SG11201504178SA - Fan containment case with thermally conforming liner - Google Patents

Fan containment case with thermally conforming liner

Info

Publication number
SG11201504178SA
SG11201504178SA SG11201504178SA SG11201504178SA SG11201504178SA SG 11201504178S A SG11201504178S A SG 11201504178SA SG 11201504178S A SG11201504178S A SG 11201504178SA SG 11201504178S A SG11201504178S A SG 11201504178SA SG 11201504178S A SG11201504178S A SG 11201504178SA
Authority
SG
Singapore
Prior art keywords
containment case
fan containment
conforming liner
thermally conforming
thermally
Prior art date
Application number
SG11201504178SA
Other languages
English (en)
Inventor
Mark W Costa
Thomas J Robertson
Darin S Lussier
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of SG11201504178SA publication Critical patent/SG11201504178SA/en

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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/12—Light metals
    • F05D2300/121—Aluminium
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/40—Organic materials
    • F05D2300/43—Synthetic polymers, e.g. plastics; Rubber
    • F05D2300/431—Rubber
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/501—Elasticity
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/502—Thermal properties
    • 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)
SG11201504178SA 2012-12-14 2013-12-10 Fan containment case with thermally conforming liner SG11201504178SA (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/714,821 US9482111B2 (en) 2012-12-14 2012-12-14 Fan containment case with thermally conforming liner
PCT/US2013/074024 WO2014093290A1 (fr) 2012-12-14 2013-12-10 Boîtier de confinement de ventilateur doté d'un chemisage conforme thermiquement

Publications (1)

Publication Number Publication Date
SG11201504178SA true SG11201504178SA (en) 2015-07-30

Family

ID=50934875

Family Applications (1)

Application Number Title Priority Date Filing Date
SG11201504178SA SG11201504178SA (en) 2012-12-14 2013-12-10 Fan containment case with thermally conforming liner

Country Status (4)

Country Link
US (1) US9482111B2 (fr)
EP (1) EP2932052B1 (fr)
SG (1) SG11201504178SA (fr)
WO (1) WO2014093290A1 (fr)

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WO2014197053A2 (fr) 2013-03-13 2014-12-11 United Technologies Corporation Cartouche de revêtement insonorisant thermiquement conformable pour un moteur à turbine à gaz
DE102013217503A1 (de) * 2013-09-03 2015-03-05 MTU Aero Engines AG Vorrichtung zur Energieabsorption, Strömungsmaschine und Verfahren zur Energieabsorption
US9915168B2 (en) 2014-06-03 2018-03-13 United Technologies Corporation Flowpath cartridge liner and gas turbine engine including same
US10731662B2 (en) 2016-01-12 2020-08-04 Rolls-Royce Corporation Apparatus and method of manufacturing a containment case with embedded containment core
US10563537B2 (en) 2016-02-05 2020-02-18 United Technologies Corporation Energy absorbing beam and sandwich panel structure
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
US10538856B2 (en) 2017-05-02 2020-01-21 General Electric Company Apparatus and method for electro-polishing complex shapes
US11215069B2 (en) 2017-05-16 2022-01-04 General Electric Company Softwall containment systems
US10480530B2 (en) 2017-08-25 2019-11-19 United Technologies Corporation Fan Containment case for gas turbine engines
US11156126B2 (en) 2018-04-13 2021-10-26 Raytheon Technologies Corporation Fan case with interleaved layers
GB201811549D0 (en) * 2018-07-13 2018-08-29 Rolls Royce Plc Fan blade containment
GB201816990D0 (en) * 2018-10-18 2018-12-05 Rolls Royce Plc Debris retention
GB201816989D0 (en) * 2018-10-18 2018-12-05 Rolls Royce Plc Debris retention
US11499448B2 (en) 2019-05-29 2022-11-15 General Electric Company Composite fan containment case
US11591958B2 (en) 2019-06-14 2023-02-28 Pratt & Whitney Canada Corp. Turbofan engine with acoustic treatment

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US4149824A (en) * 1976-12-23 1979-04-17 General Electric Company Blade containment device
US4534698A (en) * 1983-04-25 1985-08-13 General Electric Company Blade containment structure
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
GB2288639B (en) * 1994-04-20 1998-10-21 Rolls Royce Plc Ducted fan gas turbine engine nacelle assembly
US6053696A (en) 1998-05-29 2000-04-25 Pratt & Whitney Canada Inc. Impact resistant composite shell for gas turbine engine fan case
DE69940948D1 (de) 1999-01-25 2009-07-16 Gen Electric Interner Kühlkreislauf für eine Gasturbinenschaufel
GB9922618D0 (en) 1999-09-25 1999-11-24 Rolls Royce Plc A gas turbine engine blade containment assembly
GB0116988D0 (en) 2000-08-11 2001-09-05 Rolls Royce Plc A gas turbine engine blade containment assembly
US6402464B1 (en) 2000-08-29 2002-06-11 General Electric Company Enhanced heat transfer surface for cast-in-bump-covered cooling surfaces and methods of enhancing heat transfer
US6979172B1 (en) 2002-01-03 2005-12-27 Saint-Gobain Ceramics & Plastics, Inc. Engine blade containment shroud using quartz fiber composite
US6619913B2 (en) 2002-02-15 2003-09-16 General Electric Company Fan casing acoustic treatment
US6814541B2 (en) 2002-10-07 2004-11-09 General Electric Company Jet aircraft fan case containment design
DE10259943A1 (de) 2002-12-20 2004-07-01 Rolls-Royce Deutschland Ltd & Co Kg Schutzring für das Fan-Schutzgehäuse eines Gasturbinentriebswerks
GB2407343B (en) 2003-10-22 2006-04-19 Rolls Royce Plc An acoustic liner for a gas turbine engine casing
US20060093847A1 (en) 2004-11-02 2006-05-04 United Technologies Corporation Composite sandwich with improved ballistic toughness
GB0610271D0 (en) * 2006-05-24 2006-07-05 Rolls Royce Plc A gas turbine engine casing
WO2008014389A2 (fr) 2006-07-26 2008-01-31 Board Of Governors For Higher Education State Of Rhode Island And Providence Plantations Technique de refroidissement électronique dans des micro/mini canaux par 'streaming'
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US8672609B2 (en) 2009-08-31 2014-03-18 United Technologies Corporation Composite fan containment case assembly
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Also Published As

Publication number Publication date
WO2014093290A1 (fr) 2014-06-19
US20140286748A1 (en) 2014-09-25
EP2932052A4 (fr) 2016-02-17
EP2932052A1 (fr) 2015-10-21
US9482111B2 (en) 2016-11-01
EP2932052B1 (fr) 2019-07-24

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