[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

GB0718002D0 - Blade containment system for a gas turbine engine - Google Patents

Blade containment system for a gas turbine engine

Info

Publication number
GB0718002D0
GB0718002D0 GBGB0718002.9A GB0718002A GB0718002D0 GB 0718002 D0 GB0718002 D0 GB 0718002D0 GB 0718002 A GB0718002 A GB 0718002A GB 0718002 D0 GB0718002 D0 GB 0718002D0
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
containment system
blade containment
blade
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.)
Withdrawn
Application number
GBGB0718002.9A
Other versions
GB2442112A (en
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.)
General Electric Co
Original Assignee
General Electric Co
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.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of GB0718002D0 publication Critical patent/GB0718002D0/en
Publication of GB2442112A publication Critical patent/GB2442112A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B1/00Layered products having a non-planar shape
    • B32B1/08Tubular products
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04Shutting-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
    • F01D21/045Shutting-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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/08Sealings
    • F04D29/16Sealings between pressure and suction sides
    • F04D29/161Sealings between pressure and suction sides especially adapted for elastic fluid pumps
    • F04D29/164Sealings between pressure and suction sides especially adapted for elastic fluid pumps of an axial flow wheel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/522Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps
    • F04D29/526Details of the casing section radially opposing blade tips
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
  • Laminated Bodies (AREA)
  • Control Of Turbines (AREA)
GB0718002A 2006-09-25 2007-09-14 Gas turbine engine containment casing Withdrawn GB2442112A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US52640106A 2006-09-25 2006-09-25

Publications (2)

Publication Number Publication Date
GB0718002D0 true GB0718002D0 (en) 2007-10-24
GB2442112A GB2442112A (en) 2008-03-26

Family

ID=38659004

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0718002A Withdrawn GB2442112A (en) 2006-09-25 2007-09-14 Gas turbine engine containment casing

Country Status (4)

Country Link
JP (1) JP2008082332A (en)
CA (1) CA2602319A1 (en)
DE (1) DE102007045138A1 (en)
GB (1) GB2442112A (en)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2935017B1 (en) * 2008-08-13 2012-11-02 Snecma INTERNAL WALL OF A TURBOMACHINE NACELLE
EP2418387B1 (en) * 2010-08-11 2015-04-01 Techspace Aero S.A. Shroud ring of an axial turbomachine compressor
GB2489673B (en) * 2011-03-29 2015-08-12 Rolls Royce Plc A containment casing for a gas turbine engine
FR2977827B1 (en) * 2011-07-13 2015-03-13 Snecma PROCESS FOR MANUFACTURING A TURBOMACHINE BLOWER HOUSING WITH ABRADABLE AND ACOUSTIC COATINGS
EP2594742B1 (en) * 2011-11-17 2017-01-04 Hamilton Sundstrand Corporation Low cost containment ring
US9840936B2 (en) 2012-02-16 2017-12-12 United Technologies Corporation Case with ballistic liner
CN104105868B (en) 2012-02-16 2017-05-03 联合工艺公司 Composite fan containment case assembly
FR2991385B1 (en) * 2012-06-05 2017-04-28 Snecma BACK PLATE, AND TURBOMACHINE COMPRISING A BACK PLATE
GB201401932D0 (en) 2014-02-05 2014-03-19 Rolls Royce Plc A fan casing for a gas turbine engine
FR3031469B1 (en) * 2015-01-14 2017-09-22 Snecma CARRIER IN MATERIAL COMPOSITE WITH ORGANIC MATRIX AUTO-RAIDI
AT516322B1 (en) 2014-10-10 2017-04-15 Facc Ag Flight case for an aircraft engine
US10472985B2 (en) 2016-12-12 2019-11-12 Honeywell International Inc. Engine case for fan blade out retention
US10487684B2 (en) * 2017-03-31 2019-11-26 The Boeing Company Gas turbine engine fan blade containment systems
US10662813B2 (en) * 2017-04-13 2020-05-26 General Electric Company Turbine engine and containment assembly for use in a turbine engine
US10533450B2 (en) 2017-10-30 2020-01-14 United Technologies Corporation Ballistic liner install methods
EP3702263A1 (en) 2019-02-28 2020-09-02 Airbus Operations GmbH Aircraft structure for flow control
FR3097902B1 (en) * 2019-06-27 2023-03-17 Safran Aircraft Engines AIRCRAFT TURBOMACHINE ENCLOSED IN AT LEAST PARTIALLY COMPOSITE MATERIAL

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4534698A (en) * 1983-04-25 1985-08-13 General Electric Company Blade containment structure
GB2159886B (en) * 1984-06-07 1988-01-27 Rolls Royce Fan duct casing
GB2239214B (en) * 1989-12-23 1993-11-03 Rolls Royce Plc A sandwich structure and a method of manufacturing a sandwich structure
US5344280A (en) * 1993-05-05 1994-09-06 General Electric Company Impact resistant fan case liner
US6652222B1 (en) * 2002-09-03 2003-11-25 Pratt & Whitney Canada Corp. Fan case design with metal foam between Kevlar
NL1024076C2 (en) * 2003-08-08 2005-02-10 Stork Fokker Aesp Bv Method for forming a laminate with a recess.
US20050175813A1 (en) * 2004-02-10 2005-08-11 Wingert A. L. Aluminum-fiber laminate
WO2006037083A2 (en) * 2004-09-24 2006-04-06 Itochu Corporation Thin ply laminates
US20060093847A1 (en) * 2004-11-02 2006-05-04 United Technologies Corporation Composite sandwich with improved ballistic toughness

Also Published As

Publication number Publication date
CA2602319A1 (en) 2008-03-25
DE102007045138A1 (en) 2008-03-27
GB2442112A (en) 2008-03-26
JP2008082332A (en) 2008-04-10

Similar Documents

Publication Publication Date Title
GB0718002D0 (en) Blade containment system for a gas turbine engine
GB2434836B (en) Mounting system for use in mounting a gas turbine engine
GB2438696B (en) A gas turbine engine
GB2450139B (en) An aerofoil for a gas turbine engine
GB2473578B (en) Gas turbine engine system
GB0608859D0 (en) A gas turbine engine
GB0510538D0 (en) A rotor blade containment assembly for a gas turbine engine
GB0601220D0 (en) Aerofoils for gas turbine engines
GB2436128B (en) Gas turbine engine
GB0904121D0 (en) Seal for a turbine engine
GB2443194B (en) Gas turbine engine
GB0707170D0 (en) Method and apparatus for operating a gas turbine engine
GB0610271D0 (en) A gas turbine engine casing
GB0603285D0 (en) A gas turbine engine
EP2153051A4 (en) A masking arrangement for a gas turbine engine
GB0523469D0 (en) Blades for gas turbine engines
GB0502324D0 (en) A multi-shaft arrangement for a turbine engine
GB0614392D0 (en) Turbine Housing for a turbocharger
GB2434837B (en) A containment system for a gas turbine engine
GB2461778B (en) A centering device for a gas turbine engine.
GB0614518D0 (en) A fan blade for a gas turbine engine
GB2445952B (en) A gas turbine engine
GB0624294D0 (en) A transition duct for a gas turbine engine
GB0403941D0 (en) A gas turbine engine blade containment assembly
EP2235345A4 (en) A gas turbine engine

Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)