BRPI0821412A2 - Configuração otimizada de motores para aeronave - Google Patents

Configuração otimizada de motores para aeronave

Info

Publication number
BRPI0821412A2
BRPI0821412A2 BRPI0821412-3A BRPI0821412A BRPI0821412A2 BR PI0821412 A2 BRPI0821412 A2 BR PI0821412A2 BR PI0821412 A BRPI0821412 A BR PI0821412A BR PI0821412 A2 BRPI0821412 A2 BR PI0821412A2
Authority
BR
Brazil
Prior art keywords
aircraft engine
engine configuration
optimized aircraft
optimized
configuration
Prior art date
Application number
BRPI0821412-3A
Other languages
English (en)
Inventor
José Miguel Vizarro Toribio
Raúl Carlos Llamas Sandin
Stephane Viala
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
Publication of BRPI0821412A2 publication Critical patent/BRPI0821412A2/pt
Publication of BRPI0821412B1 publication Critical patent/BRPI0821412B1/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C15/00—Attitude, flight direction, or altitude control by jet reaction
    • B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
    • B64C15/12—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets the power plant being tiltable
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • B64D27/14—Aircraft characterised by the type or position of power plants of gas-turbine type  within, or attached to, fuselages
    • 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
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Transmission Devices (AREA)
  • General Details Of Gearings (AREA)
  • Tires In General (AREA)
  • Vehicle Body Suspensions (AREA)
BRPI0821412-3A 2007-12-21 2008-12-19 Configuração de motores para aeronave localizada na parte traseira da fuselagem da dita aeronave BRPI0821412B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
ES200703399A ES2335459B1 (es) 2007-12-21 2007-12-21 Configuracion optimizada de motores de aeronave.
ESP200703399 2007-12-21
PCT/EP2008/067974 WO2009080732A2 (en) 2007-12-21 2008-12-19 Optimized configuration of engines for aircraft

Publications (2)

Publication Number Publication Date
BRPI0821412A2 true BRPI0821412A2 (pt) 2015-06-16
BRPI0821412B1 BRPI0821412B1 (pt) 2020-06-02

Family

ID=40568626

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0821412-3A BRPI0821412B1 (pt) 2007-12-21 2008-12-19 Configuração de motores para aeronave localizada na parte traseira da fuselagem da dita aeronave

Country Status (7)

Country Link
US (1) US7967243B2 (pt)
EP (1) EP2234885B1 (pt)
BR (1) BRPI0821412B1 (pt)
CA (1) CA2710065C (pt)
ES (1) ES2335459B1 (pt)
RU (1) RU2485021C2 (pt)
WO (1) WO2009080732A2 (pt)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8271149B2 (en) * 2006-08-21 2012-09-18 Bell Helicopter Textron Inc. Conversion system fault management system for tiltrotor aircraft
ES2391967B1 (es) * 2010-01-14 2013-10-10 Airbus Operations, S.L. Pilón de soporte de motores de aeronaves.
ES2392617B1 (es) * 2010-01-15 2013-11-21 Airbus Operations S.L. Disposición de unión de los cajones laterales de un estabilizador horizontal de cola con un cajón central tubular y procedimiento de fabricación de dicho cajón.
ES2398861B1 (es) 2010-10-08 2014-04-29 Airbus Operations, S.L. Concepto de unión intercambiable para un cono de un fuselaje trasero de un avión.
FR3020338B1 (fr) * 2014-04-28 2016-05-20 Airbus Operations Sas Partie arriere d'aeronef pourvue d'une structure de support des moteurs de forme optimisee
EP3303140A1 (en) 2015-05-29 2018-04-11 Bombardier Inc. Method and system for aligning propulsion system and vehicle having such propulsion alignment
FR3052743B1 (fr) * 2016-06-20 2018-07-06 Airbus Operations Ensemble pour aeronef comprenant des moteurs a propulsion par ingestion de la couche limite
ES2835263T3 (es) * 2016-12-20 2021-06-22 Airbus Operations Sl Sistema de propulsión rotativo de una aeronave
US11111029B2 (en) * 2017-07-28 2021-09-07 The Boeing Company System and method for operating a boundary layer ingestion fan
US10906657B2 (en) * 2018-06-19 2021-02-02 Raytheon Technologies Corporation Aircraft system with distributed propulsion
US10759545B2 (en) 2018-06-19 2020-09-01 Raytheon Technologies Corporation Hybrid electric aircraft system with distributed propulsion

Family Cites Families (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1726062A (en) * 1928-10-16 1929-08-27 Clarence C Gilman Dirigible aircraft
US1871538A (en) * 1931-04-07 1932-08-16 Leupold Mathias Airplane
GB400735A (en) * 1931-12-31 1933-11-02 Harold Bolas Improvements in or relating to aircraft
FR811928A (fr) * 1936-10-20 1937-04-26 Dispositif permettant de faire varier la sustentation des avions et hydravions pendant le vol
GB526899A (en) * 1938-04-08 1940-09-27 Rene Tampier Improvements in aircraft
US2257940A (en) * 1938-06-22 1941-10-07 Dornier Werke Gmbh Airplane having a liftable pusher plant
US2969935A (en) * 1957-09-09 1961-01-31 Carl C Price Convertible aircraft
US3109614A (en) * 1961-10-23 1963-11-05 Boeing Co Fin-tip mounted horizontal control surface for airplanes
US3212733A (en) * 1964-07-30 1965-10-19 Gen Electric Cruise fan coupling system
GB1157822A (en) * 1965-08-21 1969-07-09 Boelkow Gmbh VTOL Aircraft
US4982914A (en) * 1966-05-18 1991-01-08 Karl Eickmann Aircraft with a plurality of propellers, a pipe structure for thereon holdable wings, for vertical take off and landing
US3756529A (en) * 1972-05-01 1973-09-04 Mc Donnell Douglas Corp Fuselage seal
US3995794A (en) * 1975-06-24 1976-12-07 Lanier Edward M Super-short take off and landing apparatus
US4034939A (en) * 1975-11-05 1977-07-12 The Boeing Company Assembly for sealing the mounting opening for a flying horizontal stabilizer on a vertical stabilizer
US4149688A (en) * 1976-10-01 1979-04-17 Aereon Corporation Lifting body aircraft for V/STOL service
GB2025864A (en) * 1978-07-18 1980-01-30 British Aerospace Aircraft
US4492353A (en) * 1982-09-30 1985-01-08 Phillips Bryan D Aircraft capable of vertical short takeoff and landing
US4966338A (en) * 1987-08-05 1990-10-30 General Electric Company Aircraft pylon
FR2647414B1 (fr) * 1989-05-23 1991-09-06 Delmotte Didier Adaptations de motoreacteurs a helices a pistons rotatifs sur cellules d'aeronefs
US5020740A (en) * 1990-03-28 1991-06-04 Thomas Hugh O Pitch control trimming system for canard design aircraft
RU2104228C1 (ru) * 1993-07-01 1998-02-10 Самарское государственное научно-производственное предприятие "Труд" Устройство для крепления авиационного двигателя к самолету
US5957405A (en) * 1997-07-21 1999-09-28 Williams International Co., L.L.C. Twin engine aircraft
US6138943A (en) * 1998-12-11 2000-10-31 Huang; Yung-Chi Foldable ascending/descending wing stand for flying apparatus
IT1308096B1 (it) * 1999-06-02 2001-11-29 Finmeccanica Spa Convertiplano
US6938408B2 (en) * 2001-04-26 2005-09-06 Propulsion Vectoring, L.P. Thrust vectoring and variable exhaust area for jet engine nozzle
DE102005003297B4 (de) * 2005-01-24 2007-03-29 Eads Deutschland Gmbh Flugzeug mit einer Rumpfhecksektion zur Anbindung von Höhen- und Seitenleitwerken
US7766275B2 (en) * 2006-06-12 2010-08-03 The Boeing Company Aircraft having a pivotable powerplant

Also Published As

Publication number Publication date
US7967243B2 (en) 2011-06-28
ES2335459A1 (es) 2010-03-26
EP2234885A2 (en) 2010-10-06
RU2010130564A (ru) 2012-01-27
CA2710065C (en) 2015-09-22
BRPI0821412B1 (pt) 2020-06-02
CA2710065A1 (en) 2009-07-02
WO2009080732A2 (en) 2009-07-02
RU2485021C2 (ru) 2013-06-20
EP2234885B1 (en) 2013-02-13
WO2009080732A3 (en) 2009-09-11
US20090159741A1 (en) 2009-06-25
ES2335459B1 (es) 2011-02-03

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
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]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 10 (DEZ) ANOS CONTADOS A PARTIR DE 02/06/2020, OBSERVADAS AS CONDICOES LEGAIS.

B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 13A ANUIDADE.

B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)

Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2649 DE 13-10-2021 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.