BRPI0912018A2 - órgão de travamento para dispositivo de fixação de setores de anel sobre um cárter de turbomáquina de aeronave, dispositivo de fixação de setores de anel sobre um cárter de turbomáquina de aeronave,turbina de turbomáquina de aeronave, e turbomáquina de aeronave. - Google Patents

órgão de travamento para dispositivo de fixação de setores de anel sobre um cárter de turbomáquina de aeronave, dispositivo de fixação de setores de anel sobre um cárter de turbomáquina de aeronave,turbina de turbomáquina de aeronave, e turbomáquina de aeronave.

Info

Publication number
BRPI0912018A2
BRPI0912018A2 BRPI0912018A BRPI0912018A BRPI0912018A2 BR PI0912018 A2 BRPI0912018 A2 BR PI0912018A2 BR PI0912018 A BRPI0912018 A BR PI0912018A BR PI0912018 A BRPI0912018 A BR PI0912018A BR PI0912018 A2 BRPI0912018 A2 BR PI0912018A2
Authority
BR
Brazil
Prior art keywords
aircraft
turbomachinery
ring sector
turbomachine
locking member
Prior art date
Application number
BRPI0912018A
Other languages
English (en)
Inventor
Alain Dominique Gendraud
Original Assignee
Snecma
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 Snecma filed Critical Snecma
Publication of BRPI0912018A2 publication Critical patent/BRPI0912018A2/pt
Publication of BRPI0912018B1 publication Critical patent/BRPI0912018B1/pt

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
    • 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
    • F01D25/246—Fastening of diaphragms or stator-rings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B2/00—Friction-grip releasable fastenings
    • F16B2/20—Clips, i.e. with gripping action effected solely by the inherent resistance to deformation of the material of the fastening
    • F16B2/22—Clips, i.e. with gripping action effected solely by the inherent resistance to deformation of the material of the fastening of resilient material, e.g. rubbery material
    • F16B2/24—Clips, i.e. with gripping action effected solely by the inherent resistance to deformation of the material of the fastening of resilient material, e.g. rubbery material of metal
    • F16B2/241—Clips, i.e. with gripping action effected solely by the inherent resistance to deformation of the material of the fastening of resilient material, e.g. rubbery material of metal of sheet metal
    • F16B2/245—Clips, i.e. with gripping action effected solely by the inherent resistance to deformation of the material of the fastening of resilient material, e.g. rubbery material of metal of sheet metal external, i.e. with contracting action
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/70—Disassembly methods
    • 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
    • Y10T29/49323—Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Clamps And Clips (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BRPI0912018-1A 2008-05-16 2009-05-14 órgão de travamento para dispositivo de fixação de setores de anel sobre um cárter de turbomáquina de aeronave, dispositivo de fixação de setores de anel sobre um cárter de turbomáquina de aeronave, turbina de turbomáquina e turbomáquina de aeronave BRPI0912018B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0853182A FR2931196B1 (fr) 2008-05-16 2008-05-16 Organe de verrouillage de secteurs d'anneau sur un carter de turbomachine, comprenant des passages radiaux permettant sa prehension
FR0853182 2008-05-16
PCT/EP2009/055811 WO2009138443A1 (fr) 2008-05-16 2009-05-14 Organe de verrouillage de secteurs d'anneau sur un carter de turbomachine, comprenant des passages radiaux permettant sa prehension

Publications (2)

Publication Number Publication Date
BRPI0912018A2 true BRPI0912018A2 (pt) 2015-10-06
BRPI0912018B1 BRPI0912018B1 (pt) 2019-11-26

Family

ID=39963086

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0912018-1A BRPI0912018B1 (pt) 2008-05-16 2009-05-14 órgão de travamento para dispositivo de fixação de setores de anel sobre um cárter de turbomáquina de aeronave, dispositivo de fixação de setores de anel sobre um cárter de turbomáquina de aeronave, turbina de turbomáquina e turbomáquina de aeronave

Country Status (9)

Country Link
US (1) US8721277B2 (pt)
EP (1) EP2297431B1 (pt)
JP (1) JP5443476B2 (pt)
CN (1) CN102027199B (pt)
BR (1) BRPI0912018B1 (pt)
CA (1) CA2724256C (pt)
FR (1) FR2931196B1 (pt)
RU (1) RU2498088C2 (pt)
WO (1) WO2009138443A1 (pt)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2931197B1 (fr) * 2008-05-16 2010-06-18 Snecma Organe de verrouillage de secteurs d'anneau sur un carter de turbomachine, comprenant des passages axiaux pour sa prehension
FR2973069B1 (fr) * 2011-03-24 2014-09-12 Snecma Anneau de carter de stator de turbomachine
FR3009739B1 (fr) * 2013-08-13 2015-09-11 Snecma Amelioration pour le verrouillage de pieces de support d'aubage
FR3009740B1 (fr) 2013-08-13 2017-12-15 Snecma Amelioration pour le verrouillage de pieces de support d'aubage
EP2846001B1 (de) * 2013-09-06 2023-01-11 MTU Aero Engines AG Montage- und Demontageverfahren eines Gasturbinenrotors und zugehörige Werkzeug
US10100659B2 (en) * 2014-12-16 2018-10-16 Rolls-Royce North American Technologies Inc. Hanger system for a turbine engine component
US9932901B2 (en) 2015-05-11 2018-04-03 General Electric Company Shroud retention system with retention springs
EP3464068B1 (en) * 2016-06-06 2023-08-02 Airbus Canada Limited Partnership Adjustment mechanism for a hoist
DE102017104981B4 (de) * 2017-03-09 2021-01-28 Schaeffler Technologies AG & Co. KG Befestigungsmittel eines Aktuators einer Nockenwellenverstellvorrichtung
FR3105996B1 (fr) 2020-01-08 2021-11-26 Safran Aircraft Engines Organe de verrouillage destiné à l’assemblage d’une première pièce et d’une seconde pièce d’une turbomachine

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1139295A (en) * 1965-07-17 1969-01-08 Colt Ventilation & Heating Ltd Improvements in or relating to fastenings
US5197853A (en) * 1991-08-28 1993-03-30 General Electric Company Airtight shroud support rail and method for assembling in turbine engine
US5669757A (en) * 1995-11-30 1997-09-23 General Electric Company Turbine nozzle retainer assembly
US5970716A (en) * 1997-10-02 1999-10-26 General Electric Company Apparatus for retaining centerbody between adjacent domes of multiple annular combustor employing interference and clamping fits
FR2780443B1 (fr) * 1998-06-25 2000-08-04 Snecma Anneau de stator de turbine haute pression d'une turbomachine
US6233822B1 (en) * 1998-12-22 2001-05-22 General Electric Company Repair of high pressure turbine shrouds
US6412149B1 (en) * 1999-08-25 2002-07-02 General Electric Company C-clip for shroud assembly
US6435820B1 (en) * 1999-08-25 2002-08-20 General Electric Company Shroud assembly having C-clip retainer
FR2800797B1 (fr) * 1999-11-10 2001-12-07 Snecma Assemblage d'un anneau bordant une turbine a la structure de turbine
FR2815668B1 (fr) * 2000-10-19 2003-01-10 Snecma Moteurs Agencement de liaison d'un anneau de stator de turbine a une entretoise de support
WO2003004834A1 (de) * 2001-07-03 2003-01-16 Abb Turbo Systems Ag Sicherungssystem für laufschaufeln axial durchströmter turbomaschinen
FR2852053B1 (fr) * 2003-03-06 2007-12-28 Snecma Moteurs Turbine haute pression pour turbomachine
FR2887920B1 (fr) * 2005-06-29 2010-09-10 Snecma Dispositif de fixation de secteurs d'anneau sur un carter de turbine
FR2921410B1 (fr) * 2007-09-24 2010-03-12 Snecma Organe de verrouillage de secteurs d'anneau sur un carter de turbomachine, comprenant des moyens permettant sa prehension
FR2922589B1 (fr) * 2007-10-22 2009-12-04 Snecma Controle du jeu en sommet d'aubes dans une turbine haute-pression de turbomachine
FR2923527B1 (fr) * 2007-11-13 2013-12-27 Snecma Etage de turbine ou de compresseur, en particulier de turbomachine

Also Published As

Publication number Publication date
EP2297431A1 (fr) 2011-03-23
EP2297431B1 (fr) 2016-06-15
CN102027199B (zh) 2013-08-28
FR2931196B1 (fr) 2010-06-18
CA2724256C (fr) 2016-08-30
WO2009138443A1 (fr) 2009-11-19
RU2498088C2 (ru) 2013-11-10
JP2011521143A (ja) 2011-07-21
FR2931196A1 (fr) 2009-11-20
JP5443476B2 (ja) 2014-03-19
BRPI0912018B1 (pt) 2019-11-26
US20110121150A1 (en) 2011-05-26
CA2724256A1 (fr) 2009-11-19
CN102027199A (zh) 2011-04-20
US8721277B2 (en) 2014-05-13
RU2010151721A (ru) 2012-06-27

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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]
B06T Formal requirements before examination [chapter 6.20 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 10 (DEZ) ANOS CONTADOS A PARTIR DE 26/11/2019, OBSERVADAS AS CONDICOES LEGAIS. (CO) 10 (DEZ) ANOS CONTADOS A PARTIR DE 26/11/2019, OBSERVADAS AS CONDICOES LEGAIS