AU2012226306B2 - Diamond shaped window for a composite and/or metallic airframe - Google Patents

Diamond shaped window for a composite and/or metallic airframe Download PDF

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Publication number
AU2012226306B2
AU2012226306B2 AU2012226306A AU2012226306A AU2012226306B2 AU 2012226306 B2 AU2012226306 B2 AU 2012226306B2 AU 2012226306 A AU2012226306 A AU 2012226306A AU 2012226306 A AU2012226306 A AU 2012226306A AU 2012226306 B2 AU2012226306 B2 AU 2012226306B2
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AU
Australia
Prior art keywords
cutout
load
fuselage
side region
path
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
AU2012226306A
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English (en)
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AU2012226306A1 (en
Inventor
Max U. Kismarton
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
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 AU2012226306A1 publication Critical patent/AU2012226306A1/en
Application granted granted Critical
Publication of AU2012226306B2 publication Critical patent/AU2012226306B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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)
AU2012226306A 2011-03-04 2012-02-03 Diamond shaped window for a composite and/or metallic airframe Active AU2012226306B2 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/041,299 US8616500B2 (en) 2011-03-04 2011-03-04 Diamond shaped window for composite and/or metallic airframe
US13/041,299 2011-03-04
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
AU2012226306A1 AU2012226306A1 (en) 2013-08-08
AU2012226306B2 true AU2012226306B2 (en) 2016-08-04

Family

ID=45582067

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2012226306A Active AU2012226306B2 (en) 2011-03-04 2012-02-03 Diamond shaped window for a composite and/or metallic airframe

Country Status (11)

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

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CN108090265A (zh) * 2017-12-08 2018-05-29 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

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US9586699B1 (en) 1999-08-16 2017-03-07 Smart Drilling And Completion, Inc. Methods and apparatus for monitoring and fixing holes in composite aircraft
US9625361B1 (en) 2001-08-19 2017-04-18 Smart Drilling And Completion, Inc. Methods and apparatus to prevent failures of fiber-reinforced composite materials under compressive stresses caused by fluids and gases invading microfractures in the materials
USD691548S1 (en) * 2011-03-04 2013-10-15 The Boeing Company Aircraft window
US8939406B2 (en) * 2012-07-02 2015-01-27 The Boeing Company Joining composite fuselage sections along window belts
EP2746149B1 (en) * 2012-12-19 2019-06-19 Airbus Operations GmbH Method for the production of a connecting element, connecting element, and aircraft or spacecraft
FR3000470B1 (fr) * 2012-12-28 2015-12-25 Airbus Operations Sas Peau auto-raidie pour fuselage d'aeronef comprenant des lisses a section fermee et procede de fabrication associe
JP6310268B2 (ja) * 2014-02-10 2018-04-11 株式会社とわに 航空機用スクラップ処理装置
JP6309324B2 (ja) 2014-03-28 2018-04-11 三菱重工業株式会社 複合材構造体、これを備えた航空機翼および航空機胴体、並びに複合材構造体の製造方法
FR3023826B1 (fr) * 2014-07-18 2018-02-23 Eads Sogerma Structure linteau pour fuselage d'aeronef et fuselage comporant un tel linteau
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
DE102016107740B4 (de) * 2016-04-26 2018-02-15 Benteler Automobiltechnik Gmbh Achsträger mit verbessertem Lastpfad
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
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
KR20210086676A (ko) 2018-10-26 2021-07-08 애리스 컴포지트 아이엔씨. 섬유 복합재 부품의 디자인 방법과 효율적인 제작 방법
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
US11383817B2 (en) * 2019-07-19 2022-07-12 The Boeing Company Modular fuselage assemblies for aircraft, aircraft including modular fuselage assemblies, and MEl'hods of assembling modular fuselage assemblies
US12552517B2 (en) 2022-07-21 2026-02-17 The Boeing Company Support structure for an aircraft

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US3429530A (en) * 1965-11-10 1969-02-25 Heinrich Hertel Window construction for fuselages of aircraft
US4278485A (en) * 1978-08-02 1981-07-14 The Boeing Company Method of forming composite wound structure
US4450661A (en) * 1981-09-30 1984-05-29 The Boeing Company Composite structures window belt and method of making
WO2007141176A1 (en) * 2006-06-02 2007-12-13 Airbus Deutschland Gmbh Fuselage structure and method for the production of a fuselage structure
WO2009098088A2 (de) * 2008-02-08 2009-08-13 Airbus Deutschland Gmbh Verfahren zur herstellung eines fvw-bauteils, fvw-bauteil sowie ein fvw-rumpfteil eines flugzeugs

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US3429530A (en) * 1965-11-10 1969-02-25 Heinrich Hertel Window construction for fuselages of aircraft
US4278485A (en) * 1978-08-02 1981-07-14 The Boeing Company Method of forming composite wound structure
US4450661A (en) * 1981-09-30 1984-05-29 The Boeing Company Composite structures window belt and method of making
WO2007141176A1 (en) * 2006-06-02 2007-12-13 Airbus Deutschland Gmbh Fuselage structure and method for the production of a fuselage structure
WO2009098088A2 (de) * 2008-02-08 2009-08-13 Airbus Deutschland Gmbh Verfahren zur herstellung eines fvw-bauteils, fvw-bauteil sowie ein fvw-rumpfteil eines flugzeugs

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Alhajahmad, Ahmad, et al. "Optimal Design of a Pressurized Fuselage Panel with a Cutout Using Tow-Placed Steered Fibers." EngOpt 2008 - International Conference on Engineering Optimization. Rio de Janeiro, Brazil, 05 June 2008. *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108090265A (zh) * 2017-12-08 2018-05-29 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

Also Published As

Publication number Publication date
ES2637594T3 (es) 2017-10-13
US20140076477A1 (en) 2014-03-20
JP2014506854A (ja) 2014-03-20
WO2012121825A1 (en) 2012-09-13
JP6029599B2 (ja) 2016-11-24
CA2826143A1 (en) 2012-09-13
US9193483B2 (en) 2015-11-24
CN103429493B (zh) 2016-11-09
BR112013022591A2 (pt) 2016-12-06
CN103429493A (zh) 2013-12-04
BR112013022591B1 (pt) 2021-03-23
US8616500B2 (en) 2013-12-31
KR20130140116A (ko) 2013-12-23
KR101928114B1 (ko) 2018-12-11
CA2826143C (en) 2017-07-11
RU2586768C2 (ru) 2016-06-10
RU2013144411A (ru) 2015-04-10
EP2681112B1 (en) 2017-05-17
EP2681112A1 (en) 2014-01-08
US20120223187A1 (en) 2012-09-06

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