BR112017012436B8 - Turbomáquina - Google Patents
TurbomáquinaInfo
- Publication number
- BR112017012436B8 BR112017012436B8 BR112017012436A BR112017012436A BR112017012436B8 BR 112017012436 B8 BR112017012436 B8 BR 112017012436B8 BR 112017012436 A BR112017012436 A BR 112017012436A BR 112017012436 A BR112017012436 A BR 112017012436A BR 112017012436 B8 BR112017012436 B8 BR 112017012436B8
- Authority
- BR
- Brazil
- Prior art keywords
- turbomachine
- blade
- propeller
- upstream
- upstream propeller
- Prior art date
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
- B64C11/46—Arrangements of, or constructional features peculiar to, multiple propellers
- B64C11/48—Units of two or more coaxial propellers
-
- 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
- B64C11/16—Blades
- B64C11/18—Aerodynamic features
-
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/072—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with counter-rotating, e.g. fan rotors
-
- 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
-
- 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
Abstract
a presente invenção se refere a uma turbomáquina (1) que compreende pelo menos duas hélices não carenadas (10, 11) sendo uma hélice a montante (10) e uma hélice a jusante (11), sendo que a hélice a montante (10) compreende uma pluralidade de pás (2) em que pelo menos uma primeira pá apresenta um comprimento diferente de pelo menos uma segunda pá.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1462652A FR3030446B1 (fr) | 2014-12-17 | 2014-12-17 | Turbomachine a helice multi-diametres |
FR1462652 | 2014-12-17 | ||
PCT/FR2015/053600 WO2016097635A1 (fr) | 2014-12-17 | 2015-12-17 | Turbomachine à hélice multi-diamètres |
Publications (3)
Publication Number | Publication Date |
---|---|
BR112017012436A2 BR112017012436A2 (pt) | 2018-01-02 |
BR112017012436B1 BR112017012436B1 (pt) | 2021-12-14 |
BR112017012436B8 true BR112017012436B8 (pt) | 2022-02-15 |
Family
ID=52477966
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112017012436A BR112017012436B8 (pt) | 2014-12-17 | 2015-12-17 | Turbomáquina |
Country Status (9)
Country | Link |
---|---|
US (1) | US10494086B2 (pt) |
EP (1) | EP3233627B1 (pt) |
JP (1) | JP6758293B2 (pt) |
CN (1) | CN107108015B (pt) |
BR (1) | BR112017012436B8 (pt) |
CA (1) | CA2970092C (pt) |
FR (1) | FR3030446B1 (pt) |
RU (1) | RU2718866C2 (pt) |
WO (1) | WO2016097635A1 (pt) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3030446B1 (fr) * | 2014-12-17 | 2018-06-01 | Safran Aircraft Engines | Turbomachine a helice multi-diametres |
US10633083B2 (en) * | 2017-09-28 | 2020-04-28 | Intel IP Corporation | Unmanned aerial vehicle and method for driving an unmanned aerial vehicle |
FR3078101B1 (fr) * | 2018-02-16 | 2020-11-27 | Safran Aircraft Engines | Turbomachine a bec de separation de flux a profil en serrations |
US20210009263A1 (en) * | 2019-07-12 | 2021-01-14 | Dotterel Technologies Limited | Rotor system |
FR3125089A1 (fr) * | 2021-07-06 | 2023-01-13 | Safran Aircraft Engines | Propulseur aeronautique |
FR3125090B1 (fr) * | 2021-07-06 | 2024-03-29 | Safran Aircraft Engines | Propulseur aeronautique |
FR3125091A1 (fr) * | 2021-07-06 | 2023-01-13 | Safran Aircraft Engines | Propulseur aeronautique |
Family Cites Families (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US921423A (en) * | 1907-01-22 | 1909-05-11 | John Barnes | Screw-propeller. |
US1021822A (en) * | 1910-07-11 | 1912-04-02 | Fernand Broussouse | Screw-propeller. |
US1717663A (en) * | 1927-12-07 | 1929-06-18 | Checkley George | Propeller |
US1913590A (en) * | 1931-02-24 | 1933-06-13 | Ftacek Steven | Aeroplane propeller |
US1946571A (en) * | 1932-08-29 | 1934-02-13 | Emil A Briner | Propeller with auxiliary blades applicable to driving aircraft |
US2222444A (en) * | 1940-03-18 | 1940-11-19 | Leopold C Schmidt | Airplane propeller |
US4486146A (en) * | 1980-08-08 | 1984-12-04 | British Aerospace Public Limited Company | Aircraft propulsion means |
SE456075B (sv) * | 1984-11-29 | 1988-09-05 | Volvo Penta Ab | Rotorsystem, foretredesvis batpropellersystem |
US4883240A (en) * | 1985-08-09 | 1989-11-28 | General Electric Company | Aircraft propeller noise reduction |
GB2182727B (en) * | 1985-11-12 | 1989-09-27 | Gen Electric | Propeller/fan pitch feathering apparatus |
DE3716326A1 (de) * | 1987-05-15 | 1988-12-01 | Schempp Hirth Gmbh & Co Kg | Propeller |
DE3832026A1 (de) | 1988-09-21 | 1990-03-22 | Bosch Gmbh Robert | Luefterrad |
US4901920A (en) * | 1989-02-13 | 1990-02-20 | Snow Machines Incorporated | Snow making apparatus and methods |
JPH0672799U (ja) * | 1993-03-29 | 1994-10-11 | 科学技術庁航空宇宙技術研究所長 | 二重反転プロペラ推力変換装置 |
US5482436A (en) * | 1993-12-30 | 1996-01-09 | Acme Engineering & Manufacturing Corp. | High specific speed fan propeller having auxiliary blades |
DE4420219A1 (de) * | 1994-06-06 | 1995-12-07 | Stemme Gmbh & Co Kg | Luftfahrzeug |
US5620303A (en) * | 1995-12-11 | 1997-04-15 | Sikorsky Aircraft Corporation | Rotor system having alternating length rotor blades for reducing blade-vortex interaction (BVI) noise |
US5735670A (en) * | 1995-12-11 | 1998-04-07 | Sikorsky Aircraft Corporation | Rotor system having alternating length rotor blades and positioning means therefor for reducing blade-vortex interaction (BVI) noise |
IT1303441B1 (it) * | 1998-12-03 | 2000-11-06 | Vladimiro Lidak | Rotore principale monopala per elicotteri |
FR2892705B1 (fr) * | 2005-11-03 | 2009-04-24 | Airbus France Sas | Aeronef a impact environnemental reduit. |
DK176357B1 (da) * | 2005-11-21 | 2007-09-24 | Lm Glasfiber As | Et vindenergianlæg med ekstra sæt vinger |
US8608441B2 (en) * | 2006-06-12 | 2013-12-17 | Energyield Llc | Rotatable blade apparatus with individually adjustable blades |
GB0702608D0 (en) * | 2007-02-10 | 2007-03-21 | Rolls Royce Plc | Aeroengine |
US8661781B2 (en) * | 2009-02-13 | 2014-03-04 | The Boeing Company | Counter rotating fan design and variable blade row spacing optimization for low environmental impact |
US8821118B2 (en) * | 2009-12-21 | 2014-09-02 | The Boeing Company | Optimization of downstream open fan propeller position |
FR2958980B1 (fr) * | 2010-04-14 | 2013-03-15 | Snecma | Dispositif redresseur pour turbomachine |
FR2963067B1 (fr) * | 2010-07-23 | 2012-08-24 | Snecma | Turbomoteur a double helice non carenee |
GB2482333A (en) * | 2010-07-30 | 2012-02-01 | Ge Aviat Systems Ltd | Aircraft propeller |
FR2974060B1 (fr) * | 2011-04-15 | 2013-11-22 | Snecma | Dispositif de propulsion a helices contrarotatives et coaxiales non-carenees |
FR2980818B1 (fr) | 2011-09-29 | 2016-01-22 | Snecma | Pale pour une helice de turbomachine, notamment a soufflante non carenee, helice et turbomachine correspondantes. |
FR2999151B1 (fr) | 2012-12-07 | 2017-01-27 | Snecma | Pale d'helice pour turbomachine |
FR3006292B1 (fr) * | 2013-05-30 | 2017-01-27 | Eurocopter France | Giravion a voilure tournante muni d'une pluralite d'helices |
US9714575B2 (en) * | 2013-11-27 | 2017-07-25 | Hamilton Sundstrand Corporation | Differential blade design for propeller noise reduction |
US20150344127A1 (en) * | 2014-05-31 | 2015-12-03 | General Electric Company | Aeroelastically tailored propellers for noise reduction and improved efficiency in a turbomachine |
FR3030446B1 (fr) * | 2014-12-17 | 2018-06-01 | Safran Aircraft Engines | Turbomachine a helice multi-diametres |
US10604245B2 (en) * | 2016-12-30 | 2020-03-31 | Wing Aviation Llc | Rotor units having asymmetric rotor blades |
US10837459B2 (en) * | 2017-10-06 | 2020-11-17 | Pratt & Whitney Canada Corp. | Mistuned fan for gas turbine engine |
-
2014
- 2014-12-17 FR FR1462652A patent/FR3030446B1/fr active Active
-
2015
- 2015-12-17 JP JP2017532777A patent/JP6758293B2/ja active Active
- 2015-12-17 BR BR112017012436A patent/BR112017012436B8/pt active IP Right Grant
- 2015-12-17 RU RU2017124871A patent/RU2718866C2/ru active
- 2015-12-17 EP EP15830811.4A patent/EP3233627B1/fr active Active
- 2015-12-17 WO PCT/FR2015/053600 patent/WO2016097635A1/fr active Application Filing
- 2015-12-17 CN CN201580069207.7A patent/CN107108015B/zh active Active
- 2015-12-17 US US15/535,773 patent/US10494086B2/en active Active
- 2015-12-17 CA CA2970092A patent/CA2970092C/fr active Active
Also Published As
Publication number | Publication date |
---|---|
US10494086B2 (en) | 2019-12-03 |
FR3030446B1 (fr) | 2018-06-01 |
EP3233627A1 (fr) | 2017-10-25 |
BR112017012436A2 (pt) | 2018-01-02 |
CA2970092C (fr) | 2022-08-16 |
JP2018501142A (ja) | 2018-01-18 |
JP6758293B2 (ja) | 2020-09-23 |
RU2017124871A3 (pt) | 2019-05-30 |
RU2017124871A (ru) | 2019-01-17 |
BR112017012436B1 (pt) | 2021-12-14 |
CN107108015B (zh) | 2019-03-08 |
RU2718866C2 (ru) | 2020-04-15 |
FR3030446A1 (fr) | 2016-06-24 |
WO2016097635A1 (fr) | 2016-06-23 |
EP3233627B1 (fr) | 2018-10-17 |
CA2970092A1 (fr) | 2016-06-23 |
CN107108015A (zh) | 2017-08-29 |
US20170369153A1 (en) | 2017-12-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
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] | ||
B09W | Correction of the decision to grant [chapter 9.1.4 patent gazette] |
Free format text: RETIFICACAO DA PUBLICACAO (9.1) |
|
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 17/12/2015, OBSERVADAS AS CONDICOES LEGAIS. |
|
B16C | Correction of notification of the grant [chapter 16.3 patent gazette] |
Free format text: REF. RPI 2658 DE 14/12/2021 QUANTO AOS DESENHOS. |