BR112014027013A2 - reforço estrutural, pá de motor de turbina, e, motor de turbina - Google Patents
reforço estrutural, pá de motor de turbina, e, motor de turbinaInfo
- Publication number
- BR112014027013A2 BR112014027013A2 BR112014027013A BR112014027013A BR112014027013A2 BR 112014027013 A2 BR112014027013 A2 BR 112014027013A2 BR 112014027013 A BR112014027013 A BR 112014027013A BR 112014027013 A BR112014027013 A BR 112014027013A BR 112014027013 A2 BR112014027013 A2 BR 112014027013A2
- Authority
- BR
- Brazil
- Prior art keywords
- turbine engine
- blade
- structural reinforcement
- reinforcement
- housing
- Prior art date
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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
-
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/02—Selection of particular materials
- F04D29/023—Selection of particular materials especially adapted for elastic fluid pumps
-
- 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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/288—Protective coatings for blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
- F04D29/324—Blades
-
- 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
- F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
-
- 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
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
- F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
-
- 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
- F05D2240/303—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 leading edge 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/13—Refractory metals, i.e. Ti, V, Cr, Zr, Nb, Mo, Hf, Ta, W
- F05D2300/133—Titanium
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/17—Alloys
- F05D2300/174—Titanium alloys, e.g. TiAl
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
- F05D2300/6032—Metal matrix composites [MMC]
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
- F05D2300/6034—Orientation of fibres, weaving, ply angle
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/614—Fibres or filaments
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/70—Treatment or modification of materials
- F05D2300/702—Reinforcement
-
- 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)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Composite Materials (AREA)
- Architecture (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
1 / 1 resumo â re fo rão estrutural, pã de motor de turbina, e, motor de t u rbin a â em reforã§o estrutural para uma pã¡ mista de um motor de turbina, o reforã§o sendo para unir adesivamente em uma borda dianteira da pã¡ e apresentando em toda sua altura uma seã§ã£o que ã© substancialmente em forma de v, com uma base que ã© estendida por dois flancos laterais, ã© provido um conjunto de uma pluralidade de feixes de fibra que ã© montada em pelo menos um alojamento na base, cujo conjunto define o teor de fibra que varia ao longo de toda a altura do alojamento.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1253977 | 2012-04-30 | ||
FR1253977A FR2989991B1 (fr) | 2012-04-30 | 2012-04-30 | Renfort structurel metallique d'aube de turbomachine |
PCT/FR2013/050917 WO2013164532A1 (fr) | 2012-04-30 | 2013-04-25 | Renfort structurel metallique d'aube en composite de turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112014027013A2 true BR112014027013A2 (pt) | 2017-06-27 |
BR112014027013B1 BR112014027013B1 (pt) | 2020-11-17 |
Family
ID=46754592
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112014027013-9A BR112014027013B1 (pt) | 2012-04-30 | 2013-04-25 | Reforço estrutural, pâ de motor de turbina, e, motor de turbina |
Country Status (9)
Country | Link |
---|---|
US (1) | US9598966B2 (pt) |
EP (1) | EP2844841B1 (pt) |
JP (1) | JP6141411B2 (pt) |
CN (1) | CN104271888B (pt) |
BR (1) | BR112014027013B1 (pt) |
CA (1) | CA2871481C (pt) |
FR (1) | FR2989991B1 (pt) |
RU (1) | RU2637163C2 (pt) |
WO (1) | WO2013164532A1 (pt) |
Families Citing this family (31)
Publication number | Priority date | Publication date | Assignee | Title |
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FR3026033B1 (fr) * | 2014-09-19 | 2017-03-24 | Snecma | Procede de fabrication de bouclier de bord d'attaque |
FR3035676B1 (fr) * | 2015-04-29 | 2017-05-12 | Snecma | Aube munie de plateformes possedant un raidisseur |
FR3045711B1 (fr) | 2015-12-21 | 2018-01-26 | Safran Aircraft Engines | Bouclier de bord d'attaque |
GB2549113A (en) * | 2016-04-05 | 2017-10-11 | Rolls Royce Plc | Composite bodies and their manufacture |
CN106762146B (zh) * | 2016-12-19 | 2018-05-15 | 北京航空航天大学 | 一种发动机导向叶片的热气防冰结构 |
GB201702698D0 (en) * | 2017-02-20 | 2017-04-05 | Rolls Royce Plc | Fan |
RU2661439C1 (ru) * | 2017-10-23 | 2018-07-16 | Николай Борисович Болотин | Лопатка вентилятора газотурбинного двигателя |
RU2661437C1 (ru) * | 2017-10-23 | 2018-07-16 | Николай Борисович Болотин | Широкохордная лопатка вентилятора газотурбинного двигателя |
RU2663559C1 (ru) * | 2017-10-24 | 2018-08-07 | Николай Борисович Болотин | Широкохордная лопатка вентилятора газотурбинного двигателя |
RU2675161C1 (ru) * | 2017-10-24 | 2018-12-17 | Николай Борисович Болотин | Лопатка вентилятора газотурбинного двигателя |
RU2663609C1 (ru) * | 2017-10-24 | 2018-08-07 | Николай Борисович Болотин | Широкохордная лопатка вентилятора газотурбинного двигателя |
RU2667220C1 (ru) * | 2017-10-24 | 2018-09-17 | Николай Борисович Болотин | Лопатка вентилятора газотурбинного двигателя |
EP3495612B1 (en) * | 2017-12-06 | 2021-05-12 | Ansaldo Energia IP UK Limited | Method for manufacturing composite component |
FR3081914B1 (fr) * | 2018-06-05 | 2020-08-28 | Safran Aircraft Engines | Aube de soufflante en materiau composite avec grand jeu integre |
FR3084400B1 (fr) * | 2018-07-24 | 2021-05-07 | Safran Aircraft Engines | Aube de turbomachine comportant un renfort structurel a adherence renforcee |
FR3084695A1 (fr) * | 2018-07-31 | 2020-02-07 | Safran Aircraft Engines | Aube composite a armature metallique et son procede de fabrication |
US11454121B2 (en) | 2018-09-28 | 2022-09-27 | General Electric Company | Airfoil with leading edge guard |
GB2585848B (en) * | 2019-07-16 | 2022-04-13 | Gkn Aerospace Sweden Ab | Injection bonding of composite vane into pocket |
FR3100270B1 (fr) * | 2019-08-28 | 2021-07-30 | Safran Aircraft Engines | Hybridation des fibres du renfort fibreux d’une aube de soufflante |
US11215054B2 (en) * | 2019-10-30 | 2022-01-04 | Raytheon Technologies Corporation | Airfoil with encapsulating sheath |
US11466576B2 (en) | 2019-11-04 | 2022-10-11 | Raytheon Technologies Corporation | Airfoil with continuous stiffness joint |
FR3116311B1 (fr) * | 2020-11-17 | 2023-05-19 | Safran Aircraft Engines | Aube de soufflante comprenant un bouclier à densité variable |
CN114961873B (zh) * | 2021-02-25 | 2024-05-31 | 中国航发商用航空发动机有限责任公司 | 可恢复变形的叶片及包含其的涡扇发动机 |
US11725524B2 (en) | 2021-03-26 | 2023-08-15 | General Electric Company | Engine airfoil metal edge |
FR3127017B1 (fr) * | 2021-09-10 | 2023-09-08 | Safran Aircraft Engines | Bouclier de protection pour un bord d’attaque d’une aube, aube associee et procede de fabrication du bouclier |
FR3127020A1 (fr) * | 2021-09-10 | 2023-03-17 | Safran Aircraft Engines | Procede de fabrication d’une aube pour une turbomachine d’aeronef et aube associee |
FR3127016B1 (fr) * | 2021-09-10 | 2023-09-08 | Safran Aircraft Engines | Procede de correction du poids moment radial d’une aube |
US11655828B2 (en) * | 2021-10-27 | 2023-05-23 | General Electric Company | Anti-icing systems and airfoils for a fan section of a turbine engine |
US11988103B2 (en) | 2021-10-27 | 2024-05-21 | General Electric Company | Airfoils for a fan section of a turbine engine |
FR3132321B1 (fr) * | 2022-02-02 | 2024-03-22 | Safran Aircraft Engines | Aube hybride métal/composite à orientation textile adaptée aux sollicitations mécaniques |
US11767607B1 (en) | 2022-07-13 | 2023-09-26 | General Electric Company | Method of depositing a metal layer on a component |
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US3762835A (en) * | 1971-07-02 | 1973-10-02 | Gen Electric | Foreign object damage protection for compressor blades and other structures and related methods |
RU1313055C (ru) * | 1984-01-09 | 1995-12-10 | Запорожское машиностроительное конструкторское бюро "Прогресс" | Композиционная лопатка турбомашины |
US4738594A (en) * | 1986-02-05 | 1988-04-19 | Ishikawajima-Harima Jukogyo Kabushiki Kaisha | Blades for axial fans |
US5439750A (en) * | 1993-06-15 | 1995-08-08 | General Electric Company | Titanium metal matrix composite inserts for stiffening turbine engine components |
JPH07223876A (ja) * | 1993-06-25 | 1995-08-22 | Hitachi Ltd | 繊維強化複合材とその製法およびそれを用いた部材 |
CN1102632A (zh) * | 1993-06-25 | 1995-05-17 | 株式会社日立制作所 | 纤维增强复合材料及其制造方法以及用它制成的部件 |
US5908285A (en) * | 1995-03-10 | 1999-06-01 | United Technologies Corporation | Electroformed sheath |
FR2732406B1 (fr) | 1995-03-29 | 1997-08-29 | Snecma | Aube de turbomachine en materiau composite |
US5674370A (en) * | 1995-03-31 | 1997-10-07 | Optical Radiation Corporation | Method of electroforming an abrasion shield |
FR2745589B1 (fr) * | 1996-02-29 | 1998-04-30 | Snecma | Piece hybride a haut rapport resistance-masse et procede de realisation |
US5725354A (en) * | 1996-11-22 | 1998-03-10 | General Electric Company | Forward swept fan blade |
DE19751129C1 (de) * | 1997-11-19 | 1999-06-17 | Mtu Muenchen Gmbh | FAN-Rotorschaufel für ein Triebwerk |
US6234912B1 (en) * | 1999-09-07 | 2001-05-22 | General Electric Company | High-stiffness composite shaft |
DE10307610A1 (de) * | 2003-02-22 | 2004-09-02 | Rolls-Royce Deutschland Ltd & Co Kg | Verdichterschaufel für ein Flugzeugtriebwerk |
FR2884550B1 (fr) * | 2005-04-15 | 2010-09-17 | Snecma Moteurs | Piece pour proteger le bord d'attaque d'une pale |
FR2906320B1 (fr) * | 2006-09-26 | 2008-12-26 | Snecma Sa | Aube composite de turbomachine a renfort metallique |
US8088498B2 (en) * | 2007-05-23 | 2012-01-03 | Hamilton Sundstrand Corporation | Electro-formed sheath for use on airfoil components |
US8814527B2 (en) * | 2009-08-07 | 2014-08-26 | Hamilton Sundstrand Corporation | Titanium sheath and airfoil assembly |
US8807931B2 (en) * | 2010-01-04 | 2014-08-19 | General Electric Company | System for impact zone reinforcement |
US9157327B2 (en) * | 2010-02-26 | 2015-10-13 | United Technologies Corporation | Hybrid metal fan blade |
US9315927B2 (en) * | 2010-07-12 | 2016-04-19 | Snecma | Method for producing a solid part |
FR2965202B1 (fr) * | 2010-09-28 | 2012-10-12 | Snecma | Procede de fabrication d'une piece et piece massive composite obtenue par ce procede |
GB2484726B (en) * | 2010-10-22 | 2012-11-07 | Rolls Royce Plc | Blade |
FR2971961B1 (fr) * | 2011-02-25 | 2014-06-13 | Snecma | Procede de fabrication d'une piece metallique |
FR2975734B1 (fr) * | 2011-05-27 | 2013-05-31 | Snecma | Procede de renforcement d'une piece mecanique de turbomachine |
US8858182B2 (en) * | 2011-06-28 | 2014-10-14 | United Technologies Corporation | Fan blade with sheath |
US9140130B2 (en) * | 2012-03-08 | 2015-09-22 | United Technologies Corporation | Leading edge protection and method of making |
-
2012
- 2012-04-30 FR FR1253977A patent/FR2989991B1/fr active Active
-
2013
- 2013-04-25 US US14/397,730 patent/US9598966B2/en active Active
- 2013-04-25 BR BR112014027013-9A patent/BR112014027013B1/pt active IP Right Grant
- 2013-04-25 JP JP2015509472A patent/JP6141411B2/ja active Active
- 2013-04-25 CA CA2871481A patent/CA2871481C/fr active Active
- 2013-04-25 WO PCT/FR2013/050917 patent/WO2013164532A1/fr active Application Filing
- 2013-04-25 RU RU2014148176A patent/RU2637163C2/ru active
- 2013-04-25 CN CN201380022738.1A patent/CN104271888B/zh active Active
- 2013-04-25 EP EP13723867.1A patent/EP2844841B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
RU2637163C2 (ru) | 2017-11-30 |
CN104271888A (zh) | 2015-01-07 |
RU2014148176A (ru) | 2016-06-27 |
CA2871481A1 (fr) | 2013-11-07 |
US20150086378A1 (en) | 2015-03-26 |
FR2989991A1 (fr) | 2013-11-01 |
US9598966B2 (en) | 2017-03-21 |
JP6141411B2 (ja) | 2017-06-07 |
EP2844841A1 (fr) | 2015-03-11 |
FR2989991B1 (fr) | 2016-01-08 |
JP2015524030A (ja) | 2015-08-20 |
CA2871481C (fr) | 2019-07-09 |
CN104271888B (zh) | 2015-11-25 |
WO2013164532A1 (fr) | 2013-11-07 |
EP2844841B1 (fr) | 2016-05-18 |
BR112014027013B1 (pt) | 2020-11-17 |
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