PT2394909T - Secções tubulares de compósito para fuselagens de aeronave e métodos para fabricar essas secções tubulares - Google Patents
Secções tubulares de compósito para fuselagens de aeronave e métodos para fabricar essas secções tubularesInfo
- Publication number
- PT2394909T PT2394909T PT111749032T PT11174903T PT2394909T PT 2394909 T PT2394909 T PT 2394909T PT 111749032 T PT111749032 T PT 111749032T PT 11174903 T PT11174903 T PT 11174903T PT 2394909 T PT2394909 T PT 2394909T
- Authority
- PT
- Portugal
- Prior art keywords
- barrel sections
- manufacturing
- methods
- composite
- aircraft fuselages
- Prior art date
Links
- 239000002131 composite material Substances 0.000 title 1
- 238000004519 manufacturing process Methods 0.000 title 1
- 238000000034 method Methods 0.000 title 1
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
- 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
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/56—Winding and joining, e.g. winding spirally
- B29C53/58—Winding and joining, e.g. winding spirally helically
- B29C53/583—Winding and joining, e.g. winding spirally helically for making tubular articles with particular features
- B29C53/587—Winding and joining, e.g. winding spirally helically for making tubular articles with particular features having a non-uniform wall-structure, e.g. with inserts, perforations, locally concentrated reinforcements
-
- 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
- B29C70/32—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 on a rotating mould, former or core
-
- 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
- B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
- B29C70/382—Automated fiber placement [AFP]
-
- 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
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
- B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
-
- 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
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3076—Aircrafts
- B29L2031/3082—Fuselages
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24628—Nonplanar uniform thickness material
- Y10T428/24636—Embodying mechanically interengaged strand[s], strand-portion[s] or strand-like strip[s] [e.g., weave, knit, etc.]
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Aviation & Aerospace Engineering (AREA)
- Robotics (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Moulding By Coating Moulds (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US55989004P | 2004-04-06 | 2004-04-06 | |
US10/851,381 US7527222B2 (en) | 2004-04-06 | 2004-05-20 | Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections |
Publications (1)
Publication Number | Publication Date |
---|---|
PT2394909T true PT2394909T (pt) | 2017-03-29 |
Family
ID=35197695
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PT111955118T PT2436595T (pt) | 2004-04-06 | 2005-03-28 | Método para fabricar secções tubulares de compósito para fuselagens de aeronave |
PT111749032T PT2394909T (pt) | 2004-04-06 | 2005-03-28 | Secções tubulares de compósito para fuselagens de aeronave e métodos para fabricar essas secções tubulares |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PT111955118T PT2436595T (pt) | 2004-04-06 | 2005-03-28 | Método para fabricar secções tubulares de compósito para fuselagens de aeronave |
Country Status (7)
Country | Link |
---|---|
US (4) | US7527222B2 (pt) |
EP (4) | EP2394909B1 (pt) |
JP (5) | JP5087390B2 (pt) |
CA (2) | CA2562632C (pt) |
ES (3) | ES2392442T3 (pt) |
PT (2) | PT2436595T (pt) |
WO (1) | WO2006001860A2 (pt) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11826976B2 (en) | 2019-03-08 | 2023-11-28 | Ihi Aerospace Co., Ltd. | FRP molding system and method |
Families Citing this family (180)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9586699B1 (en) | 1999-08-16 | 2017-03-07 | Smart Drilling And Completion, Inc. | Methods and apparatus for monitoring and fixing holes in composite aircraft |
US20140372082A1 (en) * | 2000-12-01 | 2014-12-18 | Aleksandr I. KAMENOMOSTSKIY | Tool for optimized thin wall profile member (tpm) and tpm-panel design and selection |
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 |
US8336596B2 (en) | 2002-11-22 | 2012-12-25 | The Boeing Company | Composite lamination using array of parallel material dispensing heads |
US7249943B2 (en) | 2003-08-01 | 2007-07-31 | Alliant Techsystems Inc. | Apparatus for forming composite stiffeners and reinforcing structures |
US8934702B2 (en) | 2003-12-02 | 2015-01-13 | The Boeing Company | System and method for determining cumulative tow gap width |
US7289656B2 (en) | 2003-12-02 | 2007-10-30 | The Boeing Company | Systems and methods for determining inconsistency characteristics of a composite structure |
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 |
US7837147B2 (en) | 2005-03-18 | 2010-11-23 | The Boeing Company | Systems and methods for reducing noise in aircraft fuselages and other structures |
US7410352B2 (en) * | 2005-04-13 | 2008-08-12 | The Boeing Company | Multi-ring system for fuselage barrel formation |
US7673433B2 (en) * | 2005-04-29 | 2010-03-09 | The Boeing Company | Damage-tolerant monolithic structures |
US8632653B2 (en) * | 2005-05-03 | 2014-01-21 | The Boeing Company | Method of manufacturing curved composite structural elements |
FR2894869B1 (fr) * | 2005-12-20 | 2009-10-09 | Airbus France Sas | Procede de fabrication d'un fuselage d'aeronef en materiau composite |
DE102006002248B4 (de) * | 2006-01-17 | 2008-01-03 | Airbus Deutschland Gmbh | Strukturgebende Konstruktion für einen Flugzeugrumpf |
US7913390B2 (en) * | 2006-02-16 | 2011-03-29 | The Boeing Company | Transport tool |
GB0606079D0 (en) * | 2006-03-27 | 2006-05-03 | Airbus Uk Ltd | Aircraft component |
DE102006025145B3 (de) * | 2006-05-30 | 2008-01-03 | Airbus Deutschland Gmbh | Testvorrichtung |
DE102006026170B4 (de) * | 2006-06-06 | 2012-06-21 | Airbus Operations Gmbh | Flugzeugrumpfstruktur und Verfahren zu deren Herstellung |
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 |
ITTO20060518A1 (it) | 2006-07-14 | 2008-01-15 | Alenia Aeronautica Spa | Metodo, attrezzatura e impianto per la lavorazione di strutture a guscio |
DE102006035847B4 (de) | 2006-08-01 | 2009-11-19 | Airbus Deutschland Gmbh | Strukturanordnung sowie Verfahren zum Herstellen eines Bauteils für die Luft-und Raumfahrt |
ITTO20060600A1 (it) | 2006-08-11 | 2008-02-12 | Alenia Aeronautica Spa | Metodo, impianto e attrezzatura per realizzare parti in materiale composito, in particolare parti o tronchi di fusoliera per aeromobile |
GB0616121D0 (en) * | 2006-08-14 | 2006-09-20 | Airbus Uk Ltd | Moulding tool and method of manufacturing a part |
DE102006039290A1 (de) * | 2006-08-22 | 2008-03-13 | Airbus Deutschland Gmbh | Rahmenelement, Flugzeugkomponentenmontagesystem sowie Verfahren zur Montage einer Komponente in einem Flugzeug |
WO2008025860A1 (es) | 2006-08-31 | 2008-03-06 | Airbus España, S.L. | Componentes tubulares para fuselajes aeronauticos y procedimientos y utiles para su fabricacion |
FR2906785B1 (fr) * | 2006-10-10 | 2009-12-04 | Airbus France | Fuselage d'aeronef realise a partir de panneaux longitudinaux et procede de realisation d'un tel fuselage |
US7871040B2 (en) * | 2006-11-10 | 2011-01-18 | The Boeing Company | Composite aircraft structures with hat stiffeners |
US8691037B2 (en) | 2006-12-14 | 2014-04-08 | The Boeing Company | Method for minimizing fiber distortion during fabrication of one-piece composite barrel section |
US9511571B2 (en) | 2007-01-23 | 2016-12-06 | The Boeing Company | Composite laminate having a damping interlayer and method of making the same |
JP5475465B2 (ja) * | 2007-01-30 | 2014-04-16 | エアバス オペレーションズ,ソシエダド リミタダ | 航空機の胴体のための複合材料構造物およびその製造方法 |
US8388795B2 (en) | 2007-05-17 | 2013-03-05 | The Boeing Company | Nanotube-enhanced interlayers for composite structures |
US7861969B2 (en) * | 2007-05-24 | 2011-01-04 | The Boeing Company | Shaped composite stringers and methods of making |
US8375839B2 (en) * | 2007-08-29 | 2013-02-19 | Supracor, Inc. | Lightweight armor and ballistic projectile defense apparatus |
US8042767B2 (en) * | 2007-09-04 | 2011-10-25 | The Boeing Company | Composite fabric with rigid member structure |
US8668858B2 (en) * | 2007-09-14 | 2014-03-11 | Spectrum Aeronautical, Llc | Method for manufacturing a reinforced panel of composite material |
FR2921898B1 (fr) * | 2007-10-08 | 2009-12-11 | Airbus France | Structure de fuselage pour fuselage d'aeronef en materiau composite et aeronef equipe d'une telle structure de fuselage |
DE102007060029A1 (de) * | 2007-12-13 | 2009-06-18 | Airbus Deutschland Gmbh | Verfahren und Vorrichtung zur Herstellung röhrenförmiger Strukturbauteile |
US8100361B2 (en) * | 2007-12-20 | 2012-01-24 | Airbus Deutschland Gmbh | Hull structure |
US9090028B2 (en) | 2008-04-17 | 2015-07-28 | The Boeing Company | Method for producing contoured composite structures and structures produced thereby |
US9278484B2 (en) | 2008-04-17 | 2016-03-08 | The Boeing Company | Method and apparatus for producing contoured composite structures and structures produced thereby |
US8932423B2 (en) * | 2008-04-17 | 2015-01-13 | The Boeing Company | Method for producing contoured composite structures and structures produced thereby |
US8349105B2 (en) * | 2008-04-17 | 2013-01-08 | The Boeing Company | Curved composite frames and method of making the same |
US8038099B2 (en) * | 2008-04-30 | 2011-10-18 | The Boeing Company | Bonded metal fuselage and method for making the same |
ES2352941B1 (es) | 2008-05-16 | 2012-01-25 | Airbus Operations, S.L. | Estructura integrada de aeronave en material compuesto |
US8079549B2 (en) * | 2008-06-30 | 2011-12-20 | EMBRAER—Empresa Brasileira de Aeronautica S.A. | Monolithic integrated structural panels especially useful for aircraft structures |
US9327467B2 (en) | 2008-07-10 | 2016-05-03 | The Boeing Company | Composite mandrel for autoclave curing applications |
US9238335B2 (en) * | 2008-07-10 | 2016-01-19 | The Boeing Company | Mandrel for autoclave curing applications |
US8025499B2 (en) * | 2008-11-03 | 2011-09-27 | Rohr, Inc. | Multi-segment tool and method for composite formation |
DE102009009491A1 (de) * | 2009-02-18 | 2010-09-09 | Airbus Deutschland Gmbh | Verfahren zum Herstellen eines Schalenkörpers |
US20100233424A1 (en) * | 2009-03-10 | 2010-09-16 | The Boeing Company | Composite structures employing quasi-isotropic laminates |
US8425710B2 (en) | 2009-03-13 | 2013-04-23 | The Boeing Company | Automated placement of vibration damping materials |
DE102010010685A1 (de) | 2009-03-19 | 2011-02-03 | Airbus Operations Gmbh | Verfahren zur toleranzangepassten Klebstoffapplikation im Fahrzeugbau |
DE102010010686A1 (de) * | 2009-03-19 | 2011-01-05 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Verfahren und Vorrichtung zum klebtechnischen Fügen großflächiger Komponenten im Fahrzeugbau |
DE102009019434B4 (de) * | 2009-04-29 | 2016-01-07 | Airbus Operations Gmbh | Flugzeugtür und Verfahren zur Herstellung einer derartigen Flugzeugtür |
BRPI1014554A2 (pt) * | 2009-05-04 | 2016-04-19 | Faisal H-J Knappe | processo e dispositivo para produzir uma linha a partir de uma variedade de filamentos individuais bem ocmo linha monofilamento assim produzida |
FR2946024B1 (fr) * | 2009-05-27 | 2011-07-22 | Airbus France | Installation de realisation d'un troncon de fuselage d'aeronef. |
US8282042B2 (en) * | 2009-06-22 | 2012-10-09 | The Boeing Company | Skin panel joint for improved airflow |
EP2284076A1 (de) * | 2009-08-12 | 2011-02-16 | Dermond-Forstner & Sreboth OG | Verfahren zur Herstellung eines - als Sandwichkonstruktion ausgebildeten - Hohlkörpers |
ES2383424B1 (es) * | 2009-09-29 | 2013-05-03 | Airbus Operations S.L. | Cuaderna de aeronave y metodo de obtencion de la misma |
ES2670225T3 (es) * | 2009-10-20 | 2018-05-29 | Vestas Wind Systems A/S | Método para fabricar un cuerpo de materiales compuestos y una disposición de fabricación de cuerpo de materiales compuestos |
US9662841B2 (en) | 2009-11-10 | 2017-05-30 | Orbital Atk, Inc. | Radially extending composite structures |
US8282757B2 (en) | 2009-11-10 | 2012-10-09 | Alliant Techsystems Inc. | Automated composite annular structure forming |
JP2011104906A (ja) * | 2009-11-18 | 2011-06-02 | Mitsubishi Heavy Ind Ltd | 検査方法、複合材部品の製造方法、検査装置、及び複合材部品製造装置 |
JP5576651B2 (ja) * | 2009-12-25 | 2014-08-20 | 川崎重工業株式会社 | 複合材料構造物製造用マンドレルの組立方法およびマンドレルの組立装置 |
JP5576650B2 (ja) | 2009-12-25 | 2014-08-20 | 川崎重工業株式会社 | 複合材料構造物製造用成形型 |
JP5576652B2 (ja) * | 2009-12-25 | 2014-08-20 | 川崎重工業株式会社 | 複合材料構造物製造用マンドレルの分解方法およびマンドレルの分解装置 |
DE102009060695A1 (de) * | 2009-12-29 | 2011-07-07 | Airbus Operations GmbH, 21129 | Flugzeugrumpf und Hautfeld |
US20110156304A1 (en) * | 2009-12-31 | 2011-06-30 | Bryant Walker | Die Tool Production Methods Utilizing Additive Manufacturing Techniques |
DE102010008711A1 (de) * | 2010-02-19 | 2011-08-25 | GKN Aerospace Services Limited, Isle of Wight | Verfahren und Anordnung zur Herstellung eines einstückigen Hohlprofilbauteils mit Faserverbundwerkstoff |
US9682762B1 (en) * | 2010-05-20 | 2017-06-20 | The Boeing Company | Stiffener with shaped end termination |
US8940213B2 (en) | 2010-06-25 | 2015-01-27 | The Boeing Company | Resin infusion of composite parts using a perforated caul sheet |
US8636252B2 (en) | 2010-06-25 | 2014-01-28 | The Boeing Company | Composite structures having integrated stiffeners with smooth runouts and method of making the same |
US8628717B2 (en) * | 2010-06-25 | 2014-01-14 | The Boeing Company | Composite structures having integrated stiffeners and method of making the same |
US9682514B2 (en) | 2010-06-25 | 2017-06-20 | The Boeing Company | Method of manufacturing resin infused composite parts using a perforated caul sheet |
JP5610881B2 (ja) * | 2010-07-01 | 2014-10-22 | 三菱重工業株式会社 | 複合材成形型及びその製造方法 |
CN103249542A (zh) | 2010-07-13 | 2013-08-14 | 里尔喷射机公司 | 复合结构及其形成方法 |
US8951375B2 (en) * | 2010-11-11 | 2015-02-10 | Spirit Aerosystems, Inc. | Methods and systems for co-bonding or co-curing composite parts using a rigid/malleable SMP apparatus |
JP5779593B2 (ja) * | 2010-12-27 | 2015-09-16 | 川崎重工業株式会社 | 成形治具および成形方法 |
WO2012136222A1 (en) * | 2011-04-06 | 2012-10-11 | Vestas Wind Systems A/S | Method and apparatus for preparing a fibre reinforced composite component |
US9228451B2 (en) | 2011-05-03 | 2016-01-05 | Pratt & Whitney Canada Corp. | Gas turbine engine module adapter to a carrier |
US9180960B2 (en) | 2011-06-10 | 2015-11-10 | The Boeing Company | Boron fiber reinforced structural components |
FR2980732B1 (fr) * | 2011-10-04 | 2013-10-11 | Airbus Operations Sas | Procede et dispositif pour le soudage d'un raidisseur thermoplastique |
US8993097B2 (en) * | 2011-10-10 | 2015-03-31 | The Boeing Company | Tapered height curved composite stringers and corresponding panels |
US10464656B2 (en) | 2011-11-03 | 2019-11-05 | The Boeing Company | Tubular composite strut having internal stiffening and method for making the same |
US10457011B2 (en) | 2011-11-03 | 2019-10-29 | The Boeing Company | Composite columnar structure having co-bonded reinforcement and fabrication method |
US9486965B2 (en) | 2011-11-03 | 2016-11-08 | The Boeing Company | Composite columnar structure having co-bonded reinforcement and fabrication method |
US9090357B2 (en) * | 2011-12-15 | 2015-07-28 | The Boeing Company | Method of assembling panelized aircraft fuselages |
US8771443B2 (en) * | 2012-01-05 | 2014-07-08 | The Boeing Company | Method of fabricating a composite laminate enabling structural monitoring using electromagnetic radiation |
US8714226B2 (en) * | 2012-02-27 | 2014-05-06 | The Boeing Company | Automated fiber placement including layup mandrel tool |
ITTO20120317A1 (it) * | 2012-04-12 | 2013-10-13 | Alenia Aermacchi Spa | Procedimento per la fabbricazione di barili integrali di fusoliera in materiale composito |
US8800628B2 (en) | 2012-05-23 | 2014-08-12 | Lockheed Martin Corporation | Self-propelled airship hull repair system |
US8985514B2 (en) | 2012-06-20 | 2015-03-24 | The Boeing Company | Composite structural panels and aircraft fuselages |
US8939406B2 (en) * | 2012-07-02 | 2015-01-27 | The Boeing Company | Joining composite fuselage sections along window belts |
US9333713B2 (en) | 2012-10-04 | 2016-05-10 | The Boeing Company | Method for co-curing composite skins and stiffeners in an autoclave |
US8974618B1 (en) | 2012-12-04 | 2015-03-10 | The Boeing Company | Systems and methods for assembling a skin of a composite structure |
US9278748B2 (en) | 2012-12-28 | 2016-03-08 | Embraer S.A. | Processes to fabricate composite tubular-reinforced panels integrating skin and stringers and the panels thereby fabricated |
JP6093192B2 (ja) * | 2013-01-25 | 2017-03-08 | 三菱航空機株式会社 | 航空機の機体用パネル、航空機の翼 |
US9314976B2 (en) | 2013-02-15 | 2016-04-19 | The Boeing Company | Systems and methods for compacting a charge of composite material |
US8906179B2 (en) * | 2013-02-21 | 2014-12-09 | The Boeing Company | Systems, tools, and methods for forming composite tubular stringers and stiffened composite structures having composite tubular stringers |
US9211679B1 (en) | 2013-05-03 | 2015-12-15 | The Boeing Company | Systems and methods of forming a skin for a composite structure and composite structures including the same |
US9375908B2 (en) | 2013-05-03 | 2016-06-28 | The Boeing Company | Flexible material transfer devices, flexible vacuum compaction devices, flexible vacuum chucks, and systems and methods including the same |
US9205634B2 (en) * | 2013-05-16 | 2015-12-08 | The Boeing Company | Composite structure and method |
KR101422129B1 (ko) | 2013-05-16 | 2014-07-22 | 재단법인 중소조선연구원 | 회전식 몰드를 이용한 고속 적층성형 장치 |
US9523431B2 (en) | 2013-05-31 | 2016-12-20 | The Boeing Company | Sealing and testing segmented tools |
US9144959B1 (en) | 2013-09-04 | 2015-09-29 | The Boeing Company | Methods for assembling a skin of a composite structure |
GB2519160B (en) * | 2013-10-11 | 2016-06-22 | Spirit Aerosys Inc | Method of liquid resin infusion of a composite preform |
US9511548B1 (en) | 2013-10-16 | 2016-12-06 | The Boeing Company | Systems and methods for assembling a skin of a composite structure |
US9566746B2 (en) | 2013-11-06 | 2017-02-14 | The Boeing Company | Methods and tools for forming contoured composite structures with shape memory alloy |
US9403334B1 (en) | 2013-11-18 | 2016-08-02 | The Boeing Company | Methods and tools for forming composite structures with non-planar patterns of contours |
DE102013224233A1 (de) * | 2013-11-27 | 2015-05-28 | Airbus Operations Gmbh | Druckschott für ein Flugzeug und Vorrichtung sowie Verfahren zur Herstellung eines Flugzeugstrukturbauteils |
WO2015094059A1 (en) * | 2013-12-20 | 2015-06-25 | Saab Ab | Stiffening element and reinforced structure |
US8894011B1 (en) | 2014-02-14 | 2014-11-25 | The Boeing Company | Aircraft fuselage constructed of aircraft fuselage sections screwed together |
WO2015162402A2 (en) | 2014-04-24 | 2015-10-29 | Bae Systems Plc | Machining fixture production |
GB2527887B (en) | 2014-04-24 | 2017-10-04 | Bae Systems Plc | Assembly tool production |
ES2898091T3 (es) | 2014-04-24 | 2022-03-03 | Bae Systems Plc | Producción de componentes de un armazón de aeronave |
WO2015162404A1 (en) * | 2014-04-24 | 2015-10-29 | Bae Systems Plc | Airframe production |
EP3134785B1 (en) | 2014-04-24 | 2021-06-02 | BAE Systems PLC | Aircraft airframe assembly |
WO2015162400A2 (en) | 2014-04-24 | 2015-10-29 | Bae Systems Plc | Object production |
GB2528080A (en) * | 2014-07-08 | 2016-01-13 | Airbus Operations Ltd | Structure |
US9610728B2 (en) | 2014-07-18 | 2017-04-04 | The Boeing Company | Apparatus and methods for bonding laminate structures |
USD777014S1 (en) * | 2014-08-12 | 2017-01-24 | Servi-Sure, LLC | Integrated stiffener |
US9555587B2 (en) * | 2014-08-13 | 2017-01-31 | The Boeing Company | Composite layup tools for aircraft fuselage barrels, methods of assembling the layup tools, and aircraft fuselage barrel sections formed utilizing the layup tools |
US10137607B2 (en) * | 2014-10-01 | 2018-11-27 | The Boeing Company | Methods and apparatus for curing composite nacelle structure |
GB2532451B (en) * | 2014-11-19 | 2018-12-26 | Bae Systems Plc | Object production |
CA2970070A1 (en) * | 2014-12-12 | 2016-06-16 | Bombardier Inc. | Method of making pad-ups for composite structures and composite structures including pad-ups |
US10040537B2 (en) * | 2015-01-15 | 2018-08-07 | The Boeing Company | Laminate composite wing structures |
US9545759B2 (en) | 2015-01-30 | 2017-01-17 | CGTech | Automated fiber placement with course trajectory compensation |
DE102015002777A1 (de) * | 2015-03-06 | 2016-09-08 | Broetje-Automation Gmbh | Faserlegemaschine |
DE102015002775A1 (de) | 2015-03-06 | 2016-09-08 | Brötje-Automation GmbH | System zur Fertigung von Faser-Verbundbauteilen |
US9809297B2 (en) * | 2015-08-26 | 2017-11-07 | The Boeing Company | Structures containing stiffeners having transition portions |
US10040221B2 (en) | 2015-10-16 | 2018-08-07 | The Boeing Company | Elongated elastomeric parts and mandrels for facilitating removal of elongated elastomeric parts formed thereon |
US10293519B2 (en) | 2015-10-30 | 2019-05-21 | The Boeing Company | Mandrel bladder end fitting |
WO2017095810A1 (en) | 2015-11-30 | 2017-06-08 | Cytec Industries Inc. | Surfacing materials for composite structures |
US10697470B2 (en) | 2016-02-15 | 2020-06-30 | General Electric Company | Containment case trench filler layer and method of containing releasable components from rotatable machines |
US10144497B2 (en) * | 2016-04-18 | 2018-12-04 | The Boeing Company | Hat section door frame with integral gussets |
JP6622645B2 (ja) * | 2016-04-20 | 2019-12-18 | 川崎重工業株式会社 | 航空機胴体組立治具およびその使用方法 |
US10899103B2 (en) | 2016-11-03 | 2021-01-26 | Anthony A. DUPont | Isogrid stiffening elements |
US11479333B2 (en) | 2016-12-16 | 2022-10-25 | Manuel Torres Martinez | Method for manufacturing a one-piece reinforced structure and obtained structure |
EP3659774B1 (en) * | 2017-07-25 | 2023-05-31 | Subaru Corporation | Composite material molding jig and composite material molding method |
US10940648B2 (en) * | 2018-04-19 | 2021-03-09 | The Boeing Company | Three dimensional printed fibrous interlocking interlayers |
US10562262B2 (en) * | 2018-04-19 | 2020-02-18 | The Boeing Company | Thermoplastic cellular network toughened composites |
US11052571B2 (en) * | 2018-07-26 | 2021-07-06 | The Boeing Company | Continuous fabrication for composite preforms |
US11090882B2 (en) | 2018-09-26 | 2021-08-17 | The Boeing Company | Test system and method for creating controlled and repeatable out-of-plane fiber distortion in composite laminates |
US11198267B2 (en) | 2018-10-29 | 2021-12-14 | The Boeing Company | Bulk factor compensated tool for fabrication of a composite part |
US11180238B2 (en) * | 2018-11-19 | 2021-11-23 | The Boeing Company | Shear ties for aircraft wing |
US11358348B2 (en) | 2019-01-02 | 2022-06-14 | The Boeing Company | Mold insert for use with a mandrel for forming a composite structure |
US11110671B2 (en) | 2019-03-06 | 2021-09-07 | The Boeing Company | Layup support configured to provide support for laying up composite material |
JP6780114B1 (ja) * | 2019-04-12 | 2020-11-04 | 株式会社Ihiエアロスペース | 継手構造体及びその組立方法 |
US10828880B1 (en) * | 2019-05-07 | 2020-11-10 | Spirit Aerosystems, Inc. | Method of fusing thermoplastic composite structures |
EP4269059A3 (en) * | 2019-05-14 | 2023-12-27 | Airbus Operations Limited | Aircraft wing assembly |
GB2583940A (en) * | 2019-05-14 | 2020-11-18 | Airbus Operations Ltd | Aircraft panel assembly |
US11148373B2 (en) | 2019-07-01 | 2021-10-19 | The Boeing Company | System and method for laying up a composite laminate having integrally laminated filler elements |
US11628922B2 (en) * | 2020-02-18 | 2023-04-18 | The Boeing Company | Composite plank support for stringer panel |
CN115427218A (zh) * | 2020-08-31 | 2022-12-02 | 株式会社Ihi空间技术 | Frp成形***和方法 |
JP2022080864A (ja) * | 2020-11-18 | 2022-05-30 | ザ・ボーイング・カンパニー | 未固化の胴体構成要素のための複合組立 |
NL2027415B1 (en) * | 2021-01-26 | 2022-08-26 | Boeing Co | Fabrication line, systems, and methods for fuselage sections |
EP4000846A1 (en) | 2020-11-18 | 2022-05-25 | The Boeing Company | Fabrication line and systems for fuselage sections |
EP4000845A1 (en) | 2020-11-18 | 2022-05-25 | The Boeing Company | Fabrication systems and methods for fuselage sections |
EP4000847A1 (en) | 2020-11-18 | 2022-05-25 | The Boeing Company | Fabrication system for fuselage sections |
EP4000841A1 (en) | 2020-11-18 | 2022-05-25 | The Boeing Company | Composite assembly for unhardened fuselage components |
NL2027427B1 (en) * | 2021-01-26 | 2022-08-26 | Boeing Co | Edge trimming for moving-line fabrication of aircraft |
NL2028118B1 (en) * | 2021-04-30 | 2022-11-09 | Boeing Co | Cut-out processes for moving-line structure assembly |
EP4000901A1 (en) * | 2020-11-18 | 2022-05-25 | The Boeing Company | Frame installation station for aircraft fuselage segments |
NL2027399B1 (en) * | 2021-01-26 | 2022-08-17 | Boeing Co | Composite assembly for unhardened fuselage components |
US11986917B2 (en) * | 2020-11-18 | 2024-05-21 | The Boeing Company | Indexing apparatus and method of indexing |
EP4011535A1 (en) | 2020-11-18 | 2022-06-15 | The Boeing Company | Edge trimming for moving-line fabrication of aircraft |
NL2028100B1 (en) * | 2021-04-30 | 2022-11-09 | Boeing Co | Frame installation station for aircraft fuselage segments |
JP2022080869A (ja) | 2020-11-18 | 2022-05-30 | ザ・ボーイング・カンパニー | 航空機製造のための当て板システム |
NL2027420B1 (en) * | 2021-01-26 | 2022-08-26 | Boeing Co | Fabrication line, systems, and methods for fuselage sections |
EP4011606A3 (en) * | 2020-11-18 | 2022-10-05 | The Boeing Company | Caul plate system for aircraft fabrication |
NL2027419B1 (en) * | 2021-01-26 | 2022-08-26 | Boeing Co | Fabrication line, systems, and methods for fuselage sections |
EP4002035A3 (en) | 2020-11-19 | 2022-07-20 | The Boeing Company | Continuous-line manufacturing system and method for automated machine allocation |
EP4011783B1 (en) * | 2020-12-09 | 2023-08-30 | The Boeing Company | Fractional pulse line for aircraft fuselage manufacturing |
US11911978B2 (en) * | 2021-05-07 | 2024-02-27 | The Boeing Company | Methods and associated systems for manufacturing composite barrel structures |
GB2612958B (en) * | 2021-11-08 | 2023-12-20 | Airbus Operations Ltd | Panel assembly |
GB2615755A (en) * | 2022-02-15 | 2023-08-23 | Airbus Operations Ltd | Fuel tank stringer with flow passage |
Family Cites Families (217)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US559890A (en) * | 1896-05-12 | Screw-propeller | ||
US2004A (en) | 1841-03-12 | Improvement in the manner of constructing and propelling steam-vessels | ||
US559911A (en) * | 1896-05-12 | sheridan | ||
US1976257A (en) * | 1930-03-12 | 1934-10-09 | Super Marine Systems Inc | Laminated body and method of making same |
US2367750A (en) * | 1941-01-17 | 1945-01-23 | Central Aircraft Corp | Aircraft construction |
US2292372A (en) * | 1941-07-28 | 1942-08-11 | Vultee Aircraft Inc | Structural element |
US2387219A (en) * | 1941-08-08 | 1945-10-16 | Vickers Armstrongs Ltd | Aircraft structure |
US3271917A (en) | 1959-06-12 | 1966-09-13 | Rubenstein David | Reinforced plastic constructions |
US2992711A (en) | 1959-11-16 | 1961-07-18 | Ryan Aeronautical Co | Reinforcing means for attaching structural members to lightweight corrugated panels |
US3071217A (en) | 1960-01-15 | 1963-01-01 | Avro Aircraft Ltd | Vibration damping in sheet metal structures |
US3306767A (en) | 1962-09-20 | 1967-02-28 | Boeing Co | Method of applying a resin laminar substrate to a surface |
US3306797A (en) * | 1963-08-02 | 1967-02-28 | Universal Moulded Fiber Glass | Method and apparatus for making elongated articles of fiber reinforced resin material |
US3490983A (en) * | 1965-05-17 | 1970-01-20 | Hitco | Fiber reinforced structures and methods of making the same |
US3507634A (en) | 1965-10-22 | 1970-04-21 | United Aircraft Corp | Composite metal structure |
US3452501A (en) | 1966-05-02 | 1969-07-01 | Ernest C Zimmer | Snap locking structural device |
US3603096A (en) | 1969-12-10 | 1971-09-07 | Atomic Energy Commission | Apparatus for installing a reinforced vessel in an underground cavity |
US3879245A (en) | 1972-06-27 | 1975-04-22 | Composite Structures Corp | Method of making composite cored structures |
JPS5546920B2 (pt) * | 1973-10-12 | 1980-11-27 | ||
US3974313A (en) | 1974-08-22 | 1976-08-10 | The Boeing Company | Projectile energy absorbing protective barrier |
US3995080A (en) | 1974-10-07 | 1976-11-30 | General Dynamics Corporation | Filament reinforced structural shapes |
US3976269A (en) | 1974-12-19 | 1976-08-24 | The Boeing Company | Intrinsically tuned structural panel |
US4086378A (en) | 1975-02-20 | 1978-04-25 | Mcdonnell Douglas Corporation | Stiffened composite structural member and method of fabrication |
JPS5296064A (en) | 1976-02-09 | 1977-08-12 | Seiko Epson Corp | Electronic timepiece |
US4064534A (en) | 1976-04-20 | 1977-12-20 | Leone International Sales Corporation | System for monitoring the production of items which are initially difficult to physically inspect |
US4186535A (en) | 1977-06-10 | 1980-02-05 | Verco Manufacturing, Inc. | Shear load resistant structure |
US4256790A (en) | 1978-01-19 | 1981-03-17 | Rockwell International Corporation | Reinforced composite structure and method of fabrication thereof |
US4331495A (en) * | 1978-01-19 | 1982-05-25 | Rockwell International Corporation | Method of fabricating a reinforced composite structure |
US4310132A (en) | 1978-02-16 | 1982-01-12 | Nasa | Fuselage structure using advanced technology fiber reinforced composites |
US4828202A (en) | 1979-09-27 | 1989-05-09 | The Boeing Company | Method and apparatus for wideband vibration damping of reinforced skin structures |
US4490958A (en) | 1979-12-12 | 1985-01-01 | Lowe Colin F | Sheet metal beam |
US4311661A (en) * | 1980-05-05 | 1982-01-19 | Mcdonnell Douglas Corporation | Resin impregnation process |
DE3040838C2 (de) | 1980-10-30 | 1984-10-25 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Verfahren und Vorrichtung zum Herstellen von flächigen Bauteilen aus faserverstärkten Werkstoffen |
US4331723A (en) * | 1980-11-05 | 1982-05-25 | The Boeing Company | Advanced composite |
FR2497726A1 (fr) | 1981-01-12 | 1982-07-16 | Brochier Fils J | Article textile multicouches pour le renforcement de materiaux stratifies et procede pour son obtention |
US4448838A (en) * | 1981-09-04 | 1984-05-15 | Lear Fan Corp. | Graphite fiber reinforced laminate structure capable of withstanding lightning strikes |
US4463044A (en) * | 1981-09-28 | 1984-07-31 | The Boeing Company | Composite panel of varied thickness |
JPS58179637A (ja) * | 1982-04-14 | 1983-10-20 | 宇宙開発事業団 | 高荷重用軽量中空体 |
DE3277865D1 (en) | 1982-07-19 | 1988-02-04 | Boeing Co | Method and apparatus for fiber lamination |
US4492607A (en) * | 1983-02-22 | 1985-01-08 | Rockwell International Corporation | Method for producing integrally stiffened fiber reinforced plastic panels |
US4715560A (en) | 1983-03-14 | 1987-12-29 | Lear Fan Limited | Composite cruciform structure for joining intersecting structural members of an airframe and the like |
DE3331494A1 (de) | 1983-09-01 | 1985-03-21 | Rudolf 8900 Augsburg Güthler | Mehrband-legemaschine |
US4542055A (en) | 1983-10-19 | 1985-09-17 | Conceptual Arts, Ltd. | Three-dimensional fabric painting surfaces |
DE3341564A1 (de) * | 1983-11-17 | 1985-05-30 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Gekruemmtes flaechenbauteil, insbesondere fuer luftfahrzeuge und vorrichtung zu deren herstellung |
US4736566A (en) | 1984-01-17 | 1988-04-12 | Krotsch Harold V | Modular fabrication panel system |
US4548017A (en) | 1984-01-23 | 1985-10-22 | Liverpool Industries, Inc. | Building panel |
IT1173394B (it) | 1984-02-28 | 1987-06-24 | Rockwell Rimoldi Spa | Dispositivo di trasporto del lavoro in macchina per cucire a trasporto differenziale |
DE3412846A1 (de) | 1984-04-05 | 1985-10-17 | Hoechst Ag, 6230 Frankfurt | Flaechenfoermiger sandwichformkoerper |
US4574029A (en) * | 1984-04-27 | 1986-03-04 | Ltv Aerospace And Defense Company | Apparatus for forming concave tape wrapped composite structures |
US4877471A (en) | 1984-08-24 | 1989-10-31 | The Boeing Company | Method and apparatus for delivering a resin-impregnated, multifilament band |
US4548859A (en) | 1984-10-12 | 1985-10-22 | The Boeing Company | Breather material and method of coating fabric with silicone rubber |
US4571355A (en) * | 1984-11-28 | 1986-02-18 | The Boeing Company | Fiber reinforced resin composites formed of basic ply blankets |
US4622091A (en) | 1984-11-29 | 1986-11-11 | The Boeing Company | Resin film infusion process and apparatus |
US4608220A (en) | 1984-12-20 | 1986-08-26 | The Boeing Company | Method of forming composite material articles |
JPS61169394A (ja) * | 1985-01-21 | 1986-07-31 | 日立造船株式会社 | 飛行機の胴体成形方法 |
FR2579130B1 (fr) | 1985-03-25 | 1987-10-09 | Aerospatiale | Procede et dispositif pour realiser une piece creuse de forme complexe par enroulement filamentaire au contact |
US4615935A (en) | 1985-04-29 | 1986-10-07 | The Boeing Company | Glass fiber reinforced ceramic preform and method of casting it |
US4966802A (en) | 1985-05-10 | 1990-10-30 | The Boeing Company | Composites made of fiber reinforced resin elements joined by adhesive |
JPS6219440A (ja) * | 1985-07-19 | 1987-01-28 | Hitachi Zosen Corp | 飛行機の胴体成形方法 |
US4693678A (en) | 1986-01-15 | 1987-09-15 | The Boeing Company | Male layup-female molding system for fabricating reinforced composite structures |
US4780262A (en) | 1986-01-15 | 1988-10-25 | The Boeing Company | Method for making composite structures |
US4699683A (en) | 1986-02-07 | 1987-10-13 | The Boeing Company | Multiroving fiber laminator |
DE3614618A1 (de) * | 1986-04-30 | 1987-11-05 | Messerschmitt Boelkow Blohm | Schalenstruktur aus faserverstaerktem kunststoff |
US4830298A (en) | 1986-09-30 | 1989-05-16 | The Boeing Company | Self-centering sheave for filaments |
US4760444A (en) | 1987-07-22 | 1988-07-26 | Csd International, Inc. | Machine visual inspection device and method |
US4941182A (en) | 1987-07-29 | 1990-07-10 | Phoenix Software Development Co. | Vision system and method for automated painting equipment |
JP2604607B2 (ja) | 1987-12-09 | 1997-04-30 | 三井金属鉱業株式会社 | 欠陥分布測定法および装置 |
JPH01153541U (pt) | 1988-04-14 | 1989-10-23 | ||
US4959110A (en) | 1988-05-11 | 1990-09-25 | Morton Thiokol Inc. | Method for lining the inner surface of a cylindrical or domed cylindrical member with an elastomeric material |
FR2632604B1 (fr) | 1988-06-08 | 1991-07-12 | Aerospatiale | Cadre en materiau composite notamment pour fuselage d'aeronef, et son procede de fabrication |
GB2224000B (en) * | 1988-11-10 | 1992-05-27 | Genrikh Vasilievich Novozhilov | Aircraft fuselage or other pressure vessel. |
US4942013A (en) | 1989-03-27 | 1990-07-17 | Mcdonnell Douglas Corporation | Vacuum resin impregnation process |
JP2652574B2 (ja) * | 1989-09-26 | 1997-09-10 | 三菱重工業株式会社 | 複合材継手用織物 |
US5251849A (en) | 1989-12-26 | 1993-10-12 | Florida International University For Board Of Regents | Strain reduced airplane skin |
JP2935722B2 (ja) * | 1990-02-28 | 1999-08-16 | 富士重工業株式会社 | 航空機の胴体構造およびその成形方法 |
US5223067A (en) * | 1990-02-28 | 1993-06-29 | Fuji Jukogyo Kabushiki Kaisha | Method of fabricating aircraft fuselage structure |
US5086997A (en) | 1990-04-02 | 1992-02-11 | The Boeing Company | Structural joint and a method for joining in reinforced thermoplastic fabrication |
FR2661872B1 (fr) | 1990-05-11 | 1992-09-04 | Rockwell Automotive Body Syst | Procede de fabrication d'un pare-soleil recouvert de tissu. |
US5058497A (en) | 1990-12-17 | 1991-10-22 | Mcdonnell Douglas Corporation | Compliant pressure roller |
US5152949A (en) * | 1990-12-19 | 1992-10-06 | United Technologies Corporation | Tooling method for resin transfer molding |
CA2056330C (en) * | 1990-12-19 | 2003-06-10 | Alexander C. Dublinski | Method of fabricating a complex part made of composite material |
US5262220A (en) | 1991-06-18 | 1993-11-16 | Chem-Tronics, Inc. | High strength structure assembly and method of making the same |
JPH0516248A (ja) * | 1991-07-10 | 1993-01-26 | Mitsubishi Heavy Ind Ltd | Frp製品 |
US5240376A (en) | 1991-07-31 | 1993-08-31 | Mcdonnell Douglas Corporation | SPF/DB hollow core fan blade |
US5337647A (en) | 1992-03-13 | 1994-08-16 | The Boeing Company | 3 dimensional braiding apparatus |
US5281388A (en) * | 1992-03-20 | 1994-01-25 | Mcdonnell Douglas Corporation | Resin impregnation process for producing a resin-fiber composite |
US5242523A (en) * | 1992-05-14 | 1993-09-07 | The Boeing Company | Caul and method for bonding and curing intricate composite structures |
US5429326A (en) | 1992-07-09 | 1995-07-04 | Structural Laminates Company | Spliced laminate for aircraft fuselage |
US5297760A (en) | 1992-08-21 | 1994-03-29 | Mcdonnell Douglas Corporation | Aircraft skin lap splice |
US5651600A (en) | 1992-09-28 | 1997-07-29 | The Boeing Company | Method for controlling projection of optical layup template utilizing cooperative targets |
US5450147A (en) | 1992-09-28 | 1995-09-12 | The Boeing Company | Method for controlling projection of optical layup template utilizing cooperative targets |
US5560102A (en) | 1992-10-13 | 1996-10-01 | The Boeing Company | Panel and fuselage assembly |
US5951800A (en) | 1992-11-18 | 1999-09-14 | Mcdonnell Douglas Corp. | Fiber/metal laminate splice |
JPH06226889A (ja) | 1993-02-05 | 1994-08-16 | Sky Alum Co Ltd | パネル材およびこれを用いた複合パネル |
US5765329A (en) | 1993-06-28 | 1998-06-16 | Huang; Chihshu | Roof construction of corrugated sheets |
US6045651A (en) | 1993-09-07 | 2000-04-04 | The Boeing Company | Hand assisted lamination system |
US5518208A (en) | 1993-12-28 | 1996-05-21 | The Boeing Company | Optimum aircraft body frame to body skin shear tie installation pattern for body skin/stringer circumferential splices |
US5439549A (en) | 1993-12-28 | 1995-08-08 | The Boeing Company | Double edged pressure sensitive folded tape application apparatus |
RU2083371C1 (ru) | 1994-04-28 | 1997-07-10 | Акционерное общество "Центр перспективных разработок" Акционерного общества "Центральный научно-исследовательский институт специального машиностроения | Несущая труба-оболочка из композиционных материалов, способ и оправка для ее изготовления |
US5540126A (en) | 1994-05-26 | 1996-07-30 | Piramoon Technologies | Automatic lay-up machine for composite fiber tape |
US5562788A (en) | 1994-09-20 | 1996-10-08 | The Boeing Company | Composite material laser flaw detection |
US5622733A (en) | 1994-10-04 | 1997-04-22 | Rockwell International Corporation | Tooling for the fabrication of composite hollow crown-stiffened skins and panels |
US5683646A (en) | 1995-05-10 | 1997-11-04 | Mcdonnell Douglas Corporation | Fabrication of large hollow composite structure with precisely defined outer surface |
US5619837A (en) | 1995-07-26 | 1997-04-15 | Disanto; Fabricio N. | Corrugated panel structure |
RU2099194C1 (ru) | 1995-12-01 | 1997-12-20 | Акционерное общество "Центр перспективных разработок" Акционерного общества "Центральный научно-исследовательский институт специального машиностроения" | Несущая труба-оболочка в виде тела вращения из композиционных материалов, способ и оправка для ее изготовления |
US5893534A (en) | 1995-12-22 | 1999-04-13 | The Boeing Company | Structural apparatus and design to prevent oil can movement of webs in aircraft pressure bulkheads |
US5866272A (en) * | 1996-01-11 | 1999-02-02 | The Boeing Company | Titanium-polymer hybrid laminates |
US5700337A (en) | 1996-03-01 | 1997-12-23 | Mcdonnell Douglas Corporation | Fabrication method for composite structure adapted for controlled structural deformation |
US5746553A (en) | 1996-04-08 | 1998-05-05 | The Boeing Company | Dual purpose lay-up tool |
US6205239B1 (en) | 1996-05-31 | 2001-03-20 | Texas Instruments Incorporated | System and method for circuit repair |
JPH1016085A (ja) * | 1996-07-04 | 1998-01-20 | Mitsubishi Heavy Ind Ltd | 航空機の胴体外板の製造方法 |
US6013341A (en) | 1996-08-19 | 2000-01-11 | Mcdonnell Douglas Corporation | Carrying (bearing) pipe-casing made of composite materials, the method and the setting (straightening device) for its manufacturing |
US5809805A (en) | 1996-09-03 | 1998-09-22 | Mcdonnell Douglas Corporation | Warp/knit reinforced structural fabric |
US5963660A (en) | 1996-09-26 | 1999-10-05 | The Boeing Company | Method and apparatus for detecting and measuring laps and gaps in composite materials |
US6187411B1 (en) | 1996-10-04 | 2001-02-13 | The Boeing Company | Stitch-reinforced sandwich panel and method of making same |
RU2103200C1 (ru) | 1996-10-29 | 1998-01-27 | Акционерное общество "Центр перспективных разработок" Акционерного общества "Центральный научно-исследовательский институт специального машиностроения" | Несущая труба-оболочка из композиционных материалов |
US6692681B1 (en) | 1997-01-29 | 2004-02-17 | Raytheon Aircraft Company | Method and apparatus for manufacturing composite structures |
AU6137798A (en) * | 1997-01-29 | 1998-08-18 | Raytheon Aircraft Company | Method and apparatus for manufacturing composite structures |
DE59806899D1 (de) | 1997-02-05 | 2003-02-20 | Anatoli J Vassiliev | Flugzeug für Personen- und/oder Frachttransport |
US6051089A (en) * | 1997-02-07 | 2000-04-18 | Mcdonnell Douglas Corporation | Reinforcing member for composite workpieces and associated methods |
JPH10258463A (ja) | 1997-03-19 | 1998-09-29 | Fuji Heavy Ind Ltd | 複合材の小骨およびその成形方法 |
CN1104974C (zh) | 1997-05-06 | 2003-04-09 | 波音公司 | 混合型结层机具 |
US5954917A (en) | 1997-06-02 | 1999-09-21 | Boeing North American, Inc. | Automated material delivery system |
US6074716A (en) | 1997-06-10 | 2000-06-13 | Mcdonnell Douglas Corporation | Weavable metal matrix impregnated tow composite material |
GB9713209D0 (en) * | 1997-06-20 | 1997-08-27 | British Aerospace | Friction welding metal components |
FR2766407B1 (fr) * | 1997-07-22 | 1999-10-15 | Aerospatiale | Procede de fabrication de pieces de grandes dimensions en materiau composite a matrice thermoplastique, telles que des troncons de fuselage d'aeronefs |
US5902535A (en) * | 1997-07-30 | 1999-05-11 | Mcdonnell Douglas Corporation | Resin film infusion mold tooling and molding method |
US5979531A (en) | 1997-10-01 | 1999-11-09 | Mcdonnell Douglas Corporation | Bi-directional fiber placement head |
JP3293063B2 (ja) * | 1997-12-08 | 2002-06-17 | カシオ計算機株式会社 | 蓋体の開閉構造 |
US5931107A (en) | 1997-12-22 | 1999-08-03 | Mcdonnell Douglas Corporation | Advanced stitching head for making stitches in a textile article having variable thickness |
US5953231A (en) | 1997-12-22 | 1999-09-14 | Mcdonnell Douglas Corporation | Automated quality control for stitching of textile articles |
US6198983B1 (en) * | 1997-12-22 | 2001-03-06 | Mcdonnell Douglas Corporation | Table-driven software architecture for a stitching system |
US5915317A (en) * | 1997-12-22 | 1999-06-29 | Thrash; Patrick J. | Automated gantry-type stitching system |
US6128545A (en) | 1997-12-22 | 2000-10-03 | Mcdonnell Douglas Corporation | Automated apparatus and method of generating native code for a stitching machine |
US6099906A (en) | 1998-06-22 | 2000-08-08 | Mcdonnell Douglas Corporation | Immersion process for impregnation of resin into preforms |
US6231941B1 (en) * | 1998-07-14 | 2001-05-15 | The Boeing Company | Radius fillers for a resin transfer molding process |
US6766984B1 (en) | 1998-07-16 | 2004-07-27 | Icom Engineering Corporation | Stiffeners for aircraft structural panels |
US6086696A (en) | 1998-07-21 | 2000-07-11 | The Boeing Company | Method of forming a seamless, cylindrical, thermoplastic structure with a multiple compaction roller winder |
DE19844035C1 (de) | 1998-09-25 | 1999-11-25 | Daimler Chrysler Aerospace | Schalenbauteil für ein Flugzeug und Verfahren zur Herstellung |
FI982095A (fi) | 1998-09-29 | 2000-03-30 | Nokia Networks Oy | Menetelmä muistin toteuttamiseksi ja muistijärjestely |
US6112792A (en) | 1998-11-19 | 2000-09-05 | The Boeing Company | Fiber placement mid-span redirect |
US6190484B1 (en) * | 1999-02-19 | 2001-02-20 | Kari Appa | Monolithic composite wing manufacturing process |
US6261675B1 (en) * | 1999-03-23 | 2001-07-17 | Hexcel Corporation | Core-crush resistant fabric and prepreg for fiber reinforced composite sandwich structures |
US6319447B1 (en) * | 1999-04-09 | 2001-11-20 | The Boeing Company | Resin transfer molding process |
US6136237A (en) | 1999-04-13 | 2000-10-24 | The Boeing Company | Method of fabricating a fiber-reinforced ceramic matrix composite part |
US6510961B1 (en) * | 1999-04-14 | 2003-01-28 | A&P Technology | Integrally-reinforced braided tubular structure and method of producing the same |
US6431837B1 (en) | 1999-06-01 | 2002-08-13 | Alexander Velicki | Stitched composite fan blade |
US7132161B2 (en) * | 1999-06-14 | 2006-11-07 | Energy Science Laboratories, Inc. | Fiber adhesive material |
BR0013763A (pt) | 1999-09-03 | 2002-07-02 | Lockheed Corp | Soldagem aplicada com agitação do atrito como uma tecnologia de substituição aos rebites |
US6374750B1 (en) | 1999-11-16 | 2002-04-23 | Aero Transportation Products, Inc. | Structural panel system |
US6129031A (en) | 1999-11-16 | 2000-10-10 | The Boeing Company | Robotic stitching apparatus and end effector therefor |
US6390169B1 (en) | 2000-02-23 | 2002-05-21 | The Boeing Company | Conformable compaction apparatus for use with a fiber placement machine |
AU2001262912A1 (en) * | 2000-02-25 | 2001-09-03 | The Boeing Company | Laminated composite radius filler |
ES2185443B1 (es) | 2000-03-07 | 2004-09-01 | Airbus España S.L. | Procedimiento de fabricacion de piezas precuradas en material compuesto con rigidizadores aplicados en estado fresco. |
JP4425422B2 (ja) | 2000-04-14 | 2010-03-03 | 本田技研工業株式会社 | 複合材製構造体の製造方法、及びそれにより製造される複合材製構造体 |
JP4318381B2 (ja) * | 2000-04-27 | 2009-08-19 | 本田技研工業株式会社 | 繊維強化複合材からなる胴体構造体の製造方法、及びそれにより製造される胴体構造体 |
JP4425424B2 (ja) | 2000-05-01 | 2010-03-03 | 本田技研工業株式会社 | 繊維強化複合材からなるジョグル付き半硬化物品の製造方法、及びそれを用いた予備成形構造体の製造方法 |
US6451152B1 (en) | 2000-05-24 | 2002-09-17 | The Boeing Company | Method for heating and controlling temperature of composite material during automated placement |
US6620484B1 (en) | 2000-06-06 | 2003-09-16 | The Boeing Company | Variable density stitched-composite structural elements for energy absorption |
US6415581B1 (en) | 2000-07-17 | 2002-07-09 | Deck West, Incorporated | Corrugated stiffening member |
DE10037307B4 (de) | 2000-07-28 | 2004-02-05 | Honsel Gmbh & Co Kg | Strukturelement für ein Flugzeug, insbesondere Flugzeugtür |
WO2002040254A2 (en) * | 2000-11-15 | 2002-05-23 | Toyota Motor Sales, U.S.A., Inc. | One-piece closed-shape structure and method of forming same |
JP2002154484A (ja) * | 2000-11-17 | 2002-05-28 | Toyota Motor Corp | Frp構造体 |
JP4526698B2 (ja) | 2000-12-22 | 2010-08-18 | 富士重工業株式会社 | 複合材成形品及びその製造方法 |
US6480271B1 (en) | 2001-01-08 | 2002-11-12 | The Boeing Company | Traversing laser locating system |
US6743504B1 (en) * | 2001-03-01 | 2004-06-01 | Rohr, Inc. | Co-cured composite structures and method of making them |
US7171033B2 (en) * | 2001-03-28 | 2007-01-30 | The Boeing Company | System and method for identifying defects in a composite structure |
SE519185C2 (sv) | 2001-06-07 | 2003-01-28 | Saab Ab | Flygplanspanel |
US6840750B2 (en) * | 2001-06-11 | 2005-01-11 | The Boeing Company | Resin infusion mold tool system and vacuum assisted resin transfer molding with subsequent pressure bleed |
JP2003020542A (ja) * | 2001-07-06 | 2003-01-24 | Toray Ind Inc | 炭素繊維布帛、成形方法、炭素繊維強化プラスチックおよび航空機構造部材 |
JP4639551B2 (ja) * | 2001-08-10 | 2011-02-23 | 東レ株式会社 | Cfrp製スキン−ストリンガー構造部材の製造方法 |
US6648273B2 (en) | 2001-10-30 | 2003-11-18 | The Boeing Company | Light weight and high strength fuselage |
US6799619B2 (en) | 2002-02-06 | 2004-10-05 | The Boeing Company | Composite material collation machine and associated method for high rate collation of composite materials |
JP4313539B2 (ja) * | 2002-03-14 | 2009-08-12 | フジノン株式会社 | 非球面合成樹脂レンズを有するズームレンズ |
US20030190455A1 (en) * | 2002-04-05 | 2003-10-09 | The Boeing Company | Textile joint reinforcement and associated method |
US7334782B2 (en) * | 2002-05-29 | 2008-02-26 | The Boeing Company | Controlled atmospheric pressure resin infusion process |
US6860957B2 (en) | 2002-06-13 | 2005-03-01 | Kawasaki Jukogyo Kabushiki Kaisha | Automatic prepreg laminating method and apparatus for carrying out the same |
JP2004025946A (ja) | 2002-06-24 | 2004-01-29 | Honda Motor Co Ltd | 航空機の翼構造 |
US7204951B2 (en) * | 2002-07-30 | 2007-04-17 | Rocky Mountain Composites, Inc. | Method of assembling a single piece co-cured structure |
US6871684B2 (en) | 2002-08-13 | 2005-03-29 | The Boeing Company | System for identifying defects in a composite structure |
US6622974B1 (en) | 2002-08-14 | 2003-09-23 | The Boeing Company | Geometric morphing wing with expandable spars |
US20040035979A1 (en) * | 2002-08-23 | 2004-02-26 | Mccoskey William Robert | Integrally stiffened axial load carrying skin panels for primary aircraft structure and closed loop manufacturing methods for making the same |
FR2844510B1 (fr) | 2002-09-12 | 2006-06-16 | Snecma Propulsion Solide | Structure fibreuse tridimensionnelle en fibres refractaires, procede pour sa realisation et application aux materiaux composites thermostructuraux |
US20040086341A1 (en) * | 2002-11-05 | 2004-05-06 | Conoco Inc. | Metal lined composite risers in offshore applications |
US7137182B2 (en) * | 2002-11-22 | 2006-11-21 | The Boeing Company | Parallel configuration composite material fabricator |
US20040222080A1 (en) | 2002-12-17 | 2004-11-11 | William Marsh Rice University | Use of microwaves to crosslink carbon nanotubes to facilitate modification |
US6896841B2 (en) | 2003-03-20 | 2005-05-24 | The Boeing Company | Molding process and apparatus for producing unified composite structures |
TWI221554B (en) | 2003-03-21 | 2004-10-01 | Micro Star Int Co Ltd | Method in BIOS for shadow memory assignment |
US8246882B2 (en) * | 2003-05-02 | 2012-08-21 | The Boeing Company | Methods and preforms for forming composite members with interlayers formed of nonwoven, continuous materials |
US20040219855A1 (en) | 2003-05-02 | 2004-11-04 | Tsotsis Thomas K. | Highly porous interlayers to toughen liquid-molded fabric-based composites |
JP3782072B2 (ja) | 2003-05-30 | 2006-06-07 | 川崎重工業株式会社 | 複合材型材の成形方法及び装置 |
JP3938762B2 (ja) * | 2003-05-30 | 2007-06-27 | 川崎重工業株式会社 | 板状構造体、補強材及び板状構造体の製造方法 |
CA2532190C (en) | 2003-06-16 | 2012-08-21 | William Marsh Rice University | Sidewall functionalization of carbon nanotubes with hydroxyl-terminated moieties |
US7080441B2 (en) * | 2003-07-28 | 2006-07-25 | The Boeing Company | Composite fuselage machine and method of automated composite lay up |
US7236625B2 (en) * | 2003-07-28 | 2007-06-26 | The Boeing Company | Systems and method for identifying foreign objects and debris (FOD) and defects during fabrication of a composite structure |
US7282107B2 (en) * | 2003-08-22 | 2007-10-16 | The Boeing Company | Multiple head automated composite laminating machine for the fabrication of large barrel section components |
US7048024B2 (en) | 2003-08-22 | 2006-05-23 | The Boeing Company | Unidirectional, multi-head fiber placement |
US7083698B2 (en) * | 2003-08-22 | 2006-08-01 | The Boeing Company | Automated composite lay-up to an internal fuselage mandrel |
US7228611B2 (en) * | 2003-11-18 | 2007-06-12 | The Boeing Company | Method of transferring large uncured composite laminates |
US7312274B2 (en) * | 2003-11-24 | 2007-12-25 | General Electric Company | Composition and method for use with ceramic matrix composite T-sections |
US7289656B2 (en) * | 2003-12-02 | 2007-10-30 | The Boeing Company | Systems and methods for determining inconsistency characteristics of a composite structure |
US7039485B2 (en) | 2004-03-12 | 2006-05-02 | The Boeing Company | Systems and methods enabling automated return to and/or repair of defects with a material placement machine |
US7195201B2 (en) * | 2004-03-29 | 2007-03-27 | The Boeing Company | Adaptable payload enabling architecture |
US7093797B2 (en) * | 2004-03-29 | 2006-08-22 | The Boeing Company | Adaptable payload apparatus and methods |
US7134629B2 (en) * | 2004-04-06 | 2006-11-14 | The Boeing Company | Structural panels for use in aircraft fuselages and other structures |
US7159822B2 (en) * | 2004-04-06 | 2007-01-09 | The Boeing Company | Structural panels for use in aircraft fuselages and other structures |
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 |
US7193696B2 (en) | 2004-04-12 | 2007-03-20 | United Technologies Corporation | Systems and methods for using light to indicate defect locations on a composite structure |
WO2005105641A2 (en) * | 2004-04-21 | 2005-11-10 | Ingersoll Machine Tools, Inc. | Automated fiber placement using multiple placement heads, replaceable creels, and replaceable placement heads |
US7080805B2 (en) | 2004-05-05 | 2006-07-25 | The Boeing Company | Stiffened structures and associated methods |
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 |
US20060118244A1 (en) * | 2004-12-02 | 2006-06-08 | The Boeing Company | Device for laying tape materials for aerospace applications |
US7624488B2 (en) * | 2004-12-07 | 2009-12-01 | The Boeing Company | One-piece barrel assembly cart |
US7278198B2 (en) * | 2005-02-01 | 2007-10-09 | The Boeing Company | Mandrel segment loader |
US8148276B2 (en) | 2005-11-28 | 2012-04-03 | University Of Hawaii | Three-dimensionally reinforced multifunctional nanocomposites |
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 |
-
2004
- 2004-05-20 US US10/851,381 patent/US7527222B2/en active Active
-
2005
- 2005-03-28 EP EP11174903.2A patent/EP2394909B1/en active Active
- 2005-03-28 ES ES05788126T patent/ES2392442T3/es active Active
- 2005-03-28 PT PT111955118T patent/PT2436595T/pt unknown
- 2005-03-28 EP EP11195511.8A patent/EP2436595B1/en active Active
- 2005-03-28 ES ES11174903.2T patent/ES2620776T3/es active Active
- 2005-03-28 WO PCT/US2005/010341 patent/WO2006001860A2/en active Application Filing
- 2005-03-28 EP EP12173714.2A patent/EP2561976B1/en active Active
- 2005-03-28 EP EP05788126A patent/EP1748922B1/en active Active
- 2005-03-28 CA CA2562632A patent/CA2562632C/en active Active
- 2005-03-28 JP JP2007507355A patent/JP5087390B2/ja active Active
- 2005-03-28 ES ES11195511.8T patent/ES2608704T3/es active Active
- 2005-03-28 PT PT111749032T patent/PT2394909T/pt unknown
- 2005-03-28 CA CA2857682A patent/CA2857682C/en active Active
-
2008
- 2008-01-28 US US12/020,956 patent/US8182628B2/en active Active
- 2008-03-27 JP JP2008082320A patent/JP5094497B2/ja active Active
- 2008-03-27 JP JP2008082327A patent/JP2008222221A/ja active Pending
- 2008-03-27 JP JP2008082323A patent/JP5255878B2/ja active Active
- 2008-09-23 US US12/236,355 patent/US8157212B2/en active Active
-
2012
- 2012-02-29 JP JP2012043652A patent/JP5497081B2/ja active Active
- 2012-03-02 US US13/411,439 patent/US8382037B2/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11826976B2 (en) | 2019-03-08 | 2023-11-28 | Ihi Aerospace Co., Ltd. | FRP molding system and method |
Also Published As
Similar Documents
Publication | Publication Date | Title |
---|---|---|
PT2394909T (pt) | Secções tubulares de compósito para fuselagens de aeronave e métodos para fabricar essas secções tubulares | |
EP1858368B8 (en) | Airplane trolley and method for manufacturing the trolley | |
EP2024227B8 (en) | Aircraft fuselage structure and method for producing it | |
GB2428417B (en) | Aircraft fuselage structure | |
HK1102073A1 (en) | An aircraft cabin | |
EP1958763A4 (en) | ALUMINUM RESIN-ALLOY COMPOSITE AND PROCESS FOR PRODUCING THE SAME | |
EP1651435B8 (fr) | Structure composite thermostructurale a gradient de composition et son procede de fabrication | |
EP2170698A4 (en) | AIRCRAFT DOOR AND METHOD OF USE | |
IL199092A0 (en) | Composite armor and method for making composite armor | |
EP1904564A4 (en) | SYSTEM AND METHOD FOR IMPROVING THE PERFORMANCE OF AN AIRCRAFT TURNING BOAT WITH INTERNAL / EXTERNAL LOADS | |
EP1845072A4 (en) | MIXED CERAMICS AND MANUFACTURING METHOD THEREFOR | |
GB0517062D0 (en) | Aircraft wing | |
EP2034948A4 (en) | FIBER REINFORCED COMPOSITES AND PROCESS FOR THEIR MANUFACTURE | |
GB2433483B (en) | Aircraft fuselage heating | |
TWI348967B (en) | Metallic laminate and method for preparing the same | |
EP1804562A4 (en) | COMPOUND MULTILAYER SUBSTRATE AND METHOD FOR THE PRODUCTION THEREOF | |
EP2147855A4 (en) | AIRCRAFT ASSEMBLY AND METHOD FOR THE PRODUCTION THEREOF | |
GB2415170B (en) | Pivoting aircraft wing and associated method | |
GB0606282D0 (en) | Aircraft fuselage interior | |
PL1918092T3 (pl) | Wstęga z materiału kompozytowego i sposób wytwarzania wstęgi z materiału kompozytowego | |
EP2088341A4 (en) | MULTILAYER SLIDING ELEMENT AND METHOD FOR MANUFACTURING THE SAME | |
AU2003303291A8 (en) | Composite camouflage construction and method for manufacturing composite camouflage construction | |
ZA200903689B (en) | Polymer-ceramic composite and method | |
GB0610251D0 (en) | Brightened composite shell and method for making the same | |
SG126076A1 (en) | Laminated layer structure and method for forming the same |