BRPI0918165A2 - parte traseira de aeronave - Google Patents

parte traseira de aeronave

Info

Publication number
BRPI0918165A2
BRPI0918165A2 BRPI0918165A BRPI0918165A BRPI0918165A2 BR PI0918165 A2 BRPI0918165 A2 BR PI0918165A2 BR PI0918165 A BRPI0918165 A BR PI0918165A BR PI0918165 A BRPI0918165 A BR PI0918165A BR PI0918165 A2 BRPI0918165 A2 BR PI0918165A2
Authority
BR
Brazil
Prior art keywords
support structure
connection
fuselage
opening
rear part
Prior art date
Application number
BRPI0918165A
Other languages
English (en)
Inventor
Frédéric Journade
Laurent Lafont
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 BRPI0918165A2 publication Critical patent/BRPI0918165A2/pt

Links

Classifications

    • 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
    • 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
    • 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
    • B64D2027/005—Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR]
    • 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
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Prevention Devices (AREA)
  • Connection Of Plates (AREA)
  • Radio Relay Systems (AREA)
  • Compositions Of Oxide Ceramics (AREA)
  • Motor Or Generator Frames (AREA)
BRPI0918165A 2008-09-18 2009-09-16 parte traseira de aeronave BRPI0918165A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0856300A FR2935955B1 (fr) 2008-09-18 2008-09-18 Partie arriere d'aeronef comprenant une structure de support de moteurs reliee au fuselage par au moins un element de blocage sollicite en compression.
PCT/FR2009/051741 WO2010031960A1 (fr) 2008-09-18 2009-09-16 Partie arriere d'aeronef comprenant une structure de support de moteurs reliee au fuselage par au moins un element de blocage sollicite en compression

Publications (1)

Publication Number Publication Date
BRPI0918165A2 true BRPI0918165A2 (pt) 2015-12-01

Family

ID=40566144

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0918165A BRPI0918165A2 (pt) 2008-09-18 2009-09-16 parte traseira de aeronave

Country Status (10)

Country Link
US (1) US8448897B2 (pt)
EP (1) EP2334554B1 (pt)
JP (1) JP5559796B2 (pt)
CN (1) CN102159461B (pt)
AT (1) ATE541783T1 (pt)
BR (1) BRPI0918165A2 (pt)
CA (1) CA2736803C (pt)
FR (1) FR2935955B1 (pt)
RU (1) RU2496683C2 (pt)
WO (1) WO2010031960A1 (pt)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2943623B1 (fr) * 2009-03-30 2011-04-29 Airbus France Partie arriere d'aeronef comprenant une structure de support de moteurs montee oscillante sur le fuselage
EP2631180B1 (en) * 2012-02-27 2014-04-02 Airbus Operations (S.A.S.) An engine attachment pylon
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
US9533768B2 (en) * 2014-08-12 2017-01-03 The Boeing Company Aircraft engine mounting system
FR3032419B1 (fr) * 2015-02-09 2018-06-08 Airbus Operations Pointe arriere d'aeronef
US10024270B2 (en) * 2015-10-13 2018-07-17 Rohr, Inc. Vibration damping drag link fitting for a thrust reverser

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US377068A (en) * 1888-01-31 William geeke
US386757A (en) * 1888-07-24 Third to samuel w
GB724052A (en) * 1951-11-17 1955-02-16 Sncase Improvements in aeroplanes propelled by several jet engines
US4044973A (en) * 1975-12-29 1977-08-30 The Boeing Company Nacelle assembly and mounting structures for a turbofan jet propulsion engine
GB2129498B (en) * 1982-10-29 1986-04-03 Rolls Royce Mounting system for two coupled turboshaft gas turbine engines
US4821980A (en) * 1987-09-29 1989-04-18 The Boeing Company Vibration isolating engine mount
US4821960A (en) * 1988-04-07 1989-04-18 Goldman Budd S Shower head and decorative covering therefor
US5065959A (en) * 1989-11-21 1991-11-19 The Boeing Company Vibration damping aircraft engine attachment
US5209428A (en) * 1990-05-07 1993-05-11 Lockheed Corporation Propulsion system for a vertical and short takeoff and landing aircraft
FR2862045B1 (fr) * 2003-11-12 2006-05-05 Snecma Moteurs Turboreacteur destine a etre fixe sur le fuselage d'un avion et en particulier sur sa partie arriere
US8016233B2 (en) * 2006-01-30 2011-09-13 The Boeing Company Aircraft configuration
GB2434836B (en) * 2006-02-04 2008-12-10 Rolls Royce Plc Mounting system for use in mounting a gas turbine engine
DE102006027707A1 (de) * 2006-06-14 2007-12-20 Airbus Deutschland Gmbh Heckstruktur für ein Luft- oder Raumfahrzeug
ES2341514B1 (es) * 2007-10-03 2011-04-18 Airbus España S.L. Configuracion estructural para el montaje de un motor sobre la estructura de una aeronave.
ES2391967B1 (es) * 2010-01-14 2013-10-10 Airbus Operations, S.L. Pilón de soporte de motores de aeronaves.

Also Published As

Publication number Publication date
JP2012502847A (ja) 2012-02-02
WO2010031960A1 (fr) 2010-03-25
JP5559796B2 (ja) 2014-07-23
CN102159461A (zh) 2011-08-17
EP2334554B1 (fr) 2012-01-18
RU2496683C2 (ru) 2013-10-27
CN102159461B (zh) 2013-09-18
CA2736803C (fr) 2016-06-14
RU2011115011A (ru) 2012-10-27
US8448897B2 (en) 2013-05-28
US20110226893A1 (en) 2011-09-22
CA2736803A1 (fr) 2010-03-25
ATE541783T1 (de) 2012-02-15
FR2935955A1 (fr) 2010-03-19
FR2935955B1 (fr) 2010-10-15
EP2334554A1 (fr) 2011-06-22

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Legal Events

Date Code Title Description
B11A Dismissal acc. art.33 of ipl - examination not requested within 36 months of filing
B11Y Definitive dismissal - extension of time limit for request of examination expired [chapter 11.1.1 patent gazette]