BR112015020873A2 - conjunto de pás de passo variável e uma turbomáquina - Google Patents

conjunto de pás de passo variável e uma turbomáquina

Info

Publication number
BR112015020873A2
BR112015020873A2 BR112015020873A BR112015020873A BR112015020873A2 BR 112015020873 A2 BR112015020873 A2 BR 112015020873A2 BR 112015020873 A BR112015020873 A BR 112015020873A BR 112015020873 A BR112015020873 A BR 112015020873A BR 112015020873 A2 BR112015020873 A2 BR 112015020873A2
Authority
BR
Brazil
Prior art keywords
blade
variable pitch
turbomachine
axis
pitch blades
Prior art date
Application number
BR112015020873A
Other languages
English (en)
Other versions
BR112015020873B1 (pt
Inventor
Fabre Adrien
Laurenceau Adrien
Vlastuin Jonathan
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 BR112015020873A2 publication Critical patent/BR112015020873A2/pt
Publication of BR112015020873B1 publication Critical patent/BR112015020873B1/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30Blade pitch-changing mechanisms
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D7/00Rotors with blades adjustable in operation; Control thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30Blade pitch-changing mechanisms
    • B64C11/32Blade pitch-changing mechanisms mechanical
    • B64C11/36Blade pitch-changing mechanisms mechanical non-automatic
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D2027/005Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR]
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/20Rotors
    • F05D2240/30Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/70Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/74Adjusting of angle of incidence or attack of rotating blades by turning around an axis perpendicular the rotor centre line
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/70Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/79Bearing, support or actuation arrangements therefor
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)

Abstract

resumo “conjunto de pás de passo variável e uma turbomáquina” trata-se de uma palheta de passo variável que compreende: - uma pluralidade de pás de hélice (2), sendo que cada uma é de passo variável de acordo com um eixo geométrico rotacional de pá (a1) e cada uma tem uma raiz (201), - uma pluralidade de eixos de conexão de rotor (6), cada eixo tem um pé (602) e uma cabeça (601), a raiz (201) de cada pá é montada na cabeça (601) de um eixo de conexão de rotor por meio de um pivô (8) de modo tal que permita cada pá (2) rotacione de acordo com o eixo geométrico rotacional de pá (a1), em que cada pá (2) tem um passo de pá, de modo que um eixo geométrico rotacional de pá (a-i) da mesma é inclinado em relação a um eixo geométrico radial (a2) que passa através do pés (602) do eixo correspondente.
BR112015020873-8A 2013-03-01 2014-02-27 Conjunto de pás de passo variável e turbomáquina BR112015020873B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1351848 2013-03-01
FR1351848A FR3002781B1 (fr) 2013-03-01 2013-03-01 Aubage a calage variable
PCT/FR2014/050433 WO2014132002A2 (fr) 2013-03-01 2014-02-27 Aubage à calage variable

Publications (2)

Publication Number Publication Date
BR112015020873A2 true BR112015020873A2 (pt) 2017-07-18
BR112015020873B1 BR112015020873B1 (pt) 2021-09-08

Family

ID=48521247

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015020873-8A BR112015020873B1 (pt) 2013-03-01 2014-02-27 Conjunto de pás de passo variável e turbomáquina

Country Status (8)

Country Link
US (1) US10415404B2 (pt)
EP (1) EP2961653B1 (pt)
CN (1) CN105121276B (pt)
BR (1) BR112015020873B1 (pt)
CA (1) CA2902851C (pt)
FR (1) FR3002781B1 (pt)
RU (1) RU2647397C2 (pt)
WO (1) WO2014132002A2 (pt)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3005684B1 (fr) * 2013-05-17 2015-06-05 Snecma Pivot de pale d'helice
FR3006988B1 (fr) * 2013-06-17 2015-07-03 Snecma Pivot de pale d'helice aerienne en forme de calotte spherique
FR3017667B1 (fr) * 2014-02-14 2019-05-03 Safran Aircraft Engines Dispositif pour une helice non carenee a pales a calage variable d'une turbomachine
FR3025247B1 (fr) * 2014-08-29 2016-11-11 Snecma Roue aubagee a calages variables
FR3025246B1 (fr) * 2014-08-29 2016-12-09 Snecma Roue aubagee a calages variables
FR3046439B1 (fr) * 2016-01-05 2019-01-25 Safran Aircraft Engines Soufflante a calage variable a faible pas d'un turboreacteur
US11939070B2 (en) * 2020-02-21 2024-03-26 General Electric Company Engine-mounting links that have an adjustable inclination angle
CN114109903A (zh) 2020-08-25 2022-03-01 通用电气公司 叶片燕尾榫和保持设备
CN114151381A (zh) * 2021-11-11 2022-03-08 中国航发沈阳发动机研究所 一种发动机中静子叶片角度调节机构
FR3129687A1 (fr) * 2021-11-29 2023-06-02 Safran Aircraft Engines Aube pour une hélice non carénée d’une turbomachine

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1251955A (pt) * 1967-12-29 1971-11-03
WO1984002752A1 (fr) * 1982-12-30 1984-07-19 Grp Interet Econom Aerogenerat Perfectionnements aux moteurs a vent et aerogenerateurs
US4767270A (en) * 1986-04-16 1988-08-30 The Boeing Company Hoop fan jet engine
US5154580A (en) * 1990-07-23 1992-10-13 General Electric Company Propeller pitch change mechanism
US6299412B1 (en) * 1999-12-06 2001-10-09 General Electric Company Bowed compressor airfoil
US7218013B2 (en) * 2001-10-17 2007-05-15 Steve Anderson Platt Wind powered generator
FR2911644B1 (fr) * 2007-01-23 2012-06-01 Snecma Turbopropulseur comportant une helice formee de pales a orientation reglable.
FR2911930A1 (fr) * 2007-01-26 2008-08-01 Snecma Sa Turbopropulseur a helice a pas reglable
DE102007028142B4 (de) * 2007-06-19 2018-11-15 Thomas Fischer Verstellpropeller
EP2509860B1 (fr) * 2009-12-07 2017-07-19 Safran Aircraft Engines Moyeu d'hélice à anneau polygonal renforce et turbomachine équipée d'un tel moyeu
FR2957329B1 (fr) * 2010-03-15 2012-08-03 Snecma Mecanisme de calage variable de pales pour systeme d'helices contrarotatives et systeme d'helices contrarotatives comportant au moins un tel mecanisme
FR3025246B1 (fr) * 2014-08-29 2016-12-09 Snecma Roue aubagee a calages variables

Also Published As

Publication number Publication date
US10415404B2 (en) 2019-09-17
US20160017728A1 (en) 2016-01-21
EP2961653B1 (fr) 2023-03-29
BR112015020873B1 (pt) 2021-09-08
CA2902851C (fr) 2020-06-09
WO2014132002A2 (fr) 2014-09-04
RU2015141699A (ru) 2017-04-06
EP2961653A2 (fr) 2016-01-06
WO2014132002A3 (fr) 2014-11-20
RU2647397C2 (ru) 2018-03-15
FR3002781A1 (fr) 2014-09-05
CA2902851A1 (fr) 2014-09-04
FR3002781B1 (fr) 2017-06-23
CN105121276A (zh) 2015-12-02
CN105121276B (zh) 2017-02-08

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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: 20 (VINTE) ANOS CONTADOS A PARTIR DE 27/02/2014, OBSERVADAS AS CONDICOES LEGAIS.