IL181845A0 - Fan case reinforcement in a gas turbine jet engine - Google Patents

Fan case reinforcement in a gas turbine jet engine

Info

Publication number
IL181845A0
IL181845A0 IL181845A IL18184507A IL181845A0 IL 181845 A0 IL181845 A0 IL 181845A0 IL 181845 A IL181845 A IL 181845A IL 18184507 A IL18184507 A IL 18184507A IL 181845 A0 IL181845 A0 IL 181845A0
Authority
IL
Israel
Prior art keywords
gas turbine
jet engine
fan case
turbine jet
case reinforcement
Prior art date
Application number
IL181845A
Original Assignee
James L Cardarella Jr
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
Priority claimed from PCT/US2005/033564 external-priority patent/WO2006137875A2/en
Application filed by James L Cardarella Jr filed Critical James L Cardarella Jr
Publication of IL181845A0 publication Critical patent/IL181845A0/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
    • 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
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/25—Manufacture essentially without removing material by forging
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/40—Heat treatment
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • 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
    • F05D2250/29—Three-dimensional machined; miscellaneous
    • F05D2250/292—Three-dimensional machined; miscellaneous tapered
    • 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
    • F05D2260/00—Function
    • F05D2260/30—Retaining components in desired mutual position
    • 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
    • F05D2300/13—Refractory metals, i.e. Ti, V, Cr, Zr, Nb, Mo, Hf, Ta, W
    • F05D2300/133—Titanium
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
IL181845A 2005-09-20 2007-03-11 Fan case reinforcement in a gas turbine jet engine IL181845A0 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
PCT/US2005/033564 WO2006137875A2 (en) 2004-09-23 2005-09-20 Fan case reinforcement in a gas turbine jet engine
PCT/US2005/041822 WO2007035184A2 (en) 2005-09-20 2005-11-16 Fan case reinforcement in a gas turbine jet engine

Publications (1)

Publication Number Publication Date
IL181845A0 true IL181845A0 (en) 2009-02-11

Family

ID=37835253

Family Applications (1)

Application Number Title Priority Date Filing Date
IL181845A IL181845A0 (en) 2005-09-20 2007-03-11 Fan case reinforcement in a gas turbine jet engine

Country Status (11)

Country Link
EP (1) EP1841950A2 (en)
JP (1) JP2009515075A (en)
KR (1) KR20080034086A (en)
CN (1) CN101163863A (en)
AU (1) AU2005335919A1 (en)
BR (1) BRPI0517330A (en)
CA (1) CA2584641A1 (en)
IL (1) IL181845A0 (en)
RU (1) RU2406877C2 (en)
SG (1) SG165406A1 (en)
WO (1) WO2007035184A2 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8191254B2 (en) 2004-09-23 2012-06-05 Carlton Forge Works Method and apparatus for improving fan case containment and heat resistance in a gas turbine jet engine
FR2968364B1 (en) * 2010-12-01 2012-12-28 Snecma DUAL FLOW TURBOREACTOR BLOWER ELEMENT
US9200531B2 (en) * 2012-01-31 2015-12-01 United Technologies Corporation Fan case rub system, components, and their manufacture
US9249681B2 (en) 2012-01-31 2016-02-02 United Technologies Corporation Fan case rub system
US10669936B2 (en) 2013-03-13 2020-06-02 Raytheon Technologies Corporation Thermally conforming acoustic liner cartridge for a gas turbine engine
GB201313594D0 (en) 2013-07-30 2013-09-11 Composite Technology & Applic Ltd Fan Track Liner
FR3016187B1 (en) * 2014-01-09 2016-01-01 Snecma PROTECTION AGAINST THE FIRE OF A BLOWER HOUSING OF COMPOSITE MATERIAL
US10113447B2 (en) 2014-12-12 2018-10-30 Rolls-Royce Plc Fan casing arrangement for a gas turbine engine
EP3106289B1 (en) * 2015-06-17 2023-10-18 Raytheon Technologies Corporation Co-molded metallic fan case containment ring
GB201804568D0 (en) * 2018-03-22 2018-05-09 Rolls Royce Plc Fan track liner

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1085329A (en) * 1964-01-21
US3888602A (en) * 1974-06-05 1975-06-10 United Aircraft Corp Stress restraining ring for compressor rotors
FR2574476B1 (en) * 1984-12-06 1987-01-02 Snecma RETENTION HOUSING FOR TURBOJET BLOWER
GB2192238B (en) * 1986-07-02 1990-05-23 Rolls Royce Plc Gas turbine engine power turbine
DE3704197C1 (en) * 1987-02-11 1987-08-20 Mtu Muenchen Gmbh Removable burst protection ring
US5163809A (en) * 1991-04-29 1992-11-17 Pratt & Whitney Canada, Inc. Spiral wound containment ring
GB9922618D0 (en) * 1999-09-25 1999-11-24 Rolls Royce Plc A gas turbine engine blade containment assembly
EP1197570B1 (en) * 2000-10-13 2004-12-29 General Electric Company Nickel-base alloy and its use in forging and welding operations
FR2845436B1 (en) * 2002-10-02 2004-12-31 Snecma Moteurs DRUM FORMING PARTICULARLY A TURBOMACHINE ROTOR, COMPRESSOR AND TURBOMOTOR COMPRISING SUCH A DRUM

Also Published As

Publication number Publication date
JP2009515075A (en) 2009-04-09
EP1841950A2 (en) 2007-10-10
WO2007035184A8 (en) 2008-01-03
KR20080034086A (en) 2008-04-18
WO2007035184A3 (en) 2007-08-23
CN101163863A (en) 2008-04-16
AU2005335919A1 (en) 2007-04-05
RU2406877C2 (en) 2010-12-20
WO2007035184A2 (en) 2007-03-29
SG165406A1 (en) 2010-10-28
RU2007115082A (en) 2008-10-27
CA2584641A1 (en) 2007-03-29
BRPI0517330A (en) 2008-10-07

Similar Documents

Publication Publication Date Title
IL181844A0 (en) Fan case reinforcement in a gas turbine jet engine
IL181845A0 (en) Fan case reinforcement in a gas turbine jet engine
GB2427900B (en) Vane support in a gas turbine engine
GB2438696B (en) A gas turbine engine
GB2438858B (en) A sealing arrangement in a gas turbine engine
GB2427654B (en) Gas turbine engine
GB0608859D0 (en) A gas turbine engine
GB2431435B (en) Gas turbine engine assembly
GB0610271D0 (en) A gas turbine engine casing
GB0609460D0 (en) A swirler for use in a gas turbine engine
GB2475448B (en) Gas turbine exhaust diffuser
EP1799989A4 (en) Gas turbine intermediate structure and a gas turbine engine comprising the intermediate structure
GB0523469D0 (en) Blades for gas turbine engines
GB2422641B (en) Vane for a gas turbine engine
EG25643A (en) A combined wind and gas engine
GB0603285D0 (en) A gas turbine engine
GB2427659B (en) A turbofan gas turbine engine fan blade and a turbofan gas turbine engine fan rotor arrangement
GB0614518D0 (en) A fan blade for a gas turbine engine
EP1856398A4 (en) A bleed structure for a bleed passage in a gas turbine engine
GB0403941D0 (en) A gas turbine engine blade containment assembly
GB0415376D0 (en) A turbine engine arrangement
GB2427657B (en) A gas turbine engine
EP1841562A4 (en) Gas turbine fuel nozzle manufacturing
GB0413652D0 (en) Gas turbine engine structure
GB2440127B (en) A turbine blade for a gas turbine engine