GB0019803D0 - A gas turbine engine blade containment assembly - Google Patents
A gas turbine engine blade containment assemblyInfo
- Publication number
- GB0019803D0 GB0019803D0 GBGB0019803.6A GB0019803A GB0019803D0 GB 0019803 D0 GB0019803 D0 GB 0019803D0 GB 0019803 A GB0019803 A GB 0019803A GB 0019803 D0 GB0019803 D0 GB 0019803D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbine
- turbine engine
- containment assembly
- engine blade
- blade containment
- 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
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
- 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
- F05D2250/00—Geometry
- F05D2250/10—Two-dimensional
- F05D2250/15—Two-dimensional spiral
-
- 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
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/25—Three-dimensional helical
-
- 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
- F05D2250/00—Geometry
- F05D2250/60—Structure; Surface texture
- F05D2250/61—Structure; Surface texture corrugated
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0019803A GB2365926B (en) | 2000-08-12 | 2000-08-12 | A gas turbine engine blade containment assembly |
GBGB0116988.7A GB0116988D0 (en) | 2000-08-11 | 2001-07-12 | A gas turbine engine blade containment assembly |
US09/924,104 US6575694B1 (en) | 2000-08-11 | 2001-08-08 | Gas turbine engine blade containment assembly |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0019803A GB2365926B (en) | 2000-08-12 | 2000-08-12 | A gas turbine engine blade containment assembly |
Publications (3)
Publication Number | Publication Date |
---|---|
GB0019803D0 true GB0019803D0 (en) | 2000-09-27 |
GB2365926A GB2365926A (en) | 2002-02-27 |
GB2365926B GB2365926B (en) | 2004-12-08 |
Family
ID=9897450
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0019803A Expired - Fee Related GB2365926B (en) | 2000-08-11 | 2000-08-12 | A gas turbine engine blade containment assembly |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2365926B (en) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10259943A1 (en) | 2002-12-20 | 2004-07-01 | Rolls-Royce Deutschland Ltd & Co Kg | Protective ring for the fan protective housing of a gas turbine engine |
GB0704879D0 (en) | 2007-03-14 | 2007-04-18 | Rolls Royce Plc | A Casing arrangement |
GB0916823D0 (en) | 2009-09-25 | 2009-11-04 | Rolls Royce Plc | Containment casing for an aero engine |
US8858156B2 (en) * | 2010-08-12 | 2014-10-14 | General Electric Company | Fragment containment assembly and method for adding a fragment containment assembly to a turbine |
GB2501918B (en) | 2012-05-11 | 2014-06-18 | Rolls Royce Plc | Casing |
DE102015217078A1 (en) * | 2015-09-07 | 2017-03-09 | MTU Aero Engines AG | Device for limiting a flow channel of a turbomachine |
DE102018113396A1 (en) * | 2018-06-06 | 2019-12-12 | Man Energy Solutions Se | Burst protection device for a turbomachine |
EP3885539A1 (en) * | 2020-03-26 | 2021-09-29 | Unison Industries LLC | Air turbine starter and method of containing a turbine of an air turbine starter |
EP3885538B1 (en) * | 2020-03-26 | 2023-07-26 | Unison Industries LLC | Air turbine starter for starting an engine and method of forming a containment structure for an air turbine starter |
US20230340890A1 (en) * | 2022-04-21 | 2023-10-26 | Pratt & Whitney Canada Corp. | Multi-layered containment structure for a bladed rotor of a gas turbine engine |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3916054A (en) * | 1973-02-23 | 1975-10-28 | Int Harvester Co | Compliant structural members |
US3974313A (en) * | 1974-08-22 | 1976-08-10 | The Boeing Company | Projectile energy absorbing protective barrier |
GB1533017A (en) * | 1975-11-10 | 1978-11-22 | Caterpillar Tractor Co | Modular gas turbine engine assembly |
US4618152A (en) * | 1983-01-13 | 1986-10-21 | Thomas P. Mahoney | Honeycomb seal structure |
FR2607198B1 (en) * | 1986-11-26 | 1990-05-04 | Snecma | COMPRESSOR HOUSING SUITABLE FOR ACTIVE PILOTAGE OF ITS EXPANSIONS AND MANUFACTURING METHOD THEREOF |
-
2000
- 2000-08-12 GB GB0019803A patent/GB2365926B/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
GB2365926A (en) | 2002-02-27 |
GB2365926B (en) | 2004-12-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20180812 |