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BRPI1008978A2 - avião com empenagem em cauda de bacalhau e motor traseiro - Google Patents

avião com empenagem em cauda de bacalhau e motor traseiro

Info

Publication number
BRPI1008978A2
BRPI1008978A2 BRPI1008978A BRPI1008978A BRPI1008978A2 BR PI1008978 A2 BRPI1008978 A2 BR PI1008978A2 BR PI1008978 A BRPI1008978 A BR PI1008978A BR PI1008978 A BRPI1008978 A BR PI1008978A BR PI1008978 A2 BRPI1008978 A2 BR PI1008978A2
Authority
BR
Brazil
Prior art keywords
fuselage
airplane
tailed
section
rear end
Prior art date
Application number
BRPI1008978A
Other languages
English (en)
Inventor
Genty De La Sagne Jaime
Cazals Olivier
Original Assignee
Airbus Operations Sas
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 Sas filed Critical Airbus Operations Sas
Publication of BRPI1008978A2 publication Critical patent/BRPI1008978A2/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections
    • B64C1/0685—Tail cones
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/26—Attaching the wing or tail units or stabilising surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/06—Fins
    • 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
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
    • 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
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • B64D29/04—Power-plant nacelles, fairings or cowlings associated with fuselages
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0045—Fuselages characterised by special shapes
    • 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
    • Y02T50/10—Drag reduction
    • 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)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)
  • Body Structure For Vehicles (AREA)
  • Vibration Dampers (AREA)

Abstract

"avião com empenagem em cauda de bacalhau e motor traseiro". um avião (1) comporta uma fuselagem (2) de forma alongada segundo um eixo longitudinal x do avião e pelo menos uma asa (3) fixada na fuselagem entre uma extremidade dianteira e uma extremidade traseira (25) da fuselagem. a fuselagem (2) comporta uma parte central (21) sensivelmente cilíndrica e uma parte evolutiva traseira (23) sobre a qual é fixada uma empenagem vertical (4, 4a) e um conjunto propulsivo traseiro (50). entre uma seção de ligação (231) da parte traseira (23) com a parte central (21) da fuselagem e a extremidade traseira (25):- a largura máxima de cada seção da fuselagem é constante ou crescente em direção à traseira até uma largura máxima l da fuselagem; - a altura de cada seção da fuselagem é de decrescente em direção à traseira, de tal modo que a extremidade traseira da fuselagem forma uma borda de escapamento de espessura estreita sensivelmente horizontal na marcação avião e sensivelmente retilíneo; - um reator (51) do conjunto propulsivo é instalado em uma configuração dita semienterrada na fuselagem.
BRPI1008978A 2009-03-12 2010-03-12 avião com empenagem em cauda de bacalhau e motor traseiro BRPI1008978A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0951561A FR2943039B1 (fr) 2009-03-12 2009-03-12 Avion a empennage queue-de-morue et moteur arriere.
PCT/FR2010/050437 WO2010103252A1 (fr) 2009-03-12 2010-03-12 Avion à empennage queue-de-morue et moteur arrière

Publications (1)

Publication Number Publication Date
BRPI1008978A2 true BRPI1008978A2 (pt) 2019-04-16

Family

ID=41170186

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI1008978A BRPI1008978A2 (pt) 2009-03-12 2010-03-12 avião com empenagem em cauda de bacalhau e motor traseiro

Country Status (8)

Country Link
US (1) US8651414B2 (pt)
EP (1) EP2406133B1 (pt)
CN (1) CN102414083B (pt)
BR (1) BRPI1008978A2 (pt)
CA (1) CA2755158A1 (pt)
FR (1) FR2943039B1 (pt)
RU (1) RU2522539C2 (pt)
WO (1) WO2010103252A1 (pt)

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FR3006997B1 (fr) * 2013-06-14 2016-12-23 Airbus Aeronef a moyens de propulsion electriques
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FR3020347B1 (fr) * 2014-04-28 2016-05-20 Airbus Operations Sas Procede d'assemblage d'une partie arriere d'aeronef
US10000293B2 (en) * 2015-01-23 2018-06-19 General Electric Company Gas-electric propulsion system for an aircraft
JP6437347B2 (ja) * 2015-02-27 2018-12-12 三菱重工業株式会社 推力発生装置及び航空機
US9821917B2 (en) * 2015-09-21 2017-11-21 General Electric Company Aft engine for an aircraft
US9884687B2 (en) 2015-09-21 2018-02-06 General Electric Company Non-axis symmetric aft engine
US9815560B2 (en) * 2015-09-21 2017-11-14 General Electric Company AFT engine nacelle shape for an aircraft
US9957055B2 (en) * 2015-09-21 2018-05-01 General Electric Company Aft engine for an aircraft
US10017270B2 (en) 2015-10-09 2018-07-10 General Electric Company Aft engine for an aircraft
US10442541B2 (en) 2015-10-26 2019-10-15 General Electric Company Method and system for cross engine debris avoidance
FR3043984B1 (fr) * 2015-11-25 2017-12-22 Snecma Avion propulse par une turbomachine muni d'un ecran acoustique
US9849966B2 (en) * 2015-12-18 2017-12-26 The Boeing Company Fuselage structure for accommodating tails and canards of different sizes and shapes
US10309341B2 (en) * 2016-01-15 2019-06-04 The Boeing Company Thrust reverser cascade systems and methods
US10472081B2 (en) * 2016-03-17 2019-11-12 United Technologies Corporation Cross flow fan for wide aircraft fuselage
FR3052743B1 (fr) * 2016-06-20 2018-07-06 Airbus Operations Ensemble pour aeronef comprenant des moteurs a propulsion par ingestion de la couche limite
CN106081127B (zh) * 2016-07-27 2018-12-25 冯政尧 空难逃生飞机
US10364021B2 (en) * 2016-09-26 2019-07-30 General Electric Company Aircraft having an aft engine and stabilizer root fillet
US10486796B2 (en) * 2016-09-26 2019-11-26 General Electric Company Aircraft having an AFT engine and stabilizer with a varying line of maximum thickness
FR3056556B1 (fr) * 2016-09-29 2018-10-19 Safran Aircraft Engines Aeronef a turbomachine integree au fuselage arriere comportant une helice entourant un carter d'echappement
RU2641359C1 (ru) * 2016-10-12 2018-01-17 Публичное акционерное Общество "Таганрогский авиационный научно-технический комплекс им. Г.М. Бериева" (ПАО "ТАНТК им. Г.М. Бериева") Самолет-амфибия (гидросамолет) с реактивными двигателями
EP3321186A1 (en) 2016-11-14 2018-05-16 Airbus Operations GmbH Aircraft
US10538335B2 (en) * 2016-12-19 2020-01-21 The Boeing Company Boundary layer ingestion integration into aft fuselage
FR3068002B1 (fr) * 2017-06-23 2019-07-19 Airbus Operations (S.A.S.) Fond etanche arriere presentant une membrane integrale a geometrie composee
US11111029B2 (en) * 2017-07-28 2021-09-07 The Boeing Company System and method for operating a boundary layer ingestion fan
USD957306S1 (en) * 2017-11-23 2022-07-12 Airbus Sas Aircraft nose
FR3074142A1 (fr) 2017-11-30 2019-05-31 Airbus Helicopters Giravion de type hybride comportant un empennage horizontal et deux derives agencees sur l'empennage horizontal
USD852721S1 (en) * 2018-01-29 2019-07-02 Darold B Cummings Aircraft
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
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Also Published As

Publication number Publication date
EP2406133B1 (fr) 2013-01-16
CN102414083A (zh) 2012-04-11
WO2010103252A1 (fr) 2010-09-16
US20120138736A1 (en) 2012-06-07
CA2755158A1 (fr) 2010-09-16
EP2406133A1 (fr) 2012-01-18
FR2943039A1 (fr) 2010-09-17
RU2011141267A (ru) 2013-04-20
CN102414083B (zh) 2014-12-24
RU2522539C2 (ru) 2014-07-20
US8651414B2 (en) 2014-02-18
FR2943039B1 (fr) 2012-09-28

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE AS 5A, 6A, 7A, 8A E 9A ANUIDADES.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2520 DE 25-04-2019 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.

B350 Update of information on the portal [chapter 15.35 patent gazette]