ES2398316R1 - Sistema versatil de potencia en aeronaves - Google Patents

Sistema versatil de potencia en aeronaves

Info

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
Application number
ES201131220A
Other languages
English (en)
Other versions
ES2398316B1 (es
ES2398316A2 (es
Inventor
Montero Carlos Casado
Jimenez Alfredo Ruiz
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SL
Original Assignee
Airbus Operations SL
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 Airbus Operations SL filed Critical Airbus Operations SL
Priority to ES201131220A priority Critical patent/ES2398316B1/es
Priority to EP12176470.8A priority patent/EP2548802A3/en
Priority to CA2783253A priority patent/CA2783253A1/en
Priority to US13/550,929 priority patent/US20130181088A1/en
Priority to RU2012130452/11A priority patent/RU2012130452A/ru
Priority to CN2012102478485A priority patent/CN103112592A/zh
Publication of ES2398316A2 publication Critical patent/ES2398316A2/es
Publication of ES2398316R1 publication Critical patent/ES2398316R1/es
Application granted granted Critical
Publication of ES2398316B1 publication Critical patent/ES2398316B1/es
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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; ARRANGEMENTS 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; ARRANGEMENTS 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

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).
ES201131220A 2011-07-18 2011-07-18 Sistema versátil de potencia en aeronaves Expired - Fee Related ES2398316B1 (es)

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
US13/550,929 US20130181088A1 (en) 2011-07-18 2012-07-17 Aircraft versatile power system
CN2012102478485A CN103112592A (zh) 2011-07-18 2012-07-17 飞行器通用动力系统

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)

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WO2014158247A1 (en) * 2013-03-13 2014-10-02 Pesyna Kenneth M 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
EP3931091A4 (en) 2019-03-01 2023-01-11 Pratt & Whitney Canada Corp. DISTRIBUTED PROPULSION CONFIGURATIONS FOR AIRCRAFT WITH MIXED PROPULSION SYSTEMS
US11732639B2 (en) 2019-03-01 2023-08-22 Pratt & Whitney Canada Corp. Mechanical disconnects for parallel power lanes in hybrid electric propulsion systems
US11628942B2 (en) 2019-03-01 2023-04-18 Pratt & Whitney Canada Corp. Torque ripple control for an aircraft power train
US11535392B2 (en) 2019-03-18 2022-12-27 Pratt & Whitney Canada Corp. 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
US20230123752A1 (en) * 2021-10-20 2023-04-20 Innoveering, LLC Deployable inlet assembly for aerial vehicle

Citations (4)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (4)

* Cited by examiner, † Cited by third party
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
EP2548802A2 (en) 2013-01-23
CN103112592A (zh) 2013-05-22
EP2548802A3 (en) 2017-06-21
CA2783253A1 (en) 2013-01-18
ES2398316B1 (es) 2014-04-29
US20130181088A1 (en) 2013-07-18
ES2398316A2 (es) 2013-03-15
RU2012130452A (ru) 2014-01-27

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