ES2398316R1 - Sistema versatil de potencia en aeronaves - Google Patents
Sistema versatil de potencia en aeronavesInfo
- Publication number
- ES2398316R1 ES2398316R1 ES201131220A ES201131220A ES2398316R1 ES 2398316 R1 ES2398316 R1 ES 2398316R1 ES 201131220 A ES201131220 A ES 201131220A ES 201131220 A ES201131220 A ES 201131220A ES 2398316 R1 ES2398316 R1 ES 2398316R1
- Authority
- ES
- Spain
- Prior art keywords
- aircraft
- engine
- versatile
- movement
- 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.)
- Granted
Links
- 230000009977 dual effect Effects 0.000 abstract 1
- 230000001141 propulsive effect Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/405—Powered wheels, e.g. for taxing
-
- 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
- B64D41/00—Power installations for auxiliary purposes
-
- 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
- B64D2205/00—Aircraft with means for ground manoeuvring, such as taxiing, using an auxiliary thrust system, e.g. jet-engines, propellers or compressed air
-
- 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
- Y02T50/80—Energy efficient operational measures, e.g. ground operations or mission management
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Transmission Devices (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
- Arrangement Of Transmissions (AREA)
Abstract
Sistema versátil de potencia en aeronaves. Un sistema versátil de potencia (1) en aeronaves comprende un motor de reacción atmosférico (2), un convertidor de potencia (6), y un motor (4). El convertidor de potencia (6) transforma en otro tipo de energía el movimiento que el motor de reacción atmosférico (2) proporciona al eje. El motor (4) utiliza la energía suministrada por el convertidor de potencia (6) para mover un eje (14) del motor, y el eje (14) del motor gira las ruedas del tren de aterrizaje (3), generando el movimiento de la aeronave. El motor de reacción atmosférico (2) también produce empuje, permitiendo una operación propulsiva de la aeronave dual bien por el movimiento de las ruedas del tren de aterrizaje (3), o por el empuje directo a través de la tobera (25).
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES201131220A ES2398316B1 (es) | 2011-07-18 | 2011-07-18 | Sistema versátil de potencia en aeronaves |
EP12176470.8A EP2548802A3 (en) | 2011-07-18 | 2012-07-13 | Aircraft versatile power system |
CA2783253A CA2783253A1 (en) | 2011-07-18 | 2012-07-16 | Aircraft versatile power system |
RU2012130452/11A RU2012130452A (ru) | 2011-07-18 | 2012-07-17 | Многофункциональная система энергоснабжения летательного аппарата |
CN2012102478485A CN103112592A (zh) | 2011-07-18 | 2012-07-17 | 飞行器通用动力*** |
US13/550,929 US20130181088A1 (en) | 2011-07-18 | 2012-07-17 | Aircraft versatile power system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES201131220A ES2398316B1 (es) | 2011-07-18 | 2011-07-18 | Sistema versátil de potencia en aeronaves |
Publications (3)
Publication Number | Publication Date |
---|---|
ES2398316A2 ES2398316A2 (es) | 2013-03-15 |
ES2398316R1 true ES2398316R1 (es) | 2013-06-12 |
ES2398316B1 ES2398316B1 (es) | 2014-04-29 |
Family
ID=46603574
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES201131220A Expired - Fee Related ES2398316B1 (es) | 2011-07-18 | 2011-07-18 | Sistema versátil de potencia en aeronaves |
Country Status (6)
Country | Link |
---|---|
US (1) | US20130181088A1 (es) |
EP (1) | EP2548802A3 (es) |
CN (1) | CN103112592A (es) |
CA (1) | CA2783253A1 (es) |
ES (1) | ES2398316B1 (es) |
RU (1) | RU2012130452A (es) |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9517843B2 (en) * | 2013-03-13 | 2016-12-13 | Rolls-Royce North American Technologies, Inc. | Generator for flight vehicle |
US9193451B2 (en) * | 2013-04-22 | 2015-11-24 | Ival O. Salyer | Aircraft using turbo-electric hybrid propulsion system for multi-mode operation |
US9139291B2 (en) | 2013-05-28 | 2015-09-22 | Hamilton Sundstrand Corporation | Integrated hydrostatic transmission for electronic taxiing operations |
FR3006991B1 (fr) * | 2013-06-14 | 2016-12-23 | European Aeronautic Defence & Space Co Eads France | Avion a dispositif d'assistance au decollage et procede de mise en oeuvre |
GB201315012D0 (en) * | 2013-08-22 | 2013-10-02 | Airbus Uk Ltd | Aircraft autonomous pushback |
US20150283908A1 (en) * | 2014-04-02 | 2015-10-08 | Hamilton Sundstrand Corporation | Systems utilizing a controllable voltage ac generator system |
US20170036773A1 (en) * | 2015-08-07 | 2017-02-09 | Pratt & Whitney Canada Corp. | Inflight power management for aircraft |
US9771149B2 (en) * | 2015-10-30 | 2017-09-26 | Honeywell International Inc. | Gate departure system for aircraft |
GB201519755D0 (en) * | 2015-11-09 | 2015-12-23 | Airbus Operations Ltd And Airbus Operations Gmbh | Cooling of a motor for driving an aircraft wheel |
US20180265213A1 (en) * | 2017-03-17 | 2018-09-20 | Hamilton Sundstrand Corporation | Emergency power generation via electrically driven tail cone boundary layer ingestion thruster |
US10822100B2 (en) * | 2017-06-26 | 2020-11-03 | General Electric Company | Hybrid electric propulsion system for an aircraft |
US11149649B2 (en) * | 2018-08-17 | 2021-10-19 | Raytheon Technologies Corporation | Hybrid gas turbine engine system powered warm-up |
US11628942B2 (en) | 2019-03-01 | 2023-04-18 | Pratt & Whitney Canada Corp. | Torque ripple control for an aircraft power train |
CA3132266A1 (en) | 2019-03-01 | 2020-09-10 | Pratt & Whitney Canada Corp. | Distributed propulsion configurations for aircraft having mixed drive systems |
US11732639B2 (en) | 2019-03-01 | 2023-08-22 | Pratt & Whitney Canada Corp. | Mechanical disconnects for parallel power lanes in hybrid electric propulsion systems |
WO2020190344A2 (en) | 2019-03-18 | 2020-09-24 | United Technologies Advanced Projects Inc. | Architectures for hybrid-electric propulsion |
US11486472B2 (en) | 2020-04-16 | 2022-11-01 | United Technologies Advanced Projects Inc. | Gear sytems with variable speed drive |
US11827372B2 (en) | 2020-05-15 | 2023-11-28 | Pratt & Whitney Canada Corp. | Engine characteristics matching |
US12030651B2 (en) | 2021-01-05 | 2024-07-09 | Pratt & Whitney Canada Corp. | Parallel hybrid power plant with hollow motor |
US11999500B2 (en) * | 2021-10-20 | 2024-06-04 | General Electric Company | Deployable inlet assembly for aerial vehicle |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1995029094A1 (en) * | 1994-04-22 | 1995-11-02 | Greenlite Limited | Aircraft landing-gear drive system |
US6247668B1 (en) * | 1999-07-15 | 2001-06-19 | The Boeing Company | Auxiliary power and thrust unit |
US20060065779A1 (en) * | 2004-09-28 | 2006-03-30 | The Boeing Company | Powered nose aircraft wheel system |
US20100044504A1 (en) * | 2008-02-29 | 2010-02-25 | Airbus France | Rear propulsion system with lateral air inlets for an aircraft with such system |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4936748A (en) * | 1988-11-28 | 1990-06-26 | General Electric Company | Auxiliary power source in an unducted fan gas turbine engine |
US7802757B2 (en) | 2005-11-09 | 2010-09-28 | Pratt & Whitney Canada Corp. | Method and system for taxiing an aircraft |
US7891609B2 (en) | 2006-08-29 | 2011-02-22 | Borealis Technical Limited | Turnaround methods |
CN101172523A (zh) * | 2006-10-31 | 2008-05-07 | 通用电气公司 | 辅助动力装置总成 |
US7980509B2 (en) * | 2007-03-08 | 2011-07-19 | The Ashman Group, Llc | Aircraft taxiing systems |
DE102009010243A1 (de) * | 2009-02-24 | 2010-09-02 | Airbus Deutschland Gmbh | Leistungserzeugungs-Vorrichtung sowie Rumpf-Bauteil mit einer solchen Leistungserzeugungs-Vorrichtung |
FR2954283B1 (fr) * | 2009-12-23 | 2012-03-02 | Hispano Suiza Sa | Aeronef comportant un demarreur-generateur electrique pour le ou chaque turboreacteur et un train d'aterrissage equipe d'un moteur electrique de manoeuvre au sol |
US8622342B2 (en) * | 2011-06-17 | 2014-01-07 | Embraer S.A. | On-board aircraft auxiliary power systems having dual auxiliary power units |
US8444083B2 (en) * | 2011-06-30 | 2013-05-21 | Hamilton Sundstrand Corporation | Auxiliary power unit inlet |
-
2011
- 2011-07-18 ES ES201131220A patent/ES2398316B1/es not_active Expired - Fee Related
-
2012
- 2012-07-13 EP EP12176470.8A patent/EP2548802A3/en not_active Withdrawn
- 2012-07-16 CA CA2783253A patent/CA2783253A1/en not_active Abandoned
- 2012-07-17 CN CN2012102478485A patent/CN103112592A/zh active Pending
- 2012-07-17 RU RU2012130452/11A patent/RU2012130452A/ru not_active Application Discontinuation
- 2012-07-17 US US13/550,929 patent/US20130181088A1/en not_active Abandoned
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1995029094A1 (en) * | 1994-04-22 | 1995-11-02 | Greenlite Limited | Aircraft landing-gear drive system |
US6247668B1 (en) * | 1999-07-15 | 2001-06-19 | The Boeing Company | Auxiliary power and thrust unit |
US20060065779A1 (en) * | 2004-09-28 | 2006-03-30 | The Boeing Company | Powered nose aircraft wheel system |
US20100044504A1 (en) * | 2008-02-29 | 2010-02-25 | Airbus France | Rear propulsion system with lateral air inlets for an aircraft with such system |
Also Published As
Publication number | Publication date |
---|---|
ES2398316B1 (es) | 2014-04-29 |
RU2012130452A (ru) | 2014-01-27 |
EP2548802A2 (en) | 2013-01-23 |
US20130181088A1 (en) | 2013-07-18 |
ES2398316A2 (es) | 2013-03-15 |
CA2783253A1 (en) | 2013-01-18 |
EP2548802A3 (en) | 2017-06-21 |
CN103112592A (zh) | 2013-05-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
Ref document number: 2398316 Country of ref document: ES Kind code of ref document: B1 Effective date: 20140429 |
|
FD2A | Announcement of lapse in spain |
Effective date: 20210915 |