BRPI0906234A2 - Fuselagem de aeronave resistente à requema - Google Patents

Fuselagem de aeronave resistente à requema

Info

Publication number
BRPI0906234A2
BRPI0906234A2 BRPI0906234-3A BRPI0906234A BRPI0906234A2 BR PI0906234 A2 BRPI0906234 A2 BR PI0906234A2 BR PI0906234 A BRPI0906234 A BR PI0906234A BR PI0906234 A2 BRPI0906234 A2 BR PI0906234A2
Authority
BR
Brazil
Prior art keywords
aircraft fuselage
resistant aircraft
resistant
fuselage
aircraft
Prior art date
Application number
BRPI0906234-3A
Other languages
English (en)
Inventor
Rainer Mueller
Robert Huebner
Heinz-Peter Busch
Marie-Laure Wawrzyniec
Original Assignee
Airbus Operations Gmbh
Airbus 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 Gmbh, Airbus Sas filed Critical Airbus Operations Gmbh
Publication of BRPI0906234A2 publication Critical patent/BRPI0906234A2/pt
Publication of BRPI0906234A8 publication Critical patent/BRPI0906234A8/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
    • B64C1/066—Interior liners
    • 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
    • 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
    • B64C1/12—Construction or attachment of skin panels
    • 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
    • B64C1/18—Floors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
    • 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)
  • Laminated Bodies (AREA)
BRPI0906234A 2008-03-28 2009-03-17 fuselagem de aeronave resistente à requeima BRPI0906234A8 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US7232008P 2008-03-28 2008-03-28
DE102008016104A DE102008016104A1 (de) 2008-03-28 2008-03-28 Durchbrandsicherer Flugzeugrumpf
PCT/EP2009/053122 WO2009118256A2 (en) 2008-03-28 2009-03-17 Burn through resistant aircraft fuselage

Publications (2)

Publication Number Publication Date
BRPI0906234A2 true BRPI0906234A2 (pt) 2015-06-30
BRPI0906234A8 BRPI0906234A8 (pt) 2015-09-22

Family

ID=41051287

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0906234A BRPI0906234A8 (pt) 2008-03-28 2009-03-17 fuselagem de aeronave resistente à requeima

Country Status (9)

Country Link
US (1) US9878770B2 (pt)
EP (1) EP2257466B1 (pt)
JP (1) JP5539955B2 (pt)
CN (1) CN101977810B (pt)
BR (1) BRPI0906234A8 (pt)
CA (1) CA2720088C (pt)
DE (1) DE102008016104A1 (pt)
RU (1) RU2502634C2 (pt)
WO (1) WO2009118256A2 (pt)

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* Cited by examiner, † Cited by third party
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DE102012005353A1 (de) * 2012-03-16 2013-09-19 Airbus Operations Gmbh Flugzeugrumpfstruktur mit Querprofilen und Fachwerkstruktur
FR3000020B1 (fr) * 2012-12-26 2015-01-30 Airbus Operations Sas Avion a fuselage pourvu d'excroissances laterales delimitant des espaces de stockage
ES2578427T3 (es) * 2012-12-27 2016-07-26 Airbus Operations S.L. Una carena ventral de una aeronave con una capacidad de almacenamiento mejorada
CN105923144B (zh) * 2016-05-30 2018-08-21 中国商用飞机有限责任公司 抗火焰烧穿机身和用于抗火焰烧穿机身的抗火焰烧穿地板
US11459085B2 (en) * 2019-04-30 2022-10-04 Textron Innovations Inc. Energy attenuation stabilizers and methods
CN112937833A (zh) * 2021-03-05 2021-06-11 中国商用飞机有限责任公司 用于航空飞行器的机体结构及其构造方法和航空飞行器
EP4385892A1 (de) * 2022-12-14 2024-06-19 Airbus Operations GmbH Flugzeug mit frachtraum

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BR112012011474A2 (pt) * 2009-11-23 2019-09-24 Applied Nanostructured Sols estruturas espaciais de compósito com cnt adaptado.
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Also Published As

Publication number Publication date
CA2720088A1 (en) 2009-10-01
RU2010141786A (ru) 2012-05-10
CN101977810B (zh) 2016-04-20
WO2009118256A3 (en) 2009-11-26
JP2011515272A (ja) 2011-05-19
EP2257466B1 (en) 2016-12-21
EP2257466A2 (en) 2010-12-08
DE102008016104A1 (de) 2009-10-08
BRPI0906234A8 (pt) 2015-09-22
WO2009118256A2 (en) 2009-10-01
JP5539955B2 (ja) 2014-07-02
RU2502634C2 (ru) 2013-12-27
CN101977810A (zh) 2011-02-16
US20110121133A1 (en) 2011-05-26
CA2720088C (en) 2017-11-28
WO2009118256A4 (en) 2010-01-28
US9878770B2 (en) 2018-01-30

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