GB1466385A - Containment shields for gas turbine engines - Google Patents
Containment shields for gas turbine enginesInfo
- Publication number
- GB1466385A GB1466385A GB5227273A GB5227273A GB1466385A GB 1466385 A GB1466385 A GB 1466385A GB 5227273 A GB5227273 A GB 5227273A GB 5227273 A GB5227273 A GB 5227273A GB 1466385 A GB1466385 A GB 1466385A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shield
- wall
- containment
- casing
- gas turbine
- 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
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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/327—Application in turbines in gas turbines to drive shrouded, high solidity propeller
-
- 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)
Abstract
1466385 Gas turbine ducted fan engines - containment shield ROLLS ROYCE (1971) Ltd 21 Nov 1974 [10 Nov 1973] 52272/73 Headings F1J and F1T A containment device for a gas turbine engine comprises a cylindrical containment shield, a surrounding casing and support means connecting the shield to the casing, the shield being of greater rigidity than the support means or the casing such that in the event that the containment shield is impacted on by an engine part such as a blade, the shield will be displaced so transmitting some of the force of the impact to the casing. In the embodiment, the containment shield 17 is disposed around the fan blade assembly 14 of a gas turbine ducted fan engine, the containment shield being located within the fan casing which comprises an outer wall 15 and an inner wall 16, the shield being supported from the.outer wall 15 by four radiallyextending struts 18. The outer wall 15 is of thinner section than the inner wall 16. In the event of detachment of a fan blade 14 the containment shield will be displaced laterally, the impact being absorbed by the outer wall 15 and by the struts 18.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5227273A GB1466385A (en) | 1974-11-21 | 1974-11-21 | Containment shields for gas turbine engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5227273A GB1466385A (en) | 1974-11-21 | 1974-11-21 | Containment shields for gas turbine engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1466385A true GB1466385A (en) | 1977-03-09 |
Family
ID=10463289
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5227273A Expired GB1466385A (en) | 1974-11-21 | 1974-11-21 | Containment shields for gas turbine engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1466385A (en) |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4197052A (en) * | 1977-10-11 | 1980-04-08 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Safety device for an axially rotating machine |
FR2467978A1 (en) * | 1979-10-23 | 1981-04-30 | Snecma | RETENTION DEVICE FOR A COMPRESSOR CASE OF A TURBOMACHINE |
FR2514823A1 (en) * | 1981-10-16 | 1983-04-22 | Poudres & Explosifs Ste Nale | Guard to protect against centrifugal rupture of high speed rotor - esp. aircraft gas turbine, uses sheet of fibres impregnated with organic resin |
EP0205559A1 (en) * | 1984-12-04 | 1986-12-30 | Sundstrand Corporation | Turbine wheel containment |
EP0718471A1 (en) * | 1994-12-21 | 1996-06-26 | Hispano-Suiza | Containment ring for a turbomachine |
WO1999054598A1 (en) * | 1998-04-20 | 1999-10-28 | Pratt & Whitney Canada Corp. | Containment system for containing blade burst |
US6206631B1 (en) * | 1999-09-07 | 2001-03-27 | General Electric Company | Turbomachine fan casing with dual-wall blade containment structure |
US7332049B2 (en) | 2004-12-22 | 2008-02-19 | General Electric Company | Method for fabricating reinforced composite materials |
US7335012B2 (en) | 2004-12-22 | 2008-02-26 | General Electric Company | Apparatus for fabricating reinforced composite materials |
US7431978B2 (en) | 2004-12-22 | 2008-10-07 | General Electric Company | Reinforced matrix composite containment duct |
RU2584744C2 (en) * | 2010-08-26 | 2016-05-20 | Турбомека | Method for attachment of shielding on turbine housing and mounting system therefor |
FR3054527A1 (en) * | 2016-07-29 | 2018-02-02 | Airbus Operations | AIRCRAFT ASSEMBLY COMPRISING A PROTECTIVE SHIELD AGAINST MOTOR SHOCK, MOUNTED ON THE CASING OF A TURBOMACHINE MODULE |
US10161419B2 (en) | 2015-06-09 | 2018-12-25 | Rolls-Royce Plc | Fan casing assembly |
-
1974
- 1974-11-21 GB GB5227273A patent/GB1466385A/en not_active Expired
Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4197052A (en) * | 1977-10-11 | 1980-04-08 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Safety device for an axially rotating machine |
FR2467978A1 (en) * | 1979-10-23 | 1981-04-30 | Snecma | RETENTION DEVICE FOR A COMPRESSOR CASE OF A TURBOMACHINE |
EP0028183A1 (en) * | 1979-10-23 | 1981-05-06 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Containment device for the compressor housing of a turbomachine |
FR2514823A1 (en) * | 1981-10-16 | 1983-04-22 | Poudres & Explosifs Ste Nale | Guard to protect against centrifugal rupture of high speed rotor - esp. aircraft gas turbine, uses sheet of fibres impregnated with organic resin |
EP0205559A1 (en) * | 1984-12-04 | 1986-12-30 | Sundstrand Corporation | Turbine wheel containment |
EP0205559A4 (en) * | 1984-12-04 | 1988-10-20 | Sundstrand Corp | Turbine wheel containment. |
EP0718471A1 (en) * | 1994-12-21 | 1996-06-26 | Hispano-Suiza | Containment ring for a turbomachine |
WO1996019641A1 (en) * | 1994-12-21 | 1996-06-27 | Societe Hispano Suiza | Protective shield for a turbomachine |
FR2728619A1 (en) * | 1994-12-21 | 1996-06-28 | Hispano Suiza Sa | PROTECTIVE SHIELD OF A TURBOMACHINE |
US5622472A (en) * | 1994-12-21 | 1997-04-22 | Societe Hispano-Suiza | Protective shield for a turbo-engine |
WO1999054598A1 (en) * | 1998-04-20 | 1999-10-28 | Pratt & Whitney Canada Corp. | Containment system for containing blade burst |
US6059523A (en) * | 1998-04-20 | 2000-05-09 | Pratt & Whitney Canada Inc. | Containment system for containing blade burst |
US6206631B1 (en) * | 1999-09-07 | 2001-03-27 | General Electric Company | Turbomachine fan casing with dual-wall blade containment structure |
US7332049B2 (en) | 2004-12-22 | 2008-02-19 | General Electric Company | Method for fabricating reinforced composite materials |
US7335012B2 (en) | 2004-12-22 | 2008-02-26 | General Electric Company | Apparatus for fabricating reinforced composite materials |
US7431978B2 (en) | 2004-12-22 | 2008-10-07 | General Electric Company | Reinforced matrix composite containment duct |
US7867566B2 (en) | 2004-12-22 | 2011-01-11 | General Electric Company | Method for fabricating reinforced composite materials |
RU2584744C2 (en) * | 2010-08-26 | 2016-05-20 | Турбомека | Method for attachment of shielding on turbine housing and mounting system therefor |
US10161419B2 (en) | 2015-06-09 | 2018-12-25 | Rolls-Royce Plc | Fan casing assembly |
FR3054527A1 (en) * | 2016-07-29 | 2018-02-02 | Airbus Operations | AIRCRAFT ASSEMBLY COMPRISING A PROTECTIVE SHIELD AGAINST MOTOR SHOCK, MOUNTED ON THE CASING OF A TURBOMACHINE MODULE |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1466385A (en) | Containment shields for gas turbine engines | |
SE8203975D0 (en) | KOMPOUNDDRIVAGGREGAT | |
IT1108741B (en) | COOLING SYSTEMS FOR GAS TURBINE ENGINES | |
JPS521223A (en) | Divided fan gas turbine engine | |
IT1043166B (en) | INEPAROX RADIATION SUPPRESSION SYSTEM FOR A GAS TURBO ENGINE | |
JPS5618032A (en) | Cooling shroud for gas turbine engine | |
IT1051760B (en) | COMBUSTION EQUIPMENT FOR GAS TURBINE ENGINES | |
GB1294324A (en) | Engine installations | |
JPS5449410A (en) | Fuel nozzle assembly for gas turbine engine | |
JPS5538494A (en) | Combustor dome assembly for gas turbine engine | |
GB1014260A (en) | Improvements in gas turbine ducted fan powerplant | |
JPS52118117A (en) | Rotor blade for gas turbine engine | |
GB799605A (en) | Improvements in or relating to combustion equipment for example for gas turbine engines | |
GB1062377A (en) | Improvements in coupling system for ducted fan power plant | |
GB2001410B (en) | Gas turbine engine mounting assembly | |
GB865545A (en) | Turbines | |
Stone | Flight effects on exhaust noise for turbojet and turbofan engines—comparison of experimental data with prediction | |
GB1032274A (en) | Mounting of ducted fan turbine engines in the tail of an aircraft | |
GB1514800A (en) | Ducted fan engine oil disposal means | |
GB1507914A (en) | Device for preventing foreign matters from being sucked into a gas turbine engine for an aircraft | |
Kesselring et al. | Design criteria for stationary source catalytic combustion systems | |
GB1041048A (en) | Improvements in aircraft having jet-propulsion power-plants | |
GB2014663B (en) | Gas turbine ducted fan engine | |
GB888943A (en) | Improvements in or relating to fan units | |
GB790830A (en) | Improvements relating to gas-turbine engines |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
CSNS | Application of which complete specification have been accepted and published, but patent is not sealed |