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BRPI0407749A - enrijecedores de contato para envoltórios estruturais - Google Patents

enrijecedores de contato para envoltórios estruturais

Info

Publication number
BRPI0407749A
BRPI0407749A BRPI0407749-0A BRPI0407749A BRPI0407749A BR PI0407749 A BRPI0407749 A BR PI0407749A BR PI0407749 A BRPI0407749 A BR PI0407749A BR PI0407749 A BRPI0407749 A BR PI0407749A
Authority
BR
Brazil
Prior art keywords
structural
contact
stiffening member
rib
filler
Prior art date
Application number
BRPI0407749-0A
Other languages
English (en)
Inventor
James Donn Hethcock
Original Assignee
Bell Helicopter Textron Inc
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 Bell Helicopter Textron Inc filed Critical Bell Helicopter Textron Inc
Publication of BRPI0407749A publication Critical patent/BRPI0407749A/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
    • 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
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • 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
    • 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
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Rod-Shaped Construction Members (AREA)
  • Building Environments (AREA)
  • Connection Of Plates (AREA)

Abstract

"ENRIJECEDORES DE CONTATO PARA ENVOLTóRIOS ESTRUTURAIS". Um membro de enrijecimento interno de configurações variadas em que os elementos de enrijecimento suportam o envoltório usando uma trajetória de carga de compressão somente, é revelado. Na concretização preferida, o elemento de enrijecimento tem uma borda periférica que é adaptada para ser ajustada por prensagem em contato com o envoltório. O membro de enrijecimento pode ser mantido no lugar por vários dispositivos de retenção. Outra configuração é uma nervura em deslizamento tendo um flange com um canal periférico no qual um material de carga é disposto. A nervura é inserida em uma viga de caixa estrutural montada, e o material de carga é usado para preencher quaisquer folgas entre a nervura em deslizamento e a superfície interior da viga de caixa estrutural. O material de carga é preferivelmente um material expansível, tal como um material tipo espuma expansível. Contudo, em situações onde uma ranhura em deslizamento forma uma ranhura estrutural primária, o material de carga é preferivelmente um adesivo estrutural ou material de cunha líquido. Um adesivo sólido ou carga não se trituraria sob as forças de prendimento a partir dos prendedores ou parafusos em fixações de ajustes localizadas.
BRPI0407749-0A 2003-02-24 2004-02-24 enrijecedores de contato para envoltórios estruturais BRPI0407749A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US45009603P 2003-02-24 2003-02-24
PCT/US2004/005585 WO2004076769A2 (en) 2003-02-24 2004-02-24 Contact stiffeners for structural skins

Publications (1)

Publication Number Publication Date
BRPI0407749A true BRPI0407749A (pt) 2006-02-14

Family

ID=32927611

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0407749-0A BRPI0407749A (pt) 2003-02-24 2004-02-24 enrijecedores de contato para envoltórios estruturais

Country Status (7)

Country Link
US (2) US8156711B2 (pt)
EP (1) EP1616061B1 (pt)
CN (1) CN100434634C (pt)
BR (1) BRPI0407749A (pt)
CA (1) CA2515149C (pt)
DE (2) DE04714198T8 (pt)
WO (1) WO2004076769A2 (pt)

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US10513324B2 (en) 2016-02-08 2019-12-24 Bell Helicopter Textron Inc. Composite rib assembly
US11142297B2 (en) 2016-02-08 2021-10-12 Bell Helicopter Textron Inc. Heating tool
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Also Published As

Publication number Publication date
US20120199269A1 (en) 2012-08-09
CA2515149A1 (en) 2004-09-10
EP1616061B1 (en) 2011-04-06
CA2515149C (en) 2011-01-11
CN100434634C (zh) 2008-11-19
EP1616061A2 (en) 2006-01-18
WO2004076769A3 (en) 2006-05-11
WO2004076769A2 (en) 2004-09-10
US20070011970A1 (en) 2007-01-18
US8632712B2 (en) 2014-01-21
DE04714198T1 (de) 2006-12-28
CN1826451A (zh) 2006-08-30
US8156711B2 (en) 2012-04-17
DE04714198T8 (de) 2007-06-06
EP1616061A4 (en) 2009-04-29
DE602004032122D1 (de) 2011-05-19

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Legal Events

Date Code Title Description
B15K Others concerning applications: alteration of classification

Free format text: AS CLASSIFICACOES ANTERIORES ERAM: E04C 3/30 , B64C 3/00

Ipc: B64C 1/12 (2006.01), B64C 3/18 (2006.01), B64C 1/0

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

Free format text: REFERENTE A 12A 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 2366 DE 10-05-2016 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.