KR101928114B1 - 복합재 및/또는 금속재 기체를 위한 다이아몬드형 창 - Google Patents

복합재 및/또는 금속재 기체를 위한 다이아몬드형 창 Download PDF

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Publication number
KR101928114B1
KR101928114B1 KR1020137018805A KR20137018805A KR101928114B1 KR 101928114 B1 KR101928114 B1 KR 101928114B1 KR 1020137018805 A KR1020137018805 A KR 1020137018805A KR 20137018805 A KR20137018805 A KR 20137018805A KR 101928114 B1 KR101928114 B1 KR 101928114B1
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South Korea
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incision
load
region
shear
aircraft
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Korean (ko)
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KR20130140116A (ko
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맥스 유. 키스마톤
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더 보잉 컴파니
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    • 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

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  • 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)
KR1020137018805A 2011-03-04 2012-02-03 복합재 및/또는 금속재 기체를 위한 다이아몬드형 창 Active KR101928114B1 (ko)

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
KR20130140116A KR20130140116A (ko) 2013-12-23
KR101928114B1 true KR101928114B1 (ko) 2018-12-11

Family

ID=45582067

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020137018805A Active KR101928114B1 (ko) 2011-03-04 2012-02-03 복합재 및/또는 금속재 기체를 위한 다이아몬드형 창

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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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
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
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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RU2103198C1 (ru) * 1996-10-29 1998-01-27 Акционерное общество "Центр перспективных разработок акционерного общества "Центральный научно-исследовательский институт специального машиностроения" Несущая труба-оболочка, панель из композиционных материалов и узел соединения панелей
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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
AU2012226306B2 (en) 2016-08-04
US8616500B2 (en) 2013-12-31
KR20130140116A (ko) 2013-12-23
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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