (en) * | 1994-12-29 | 1995-12-12 | United Technologies Corporation | Cast casing treatment for compressor blades |
US5538393A (en) * | 1995-01-31 | 1996-07-23 | United Technologies Corporation | Turbine shroud segment with serpentine cooling channels having a bend passage |
GB2310255B (en) * | 1996-02-13 | 1999-06-16 | Rolls Royce Plc | A turbomachine |
US5791871A (en) * | 1996-12-18 | 1998-08-11 | United Technologies Corporation | Turbine engine rotor assembly blade outer air seal |
-
1998
- 1998-11-13 US US09/191,659 patent/US6120242A/en not_active Expired - Lifetime
-
1999
- 1999-10-26 EP EP99308435A patent/EP1001140B1/de not_active Expired - Lifetime
- 1999-10-26 DE DE69936176T patent/DE69936176T2/de not_active Expired - Lifetime
- 1999-11-12 JP JP32186699A patent/JP4495283B2/ja not_active Expired - Fee Related
-
2000
- 2000-09-18 US US09/664,145 patent/US6468026B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP1001140A3 (de) | 2001-10-04 |
US6120242A (en) | 2000-09-19 |
DE69936176T2 (de) | 2008-01-17 |
EP1001140B1 (de) | 2007-05-30 |
US6468026B1 (en) | 2002-10-22 |
JP2000257402A (ja) | 2000-09-19 |
EP1001140A2 (de) | 2000-05-17 |
JP4495283B2 (ja) | 2010-06-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |