ES2659427T3 - Conjunto de transmisión para aeronave y helicóptero - Google Patents
Conjunto de transmisión para aeronave y helicóptero Download PDFInfo
- Publication number
- ES2659427T3 ES2659427T3 ES15717024.2T ES15717024T ES2659427T3 ES 2659427 T3 ES2659427 T3 ES 2659427T3 ES 15717024 T ES15717024 T ES 15717024T ES 2659427 T3 ES2659427 T3 ES 2659427T3
- Authority
- ES
- Spain
- Prior art keywords
- coupled
- transmission assembly
- rotor
- helicopter
- output shaft
- Prior art date
- Legal status (The legal status 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 status listed.)
- Active
Links
- 230000005540 biological transmission Effects 0.000 title abstract 6
- 230000001105 regulatory effect Effects 0.000 abstract 2
- 230000002441 reversible effect Effects 0.000 abstract 2
Classifications
-
- 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
- F16H—GEARING
- F16H3/00—Toothed gearings for conveying rotary motion with variable gear ratio or for reversing rotary motion
- F16H3/44—Toothed gearings for conveying rotary motion with variable gear ratio or for reversing rotary motion using gears having orbital motion
- F16H3/72—Toothed gearings for conveying rotary motion with variable gear ratio or for reversing rotary motion using gears having orbital motion with a secondary drive, e.g. regulating motor, in order to vary speed continuously
- F16H3/724—Toothed gearings for conveying rotary motion with variable gear ratio or for reversing rotary motion using gears having orbital motion with a secondary drive, e.g. regulating motor, in order to vary speed continuously using external powered electric machines
- F16H3/725—Toothed gearings for conveying rotary motion with variable gear ratio or for reversing rotary motion using gears having orbital motion with a secondary drive, e.g. regulating motor, in order to vary speed continuously using external powered electric machines with means to change ratio in the mechanical gearing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K6/00—Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines ; Control systems therefor, i.e. systems controlling two or more prime movers, or controlling one of these prime movers and any of the transmission, drive or drive units Informative references: mechanical gearings with secondary electric drive F16H3/72; arrangements for handling mechanical energy structurally associated with the dynamo-electric machine H02K7/00; machines comprising structurally interrelated motor and generator parts H02K51/00; dynamo-electric machines not otherwise provided for in H02K see H02K99/00
- B60K6/08—Prime-movers comprising combustion engines and mechanical or fluid energy storing means
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
- B64C27/14—Direct drive between power plant and rotor hub
-
- 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
- F16H—GEARING
- F16H3/00—Toothed gearings for conveying rotary motion with variable gear ratio or for reversing rotary motion
- F16H3/44—Toothed gearings for conveying rotary motion with variable gear ratio or for reversing rotary motion using gears having orbital motion
- F16H3/72—Toothed gearings for conveying rotary motion with variable gear ratio or for reversing rotary motion using gears having orbital motion with a secondary drive, e.g. regulating motor, in order to vary speed continuously
-
- 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
- F16H—GEARING
- F16H3/00—Toothed gearings for conveying rotary motion with variable gear ratio or for reversing rotary motion
- F16H3/44—Toothed gearings for conveying rotary motion with variable gear ratio or for reversing rotary motion using gears having orbital motion
- F16H3/72—Toothed gearings for conveying rotary motion with variable gear ratio or for reversing rotary motion using gears having orbital motion with a secondary drive, e.g. regulating motor, in order to vary speed continuously
- F16H3/724—Toothed gearings for conveying rotary motion with variable gear ratio or for reversing rotary motion using gears having orbital motion with a secondary drive, e.g. regulating motor, in order to vary speed continuously using external powered electric machines
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Transportation (AREA)
- Retarders (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Testing Of Balance (AREA)
Abstract
Helicóptero que comprende un primer motor, que incluye al menos una primera turbomáquina (10), un rotor (90) y un conjunto de transmisión, estando el conjunto de transmisión configurado para transmitir un par mecánico proveniente del primer motor (10) hacia el rotor (90), en el que el conjunto de transmisión comprende un primer árbol de entrada (10a), configurado para recibir un par mecánico desde el primer motor (10), un árbol de salida (60a), configurado para transmitir un par mecánico hacia el rotor (90), caracterizado por que el conjunto de transmisión comprende un primer órgano de transmisión (20) con al menos dos grados de movilidad que comprende unas primera, segunda y tercera partes móviles, una primera máquina eléctrica reversible de regulación (30), pilotable, y una primera máquina eléctrica reversible de equilibrado (40), por que el árbol de entrada (10a) está acoplado a la primera parte móvil (22a), el árbol de salida (60a) está acoplado a la segunda parte móvil (23), la primera máquina eléctrica de regulación (30) está acoplada a la tercera parte móvil (21), y la primera máquina eléctrica de equilibrado (40) está acoplada en serie en el árbol de entrada o el árbol de salida (60a).
Description
Claims (1)
-
imagen1 imagen2
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1452615A FR3019247B1 (fr) | 2014-03-27 | 2014-03-27 | Ensemble de transmission pour aeronef et helicoptere |
FR1452615 | 2014-03-27 | ||
PCT/FR2015/050707 WO2015145046A1 (fr) | 2014-03-27 | 2015-03-20 | Ensemble de transmission pour aeronef et helicoptere |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2659427T3 true ES2659427T3 (es) | 2018-03-15 |
Family
ID=51483523
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES15717024.2T Active ES2659427T3 (es) | 2014-03-27 | 2015-03-20 | Conjunto de transmisión para aeronave y helicóptero |
Country Status (11)
Country | Link |
---|---|
US (1) | US9982758B2 (es) |
EP (1) | EP3122627B1 (es) |
JP (1) | JP6651458B2 (es) |
KR (1) | KR102255162B1 (es) |
CN (1) | CN106461031B (es) |
CA (1) | CA2943918C (es) |
ES (1) | ES2659427T3 (es) |
FR (1) | FR3019247B1 (es) |
PL (1) | PL3122627T3 (es) |
RU (1) | RU2672536C2 (es) |
WO (1) | WO2015145046A1 (es) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP6879865B2 (ja) * | 2017-08-28 | 2021-06-02 | 本田技研工業株式会社 | マルチコプタ |
US11753178B2 (en) | 2019-11-12 | 2023-09-12 | General Electric Company | Systems and methods for removing heat from aircraft components |
CN113404595A (zh) | 2020-03-16 | 2021-09-17 | 通用电气公司 | 燃气涡轮发动机及其操作方法 |
FR3115825A1 (fr) * | 2020-11-04 | 2022-05-06 | Airbus Helicopters | Procédé de pilotage d’une installation motrice d’un giravion comprenant au moins deux turbomoteurs |
JP7365325B2 (ja) * | 2020-12-22 | 2023-10-19 | 本田技研工業株式会社 | ガスタービンシステム |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB8625712D0 (en) * | 1986-10-28 | 1987-03-18 | Westland Plc | Transmission system |
JP3029976B2 (ja) * | 1995-01-27 | 2000-04-10 | 株式会社コミュータヘリコプタ先進技術研究所 | ヘリコプタの動力伝達装置 |
JP2948116B2 (ja) * | 1995-01-27 | 1999-09-13 | 株式会社コミュータヘリコプタ先進技術研究所 | ヘリコプタの動力伝達装置 |
JP3402236B2 (ja) * | 1999-01-13 | 2003-05-06 | トヨタ自動車株式会社 | 動力出力装置およびハイブリッド車両並びにその制御方法 |
US6835154B2 (en) * | 1999-10-15 | 2004-12-28 | New Venture Gear, Inc. | On-demand transfer case |
FR2871138B1 (fr) * | 2004-06-07 | 2006-08-04 | Eurocopter France | Mecanisme de transmission entre des accessoires et les organes moteurs d'entrainement du rotor d'un giravion, selectivement isolement ou conjointement |
US7296767B2 (en) * | 2005-05-31 | 2007-11-20 | Sikorsky Aircraft Corporation | Variable speed transmission for a rotary wing aircraft |
JP4450017B2 (ja) * | 2007-06-22 | 2010-04-14 | トヨタ自動車株式会社 | 動力出力装置およびそれを備えたハイブリッド自動車 |
FR2929324B1 (fr) * | 2008-03-25 | 2012-10-12 | Turbomeca | Turbomoteur comportant une machine electrique reversible |
JP5628339B2 (ja) * | 2009-12-10 | 2014-11-19 | ルノー・トラックス | 乗り物の補機のための駆動アレンジメント |
FR2962404B1 (fr) * | 2010-07-08 | 2012-07-20 | Eurocopter France | Architecture electrique pour aeronef a voilure tournante a motorisation hybride |
US20130133480A1 (en) * | 2011-11-28 | 2013-05-30 | Icr Turbine Engine Corporation | Hybrid drive train for a gas turbine engine |
CA2820254C (en) * | 2012-07-09 | 2020-02-18 | Mcmaster University | Hybrid powertrain system |
US9290266B2 (en) * | 2013-03-15 | 2016-03-22 | Bell Helicopter Textron Inc. | Speed control assembly and methods of using same |
JP2016098986A (ja) * | 2014-11-26 | 2016-05-30 | トヨタ自動車株式会社 | 車両用駆動装置 |
EP3051177B1 (en) * | 2014-12-15 | 2021-03-17 | Rolls-Royce plc | Variable speed drive arrangement |
US20160252063A1 (en) * | 2015-02-27 | 2016-09-01 | Avl Powertrain Engineering, Inc. | Variable Drive For Liquified Natural Gas Pump |
-
2014
- 2014-03-27 FR FR1452615A patent/FR3019247B1/fr active Active
-
2015
- 2015-03-20 ES ES15717024.2T patent/ES2659427T3/es active Active
- 2015-03-20 EP EP15717024.2A patent/EP3122627B1/fr active Active
- 2015-03-20 RU RU2016141938A patent/RU2672536C2/ru active
- 2015-03-20 CN CN201580016712.5A patent/CN106461031B/zh active Active
- 2015-03-20 US US15/129,356 patent/US9982758B2/en active Active
- 2015-03-20 KR KR1020167030207A patent/KR102255162B1/ko active IP Right Grant
- 2015-03-20 WO PCT/FR2015/050707 patent/WO2015145046A1/fr active Application Filing
- 2015-03-20 JP JP2016559225A patent/JP6651458B2/ja not_active Expired - Fee Related
- 2015-03-20 PL PL15717024T patent/PL3122627T3/pl unknown
- 2015-03-20 CA CA2943918A patent/CA2943918C/fr active Active
Also Published As
Publication number | Publication date |
---|---|
KR102255162B1 (ko) | 2021-05-24 |
JP6651458B2 (ja) | 2020-02-19 |
KR20160138264A (ko) | 2016-12-02 |
FR3019247B1 (fr) | 2017-09-01 |
CN106461031B (zh) | 2019-05-03 |
FR3019247A1 (fr) | 2015-10-02 |
EP3122627B1 (fr) | 2018-01-10 |
CA2943918C (fr) | 2022-10-25 |
CA2943918A1 (fr) | 2015-10-01 |
JP2017512699A (ja) | 2017-05-25 |
RU2016141938A3 (es) | 2018-09-12 |
WO2015145046A1 (fr) | 2015-10-01 |
EP3122627A1 (fr) | 2017-02-01 |
US20170175856A1 (en) | 2017-06-22 |
PL3122627T3 (pl) | 2018-04-30 |
RU2016141938A (ru) | 2018-04-27 |
US9982758B2 (en) | 2018-05-29 |
RU2672536C2 (ru) | 2018-11-15 |
CN106461031A (zh) | 2017-02-22 |
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