DE69011069D1 - Zellenbauteil eines Flugzeuges. - Google Patents

Zellenbauteil eines Flugzeuges.

Info

Publication number
DE69011069D1
DE69011069D1 DE69011069T DE69011069T DE69011069D1 DE 69011069 D1 DE69011069 D1 DE 69011069D1 DE 69011069 T DE69011069 T DE 69011069T DE 69011069 T DE69011069 T DE 69011069T DE 69011069 D1 DE69011069 D1 DE 69011069D1
Authority
DE
Germany
Prior art keywords
foam
aircraft
bulkheads
resin
airplane
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.)
Expired - Fee Related
Application number
DE69011069T
Other languages
English (en)
Other versions
DE69011069T2 (de
Inventor
Milton J Torres
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.)
STATE OF FLORIDA FOR BENEF
Florida International University FIU
Original Assignee
STATE OF FLORIDA FOR BENEF
Florida International University FIU
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 STATE OF FLORIDA FOR BENEF, Florida International University FIU filed Critical STATE OF FLORIDA FOR BENEF
Application granted granted Critical
Publication of DE69011069D1 publication Critical patent/DE69011069D1/de
Publication of DE69011069T2 publication Critical patent/DE69011069T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • 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
    • B29C44/00—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
    • B29C44/02—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles for articles of definite length, i.e. discrete articles
    • B29C44/12—Incorporating or moulding on preformed parts, e.g. inserts or reinforcements
    • B29C44/18—Filling preformed cavities
    • B29C44/186—Filling multiple cavities
    • 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
    • B64C1/10—Bulkheads
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Laminated Bodies (AREA)
  • Toys (AREA)
  • Primary Cells (AREA)
  • Medicines Containing Material From Animals Or Micro-Organisms (AREA)
  • Body Structure For Vehicles (AREA)
  • Manufacture Of Porous Articles, And Recovery And Treatment Of Waste Products (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)
DE69011069T 1989-12-26 1990-12-24 Zellenbauteil eines Flugzeuges. Expired - Fee Related DE69011069T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/456,533 US5251849A (en) 1989-12-26 1989-12-26 Strain reduced airplane skin

Publications (2)

Publication Number Publication Date
DE69011069D1 true DE69011069D1 (de) 1994-09-01
DE69011069T2 DE69011069T2 (de) 1995-03-30

Family

ID=23813139

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69011069T Expired - Fee Related DE69011069T2 (de) 1989-12-26 1990-12-24 Zellenbauteil eines Flugzeuges.

Country Status (10)

Country Link
US (1) US5251849A (de)
EP (1) EP0435650B1 (de)
JP (1) JPH04218493A (de)
KR (1) KR910011586A (de)
AT (1) ATE109091T1 (de)
AU (2) AU6811890A (de)
BR (1) BR9006576A (de)
CA (1) CA2031928A1 (de)
DE (1) DE69011069T2 (de)
ES (1) ES2063297T3 (de)

Families Citing this family (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2640078B2 (ja) * 1993-02-08 1997-08-13 株式会社神戸製鋼所 制振形材及び輸送機用構造体
KR100239983B1 (ko) * 1997-04-28 2000-01-15 허기호 래피어 직기의 위사선택장치
US5823467A (en) * 1997-04-01 1998-10-20 Mcdonnell Douglas Corp Passive damping wedge
US5985362A (en) * 1997-12-22 1999-11-16 Mcdonnell Douglas Corporation Insulation system for transport aircraft
US6266427B1 (en) 1998-06-19 2001-07-24 Mcdonnell Douglas Corporation Damped structural panel and method of making same
DE19844035C1 (de) * 1998-09-25 1999-11-25 Daimler Chrysler Aerospace Schalenbauteil für ein Flugzeug und Verfahren zur Herstellung
US6361055B1 (en) * 1999-08-23 2002-03-26 Northrop Grumman Corporation Cryogenic composite tank seals
US6722611B1 (en) * 1999-09-20 2004-04-20 Kuang-Hsi Wu Reinforced aircraft skin and method
DE10007995C2 (de) * 2000-02-22 2002-03-07 Airbus Gmbh Strukturbauteil, insbesondere für ein Flugzeug und Verfahren zur Herstellung eines Strukturbauteils
DE10035349C1 (de) * 2000-07-20 2001-09-27 Eurocopter Deutschland Flugzeugtür
US6386481B1 (en) * 2001-01-08 2002-05-14 Patria Finavicomp Oy Arrangement for fastening stringers to aircraft wing ribs
US8156711B2 (en) * 2003-02-24 2012-04-17 Bell Helicopter Textron Inc. Contact stiffeners for structural skins
EP1495859B1 (de) * 2003-07-08 2008-09-03 Airbus Deutschland GmbH Leichtbaustruktur
US7284726B2 (en) * 2004-02-17 2007-10-23 Sikorsky Aircraft Corporation Self extinguishing composite primary structure
US7083147B2 (en) * 2004-03-11 2006-08-01 The Boeing Company Modularized insulation, systems, apparatus, and methods
US7040575B2 (en) * 2004-03-29 2006-05-09 The Boeing Company Foam composite insulation for aircraft
US7527222B2 (en) 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US7134629B2 (en) * 2004-04-06 2006-11-14 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7325771B2 (en) 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US7503368B2 (en) 2004-11-24 2009-03-17 The Boeing Company Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections
US7246772B2 (en) * 2004-12-20 2007-07-24 Sikorsky Aircraft Corporation Acoustic absorption system for an aircraft interior trim panel system
US7578468B2 (en) * 2004-12-20 2009-08-25 Sikorsky Aircraft Corporation Acoustic absorption system for an aircraft airframe
US7997529B2 (en) * 2006-01-19 2011-08-16 The Boeing Company Compliant panel for aircraft
US7766277B2 (en) * 2006-01-19 2010-08-03 The Boeing Company Deformable forward pressure bulkhead for an aircraft
DE102006026169B4 (de) * 2006-06-06 2012-06-21 Airbus Operations Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
DE102006026168A1 (de) 2006-06-06 2008-01-31 Airbus Deutschland Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
DE102006026170B4 (de) * 2006-06-06 2012-06-21 Airbus Operations Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
US20090274892A1 (en) * 2006-06-14 2009-11-05 Feng Qin Hydrophobic open celled foam and method of making the same
DE102007003278B4 (de) * 2007-01-23 2013-10-31 Airbus Operations Gmbh Rumpfstrukturbauteil eines Luft- oder Raumfahrzeuges mit einer Schaumstoffschicht als thermische Isolierung
DE102007008988A1 (de) 2007-02-23 2008-08-28 Airbus Deutschland Gmbh Rumpf eines Luft-oder Raumfahrzeugs und ein entsprechendes Luft-oder Raumfahrzeug
US8388795B2 (en) 2007-05-17 2013-03-05 The Boeing Company Nanotube-enhanced interlayers for composite structures
US8042767B2 (en) 2007-09-04 2011-10-25 The Boeing Company Composite fabric with rigid member structure
DE102009029245B4 (de) * 2009-09-07 2021-12-02 EUKLIT GmbH Tank für Flugzeuge
DE102009060706B4 (de) * 2009-12-29 2014-12-04 Airbus Operations Gmbh Verfahren sowie Vorrichtung zur Herstellung einer Versteifungsstruktur für ein Flugzeugrumpfsegment sowie eine Versteifungsstruktur
US8360355B2 (en) 2010-08-04 2013-01-29 The Boeing Company Wing-to-body fairing with spray-on foam and noise reduction method
KR102044471B1 (ko) 2013-01-14 2019-11-12 삼성전자주식회사 변형 방지를 위한 프레임 조립 구조 및 이것을 갖는 전자 장치
CN104787301B (zh) * 2015-02-03 2017-09-29 新誉集团有限公司 一种分段式超轻飞机蒙皮快速连接结构及制作方法
DE102016201928B4 (de) * 2016-02-09 2024-02-08 Airbus Operations Gmbh Isolationsbauteil
EP3309243B1 (de) 2016-10-11 2020-03-25 The Procter & Gamble Company Reiniger für harte oberflächen
US20210245859A1 (en) * 2020-02-11 2021-08-12 The Boeing Company Liquid-diverting panel assemblies and methods

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2819032A (en) * 1953-10-20 1958-01-07 Douglas Aircraft Co Inc Aircraft fuselage having panel damping material
US3087571A (en) * 1959-05-05 1963-04-30 Bolt Beranek & Newman Apparatus for damping
US3160549A (en) * 1960-12-29 1964-12-08 Minnesota Mining & Mfg Vibration damping structures
US3211703A (en) * 1962-03-23 1965-10-12 Monsanto Res Corp Polyaliphatic polyisocyanurate laminating resin prepared in the presence of a cocatalyst system
US3229935A (en) * 1962-12-06 1966-01-18 August T Bellanca Aircraft wing construction
US3305196A (en) * 1964-11-04 1967-02-21 Dow Chemical Co Vehicular structures made from foamed plastic materials
US3416756A (en) * 1966-08-03 1968-12-17 Dow Chemical Co Airfoil structure
DE2607380C3 (de) * 1976-02-24 1981-07-23 Bayer Ag, 5090 Leverkusen Verfahren zur Herstellung von warmformbaren Polyisocyanuratschaumstoffen
US4671471A (en) * 1984-05-21 1987-06-09 Mitchell Wing, Inc. Foam reinforced aluminum wing structure
US4692477A (en) * 1986-05-15 1987-09-08 The Celotex Corporation Polyisocyanurate foams derived from oxypropylated polyols and insulating structures therefrom
US4695618A (en) * 1986-05-23 1987-09-22 Ameron, Inc. Solventless polyurethane spray compositions and method for applying them
US4791148A (en) * 1987-02-12 1988-12-13 Basf Corporation Isocyanate terminated quasi-prepolymers useful for preparing polyurethane/polyisocyanurate foams having low thermal conductivity
JPS6432995A (en) * 1987-07-30 1989-02-02 Yokohama Rubber Co Ltd Interior structure for aircraft

Also Published As

Publication number Publication date
EP0435650B1 (de) 1994-07-27
ES2063297T3 (es) 1995-01-01
ATE109091T1 (de) 1994-08-15
CA2031928A1 (en) 1991-06-27
DE69011069T2 (de) 1995-03-30
AU6811890A (en) 1991-07-04
JPH04218493A (ja) 1992-08-10
KR910011586A (ko) 1991-08-07
AU6848190A (en) 1991-07-04
AU637441B2 (en) 1993-05-27
BR9006576A (pt) 1991-10-01
EP0435650A1 (de) 1991-07-03
US5251849A (en) 1993-10-12

Similar Documents

Publication Publication Date Title
DE69011069D1 (de) Zellenbauteil eines Flugzeuges.
DE69310673D1 (de) Hilfssteuerung der Bewegung des Fahrwerks eines Flugzeugs
JPS6485714A (en) Method and device for manufacturing article having fixed section including core and skin and article manufactured by said method
JPS52118798A (en) Tandem wing aeroplane having body and lifting surface
GB2172861B (en) Aileron for an airplane wing
Wong Sandwich construction in the Starship
DE3378036D1 (en) Air craft structure for take-off and landing on the feet of the pilot
SE8106271L (sv) Flygplan med arrangemang for montering av en sond
JPS55160691A (en) Fitting structure of protector for body of small boat
BR8201234A (pt) Composicoes de suprimento de camada fina de borracha curada e pneumatico que tem elementos de reforco acamados em suprimento de camada fina de borracha vulcanizada
Chaumette Certification problems for composite airplane structures
GB1354875A (en) Composite structures for use in the control of icing
GB1040948A (en) Improved airfoil structure and method of manufacture
RU94018410A (ru) Привод уборки и выпуска шасси летательного аппарата
JOHNSON et al. Application study of filamentary composites in a commercial jet aircraft fuselage(Filamentary composite materials for aircraft fuselage structures)[Final Report, Oct. 1971- Jun. 1972]
Wolfe et al. Durability of adhesive bonded structures subjected to acoustic loads
Greben'kov Aircraft Design(Konstruktsiya Samoletov)
FR2450157A1 (fr) Structures gonflables, leur procede de fixation et embarcations pneumatiques comportant de telles structures
Padden Composite focused load control surface
JPS57136808A (en) Reflector of electromagnetic wave
IT8040056A0 (it) Carenatura, in particolare da applicarsi sul tetto della cabina degli autocarri
GRITSIUK Vibrations of three-layer panels of unsymmetric structure
SU1828025A1 (ru) Пилон подвески двигателя летательного аппарата
Greben'kov Aircraft Design(Konstruktsiya Samoletov).(Book)
Neise Composite Materials in Commercial Aircraft--Interpretation for Airbus A 320

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee