BR112014030695A2 - mancal, sistema para mudar o ângulo de inclinação das pás de uma hélice de motor de turboeixo, e, motor de turbina - Google Patents

mancal, sistema para mudar o ângulo de inclinação das pás de uma hélice de motor de turboeixo, e, motor de turbina

Info

Publication number
BR112014030695A2
BR112014030695A2 BR112014030695A BR112014030695A BR112014030695A2 BR 112014030695 A2 BR112014030695 A2 BR 112014030695A2 BR 112014030695 A BR112014030695 A BR 112014030695A BR 112014030695 A BR112014030695 A BR 112014030695A BR 112014030695 A2 BR112014030695 A2 BR 112014030695A2
Authority
BR
Brazil
Prior art keywords
bearing
blades
changing
inclination angle
turbine engine
Prior art date
Application number
BR112014030695A
Other languages
English (en)
Other versions
BR112014030695B1 (pt
Inventor
Curlier Augustin
Frantz Caroline
Igel Dominik
Hugon Nadège
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 BR112014030695A2 publication Critical patent/BR112014030695A2/pt
Publication of BR112014030695B1 publication Critical patent/BR112014030695B1/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/02—Hub construction
    • B64C11/04—Blade mountings
    • B64C11/06—Blade mountings for variable-pitch 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/18—Lubricating arrangements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30—Blade pitch-changing mechanisms
    • B64C11/306—Blade pitch-changing mechanisms specially adapted for contrarotating propellers
    • 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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • 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
    • F01D7/00—Rotors with blades adjustable in operation; Control thereof
    • 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
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C29/00—Bearings for parts moving only linearly
    • F16C29/04—Ball or roller bearings
    • 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
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/30—Parts of ball or roller bearings
    • F16C33/66—Special parts or details in view of lubrication
    • F16C33/6637—Special parts or details in view of lubrication with liquid lubricant
    • F16C33/6659—Details of supply of the liquid to the bearing, e.g. passages or nozzles
    • 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
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/30—Parts of ball or roller bearings
    • F16C33/66—Special parts or details in view of lubrication
    • F16C33/6637—Special parts or details in view of lubrication with liquid lubricant
    • F16C33/6659—Details of supply of the liquid to the bearing, e.g. passages or nozzles
    • F16C33/6677—Details of supply of the liquid to the bearing, e.g. passages or nozzles from radial inside, e.g. via a passage through the shaft and/or inner ring
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D2027/005—Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR]
    • 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
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C23/00—Bearings for exclusively rotary movement adjustable for aligning or positioning
    • F16C23/06—Ball or roller bearings
    • 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
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2326/00—Articles relating to transporting
    • F16C2326/43—Aeroplanes; Helicopters
    • 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
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2360/00—Engines or pumps
    • F16C2360/23—Gas turbine engines
    • 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)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Rolling Contact Bearings (AREA)
  • Sliding-Contact Bearings (AREA)
  • Supercharger (AREA)
  • General Details Of Gearings (AREA)

Abstract

1 / 1 resumo “mancal, sistema para mudar o ã‚ngulo de inclinaã‡ãƒo das pãs de uma hã‰lice de motor de turboeixo, e, motor de turbina ㉠descrito um mancal, tal como um mancal de rolamento, que ã© montado em um suporte (31) mã³vel em translaã§ã£o e compreende um dispositivo de lubrificaã§ã£o (29). vantajosamente, o dispositivo de lubrificaã§ã£o (29) do mancal (27) compreende pelo menos uma tubulaã§ã£o (50) para entregar um lubrificante, ligada em uma fonte de suprimento de lubrificante (51), e encaixando pelo menos parcialmente no suporte (31) mã³vel em translaã§ã£o para entregar o lubrificante do dito suporte mã³vel (31) ao longo de um canal interno (ch) no mancal (27), passando atravã©s do anel interno (39) do mesmo.
BR112014030695-8A 2012-06-27 2013-06-27 Mancal, sistema para mudar o ângulo de inclinação das pás de uma hélice de motor de turboeixo, e, motor de turbina BR112014030695B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1256140 2012-06-27
FR1256140A FR2992703B1 (fr) 2012-06-27 2012-06-27 Palier a moyen de lubrification et systeme pour changer le pas des pales d'une helice de turbopropulseur d'aeronef, equipe dudit palier
PCT/FR2013/051502 WO2014001723A1 (fr) 2012-06-27 2013-06-27 Palier a moyen de lubrification et systeme pour changer le pas des pales d'une helice de turbopropulseur d'aeronef, equipe dudit palier

Publications (2)

Publication Number Publication Date
BR112014030695A2 true BR112014030695A2 (pt) 2017-06-27
BR112014030695B1 BR112014030695B1 (pt) 2021-11-03

Family

ID=48914333

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112014030695-8A BR112014030695B1 (pt) 2012-06-27 2013-06-27 Mancal, sistema para mudar o ângulo de inclinação das pás de uma hélice de motor de turboeixo, e, motor de turbina

Country Status (8)

Country Link
US (1) US9951651B2 (pt)
EP (1) EP2867551B1 (pt)
CN (1) CN104395627B (pt)
BR (1) BR112014030695B1 (pt)
CA (1) CA2874707C (pt)
FR (1) FR2992703B1 (pt)
RU (1) RU2630823C2 (pt)
WO (1) WO2014001723A1 (pt)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2887262A1 (en) * 2012-10-23 2014-05-01 General Electric Company Unducted thrust producing system architecture
FR3021296B1 (fr) * 2014-05-21 2017-12-22 Snecma Ensemble de propulsion a doublet d'helices pour aeronef
FR3022587B1 (fr) * 2014-06-23 2019-03-22 Safran Aircraft Engines Dispositif et procede de lubrification d’un palier a roulement de turbomachine
PL226826B1 (pl) * 2015-09-03 2017-09-29 Gen Electric Układ sterowania skokiem dozespołu wirnika, silnik turbospalinowy isposób sterowania katem skoku wielu łopat smigła
JP6649147B2 (ja) * 2016-03-25 2020-02-19 三菱日立パワーシステムズ株式会社 回転機械のケーシング支持部の冷却装置及び回転機械、並びに回転機械のケーシング支持部の冷却方法
FR3055309B1 (fr) * 2016-08-26 2018-08-17 Safran Aircraft Engines Systeme de changement de pas equipe de moyens de lubrification d'un palier de transfert de charge
FR3055308B1 (fr) 2016-08-26 2018-08-17 Safran Aircraft Engines Moyen de commande d'un systeme de changement de pas comprenant un dispositif anti-rotation, systeme de changement de pas equipe dudit moyen de commande et turbomachine correspondante
US11131244B2 (en) * 2017-11-03 2021-09-28 General Electric Company Power transmission system and gas turbine engine comprising the same
FR3080650B1 (fr) * 2018-04-26 2020-04-03 Safran Aircraft Engines Ensemble de lubrification pour une turbomachine
FR3082553B1 (fr) * 2018-06-18 2020-09-25 Safran Aircraft Engines Ensemble pour turbomachine d'aeronef comportant un systeme ameliore de lubrification d'un reducteur d'entrainement de soufflante en cas d'autorotation de la soufflante
US11459727B2 (en) * 2019-06-26 2022-10-04 Caterpillar Global Mining Llc Coupling assembly for a machine
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1556460A (en) * 1925-02-09 1925-10-06 Thill Frank Spring oiler
FR1158891A (fr) 1956-09-27 1958-06-20 Dispositif de brosse à dents rotative
CA1328433C (en) * 1988-10-03 1994-04-12 Clarence Isert Variable pitch fan with fan cranks and axle housed shifting means
US7278516B2 (en) * 2004-03-09 2007-10-09 Honeywell International, Inc. Apparatus and method for bearing lubrication in turbine engines
FR2908451B1 (fr) * 2006-11-09 2009-03-20 Snecma Sa Turbopropulseur comportant un ensemble de pales a orientation reglable
WO2009000268A2 (en) * 2007-06-22 2008-12-31 Vestas Wind Systems A/S Lubrication system for a gearbox and wind turbine
RU2383465C1 (ru) * 2008-11-19 2010-03-10 Геннадий Мстиславич Кормильченко Втулка воздушного винта изменяемого шага с механизмом автоматического флюгирования лопастей

Also Published As

Publication number Publication date
CA2874707A1 (fr) 2014-01-03
US20150147178A1 (en) 2015-05-28
FR2992703A1 (fr) 2014-01-03
FR2992703B1 (fr) 2015-01-30
RU2630823C2 (ru) 2017-09-13
CN104395627A (zh) 2015-03-04
EP2867551B1 (fr) 2016-05-25
EP2867551A1 (fr) 2015-05-06
US9951651B2 (en) 2018-04-24
CN104395627B (zh) 2017-04-05
RU2014150069A (ru) 2016-08-20
BR112014030695B1 (pt) 2021-11-03
CA2874707C (fr) 2020-04-28
WO2014001723A1 (fr) 2014-01-03

Similar Documents

Publication Publication Date Title
BR112014030695A2 (pt) mancal, sistema para mudar o ângulo de inclinação das pás de uma hélice de motor de turboeixo, e, motor de turbina
BR112014007754A2 (pt) sistema de engrenagens de acionamento de ventoinha, e, motor de turbina a gás
WO2015060912A3 (en) Dual direction windmill pump for geared turbofan engine
EP4273374A3 (en) Lubrication of journal bearing during clockwise and counter-clockwise rotation
BR112015004700A8 (pt) redutor com trem epicicloidal notavelmente para turbomáquina
WO2014130103A3 (en) Integrated heat exchangers for low fan pressure ratio geared turbofan
WO2014123863A3 (en) Multi-circuit lubrication system for a turbine engine
ATE549244T1 (de) Gondel für ein flugzeugtriebwerk
WO2015147949A3 (en) Auxiliary oil system for geared gas turbine engine
BR112015012287A2 (pt) dispositivo de controle de motor, computador de controle de motor digital de autoridade total, turboélice, e, motor de ventoinha sem duto
BR112015002317A2 (pt) motor de turbina de desvio
BR112014010582A2 (pt) mancal axial hidrodinâmico
BR112013005250A2 (pt) motor de turbina a gás que compreende meios de retenção axial de uma ventoinha do dito motor
EP3779167A3 (en) Gas turbine engine architecture with low pressure compressor hub between high and low rotor thrust bearings
BR112015010811A2 (pt) seção de turbina de um motor de turbina de gás, e, motor de turbina de gás
EP2778391A3 (en) System and method for installing a blade insert between separate portions of a wind turbine rotor blade
BR112012031972A2 (pt) sistema hidroelétrico em um duto e método para manter as lâminas da turbina em um alojamento substancialmente livre de água
BR112015010038A2 (pt) turbina eólica, seção de eixo de uma turbina eólica, e, método para projetar uma turbina eólica
GB201904358D0 (en) Lubricated enclosure for an aircraft turbine engine, limiting the retention of lubricant during pictching
EP3049655A4 (en) REAR BEARING GAS TURBINE BEARING ARRANGEMENT
BR112014026079A2 (pt) motor de turbina de aeronave, e, método para monitorar um motor de turbina de aeronave
PL413811A1 (pl) Układ i sposób regulacji skoku śmigła
EP3070264A4 (en) Vane structure for axial flow turbomachine and gas turbine engine
EP3027864A4 (en) Gas turbine engine shaft bearing configuration
GB201918778D0 (en) Gas turbine engine with shaft bearings

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 27/06/2013, OBSERVADAS AS CONDICOES LEGAIS.