BRPI0912082A2 - blindagem para rotor de turbomáquina e conjunto de propulsão - Google Patents

blindagem para rotor de turbomáquina e conjunto de propulsão

Info

Publication number
BRPI0912082A2
BRPI0912082A2 BRPI0912082A BRPI0912082A BRPI0912082A2 BR PI0912082 A2 BRPI0912082 A2 BR PI0912082A2 BR PI0912082 A BRPI0912082 A BR PI0912082A BR PI0912082 A BRPI0912082 A BR PI0912082A BR PI0912082 A2 BRPI0912082 A2 BR PI0912082A2
Authority
BR
Brazil
Prior art keywords
propulsion assembly
turbocharger rotor
rotor shield
shield
turbocharger
Prior art date
Application number
BRPI0912082A
Other languages
English (en)
Portuguese (pt)
Inventor
Guy Bernard Vauchel
PIERRE ANDRé MARCEL BAUDU
Original Assignee
Aircelle Sa
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 Aircelle Sa filed Critical Aircelle Sa
Publication of BRPI0912082A2 publication Critical patent/BRPI0912082A2/pt

Links

Classifications

    • 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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • 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
    • 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
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • 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
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • 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)
BRPI0912082A 2008-06-06 2009-03-30 blindagem para rotor de turbomáquina e conjunto de propulsão BRPI0912082A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0803156A FR2932233B1 (fr) 2008-06-06 2008-06-06 Carter pour rotor de turbomachine
PCT/FR2009/000366 WO2009147307A1 (fr) 2008-06-06 2009-03-30 Carter comprenant une ceinture peripherique pour rotor de turbomachine

Publications (1)

Publication Number Publication Date
BRPI0912082A2 true BRPI0912082A2 (pt) 2015-10-06

Family

ID=40184857

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0912082A BRPI0912082A2 (pt) 2008-06-06 2009-03-30 blindagem para rotor de turbomáquina e conjunto de propulsão

Country Status (8)

Country Link
US (1) US20110085897A1 (fr)
EP (1) EP2288798A1 (fr)
CN (1) CN102016265B (fr)
BR (1) BRPI0912082A2 (fr)
CA (1) CA2726024A1 (fr)
FR (1) FR2932233B1 (fr)
RU (1) RU2511960C2 (fr)
WO (1) WO2009147307A1 (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8206102B2 (en) * 2007-08-16 2012-06-26 United Technologies Corporation Attachment interface for a gas turbine engine composite duct structure
FR2963469B1 (fr) * 2010-07-27 2012-07-27 Aircelle Sa Panneau acoustique
FR2966508B1 (fr) * 2010-10-22 2015-04-03 Snecma Carter de soufflante de moteur aeronautique en materiau composite et procede pour sa fabrication
WO2013084308A1 (fr) * 2011-12-07 2013-06-13 株式会社Ihi Protubérance d'intallation et carter de soufflante
FR2995038B1 (fr) * 2012-08-30 2014-09-19 Snecma Carter de soufflante de turbine a gaz ayant une ceinture de fixation d'equipements
EP2733314B1 (fr) * 2012-11-15 2017-04-05 Safran Aero Boosters SA Brides radiales de fixation et de positionnement pour viroles de carter de turbomachine axiale
US10107202B2 (en) * 2014-11-26 2018-10-23 United Technologies Corporation Composite fan housing assembly of a turbofan engine and method of manufacture
FR3058343B1 (fr) * 2016-11-04 2020-02-28 Safran Aircraft Engines Systeme d'usinage ameliore d'une bride de fixation d'un carter de turbomachine d'aeronef
FR3074855A1 (fr) * 2017-12-11 2019-06-14 Airbus Operations Grille pour la formation d'un flux d'inversion d'un turboreacteur d'aeronef
CN108412644A (zh) * 2018-03-05 2018-08-17 安徽江淮汽车集团股份有限公司 具有减震功能的空气滤清器安装底座

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2548249A (en) * 1946-07-01 1951-04-10 Marman Products Co Inc Band clamp
US2997958A (en) * 1960-06-13 1961-08-29 Heinicke Pump Co Centrifugal pump
FR2514823B1 (fr) * 1981-10-16 1986-06-27 Poudres & Explosifs Ste Nale Dispositif de protection contre l'eclatement d'elements rotatifs d'une machine tournante
US4934899A (en) * 1981-12-21 1990-06-19 United Technologies Corporation Method for containing particles in a rotary machine
US4759521A (en) * 1984-04-18 1988-07-26 Aluma-Form, Inc. Flexible banding and instrument support system
US5226789A (en) * 1991-05-13 1993-07-13 General Electric Company Composite fan stator assembly
US5208569A (en) * 1992-06-03 1993-05-04 The United States Of America As Represented By The United States Department Of Energy Simplified flangeless unisex waveguide coupler assembly
DE4232385A1 (de) * 1992-09-26 1994-03-31 Asea Brown Boveri Gasturbine mit angeflanschtem Abgasgehäuse
DE4329014C1 (de) * 1993-08-28 1995-01-05 Mtu Muenchen Gmbh Rotorgehäuse, insbesondere Gehäuse für Turbotriebwerke
US20010048048A1 (en) * 1999-01-13 2001-12-06 Brian L Riedel Backside fitting attachment for nacelle acoustic panels
GB9922618D0 (en) * 1999-09-25 1999-11-24 Rolls Royce Plc A gas turbine engine blade containment assembly
GB0206136D0 (en) * 2002-03-15 2002-04-24 Rolls Royce Plc Improvements in or relating to cellular materials
US6824471B2 (en) * 2002-09-06 2004-11-30 S. A. Armstrong Limited Motor and pump shaft connecting assembly with shaft locating jack ring
US6899574B1 (en) * 2003-08-28 2005-05-31 Garmin Ltd. Transducer bracket
GB2406627B (en) * 2003-10-03 2008-05-07 Rolls Royce Plc Connecting arrangement
FR2887931B1 (fr) * 2005-06-29 2007-08-17 Snecma Dispositif de support et de logement de servitudes dans un turboreacteur a double flux
DE102005033860A1 (de) * 2005-07-13 2007-01-25 Rolls-Royce Deutschland Ltd. & Co. Kg Schutzring für das Fangehäuse eines Gasturbinentriebwerks
FR2903732B1 (fr) * 2006-07-12 2008-09-12 Airbus France Sas Entree d'air pour turbomoteur d'aeronef.
US8475895B2 (en) * 2006-11-21 2013-07-02 General Electric Company Articles comprising composite structures having mounting flanges
US8021102B2 (en) * 2006-11-30 2011-09-20 General Electric Company Composite fan containment case and methods of fabricating the same

Also Published As

Publication number Publication date
EP2288798A1 (fr) 2011-03-02
WO2009147307A1 (fr) 2009-12-10
CN102016265B (zh) 2014-06-18
CN102016265A (zh) 2011-04-13
FR2932233B1 (fr) 2012-09-28
FR2932233A1 (fr) 2009-12-11
RU2010152292A (ru) 2012-07-20
US20110085897A1 (en) 2011-04-14
CA2726024A1 (fr) 2009-12-10
RU2511960C2 (ru) 2014-04-10

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]