BR112013022591A2 - janela em formato de losango para uma armação de avião compósita e/ou metálica - Google Patents

janela em formato de losango para uma armação de avião compósita e/ou metálica

Info

Publication number
BR112013022591A2
BR112013022591A2 BR112013022591A BR112013022591A BR112013022591A2 BR 112013022591 A2 BR112013022591 A2 BR 112013022591A2 BR 112013022591 A BR112013022591 A BR 112013022591A BR 112013022591 A BR112013022591 A BR 112013022591A BR 112013022591 A2 BR112013022591 A2 BR 112013022591A2
Authority
BR
Brazil
Prior art keywords
cutout
composite
shaped window
diamond
fuselage
Prior art date
Application number
BR112013022591A
Other languages
English (en)
Other versions
BR112013022591B1 (pt
Inventor
Max U Kismarton
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of BR112013022591A2 publication Critical patent/BR112013022591A2/pt
Publication of BR112013022591B1 publication Critical patent/BR112013022591B1/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
    • B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • 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
    • B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1476—Canopies; Windscreens or similar transparent elements
    • B64C1/1484—Windows
    • 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
    • B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1476—Canopies; Windscreens or similar transparent elements
    • B64C1/1492—Structure and mounting of the transparent elements in the window or windscreen
    • 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
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1052—Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
    • Y10T156/1062—Prior to assembly
    • Y10T156/1064—Partial cutting [e.g., grooving or incising]
    • 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
    • Y10T83/00—Cutting
    • Y10T83/04—Processes

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)

Abstract

resumo patente de invenção: "janela em formato de losango para uma armação de avião compósita e/ou metálica". a presente invenção refere-se a uma fuselagem de aeronave que pode incluir uma seção cilíndrica (34) que tem uma região lateral. a fuselagem pode incluir um primeiro recorte (52a) e um segundo recorte (52b) formados na região lateral em uma relação lado a lado um com o outro. a fuselagem pode prover um percurso de carga direto se estendendo ao longo da seção cilíndrica. o percurso de carga pode se estender de forma substancialmente contínua a partir de uma porção inferior da região lateral geralmente sob o primeiro recorte até uma porção superior da região lateral geralmente sobre o segundo recorte.
BR112013022591-2A 2011-03-04 2012-02-03 Fuselagem de aeronave e método de formação de recortes em uma região lateral de uma fuselagem de aeronave BR112013022591B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/041,299 2011-03-04
US13/041,299 US8616500B2 (en) 2011-03-04 2011-03-04 Diamond shaped window for composite and/or metallic airframe
PCT/US2012/023819 WO2012121825A1 (en) 2011-03-04 2012-02-03 Diamond shaped window for a composite and/or metallic airframe

Publications (2)

Publication Number Publication Date
BR112013022591A2 true BR112013022591A2 (pt) 2016-12-06
BR112013022591B1 BR112013022591B1 (pt) 2021-03-23

Family

ID=45582067

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112013022591-2A BR112013022591B1 (pt) 2011-03-04 2012-02-03 Fuselagem de aeronave e método de formação de recortes em uma região lateral de uma fuselagem de aeronave

Country Status (11)

Country Link
US (2) US8616500B2 (pt)
EP (1) EP2681112B1 (pt)
JP (1) JP6029599B2 (pt)
KR (1) KR101928114B1 (pt)
CN (1) CN103429493B (pt)
AU (1) AU2012226306B2 (pt)
BR (1) BR112013022591B1 (pt)
CA (1) CA2826143C (pt)
ES (1) ES2637594T3 (pt)
RU (1) RU2586768C2 (pt)
WO (1) WO2012121825A1 (pt)

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FR3027273B1 (fr) * 2014-10-17 2018-04-27 Arianegroup Sas Architecture de paroi de face de voiture telle qu'une voiture de train en composite sandwich
DE102015110165B4 (de) * 2015-06-24 2017-03-02 Airbus Operations Gmbh Hautfeldfenstereinheit für ein Luftfahrzeug
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JP6768348B2 (ja) 2016-05-26 2020-10-14 三菱重工業株式会社 胴体の断面形状設計方法、設計装置及び設計プログラム
US10308342B2 (en) * 2016-09-07 2019-06-04 The Boeing Company Method of repairing damage to fuselage barrel and associated apparatus and system
US10293915B2 (en) 2016-12-13 2019-05-21 The Boeing Company Apparatuses and methods for aerodynamic window assemblies
CN108090265B (zh) * 2017-12-08 2021-05-25 中国航空工业集团公司西安飞机设计研究所 一种飞机机身普通框在弯曲载荷下的应力计算方法
US11338899B2 (en) * 2018-04-05 2022-05-24 The Boeing Company Joint for a metal airplane skin using metal matrix composite
US10516232B2 (en) * 2018-05-21 2019-12-24 The Boeing Company Electrical multi-connector feedthrough panel and method therefor
CN108725743B (zh) * 2018-06-14 2023-07-14 中国水利水电科学研究院 一种仰首式手抛小型固定翼无人机机身
AU2019423287B2 (en) 2018-10-26 2022-11-17 Arris Composites Inc. Method for the design and efficient manufacture of fiber-composite parts
JP7344029B2 (ja) * 2019-07-19 2023-09-13 株式会社Subaru 移動体の構造体、および移動体の構造体の製造方法
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US20240025532A1 (en) * 2022-07-21 2024-01-25 The Boeing Company Support structure for an aircraft

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Also Published As

Publication number Publication date
AU2012226306B2 (en) 2016-08-04
ES2637594T3 (es) 2017-10-13
CA2826143C (en) 2017-07-11
RU2013144411A (ru) 2015-04-10
RU2586768C2 (ru) 2016-06-10
BR112013022591B1 (pt) 2021-03-23
CN103429493B (zh) 2016-11-09
EP2681112B1 (en) 2017-05-17
US9193483B2 (en) 2015-11-24
US8616500B2 (en) 2013-12-31
CA2826143A1 (en) 2012-09-13
KR20130140116A (ko) 2013-12-23
US20140076477A1 (en) 2014-03-20
JP2014506854A (ja) 2014-03-20
KR101928114B1 (ko) 2018-12-11
EP2681112A1 (en) 2014-01-08
JP6029599B2 (ja) 2016-11-24
WO2012121825A1 (en) 2012-09-13
US20120223187A1 (en) 2012-09-06
CN103429493A (zh) 2013-12-04

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 03/02/2012, OBSERVADAS AS CONDICOES LEGAIS.