GB1466385A – Containment shields for gas turbine engines
– Google Patents
GB1466385A – Containment shields for gas turbine engines
– Google Patents
Containment shields for gas turbine engines
Info
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
1974-11-21
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
Application number
GB5227273A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
Priority date (The priority date 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 date listed.)
1974-11-21
Filing date
1974-11-21
Publication date
1977-03-09
1974-11-21
Application filed by Rolls Royce PLC
filed
Critical
Rolls Royce PLC
1974-11-21
Priority to GB5227273A
priority
Critical
patent/GB1466385A/en
1977-03-09
Publication of GB1466385A
publication
Critical
patent/GB1466385A/en
Status
Expired
legal-status
Critical
Current
Links
Espacenet
Global Dossier
Discuss
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
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.
GB5227273A
1974-11-21
1974-11-21
Containment shields for gas turbine engines
Expired
GB1466385A
(en)
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)
* Cited by examiner, † Cited by third party
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)
* Cited by examiner, † Cited by third party
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
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Legal Events
Date
Code
Title
Description
1977-11-02
CSNS
Application of which complete specification have been accepted and published, but patent is not sealed
