BRPI0921247A2 - método para produzir um componente plano de uma aeronave, componete plano e aeronave. - Google Patents

método para produzir um componente plano de uma aeronave, componete plano e aeronave.

Info

Publication number
BRPI0921247A2
BRPI0921247A2 BRPI0921247A BRPI0921247A BRPI0921247A2 BR PI0921247 A2 BRPI0921247 A2 BR PI0921247A2 BR PI0921247 A BRPI0921247 A BR PI0921247A BR PI0921247 A BRPI0921247 A BR PI0921247A BR PI0921247 A2 BRPI0921247 A2 BR PI0921247A2
Authority
BR
Brazil
Prior art keywords
aircraft
plane component
producing
plane
component
Prior art date
Application number
BRPI0921247A
Other languages
English (en)
Inventor
Nolan Richmond
Thomas Ritschel
Original Assignee
Gkn Aerospace Services Ltd
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 Gkn Aerospace Services Ltd filed Critical Gkn Aerospace Services Ltd
Publication of BRPI0921247A2 publication Critical patent/BRPI0921247A2/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
    • B64C1/12—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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/064—Stringers; Longerons
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/187—Ribs
    • 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
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1007—Running or continuous length work
    • 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
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24752—Laterally noncoextensive components
    • 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.]
    • Y10T428/24802—Discontinuous or differential coating, impregnation or bond [e.g., artwork, printing, retouched photograph, etc.]

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Laminated Bodies (AREA)
BRPI0921247A 2008-11-28 2009-11-24 método para produzir um componente plano de uma aeronave, componete plano e aeronave. BRPI0921247A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102008059653.1A DE102008059653B4 (de) 2008-11-28 2008-11-28 Flächiges Bauteil eines Fluggerätes und Verfahren zu dessen Herstellung
PCT/EP2009/065764 WO2010060908A2 (de) 2008-11-28 2009-11-24 Flächiges bauteil eines fluggerätes und verfahren zu dessen herstellung

Publications (1)

Publication Number Publication Date
BRPI0921247A2 true BRPI0921247A2 (pt) 2016-02-23

Family

ID=42145386

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0921247A BRPI0921247A2 (pt) 2008-11-28 2009-11-24 método para produzir um componente plano de uma aeronave, componete plano e aeronave.

Country Status (8)

Country Link
US (1) US20110311782A1 (pt)
EP (1) EP2370315B1 (pt)
JP (1) JP5731392B2 (pt)
CN (1) CN102232037B (pt)
BR (1) BRPI0921247A2 (pt)
DE (1) DE102008059653B4 (pt)
ES (1) ES2404698T3 (pt)
WO (1) WO2010060908A2 (pt)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8636252B2 (en) * 2010-06-25 2014-01-28 The Boeing Company Composite structures having integrated stiffeners with smooth runouts and method of making the same
US9682514B2 (en) 2010-06-25 2017-06-20 The Boeing Company Method of manufacturing resin infused composite parts using a perforated caul sheet
US8940213B2 (en) 2010-06-25 2015-01-27 The Boeing Company Resin infusion of composite parts using a perforated caul sheet
GB2485215B (en) 2010-11-05 2013-12-25 Gkn Aerospace Services Ltd Laminate Structure
WO2013078647A1 (en) * 2011-11-30 2013-06-06 Airbus S.A.S. Panel,component for an airplane airfoil comprising the panel,and method for producing the panel
US10099765B2 (en) 2012-08-08 2018-10-16 The Boeing Company Monolithic composite structures for vehicles
EP3023669B1 (fr) * 2014-11-20 2020-12-30 Airbus (Sas) Dispositif d'absorption d'énergie cinétique et aéronef comportant un tel dispositif

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3029910A (en) * 1958-11-07 1962-04-17 Gen Dynamics Corp Composite structural unit
US3623203A (en) * 1970-03-24 1971-11-30 Avco Corp Reinforced structural members and method of making same
US4012549A (en) * 1974-10-10 1977-03-15 General Dynamics Corporation High strength composite structure
US4966802A (en) * 1985-05-10 1990-10-30 The Boeing Company Composites made of fiber reinforced resin elements joined by adhesive
FR2632604B1 (fr) * 1988-06-08 1991-07-12 Aerospatiale Cadre en materiau composite notamment pour fuselage d'aeronef, et son procede de fabrication
CA2056330C (en) * 1990-12-19 2003-06-10 Alexander C. Dublinski Method of fabricating a complex part made of composite material
US5271986A (en) * 1991-04-19 1993-12-21 United Technologies Corporation Structural member having a stiffener bead therein and comprising plies of composite material extending for the full length and width of the structural member and continuously through the stiffener bead, and the article so made
CN1102632A (zh) * 1993-06-25 1995-05-17 株式会社日立制作所 纤维增强复合材料及其制造方法以及用它制成的部件
JP3894035B2 (ja) * 2001-07-04 2007-03-14 東レ株式会社 炭素繊維強化基材、それからなるプリフォームおよび複合材料
US20040035979A1 (en) * 2002-08-23 2004-02-26 Mccoskey William Robert Integrally stiffened axial load carrying skin panels for primary aircraft structure and closed loop manufacturing methods for making the same
US8211530B2 (en) * 2003-02-03 2012-07-03 Northrop Grumman Systems Corporation Adhesive fillets and method and apparatus for making same
DE102005028765B4 (de) * 2005-06-22 2016-01-21 Airbus Operations Gmbh Verfahren zur Herstellung eines Verstärkungsprofils
FI119726B (fi) * 2006-09-26 2009-02-27 Patria Aerostructures Oy Ilma-aluksen kaarielementti, siipi, ohjainpinta sekä vakaaja
US20080138586A1 (en) * 2006-12-11 2008-06-12 Frank Robert Mooijman Hybrid structure and method

Also Published As

Publication number Publication date
DE102008059653A1 (de) 2010-06-10
JP5731392B2 (ja) 2015-06-10
EP2370315A2 (de) 2011-10-05
WO2010060908A3 (de) 2010-09-30
CN102232037B (zh) 2014-12-17
DE102008059653B4 (de) 2015-07-09
CN102232037A (zh) 2011-11-02
JP2012510395A (ja) 2012-05-10
US20110311782A1 (en) 2011-12-22
EP2370315B1 (de) 2013-01-09
WO2010060908A2 (de) 2010-06-03
ES2404698T3 (es) 2013-05-28

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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 A 9A ANUIDADE.

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 2494 DE 23-10-2018 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.