BRPI0922104A2 - flange anular radical de um elemento de rotor ou de estator de uma turbina para turbomáquina, turbina de baixa pressão para tubomáquina, e, turbomáquina, tal como um turborreator ou um turbopropulsor. - Google Patents

flange anular radical de um elemento de rotor ou de estator de uma turbina para turbomáquina, turbina de baixa pressão para tubomáquina, e, turbomáquina, tal como um turborreator ou um turbopropulsor.

Info

Publication number
BRPI0922104A2
BRPI0922104A2 BRPI0922104A BRPI0922104A BRPI0922104A2 BR PI0922104 A2 BRPI0922104 A2 BR PI0922104A2 BR PI0922104 A BRPI0922104 A BR PI0922104A BR PI0922104 A BRPI0922104 A BR PI0922104A BR PI0922104 A2 BRPI0922104 A2 BR PI0922104A2
Authority
BR
Brazil
Prior art keywords
turbocharger
turbocharger turbine
turborreator
turboprop
radical
Prior art date
Application number
BRPI0922104A
Other languages
English (en)
Inventor
Olivier Belmonte
Stevan Le Goff
Thomas Langevin
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 BRPI0922104A2 publication Critical patent/BRPI0922104A2/pt
Publication of BRPI0922104B1 publication Critical patent/BRPI0922104B1/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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
    • F01D5/066—Connecting means for joining rotor-discs or rotor-elements together, e.g. by a central bolt, by clamps
    • 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
    • F01D25/243—Flange connections; Bolting arrangements
    • 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
    • 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
    • F05D2260/00—Function
    • F05D2260/30—Retaining components in desired mutual position
    • F05D2260/31—Retaining bolts or nuts

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
  • Connection Of Plates (AREA)
BRPI0922104A 2008-11-07 2009-09-29 flange anular radical de um elemento de rotor ou de estator de uma turbina para turbomáquina, turbina de baixa pressão para tubomáquina, e, turbomáquina, tal como um turborreator ou um turbopropulsor. BRPI0922104B1 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0806241A FR2938292B1 (fr) 2008-11-07 2008-11-07 Bride annulaire de fixation d'un element de rotor ou de stator dans une turbomachine
PCT/FR2009/001164 WO2010052379A1 (fr) 2008-11-07 2009-09-29 Bride annulaire de fixation d'un element de rotor ou de stator dans une turbomachine

Publications (2)

Publication Number Publication Date
BRPI0922104A2 true BRPI0922104A2 (pt) 2016-01-05
BRPI0922104B1 BRPI0922104B1 (pt) 2020-04-14

Family

ID=40651288

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0922104A BRPI0922104B1 (pt) 2008-11-07 2009-09-29 flange anular radical de um elemento de rotor ou de estator de uma turbina para turbomáquina, turbina de baixa pressão para tubomáquina, e, turbomáquina, tal como um turborreator ou um turbopropulsor.

Country Status (9)

Country Link
US (1) US8727719B2 (pt)
EP (1) EP2344719B1 (pt)
JP (1) JP5674672B2 (pt)
CN (1) CN102209837B (pt)
BR (1) BRPI0922104B1 (pt)
CA (1) CA2742045C (pt)
FR (1) FR2938292B1 (pt)
RU (1) RU2514462C2 (pt)
WO (1) WO2010052379A1 (pt)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2974865B1 (fr) * 2011-05-04 2013-07-05 Snecma Rotor haute pression pour turbomachine d'aeronef, comprenant des moyens de detrompage associes a des boulons de prefixation de module de turbine
FR2983518B1 (fr) * 2011-12-06 2014-02-07 Snecma Dispositif deverrouillable d'arret axial d'une couronne d'etancheite contactee par une roue mobile de module de turbomachine d'aeronef
US9664062B2 (en) 2011-12-08 2017-05-30 Siemens Energy, Inc. Gas turbine engine with multiple component exhaust diffuser operating in conjunction with an outer case ambient external cooling system
US9410427B2 (en) * 2012-06-05 2016-08-09 United Technologies Corporation Compressor power and torque transmitting hub
US9200520B2 (en) * 2012-06-22 2015-12-01 General Electric Company Gas turbine conical flange bolted joint
EP2948646A2 (en) * 2013-01-22 2015-12-02 Siemens Energy, Inc. Gas turbine engine with multiple component exhaust diffuser operating in conjunction with an outer case ambient external cooling system
FR3008912B1 (fr) * 2013-07-29 2017-12-15 Snecma Carter de turbomachine et procede de fabrication
FR3021066B1 (fr) * 2014-05-19 2019-05-10 Safran Aircraft Engines Disque de rotor equilibre, et procede d'equilibrage
DK3104954T3 (da) * 2014-06-02 2020-09-28 ULMATEC GmbH Patronflange og filtersystem
JP6472362B2 (ja) * 2015-10-05 2019-02-20 三菱重工航空エンジン株式会社 ガスタービン用ケーシング及びガスタービン
FR3074215B1 (fr) * 2017-11-29 2019-12-27 Safran Aircraft Engines Accouplement de deux brides
US11578599B2 (en) * 2021-02-02 2023-02-14 Pratt & Whitney Canada Corp. Rotor balance assembly
FR3121472B1 (fr) * 2021-04-01 2023-07-14 Safran Aircraft Engines Procede de fabrication d’une piece de turbomachine comprenant des portions arrondies optimisees et piece de turbomachine correspondante
IT202100009716A1 (it) 2021-04-16 2022-10-16 Ge Avio Srl Copertura di un dispositivo di fissaggio per una giunzione flangiata
US11788413B2 (en) 2021-09-09 2023-10-17 Pratt & Whitney Canada Corp. Gas turbine engine shaft with lobed support structure
DE102023111513A1 (de) * 2023-05-03 2024-11-07 MTU Aero Engines AG Rotorscheibe für einen Schaufelkranz
FR3159411A1 (fr) * 2024-02-15 2025-08-22 Safran Aircraft Engines Piece annulaire pour une turbomachine d’aeronef
FR3160204A1 (fr) * 2024-03-15 2025-09-19 Safran Aircraft Engines Assemblage de pieces pour une turbomachine d’aeronef

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB785002A (en) * 1955-04-20 1957-10-23 Power Jets Res & Dev Ltd Rotor for a compressor, turbine or like fluid flow machine
RU2226609C2 (ru) * 2002-06-17 2004-04-10 Открытое акционерное общество "Авиадвигатель" Турбина газотурбинного двигателя
GB0216362D0 (en) * 2002-07-13 2002-08-21 Rolls Royce Plc Stress defender holes
US6893222B2 (en) * 2003-02-10 2005-05-17 United Technologies Corporation Turbine balancing
FR2868814B1 (fr) * 2004-04-09 2009-12-18 Snecma Moteurs Dispositif d'assemblage de brides annulaires, en particulier dans une turbomachine
FR2885167B1 (fr) * 2005-04-29 2007-06-29 Snecma Moteurs Sa Module de turbine pour moteur a turbine a gaz
FR2931869B1 (fr) 2008-05-29 2014-12-12 Snecma Bride annulaire de fixation d'un element de rotor ou de stator

Also Published As

Publication number Publication date
JP5674672B2 (ja) 2015-02-25
RU2514462C2 (ru) 2014-04-27
CN102209837A (zh) 2011-10-05
RU2011122783A (ru) 2012-12-20
BRPI0922104B1 (pt) 2020-04-14
EP2344719B1 (fr) 2014-01-22
WO2010052379A1 (fr) 2010-05-14
FR2938292A1 (fr) 2010-05-14
EP2344719A1 (fr) 2011-07-20
JP2012508347A (ja) 2012-04-05
CA2742045A1 (fr) 2010-05-14
CN102209837B (zh) 2016-05-04
US20110274541A1 (en) 2011-11-10
FR2938292B1 (fr) 2010-12-24
US8727719B2 (en) 2014-05-20
CA2742045C (fr) 2016-11-29

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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]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 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 14/04/2020, OBSERVADAS AS CONDICOES LEGAIS.