BRPI0920642A2 - elemento estrutural para reforço de uma fuselagem de uma aeronave. - Google Patents

elemento estrutural para reforço de uma fuselagem de uma aeronave.

Info

Publication number
BRPI0920642A2
BRPI0920642A2 BRPI0920642A BRPI0920642A BRPI0920642A2 BR PI0920642 A2 BRPI0920642 A2 BR PI0920642A2 BR PI0920642 A BRPI0920642 A BR PI0920642A BR PI0920642 A BRPI0920642 A BR PI0920642A BR PI0920642 A2 BRPI0920642 A2 BR PI0920642A2
Authority
BR
Brazil
Prior art keywords
reinforcement
structural element
aircraft fuselage
fuselage
aircraft
Prior art date
Application number
BRPI0920642A
Other languages
English (en)
Inventor
Derk Daverschot
Matthijs Plokker
Nikolaus Ohrloff
Thomas Beumler
Original Assignee
Airbus Operations Gmbh
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 filed Critical Airbus Operations Gmbh
Publication of BRPI0920642A2 publication Critical patent/BRPI0920642A2/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
    • B64C1/065—Spars
    • 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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12347—Plural layers discontinuously bonded [e.g., spot-weld, mechanical fastener, etc.]
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12389—All metal or with adjacent metals having variation in thickness
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12486—Laterally noncoextensive components [e.g., embedded, etc.]
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
    • Y10T428/12556—Organic component
    • Y10T428/12569—Synthetic resin
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24479—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
    • Y10T428/24612—Composite web or sheet
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/31504—Composite [nonstructural laminate]
    • Y10T428/31678—Of metal

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
BRPI0920642A 2008-10-13 2009-10-06 elemento estrutural para reforço de uma fuselagem de uma aeronave. BRPI0920642A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US10484908P 2008-10-13 2008-10-13
DE200810042782 DE102008042782A1 (de) 2008-10-13 2008-10-13 Strukturelement zur Verstärkung einer Rumpfzelle eines Flugzeugs
PCT/EP2009/062979 WO2010043516A1 (de) 2008-10-13 2009-10-06 Strukturelement zur verstärkung einer rumpfzelle eines flugzeugs

Publications (1)

Publication Number Publication Date
BRPI0920642A2 true BRPI0920642A2 (pt) 2016-01-12

Family

ID=42054810

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0920642A BRPI0920642A2 (pt) 2008-10-13 2009-10-06 elemento estrutural para reforço de uma fuselagem de uma aeronave.

Country Status (9)

Country Link
US (1) US8974885B2 (pt)
EP (1) EP2334547B1 (pt)
JP (1) JP2012505120A (pt)
CN (1) CN102186722B (pt)
BR (1) BRPI0920642A2 (pt)
CA (1) CA2771114C (pt)
DE (1) DE102008042782A1 (pt)
RU (1) RU2011117089A (pt)
WO (1) WO2010043516A1 (pt)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011112518B4 (de) 2011-05-27 2020-01-09 Airbus Defence and Space GmbH Verfahren zur Herstellung einer Oberflächenstruktur mit Blitzschutz sowie Fahrzeugbauteilherstellverfahren
US10227127B2 (en) 2016-07-26 2019-03-12 Embraer S.A. Fiber metal laminate reinforced wing spar for retractable underwing mounted landing gear assemblies
JP2018100703A (ja) * 2016-12-20 2018-06-28 株式会社エクセディ トルクコンバータ
JP6727110B2 (ja) * 2016-12-20 2020-07-22 株式会社エクセディ トルクコンバータ
DE102017112804A1 (de) 2017-06-09 2018-12-13 Airbus Defence and Space GmbH Steuervorrichtung zum Steuern einer Rissfortschrittsversuchsvorrichtung, Rissfortschrittsversuchsvorrichtung sowie Verfahren zum Durchführen von Rissfortschrittsversuchen
US10760600B2 (en) * 2017-10-27 2020-09-01 General Electric Company Method of applying riblets to an aerodynamic surface
US11603612B2 (en) 2018-05-29 2023-03-14 Owens Corning Intellectual Capital, Llc Glass fiber mat with low-density fibers
CN111114821B (zh) * 2019-12-24 2024-01-12 中国特种飞行器研究所 一种先进增强结构的结构处理方法
RU209613U1 (ru) * 2021-09-01 2022-03-17 Акционерное общество «Информационные спутниковые системы» имени академика М.Ф. Решетнёва» Узел усиления силовой сетчатой конструкции космического аппарата
JP2023093151A (ja) * 2021-12-22 2023-07-04 三菱ケミカル株式会社 金属－ｆｒｐ複合体の製造方法および金属－ｆｒｐ複合体

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5866272A (en) * 1996-01-11 1999-02-02 The Boeing Company Titanium-polymer hybrid laminates
DE10031510A1 (de) * 2000-06-28 2002-01-17 Airbus Gmbh Strukturbauteil für ein Flugzeug
US6648273B2 (en) * 2001-10-30 2003-11-18 The Boeing Company Light weight and high strength fuselage
EP1336469A1 (en) * 2002-02-19 2003-08-20 Alenia Aeronautica S.P.A. Methods of manufacturing a stiffening element for an aircraft skin panel and a skin panel provided with the stiffening element
EP1495858B1 (de) * 2003-07-08 2019-08-07 Airbus Operations GmbH Leichtbaustruktur aus metallischen schichtwerkstoffen
US7080805B2 (en) * 2004-05-05 2006-07-25 The Boeing Company Stiffened structures and associated methods
US7281685B2 (en) * 2004-08-20 2007-10-16 Airbus Deutschland Gmbh Flush-top seat mounting rail for passenger aircraft
WO2007091990A2 (en) * 2006-01-11 2007-08-16 The Boeing Company Aircraft wing composed of composite and metal panels
NL2000232C2 (nl) * 2006-09-12 2008-03-13 Gtm Consulting B V Huidpaneel voor een vliegtuigromp.

Also Published As

Publication number Publication date
WO2010043516A1 (de) 2010-04-22
US8974885B2 (en) 2015-03-10
CN102186722B (zh) 2015-07-08
US20110236711A1 (en) 2011-09-29
CN102186722A (zh) 2011-09-14
CA2771114A1 (en) 2010-04-22
EP2334547A1 (de) 2011-06-22
JP2012505120A (ja) 2012-03-01
DE102008042782A1 (de) 2010-04-29
EP2334547B1 (de) 2016-03-02
RU2011117089A (ru) 2012-11-20
WO2010043516A4 (de) 2010-06-24
CA2771114C (en) 2016-12-06

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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]