GB1364076A - Structural materials - Google Patents
Structural materialsInfo
- Publication number
- GB1364076A GB1364076A GB4133571A GB4133571A GB1364076A GB 1364076 A GB1364076 A GB 1364076A GB 4133571 A GB4133571 A GB 4133571A GB 4133571 A GB4133571 A GB 4133571A GB 1364076 A GB1364076 A GB 1364076A
- Authority
- GB
- United Kingdom
- Prior art keywords
- structural materials
- structural
- materials
- 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
Links
Classifications
-
- 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
- B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
- B29C70/088—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of non-plastics material or non-specified material, e.g. supports
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
-
- 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
- B29C70/20—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres
- B29C70/202—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres arranged in parallel planes or structures of fibres crossing at substantial angles, e.g. cross-moulding compound [XMC]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2705/00—Use of metals, their alloys or their compounds, for preformed parts, e.g. for inserts
- B29K2705/08—Transition metals
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2707/00—Use of elements other than metals for preformed parts, e.g. for inserts
- B29K2707/02—Boron
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2707/00—Use of elements other than metals for preformed parts, e.g. for inserts
- B29K2707/04—Carbon
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2709/00—Use of inorganic materials not provided for in groups B29K2703/00 - B29K2707/00, for preformed parts, e.g. for inserts
- B29K2709/08—Glass
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—Fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/04—Impregnation, embedding, or binder material
- B32B2260/046—Synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/08—Reinforcements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2311/00—Metals, their alloys or their compounds
- B32B2311/18—Titanium
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Textile Engineering (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4133571A GB1364076A (en) | 1972-08-29 | 1972-08-29 | Structural materials |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4133571A GB1364076A (en) | 1972-08-29 | 1972-08-29 | Structural materials |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1364076A true GB1364076A (en) | 1974-08-21 |
Family
ID=10419210
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4133571A Expired GB1364076A (en) | 1972-08-29 | 1972-08-29 | Structural materials |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1364076A (en) |
Cited By (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2309334A1 (en) * | 1975-04-30 | 1976-11-26 | United Technologies Corp | PROCESS FOR THE PREPARATION OF A MULTI-LAYER COMPOSITE ARTICLE |
FR2312369A1 (en) * | 1975-05-26 | 1976-12-24 | Dassault Avions | POROUS STRUCTURE |
FR2374158A1 (en) * | 1976-12-18 | 1978-07-13 | Messerschmitt Boelkow Blohm | CORNERS IN FIBER REINFORCED MATERIALS FOR CONSTRUCTION ELEMENTS |
DE2825191A1 (en) * | 1977-06-10 | 1979-01-04 | Tuguo Kobayashi | METHOD OF MANUFACTURING A COAL FIBER REINFORCED GEAR MATERIAL AND THE MATERIAL OBTAINED THEREOF |
FR2431674A1 (en) * | 1978-07-18 | 1980-02-15 | Fontauto Spa | Bulletproof vests of metallic sheet backed by high tensile fabrics - to restrict deformation and penetration of the fibres |
EP0230682A2 (en) * | 1985-12-30 | 1987-08-05 | The Boeing Company | Aerodynamic structures of composite construction |
EP0326577A1 (en) * | 1986-09-15 | 1989-08-09 | Compositech Ltd | Reinforced plastic laminates for use in the production of printed circuit boards and process for making such laminates and resulting products. |
US4909690A (en) * | 1987-12-16 | 1990-03-20 | Textron Inc. | Composite fastener |
WO1991002906A1 (en) * | 1989-08-23 | 1991-03-07 | Textron Inc. | Improved composite fastener and method and apparatus for making same |
DE3934555A1 (en) * | 1989-10-17 | 1991-04-18 | Audi Ag | Rigid for laminate for coachwork parts - has laminar construction reinforced with core of polymer fibres and multilayer skins of carbon fibre, all impregnated with epoxy] resin |
US5037691A (en) * | 1986-09-15 | 1991-08-06 | Compositech, Ltd. | Reinforced plastic laminates for use in the production of printed circuit boards and process for making such laminates and resulting products |
WO1991011633A1 (en) * | 1990-01-30 | 1991-08-08 | Textron Inc. | Composite threaded collar |
US5098240A (en) * | 1990-05-23 | 1992-03-24 | Textron Inc. | Composite fastener |
EP0478051A2 (en) * | 1990-09-24 | 1992-04-01 | AMP-Akzo LinLam VOF | Method for the manufacture, in a continuous process, of substrates for printed wire boards, and printed wire boards so manufactured |
GB2250470A (en) * | 1990-11-06 | 1992-06-10 | Shrinemark Limited | Protective sheet material |
US5269863A (en) * | 1990-09-24 | 1993-12-14 | Akzo Nv | Continuous process for the manufacture of substrates for printed wire boards |
EP0606830A1 (en) * | 1993-01-15 | 1994-07-20 | GFM Gesellschaft für Fertigungstechnik und Maschinenbau Aktiengesellschaft | Process for the manufacture of a fibre-reinforced resin preimpregnated sheet |
EP0719635A2 (en) * | 1994-12-26 | 1996-07-03 | Honda Giken Kogyo Kabushiki Kaisha | Laminated structure of fiber reinforced plastics and shock-absorbing structure |
WO1997037874A1 (en) * | 1996-04-05 | 1997-10-16 | Minnesota Mining And Manufacturing Company | Air bag fabric |
EP0783960A3 (en) * | 1996-01-11 | 1998-11-18 | The Boeing Company | Titanium-polymer hybrid laminates |
WO2000003869A1 (en) * | 1998-07-17 | 2000-01-27 | Adprotech B.V. | Method for producing a web-like fibrous structure |
WO2004113058A1 (en) * | 2003-06-25 | 2004-12-29 | Joseph Steven Egan | Method of construction of moulded products |
US6861119B2 (en) | 1997-09-18 | 2005-03-01 | Ahlstrom Glassfibre Oy | Pressure-loaded panel and use for boat and container construction |
DE102008042452A1 (en) * | 2008-09-29 | 2010-04-08 | Airbus Deutschland Gmbh | Fiber composite for energy absorption in the event of a crash for an aircraft or spacecraft, fuselage structure section of an aircraft or spacecraft and aircraft or spacecraft |
US10328660B2 (en) * | 2014-03-13 | 2019-06-25 | Aisin Takaoka Co., Ltd. | Composite structure and manufacturing method thereof |
-
1972
- 1972-08-29 GB GB4133571A patent/GB1364076A/en not_active Expired
Cited By (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2309334A1 (en) * | 1975-04-30 | 1976-11-26 | United Technologies Corp | PROCESS FOR THE PREPARATION OF A MULTI-LAYER COMPOSITE ARTICLE |
FR2312369A1 (en) * | 1975-05-26 | 1976-12-24 | Dassault Avions | POROUS STRUCTURE |
FR2374158A1 (en) * | 1976-12-18 | 1978-07-13 | Messerschmitt Boelkow Blohm | CORNERS IN FIBER REINFORCED MATERIALS FOR CONSTRUCTION ELEMENTS |
DE2825191A1 (en) * | 1977-06-10 | 1979-01-04 | Tuguo Kobayashi | METHOD OF MANUFACTURING A COAL FIBER REINFORCED GEAR MATERIAL AND THE MATERIAL OBTAINED THEREOF |
FR2431674A1 (en) * | 1978-07-18 | 1980-02-15 | Fontauto Spa | Bulletproof vests of metallic sheet backed by high tensile fabrics - to restrict deformation and penetration of the fibres |
EP0230682A2 (en) * | 1985-12-30 | 1987-08-05 | The Boeing Company | Aerodynamic structures of composite construction |
EP0230682A3 (en) * | 1985-12-30 | 1989-03-15 | The Boeing Company | Aerodynamic structures of composite construction |
US4943334A (en) * | 1986-09-15 | 1990-07-24 | Compositech Ltd. | Method for making reinforced plastic laminates for use in the production of circuit boards |
EP0326577A1 (en) * | 1986-09-15 | 1989-08-09 | Compositech Ltd | Reinforced plastic laminates for use in the production of printed circuit boards and process for making such laminates and resulting products. |
EP0326577A4 (en) * | 1986-09-15 | 1990-07-04 | Compositech Ltd | Reinforced plastic laminates for use in the production of printed circuit boards and process for making such laminates and resulting products. |
US5478421A (en) * | 1986-09-15 | 1995-12-26 | Compositech Ltd. | Method for making composite structures by filament winding |
US5037691A (en) * | 1986-09-15 | 1991-08-06 | Compositech, Ltd. | Reinforced plastic laminates for use in the production of printed circuit boards and process for making such laminates and resulting products |
US5376326A (en) | 1986-09-15 | 1994-12-27 | Compositech Ltd. | Methods for making multilayer printed circuit boards |
US5512224A (en) * | 1986-09-15 | 1996-04-30 | Compositech Ltd. | Methods for making circuit boards by vacuum impregnation |
US4909690A (en) * | 1987-12-16 | 1990-03-20 | Textron Inc. | Composite fastener |
WO1991002906A1 (en) * | 1989-08-23 | 1991-03-07 | Textron Inc. | Improved composite fastener and method and apparatus for making same |
DE3934555A1 (en) * | 1989-10-17 | 1991-04-18 | Audi Ag | Rigid for laminate for coachwork parts - has laminar construction reinforced with core of polymer fibres and multilayer skins of carbon fibre, all impregnated with epoxy] resin |
WO1991011633A1 (en) * | 1990-01-30 | 1991-08-08 | Textron Inc. | Composite threaded collar |
US5083888A (en) * | 1990-01-30 | 1992-01-28 | Textron Inc. | Composite threaded collar |
US5098240A (en) * | 1990-05-23 | 1992-03-24 | Textron Inc. | Composite fastener |
EP0478051A2 (en) * | 1990-09-24 | 1992-04-01 | AMP-Akzo LinLam VOF | Method for the manufacture, in a continuous process, of substrates for printed wire boards, and printed wire boards so manufactured |
EP0478051A3 (en) * | 1990-09-24 | 1992-06-10 | Akzo N.V. | Method for the manufacture, in a continuous process, of substrates for printed wire boards, and printed wire boards so manufactured |
US5269863A (en) * | 1990-09-24 | 1993-12-14 | Akzo Nv | Continuous process for the manufacture of substrates for printed wire boards |
GB2250470A (en) * | 1990-11-06 | 1992-06-10 | Shrinemark Limited | Protective sheet material |
EP0606830A1 (en) * | 1993-01-15 | 1994-07-20 | GFM Gesellschaft für Fertigungstechnik und Maschinenbau Aktiengesellschaft | Process for the manufacture of a fibre-reinforced resin preimpregnated sheet |
EP0719635A2 (en) * | 1994-12-26 | 1996-07-03 | Honda Giken Kogyo Kabushiki Kaisha | Laminated structure of fiber reinforced plastics and shock-absorbing structure |
EP0719635A3 (en) * | 1994-12-26 | 1998-04-08 | Honda Giken Kogyo Kabushiki Kaisha | Laminated structure of fiber reinforced plastics and shock-absorbing structure |
EP0783960A3 (en) * | 1996-01-11 | 1998-11-18 | The Boeing Company | Titanium-polymer hybrid laminates |
EP1614531A3 (en) * | 1996-01-11 | 2013-07-24 | The Boeing Company | Titanium-polymer hybrid laminates |
WO1997037874A1 (en) * | 1996-04-05 | 1997-10-16 | Minnesota Mining And Manufacturing Company | Air bag fabric |
US6861119B2 (en) | 1997-09-18 | 2005-03-01 | Ahlstrom Glassfibre Oy | Pressure-loaded panel and use for boat and container construction |
WO2000003869A1 (en) * | 1998-07-17 | 2000-01-27 | Adprotech B.V. | Method for producing a web-like fibrous structure |
WO2004113058A1 (en) * | 2003-06-25 | 2004-12-29 | Joseph Steven Egan | Method of construction of moulded products |
DE102008042452A1 (en) * | 2008-09-29 | 2010-04-08 | Airbus Deutschland Gmbh | Fiber composite for energy absorption in the event of a crash for an aircraft or spacecraft, fuselage structure section of an aircraft or spacecraft and aircraft or spacecraft |
US9079653B2 (en) | 2008-09-29 | 2015-07-14 | Airbus Operations Gmbh | Fiber composite component for absorbing energy |
US10328660B2 (en) * | 2014-03-13 | 2019-06-25 | Aisin Takaoka Co., Ltd. | Composite structure and manufacturing method thereof |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
732 | Registration of transactions, instruments or events in the register (sect. 32/1977) | ||
PCNP | Patent ceased through non-payment of renewal fee |