SG155956A1 - Fan case reinforcement in a gas turbine jet engine - Google Patents

Fan case reinforcement in a gas turbine jet engine

Info

Publication number
SG155956A1
SG155956A1 SG200906312-4A SG2009063124A SG155956A1 SG 155956 A1 SG155956 A1 SG 155956A1 SG 2009063124 A SG2009063124 A SG 2009063124A SG 155956 A1 SG155956 A1 SG 155956A1
Authority
SG
Singapore
Prior art keywords
fan case
fan
ring
containment
gas turbine
Prior art date
Application number
SG200906312-4A
Other languages
English (en)
Inventor
James L Cardarella Jr
Original Assignee
Carlton Forge Works
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 Carlton Forge Works filed Critical Carlton Forge Works
Publication of SG155956A1 publication Critical patent/SG155956A1/en

Links

Classifications

    • 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
    • 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
    • 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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00—Pumping installations or systems
    • F04D25/16—Combinations of two or more pumps ; Producing two or more separate gas flows
    • 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
    • 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
    • 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
    • F05D2300/433—Polyamides, e.g. NYLON
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • Y10T29/49863—Assembling or joining with prestressing of part
    • Y10T29/49865—Assembling or joining with prestressing of part by temperature differential [e.g., shrink fit]

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)
SG200906312-4A 2004-09-23 2005-09-20 Fan case reinforcement in a gas turbine jet engine SG155956A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/947,923 US8191254B2 (en) 2004-09-23 2004-09-23 Method and apparatus for improving fan case containment and heat resistance in a gas turbine jet engine

Publications (1)

Publication Number Publication Date
SG155956A1 true SG155956A1 (en) 2009-10-29

Family

ID=36072433

Family Applications (1)

Application Number Title Priority Date Filing Date
SG200906312-4A SG155956A1 (en) 2004-09-23 2005-09-20 Fan case reinforcement in a gas turbine jet engine

Country Status (17)

Country Link
US (3) US8191254B2 (ru)
EP (1) EP1809862A2 (ru)
JP (1) JP2008514850A (ru)
KR (1) KR20070057893A (ru)
CN (1) CN101107424A (ru)
AU (1) AU2005333173A1 (ru)
BR (1) BRPI0517368A (ru)
CA (1) CA2579887A1 (ru)
IL (1) IL181844A0 (ru)
NO (2) NO20071540L (ru)
NZ (2) NZ589158A (ru)
RU (1) RU2398135C2 (ru)
SA (1) SA05260302B1 (ru)
SG (1) SG155956A1 (ru)
TW (1) TW200610874A (ru)
WO (1) WO2006137875A2 (ru)
ZA (1) ZA200702030B (ru)

Families Citing this family (44)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2006144869A (ru) * 2004-05-17 2008-06-27 Л. Джеймс Мл. КАРДАРЕЛЛА (US) Упрочнение кожуха турбины в газотурбинном реактивном двигателе
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
FR2903734B1 (fr) * 2006-07-12 2008-09-12 Airbus France Sas Turbomoteur pour aeronef.
US7914256B2 (en) * 2007-04-17 2011-03-29 General Electric Company Articles made from composite materials having toughened and untoughened regions
FR2920137B1 (fr) * 2007-08-20 2009-09-18 Aircelle Sa Fixation d'une structure d'une nacelle de turboreacteur par bride couteau/gorge renforcee
TWI467087B (zh) * 2008-03-25 2015-01-01 Amicable Inv S Llc 與空氣或氣體交互作用的設備及其噴射發動機
GB2459646B (en) * 2008-04-28 2011-03-30 Rolls Royce Plc A fan assembly
US8672609B2 (en) 2009-08-31 2014-03-18 United Technologies Corporation Composite fan containment case assembly
US9114882B2 (en) 2010-10-26 2015-08-25 United Technologies Corporation Fan case and mount ring snap fit assembly
US20110126508A1 (en) * 2009-12-01 2011-06-02 Edward Claude Rice Fan case having penetration resistant blanket
US9062565B2 (en) * 2009-12-31 2015-06-23 Rolls-Royce Corporation Gas turbine engine containment device
US8661678B1 (en) * 2010-02-16 2014-03-04 Uremet Corporation Combination roller coaster wheel
US8753075B2 (en) * 2010-07-20 2014-06-17 Rolls-Royce Corporation Fan case assembly and method
US8511971B2 (en) * 2010-07-23 2013-08-20 Hamilton Sundstrand Corporation One-piece compressor and turbine containment system
US8858156B2 (en) * 2010-08-12 2014-10-14 General Electric Company Fragment containment assembly and method for adding a fragment containment assembly to a turbine
US8932002B2 (en) * 2010-12-03 2015-01-13 Hamilton Sundstrand Corporation Air turbine starter
GB201103583D0 (en) * 2011-03-03 2011-04-13 Rolls Royce Plc Fan casing for a turbofan engine
US8887486B2 (en) * 2011-10-24 2014-11-18 Hamilton Sundstrand Corporation Ram air fan inlet housing
US20130156584A1 (en) * 2011-12-16 2013-06-20 Carney R. Anderson Compressor rotor with internal stiffening ring of distinct material
GB2501918B (en) 2012-05-11 2014-06-18 Rolls Royce Plc Casing
US9322337B2 (en) 2012-06-20 2016-04-26 United Technologies Corporation Aerodynamic intercompressor bleed ports
FR2997726B1 (fr) * 2012-11-05 2018-03-02 Safran Aircraft Engines Carter de turbomachine
US10024191B2 (en) 2013-03-11 2018-07-17 Rolls-Royce Corporation Fan track liner designed to yield next to fan case hook
JP6118721B2 (ja) * 2013-12-20 2017-04-19 株式会社Ihi ファンケース及びファンケースの製造方法
FR3016187B1 (fr) * 2014-01-09 2016-01-01 Snecma Protection contre le feu d'un carter de soufflante en materiau composite
EP2930316B1 (fr) * 2014-04-10 2021-01-27 Safran Aero Boosters SA Carter composite de compresseur de turbomachine axiale
US10012389B2 (en) * 2014-05-08 2018-07-03 United Technologies Corporation Case with integral heat shielding
FR3031469B1 (fr) * 2015-01-14 2017-09-22 Snecma Carter en materiau composite a matrice organique auto-raidi
US9726036B2 (en) * 2015-04-14 2017-08-08 Honeywell International Inc. Bi-metallic containment ring
US10458433B2 (en) * 2015-06-17 2019-10-29 United Technologies Corporation Co-molded metallic fan case containment ring
US10704511B2 (en) 2016-08-15 2020-07-07 Denso International America, Inc. Clamped joint device
CN107829980B (zh) * 2016-09-16 2021-05-25 通用电气公司 沿周向变化厚度的复合风扇壳
RU2652857C1 (ru) * 2017-01-24 2018-05-03 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Способ защиты корпуса лопаточных машин и устройство, реализующее способ
US10677260B2 (en) * 2017-02-21 2020-06-09 General Electric Company Turbine engine and method of manufacturing
US10704414B2 (en) 2017-03-10 2020-07-07 General Electric Company Airfoil containment structure including a notched and tapered inner shell
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
US10436061B2 (en) 2017-04-13 2019-10-08 General Electric Company Tapered composite backsheet for use in a turbine engine containment assembly
US10934943B2 (en) * 2017-04-27 2021-03-02 General Electric Company Compressor apparatus with bleed slot and supplemental flange
US11261753B2 (en) 2017-12-06 2022-03-01 General Electric Company Method and device for connecting fan rotor to low pressure turbine rotor
DE102018113396A1 (de) * 2018-06-06 2019-12-12 Man Energy Solutions Se Berstschutzvorrichtung für eine Strömungsmaschine
US11242866B2 (en) 2018-08-01 2022-02-08 General Electric Company Casing having a non-axisymmetric composite wall
US11499448B2 (en) 2019-05-29 2022-11-15 General Electric Company Composite fan containment case
US11846199B2 (en) * 2022-01-28 2023-12-19 Hamilton Sundstrand Corporation Rotor containment structure

Family Cites Families (62)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3085398A (en) * 1961-01-10 1963-04-16 Gen Electric Variable-clearance shroud structure for gas turbine engines
GB1085329A (ru) * 1964-01-21
US3859008A (en) * 1971-07-06 1975-01-07 Andritz Ag Maschf Pump with offset inflow and discharge chambers
US3719365A (en) * 1971-10-18 1973-03-06 Gen Motors Corp Seal structure
BE792224A (fr) * 1971-12-01 1973-03-30 Penny Robert N Element composite long ayant un coefficient de dilatation lineaire effectif predetermine
US3798899A (en) * 1971-12-29 1974-03-26 Power Technology Corp Gas turbine engine
JPS5548157Y2 (ru) * 1974-05-31 1980-11-11
US3888602A (en) * 1974-06-05 1975-06-10 United Aircraft Corp Stress restraining ring for compressor rotors
US3928963A (en) * 1974-11-04 1975-12-30 Gen Motors Corp Cast in place gas turbine containment ring and method of manufacture
FR2298759A1 (fr) 1975-01-23 1976-08-20 Mtu Muenchen Gmbh Dispositif de protection contre l'eclatement de rotors a haute vitesse
GB1501916A (en) * 1975-06-20 1978-02-22 Rolls Royce Matching thermal expansions of components of turbo-machines
SU926369A1 (ru) 1978-10-19 1982-05-07 Предприятие П/Я Р-6131 Кожух вентил тора
GB2087979B (en) * 1980-11-22 1984-02-22 Rolls Royce Gas turbine engine blade tip seal
US4513567A (en) * 1981-11-02 1985-04-30 United Technologies Corporation Gas turbine engine active clearance control
US4452563A (en) * 1981-12-21 1984-06-05 United Technologies Corporation Containment structure
US4484856A (en) * 1981-12-21 1984-11-27 United Technologies Corporation Containment structure
US4934899A (en) * 1981-12-21 1990-06-19 United Technologies Corporation Method for containing particles in a rotary machine
US4417848A (en) * 1982-02-01 1983-11-29 United Technologies Corporation Containment shell for a fan section of a gas turbine engine
FR2574476B1 (fr) * 1984-12-06 1987-01-02 Snecma Carter de retention pour soufflante de turboreacteur
GB2192238B (en) 1986-07-02 1990-05-23 Rolls Royce Plc Gas turbine engine power turbine
FR2610673B1 (fr) * 1987-02-05 1991-03-15 Snecma Turboreacteur multiflux a couronne externe de redresseur de soufflante frettee sur le carter
DE3704197C1 (de) * 1987-02-11 1987-08-20 Mtu Muenchen Gmbh Demontierbarer Berstschutzring
US4734007A (en) * 1987-03-03 1988-03-29 Rolls-Royce Plc Fan casing and fan blade loading/unloading
SU1638371A1 (ru) 1988-09-22 1991-03-30 Предприятие П/Я Р-6678 Кожух компрессора
SU1590683A1 (ru) 1988-12-07 1990-09-07 Ярославский моторный завод Кожух вентил тора
SU1758292A1 (ru) 1989-08-07 1992-08-30 Сумское Машиностроительное Научно-Производственное Объединение Им.Фрунзе Корпус турбокомпрессора
US5018942A (en) * 1989-09-08 1991-05-28 General Electric Company Mechanical blade tip clearance control apparatus for a gas turbine engine
US5163809A (en) * 1991-04-29 1992-11-17 Pratt & Whitney Canada, Inc. Spiral wound containment ring
US5154575A (en) * 1991-07-01 1992-10-13 United Technologies Corporation Thermal blade tip clearance control for gas turbine engines
FR2683851A1 (fr) * 1991-11-20 1993-05-21 Snecma Turbomachine equipee de moyens facilitant le reglage des jeux du stator entree stator et rotor.
US5267828A (en) * 1992-11-13 1993-12-07 General Electric Company Removable fan shroud panel
US5332358A (en) * 1993-03-01 1994-07-26 General Electric Company Uncoupled seal support assembly
US5336044A (en) * 1993-08-06 1994-08-09 General Electric Company Blade containment system and method
US5403148A (en) * 1993-09-07 1995-04-04 General Electric Company Ballistic barrier for turbomachinery blade containment
US5724816A (en) * 1996-04-10 1998-03-10 General Electric Company Combustor for a gas turbine with cooling structure
US5823739A (en) * 1996-07-03 1998-10-20 United Technologies Corporation Containment case for a turbine engine
US6637186B1 (en) * 1997-11-11 2003-10-28 United Technologies Corporation Fan case liner
RU2172871C2 (ru) 1998-04-23 2001-08-27 Акционерное общество "Сумское машиностроительное научно-производственное объединение им. М.В. Фрунзе" Корпус турбокомпрессора, преимущественно для сжатия сероводородных газов
US6053696A (en) * 1998-05-29 2000-04-25 Pratt & Whitney Canada Inc. Impact resistant composite shell for gas turbine engine fan case
US6231301B1 (en) 1998-12-10 2001-05-15 United Technologies Corporation Casing treatment for a fluid compressor
US6149380A (en) * 1999-02-04 2000-11-21 Pratt & Whitney Canada Corp. Hardwall fan case with structured bumper
RU2171382C2 (ru) 1999-07-21 2001-07-27 Открытое акционерное общество "Авиадвигатель" Устройство для удерживания обломков ротора турбомашины
GB9922618D0 (en) 1999-09-25 1999-11-24 Rolls Royce Plc A gas turbine engine blade containment assembly
US6290455B1 (en) * 1999-12-03 2001-09-18 General Electric Company Contoured hardwall containment
US6368054B1 (en) * 1999-12-14 2002-04-09 Pratt & Whitney Canada Corp. Split ring for tip clearance control
DE50012259D1 (de) * 2000-01-11 2006-04-27 Sulzer Pumpen Ag Winterthur Strömungsmaschine für ein Fluid mit einem radialen Dichtspalt zwischen Statorteilen und einem Rotor
GB0008193D0 (en) * 2000-04-05 2000-05-24 Rolls Royce Plc A gas turbine engine blade containment assembly
US6382905B1 (en) * 2000-04-28 2002-05-07 General Electric Company Fan casing liner support
DE60108037T2 (de) 2000-10-13 2005-09-15 General Electric Co. Legierung auf Nickel-Basis und deren Verwendung bei Schmiede- oder Schweissvorgängen
US6719242B2 (en) * 2000-12-01 2004-04-13 Sonoco Development, Inc. Composite core
US6896483B2 (en) * 2001-07-02 2005-05-24 Allison Advanced Development Company Blade track assembly
US6514041B1 (en) * 2001-09-12 2003-02-04 Alstom (Switzerland) Ltd Carrier for guide vane and heat shield segment
US6487491B1 (en) * 2001-11-21 2002-11-26 United Technologies Corporation System and method of controlling clearance between turbine engine blades and case based on engine components thermal growth model
FR2845436B1 (fr) * 2002-10-02 2004-12-31 Snecma Moteurs Tambour formant en particulier un rotor de turbomachine, compresseur et turbomoteur comprenant un tel tambour
RU2232276C1 (ru) 2003-04-22 2004-07-10 Открытое акционерное общество "Теплоэнергосервис" Турбомашина
US20040219011A1 (en) 2003-05-02 2004-11-04 General Electric Company High pressure turbine elastic clearance control system and method
US6848885B1 (en) * 2003-08-18 2005-02-01 General Electric Company Methods and apparatus for fabricating gas turbine engines
GB2407343B (en) * 2003-10-22 2006-04-19 Rolls Royce Plc An acoustic liner for a gas turbine engine casing
RU2006144869A (ru) 2004-05-17 2008-06-27 Л. Джеймс Мл. КАРДАРЕЛЛА (US) Упрочнение кожуха турбины в газотурбинном реактивном двигателе
US20050252000A1 (en) 2004-05-17 2005-11-17 Cardarella Louis J Jr Method and system for improved blade tip clearance in a gas turbine jet engine
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
EP1841950A2 (en) 2005-09-20 2007-10-10 L. James Cardarella Jr. Fan case reinforcement in a gas turbine jet engine

Also Published As

Publication number Publication date
US8191254B2 (en) 2012-06-05
US8454298B2 (en) 2013-06-04
NO20071540L (no) 2007-04-23
CN101107424A (zh) 2008-01-16
US20080199301A1 (en) 2008-08-21
NZ554496A (en) 2010-12-24
WO2006137875A3 (en) 2007-08-23
KR20070057893A (ko) 2007-06-07
JP2008514850A (ja) 2008-05-08
WO2006137875A2 (en) 2006-12-28
CA2579887A1 (en) 2006-12-28
NZ589158A (en) 2012-06-29
IL181844A0 (en) 2008-06-05
SA05260302B1 (ar) 2010-12-01
RU2007115081A (ru) 2008-10-27
NO20071539L (no) 2007-04-23
US20080232951A1 (en) 2008-09-25
US20060059889A1 (en) 2006-03-23
TW200610874A (en) 2006-04-01
EP1809862A2 (en) 2007-07-25
US8317456B2 (en) 2012-11-27
AU2005333173A1 (en) 2006-12-28
BRPI0517368A (pt) 2008-10-07
WO2006137875A9 (en) 2007-05-24
RU2398135C2 (ru) 2010-08-27
ZA200702030B (en) 2008-09-25

Similar Documents

Publication Publication Date Title
SG155956A1 (en) Fan case reinforcement in a gas turbine jet engine
SG165406A1 (en) Fan case reinforcement in a gas turbine jet engine
EP2149679A3 (en) A fan casing for a gas turbine engine
WO2007114698A3 (en) Wind turbine with slender blade
RU2006112535A (ru) Деталь для защиты передней кромки пера лопатки
WO2008047238A3 (en) Vertical axis wind turbine system
SG130089A1 (en) Turbine blades
US20110179805A1 (en) Rotor containment structure for gas turbine engine
US10392946B2 (en) Turbine blade with reinforced platform for composite material construction
Ford et al. Development of single crystal alloys for specific engine applications
EP1746252A3 (en) Structural strut and shroud element
CN204783125U (zh) 一种双层金属衬套
WO2014074370A3 (en) Turbine airfoil abradable coating system and corresponding turbine blades
CN205225826U (zh) 离心风叶
US20140199164A1 (en) Nickel-based alloy and turbine component having nickel-based alloy
Boulbin et al. Turbine blade forces due to partial admission
CN206037018U (zh) 生物质颗粒燃料炉
Mao et al. Dynamics of helical vortices behind a wind turbine in a stratified atmosphere
CN206668595U (zh) 一种驻车加热器风叶结构
Petit et al. Microstructural study of niobium silicide based alloys
Mishra Development of High Temperature Materials for Aero Engine Hot End Components: An Overview
CN202646150U (zh) 风机
Pytlinski et al. Variable geometry Darrieus wind machine
Brody et al. Hunters vs farmers [The other side of Eden: hunters, farmers and the shaping of the world]
Felten et al. Large Eddy simulation of parallel blade-vortex interaction