WO2003024700A3 - Composite structure and method for constructing same - Google Patents
Composite structure and method for constructing same Download PDFInfo
- Publication number
- WO2003024700A3 WO2003024700A3 PCT/US2002/029912 US0229912W WO03024700A3 WO 2003024700 A3 WO2003024700 A3 WO 2003024700A3 US 0229912 W US0229912 W US 0229912W WO 03024700 A3 WO03024700 A3 WO 03024700A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- panel
- composite structure
- stiffening
- constructing same
- skin
- Prior art date
Links
Classifications
-
- 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
- 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
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
- B29C70/222—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure the structure being shaped to form a three dimensional configuration
-
- 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
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Textile Engineering (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Laminated Bodies (AREA)
Abstract
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP02763675A EP1427581A2 (en) | 2001-09-20 | 2002-09-19 | Composite structure and method for constructing same |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/961,084 US20030051434A1 (en) | 2001-09-20 | 2001-09-20 | Composite structure and method for constructing same |
US09/961,084 | 2001-09-20 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2003024700A2 WO2003024700A2 (en) | 2003-03-27 |
WO2003024700A3 true WO2003024700A3 (en) | 2003-07-10 |
Family
ID=25504033
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2002/029912 WO2003024700A2 (en) | 2001-09-20 | 2002-09-19 | Composite structure and method for constructing same |
Country Status (3)
Country | Link |
---|---|
US (1) | US20030051434A1 (en) |
EP (1) | EP1427581A2 (en) |
WO (1) | WO2003024700A2 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7374715B2 (en) * | 2002-05-22 | 2008-05-20 | Northrop Grumman Corporation | Co-cured resin transfer molding manufacturing method |
US7419627B2 (en) * | 2002-09-13 | 2008-09-02 | Northrop Grumman Corporation | Co-cured vacuum-assisted resin transfer molding manufacturing method |
DE102011120636A1 (en) * | 2011-12-09 | 2013-06-13 | Airbus Operations Gmbh | Fiber composite component assembly having at least two plate-shaped fiber composite components and method for producing the same |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3700512A (en) * | 1969-09-05 | 1972-10-24 | Owens Corning Fiberglass Corp | Method of forming a fluid retaining wall |
US4009067A (en) * | 1975-07-07 | 1977-02-22 | Rogers Charles W | Process of fabricating composite structural members |
GB2110736A (en) * | 1981-11-07 | 1983-06-22 | British Aerospace | Stiffened panel of fibre reinforced plastics material |
GB2224969A (en) * | 1988-09-12 | 1990-05-23 | Tetronel Limited | Improvements in and relating to the manufacture of laminates |
US4966802A (en) * | 1985-05-10 | 1990-10-30 | The Boeing Company | Composites made of fiber reinforced resin elements joined by adhesive |
US5242523A (en) * | 1992-05-14 | 1993-09-07 | The Boeing Company | Caul and method for bonding and curing intricate composite structures |
US5589015A (en) * | 1994-06-07 | 1996-12-31 | Foster-Miller, Inc. | Method and system for inserting reinforcing elements in a composite structure |
US5622733A (en) * | 1994-10-04 | 1997-04-22 | Rockwell International Corporation | Tooling for the fabrication of composite hollow crown-stiffened skins and panels |
US5827383A (en) * | 1996-02-13 | 1998-10-27 | Foster-Miller, Inc. | Stiffener reinforced assembly and method of manufacturing same |
US5980665A (en) * | 1996-05-31 | 1999-11-09 | The Boeing Company | Z-pin reinforced bonds for connecting composite structures |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1398077A (en) * | 1964-03-25 | 1965-05-07 | Nord Aviation | Process for joining corrugated core panels together |
GB1104490A (en) * | 1964-08-10 | 1968-02-28 | Desmond Harold Bleasdale | Former for use in the manufacture of fibreglass articles |
US3669821A (en) * | 1968-08-02 | 1972-06-13 | Robertson Co H H | Fiber-reinforced plastic structural member |
US3837985A (en) * | 1972-02-24 | 1974-09-24 | Whittaker Corp | Multi-directional reinforced composite and method of making the same |
US4368674A (en) * | 1981-01-28 | 1983-01-18 | Aero Plastics Of K.C., Inc. | Hatch cover for railroad hopper cars |
US4675061A (en) * | 1985-09-24 | 1987-06-23 | Grumman Aerospace Corporation | Method for forming corrugated materials using memory metal cores |
US4865788A (en) * | 1985-12-02 | 1989-09-12 | Sheller-Globe Corporation | Method for forming fiber web for compression molding structural substrates for panels and fiber web |
US5238725A (en) * | 1990-12-21 | 1993-08-24 | E. I. Du Pont De Nemours And Company | Method for forming a structural panel with decorative facing and product thereof |
US6106646A (en) * | 1992-09-14 | 2000-08-22 | General Electric Company | Method for joining composite materials |
US5904992A (en) * | 1996-09-26 | 1999-05-18 | Mcdonnell Douglas Corporation | Floating superplastic forming/diffusion bonding die, product and process |
US6110567A (en) * | 1999-01-27 | 2000-08-29 | Scaled Composites, Inc. | Composite structural panel having a face sheet reinforced with a channel stiffener grid |
-
2001
- 2001-09-20 US US09/961,084 patent/US20030051434A1/en not_active Abandoned
-
2002
- 2002-09-19 EP EP02763675A patent/EP1427581A2/en not_active Withdrawn
- 2002-09-19 WO PCT/US2002/029912 patent/WO2003024700A2/en not_active Application Discontinuation
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3700512A (en) * | 1969-09-05 | 1972-10-24 | Owens Corning Fiberglass Corp | Method of forming a fluid retaining wall |
US4009067A (en) * | 1975-07-07 | 1977-02-22 | Rogers Charles W | Process of fabricating composite structural members |
GB2110736A (en) * | 1981-11-07 | 1983-06-22 | British Aerospace | Stiffened panel of fibre reinforced plastics material |
US4966802A (en) * | 1985-05-10 | 1990-10-30 | The Boeing Company | Composites made of fiber reinforced resin elements joined by adhesive |
GB2224969A (en) * | 1988-09-12 | 1990-05-23 | Tetronel Limited | Improvements in and relating to the manufacture of laminates |
US5242523A (en) * | 1992-05-14 | 1993-09-07 | The Boeing Company | Caul and method for bonding and curing intricate composite structures |
US5589015A (en) * | 1994-06-07 | 1996-12-31 | Foster-Miller, Inc. | Method and system for inserting reinforcing elements in a composite structure |
US5622733A (en) * | 1994-10-04 | 1997-04-22 | Rockwell International Corporation | Tooling for the fabrication of composite hollow crown-stiffened skins and panels |
US5827383A (en) * | 1996-02-13 | 1998-10-27 | Foster-Miller, Inc. | Stiffener reinforced assembly and method of manufacturing same |
US5980665A (en) * | 1996-05-31 | 1999-11-09 | The Boeing Company | Z-pin reinforced bonds for connecting composite structures |
Also Published As
Publication number | Publication date |
---|---|
EP1427581A2 (en) | 2004-06-16 |
US20030051434A1 (en) | 2003-03-20 |
WO2003024700A2 (en) | 2003-03-27 |
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