BR112015003808A2 - casing apparatus for a gas turbine engine and propeller apparatus for a gas turbine engine - Google Patents

casing apparatus for a gas turbine engine and propeller apparatus for a gas turbine engine

Info

Publication number
BR112015003808A2
BR112015003808A2 BR112015003808A BR112015003808A BR112015003808A2 BR 112015003808 A2 BR112015003808 A2 BR 112015003808A2 BR 112015003808 A BR112015003808 A BR 112015003808A BR 112015003808 A BR112015003808 A BR 112015003808A BR 112015003808 A2 BR112015003808 A2 BR 112015003808A2
Authority
BR
Brazil
Prior art keywords
gas turbine
turbine engine
propeller
casing
casing apparatus
Prior art date
Application number
BR112015003808A
Other languages
Portuguese (pt)
Inventor
Thomas Scorse Daniel
Alexander Pauley Gerald
Edward Eriksen Michael
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of BR112015003808A2 publication Critical patent/BR112015003808A2/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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
BR112015003808A 2012-09-06 2013-08-01 casing apparatus for a gas turbine engine and propeller apparatus for a gas turbine engine BR112015003808A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/604,722 US20140064938A1 (en) 2012-09-06 2012-09-06 Rub tolerant fan case
PCT/US2013/053190 WO2014039188A1 (en) 2012-09-06 2013-08-01 Rub tolerant fan case

Publications (1)

Publication Number Publication Date
BR112015003808A2 true BR112015003808A2 (en) 2018-04-10

Family

ID=49001051

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015003808A BR112015003808A2 (en) 2012-09-06 2013-08-01 casing apparatus for a gas turbine engine and propeller apparatus for a gas turbine engine

Country Status (7)

Country Link
US (1) US20140064938A1 (en)
EP (1) EP2912281A1 (en)
JP (1) JP6184036B2 (en)
CN (1) CN104603400B (en)
BR (1) BR112015003808A2 (en)
CA (1) CA2883295A1 (en)
WO (1) WO2014039188A1 (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016114888A1 (en) * 2015-01-13 2016-07-21 General Electric Company A composite airfoil with fuse architecture
CA2955646A1 (en) 2016-01-19 2017-07-19 Pratt & Whitney Canada Corp. Gas turbine engine rotor blade casing
US10648511B2 (en) 2016-07-15 2020-05-12 Ihi Corporation Seal structure and turbocharger
US10724403B2 (en) 2018-07-16 2020-07-28 Raytheon Technologies Corporation Fan case assembly for gas turbine engine
JP6990639B2 (en) * 2018-09-26 2022-01-12 本田技研工業株式会社 Turbofan engine
US20200308986A1 (en) * 2019-03-26 2020-10-01 Hamilton Sundstrand Corporation Turbine containment arrangement
US11499448B2 (en) * 2019-05-29 2022-11-15 General Electric Company Composite fan containment case
US20240011410A1 (en) * 2022-07-05 2024-01-11 General Electric Company Variable flowpath casings for blade tip clearance control
US11808157B1 (en) 2022-07-13 2023-11-07 General Electric Company Variable flowpath casings for blade tip clearance control

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4490092A (en) * 1981-12-21 1984-12-25 United Technologies Corporation Containment structure
US4534698A (en) * 1983-04-25 1985-08-13 General Electric Company Blade containment structure
CA2042198A1 (en) * 1990-06-18 1991-12-19 Stephen C. Mitchell Projectile shield
US5545007A (en) * 1994-11-25 1996-08-13 United Technologies Corp. Engine blade clearance control system with piezoelectric actuator
US6619913B2 (en) * 2002-02-15 2003-09-16 General Electric Company Fan casing acoustic treatment
GB2407343B (en) * 2003-10-22 2006-04-19 Rolls Royce Plc An acoustic liner for a gas turbine engine casing
US7094033B2 (en) * 2004-01-21 2006-08-22 General Electric Company Methods and apparatus for assembling gas turbine engines
GB0501284D0 (en) * 2005-01-21 2005-03-02 Rolls Royce Plc Aerofoil containment structure
US7909335B2 (en) * 2008-02-04 2011-03-22 General Electric Company Retractable compliant plate seals
US8333558B2 (en) * 2008-03-05 2012-12-18 General Electric Company Containment cases and method of manufacture
GB0914523D0 (en) * 2009-08-20 2009-09-30 Rolls Royce Plc A turbomachine casing assembly
GB0914679D0 (en) * 2009-08-24 2009-09-30 Rolls Royce Plc Adjustable fan case liner and mounting method
GB201103682D0 (en) * 2011-03-04 2011-04-20 Rolls Royce Plc A turbomachine casing assembly
CA2875928C (en) * 2012-06-21 2017-01-17 Kawasaki Jukogyo Kabushiki Kaisha Fan case for aircraft engine

Also Published As

Publication number Publication date
CN104603400A (en) 2015-05-06
CA2883295A1 (en) 2014-03-13
JP2015531444A (en) 2015-11-02
EP2912281A1 (en) 2015-09-02
CN104603400B (en) 2017-03-08
WO2014039188A1 (en) 2014-03-13
US20140064938A1 (en) 2014-03-06
JP6184036B2 (en) 2017-08-23

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 6A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2525 DE 28-05-2019 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.