BR112016006514A2 - estágio de rotor de turbina axial com uma variação de velocidade adaptativa para tensões dinâmicas - Google Patents

estágio de rotor de turbina axial com uma variação de velocidade adaptativa para tensões dinâmicas

Info

Publication number
BR112016006514A2
BR112016006514A2 BR112016006514A BR112016006514A BR112016006514A2 BR 112016006514 A2 BR112016006514 A2 BR 112016006514A2 BR 112016006514 A BR112016006514 A BR 112016006514A BR 112016006514 A BR112016006514 A BR 112016006514A BR 112016006514 A2 BR112016006514 A2 BR 112016006514A2
Authority
BR
Brazil
Prior art keywords
axial turbine
turbine rotor
adaptive speed
dynamic stresses
speed range
Prior art date
Application number
BR112016006514A
Other languages
English (en)
Inventor
Pesatori Emanuel
Polloni Marco
Sanvito Massimiliano
Ferrante Michele
Bachschmid Nicolo
Bistolfi Simone
Original Assignee
Franco Tosi Mecc S P A
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 Franco Tosi Mecc S P A filed Critical Franco Tosi Mecc S P A
Publication of BR112016006514A2 publication Critical patent/BR112016006514A2/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
    • F01D5/12—Blades
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • 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
    • F01D25/005—Selecting particular materials
    • 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
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
    • 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
    • F01D5/12—Blades
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • 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
    • F01D5/12—Blades
    • F01D5/26—Antivibration means not restricted to blade form or construction or to blade-to-blade connections or to the use of particular materials
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • 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
    • F05D2240/00—Components
    • F05D2240/20—Rotors
    • F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/305—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the pressure side of a rotor blade
    • 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
    • F05D2240/00—Components
    • F05D2240/20—Rotors
    • F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/306—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the suction side of a rotor blade
    • 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
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise
    • 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)
  • Architecture (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

resumo “estágio de rotor de turbina axial com uma variação de velocidade adaptativa para tensões dinâmicas” estágio de rotor de uma turbina axial compreendendo uma pluralidade de palhetas e uma pluralidade de atenuadores interpostos entre cada par de palhetas subsequentes, o referido atenuador impedindo a rotação dos perfis de palheta cau-sada pela força centrífuga durante a operação e atingindo um reforço do arranjo de palheta do rotor.
BR112016006514A 2013-09-26 2013-09-26 estágio de rotor de turbina axial com uma variação de velocidade adaptativa para tensões dinâmicas BR112016006514A2 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/IB2013/002140 WO2015044699A1 (en) 2013-09-26 2013-09-26 Rotor stage of axial turbine with an adaptive regulation to dynamic stresses

Publications (1)

Publication Number Publication Date
BR112016006514A2 true BR112016006514A2 (pt) 2017-08-01

Family

ID=49683779

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112016006514A BR112016006514A2 (pt) 2013-09-26 2013-09-26 estágio de rotor de turbina axial com uma variação de velocidade adaptativa para tensões dinâmicas

Country Status (7)

Country Link
US (1) US20160208623A1 (pt)
EP (1) EP3049634B1 (pt)
JP (1) JP2017502187A (pt)
KR (1) KR20160070076A (pt)
BR (1) BR112016006514A2 (pt)
CA (1) CA2925002A1 (pt)
WO (1) WO2015044699A1 (pt)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3521565A1 (de) * 2018-01-31 2019-08-07 Siemens Aktiengesellschaft Turbinenschaufel mit stabilisierungselement und zugehöriger rotor
FR3086693B1 (fr) * 2018-10-01 2021-01-22 Safran Aircraft Engines Cale pour turbomachine, ensemble pour turbomachine, turbomachine et procede associes

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1252766A (fr) * 1959-12-18 1961-02-03 Alsthom Cgee Entretoises pour aubes de turbines
JPS49120901U (pt) * 1973-02-15 1974-10-16
JPS533442B2 (pt) * 1973-11-05 1978-02-07
JPS5632441B2 (pt) * 1973-11-30 1981-07-28
JPS5337964B2 (pt) 1974-05-15 1978-10-12
JPS54125307A (en) * 1978-03-24 1979-09-28 Toshiba Corp Connecting device for turbine movable blades
JPS54138910A (en) 1978-04-19 1979-10-27 Hitachi Ltd Movable vane connection apparatus
JPS56143301A (en) 1980-04-09 1981-11-09 Toshiba Corp Turbine blades
JPS572405A (en) * 1980-06-05 1982-01-07 Hitachi Ltd Rotary blade connector of axial-flow rotary machine
JPS5756606A (en) 1980-09-22 1982-04-05 Hitachi Ltd Connecting device of rotary blade
JPS58176402A (ja) * 1982-04-10 1983-10-15 Toshiba Corp タ−ビン動翼の制振装置
GB2171151B (en) * 1985-02-20 1988-05-18 Rolls Royce Rotors for gas turbine engines
US5288209A (en) * 1991-12-19 1994-02-22 General Electric Company Automatic adaptive sculptured machining
DE10340773A1 (de) 2003-09-02 2005-03-24 Man Turbomaschinen Ag Rotor einer Dampf- oder Gasturbine
JP2005256786A (ja) * 2004-03-12 2005-09-22 Mitsubishi Heavy Ind Ltd 回転機械、及び、回転機械の連成方法
JP4765882B2 (ja) * 2006-10-05 2011-09-07 株式会社日立製作所 蒸気タービン動翼
US7758311B2 (en) * 2006-10-12 2010-07-20 General Electric Company Part span shrouded fan blisk
GB2467582B (en) 2009-02-10 2011-07-06 Rolls Royce Plc Vibration damper assembly
US8540488B2 (en) 2009-12-14 2013-09-24 Siemens Energy, Inc. Turbine blade damping device with controlled loading
FR2955142B1 (fr) 2010-01-13 2013-08-23 Snecma Amortisseur de vibrations a pion entre talons d'aubes adjacentes en materiau composite d'une roue mobile de turbomachine.
US8523525B2 (en) * 2010-02-05 2013-09-03 Siemens Energy, Inc. Snubber assembly for turbine blades
US8066479B2 (en) 2010-04-05 2011-11-29 Pratt & Whitney Rocketdyne, Inc. Non-integral platform and damper for an airfoil
US20140255207A1 (en) * 2012-12-21 2014-09-11 General Electric Company Turbine rotor blades having mid-span shrouds

Also Published As

Publication number Publication date
US20160208623A1 (en) 2016-07-21
WO2015044699A1 (en) 2015-04-02
KR20160070076A (ko) 2016-06-17
JP2017502187A (ja) 2017-01-19
EP3049634A1 (en) 2016-08-03
CA2925002A1 (en) 2015-04-02
EP3049634B1 (en) 2019-02-27

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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]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B11B Dismissal acc. art. 36, par 1 of ipl - no reply within 90 days to fullfil the necessary requirements