FR2396645A1 - Poutres profilees en un materiau renforce par des fibres - Google Patents
Poutres profilees en un materiau renforce par des fibresInfo
- Publication number
- FR2396645A1 FR2396645A1 FR7715147A FR7715147A FR2396645A1 FR 2396645 A1 FR2396645 A1 FR 2396645A1 FR 7715147 A FR7715147 A FR 7715147A FR 7715147 A FR7715147 A FR 7715147A FR 2396645 A1 FR2396645 A1 FR 2396645A1
- Authority
- FR
- France
- Prior art keywords
- layers
- reinforced material
- layer
- fiber reinforced
- profiled beams
- 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.)
- Granted
Links
Classifications
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- 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
- B29D99/0003—Producing profiled members, e.g. beams
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- 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
- B29C70/083—Combinations of continuous fibres or fibrous profiled structures oriented in one direction and reinforcements forming a two dimensional structure, e.g. mats
- B29C70/085—Combinations of continuous fibres or fibrous profiled structures oriented in one direction and reinforcements forming a two dimensional structure, e.g. mats the structure being deformed in a three dimensional configuration
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- 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
- B29C70/304—In-plane lamination by juxtaposing or interleaving of plies, e.g. scarf joining
-
- 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
- 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
- B29C70/446—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/29—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces built-up from parts of different material, i.e. composite structures
-
- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
- B29C43/10—Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies
- B29C43/12—Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies using bags surrounding the moulding material or using membranes contacting the moulding material
-
- 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.]
- Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
- Y10T428/24074—Strand or strand-portions
-
- 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.]
- Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
- Y10T428/24074—Strand or strand-portions
- Y10T428/24116—Oblique to direction of web
-
- 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.]
- Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
- Y10T428/24124—Fibers
-
- 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.]
- Y10T428/24132—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in different layers or components parallel
-
- 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.]
- Y10T428/24174—Structurally defined web or sheet [e.g., overall dimension, etc.] including sheet or component perpendicular to plane of web or sheet
-
- 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.]
- Y10T428/24174—Structurally defined web or sheet [e.g., overall dimension, etc.] including sheet or component perpendicular to plane of web or sheet
- Y10T428/24182—Inward from edge of web or sheet
-
- 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
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Rod-Shaped Construction Members (AREA)
- Laminated Bodies (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
Poutres profilées en un matériau renforcé par des fibres, comportant des âmes et des ailes qui sont composées d'au moins deux couches chacune, et dont au moins une couche sert en même temps de couche d'âme et de couche d'aile (couche de liaison). Pour permettre à de telles poutres de transmettre aussi de grandes forces de poussée, les couches de liaison 5 sont constituées par des profilés préfabriqués entre lesquels ou à l'extérieur desquels sont disposées des couches supplémentaires 4, 6, 7. Les couches de liaison 5 et des couches supplémentaires, situées dans la zone des ailes 3 sont de préférence réalisées avec des strates de fibres imprégnées de résine synthétique
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2622163A DE2622163C3 (de) | 1976-05-19 | 1976-05-19 | Profilträger aus faserverstärktem Werkstoff |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2396645A1 true FR2396645A1 (fr) | 1979-02-02 |
FR2396645B1 FR2396645B1 (fr) | 1982-07-30 |
Family
ID=5978315
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7715147A Granted FR2396645A1 (fr) | 1976-05-19 | 1977-05-17 | Poutres profilees en un materiau renforce par des fibres |
Country Status (7)
Country | Link |
---|---|
US (1) | US4177306A (fr) |
JP (2) | JPS52140587A (fr) |
DE (1) | DE2622163C3 (fr) |
ES (1) | ES458963A1 (fr) |
FR (1) | FR2396645A1 (fr) |
GB (1) | GB1586184A (fr) |
IT (1) | IT1076056B (fr) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2463055A1 (fr) * | 1979-08-09 | 1981-02-20 | Alkan R & Cie | Structure de mats d'accrochage de charges sous avion |
FR2514695A1 (fr) * | 1981-10-20 | 1983-04-22 | Aerospatiale | Demi-produit a base de fibres preimpregnees de resine polymerisable |
EP0325221A1 (fr) * | 1988-01-19 | 1989-07-26 | Tene Yair | Structure en treillis |
Families Citing this family (94)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4291081A (en) * | 1979-07-26 | 1981-09-22 | Northrop Corporation | Laced composite structure |
US4312162A (en) * | 1979-08-15 | 1982-01-26 | Jonas Medney | Reinforced pole |
US4305903A (en) * | 1980-02-25 | 1981-12-15 | Norris Industries, Inc. | Composite fiber reinforced member and method |
US4350728A (en) * | 1980-10-02 | 1982-09-21 | The United States Of America As Represented By The Secretary Of The Navy | Cross reinforcement in a graphite-epoxy laminate |
EP0051246A1 (fr) * | 1980-10-31 | 1982-05-12 | A. Rudolf | Procédé pour fabriquer des produits moulés en matière plastique renforcée par une nappe non-tissée de fibres |
DE3041021A1 (de) * | 1980-10-31 | 1982-06-09 | Artur 5221 Hermesdorf Rudolf | Faser-verstaerktes kunststoff-formteil |
NL8201677A (nl) * | 1981-05-01 | 1982-12-01 | Bpb Industries Plc | Bouwcomponent. |
US4384802A (en) * | 1981-06-11 | 1983-05-24 | Shell Oil Company | Double I-beam structural joint for connecting fiber-reinforced plastic beams or girders |
JPS5887042A (ja) * | 1981-11-19 | 1983-05-24 | 東レ株式会社 | 繊維強化樹脂用補強材 |
JPS58117160A (ja) * | 1981-12-28 | 1983-07-12 | 東レ株式会社 | 桁材 |
US4532097A (en) * | 1981-12-28 | 1985-07-30 | Ford Motor Company | Method of forming fiber reinforced synthetic material wheel |
JPS58118402A (ja) * | 1982-01-07 | 1983-07-14 | Honda Motor Co Ltd | 炭素繊維強化プラスチツク製スポ−クプレ−ト |
US4452657A (en) * | 1982-09-15 | 1984-06-05 | The Boeing Company | Composite integral web stiffening method |
DE3238587A1 (de) * | 1982-10-19 | 1984-05-03 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Traeger, insbesondere zur motor- oder getriebeaufhaengung eines kraftfahrzeuges |
US4576849A (en) * | 1983-06-06 | 1986-03-18 | Hercules Incorporated | Curved composite beam |
US4512835A (en) * | 1983-06-06 | 1985-04-23 | Hercules Incorporated | Method of making a curved composite beam |
US4966802A (en) * | 1985-05-10 | 1990-10-30 | The Boeing Company | Composites made of fiber reinforced resin elements joined by adhesive |
US4734146A (en) * | 1986-03-31 | 1988-03-29 | Rockwell International Corporation | Method of producing a composite sine wave beam |
DE3612176A1 (de) * | 1986-04-11 | 1987-10-15 | Messerschmitt Boelkow Blohm | Biegetraeger |
US4789594A (en) * | 1987-04-15 | 1988-12-06 | The Boeing Company | Method of forming composite radius fillers |
US4808461A (en) * | 1987-12-14 | 1989-02-28 | Foster-Miller, Inc. | Composite structure reinforcement |
FR2632604B1 (fr) * | 1988-06-08 | 1991-07-12 | Aerospatiale | Cadre en materiau composite notamment pour fuselage d'aeronef, et son procede de fabrication |
US5076873A (en) * | 1988-11-04 | 1991-12-31 | The Boeing Company | Method for forming and curing an I-section workpiece |
US5342465A (en) * | 1988-12-09 | 1994-08-30 | Trw Inc. | Viscoelastic damping structures and related manufacturing method |
US5030490A (en) * | 1988-12-09 | 1991-07-09 | Tew Inc. | Viscoelastic damping structures and related manufacturing method |
DE3910529A1 (de) * | 1989-04-01 | 1990-04-05 | Daimler Benz Ag | Gehaeuseartiges bauteil aus faserverstaerktem kunststoff |
JPH0823095B2 (ja) * | 1989-06-06 | 1996-03-06 | 東レ株式会社 | 補強繊維織物 |
US5061542A (en) * | 1989-08-28 | 1991-10-29 | United Technologies Corporation | Stabilizing foam inserts for resin transfer molding |
US5064705A (en) * | 1989-08-28 | 1991-11-12 | United Technologies Corporation | Stabilizing laminate inserts for resin transfer molding |
US5225020A (en) * | 1991-08-20 | 1993-07-06 | W. R. Grace & Co.-Conn. | Pultrusion mandrel with integral, intercooled resin injector and method of using the same |
FR2687174B1 (fr) * | 1992-02-11 | 1995-09-22 | Aerospatiale | Procede pour la realisation d'une armature de fibres pour piece de matiere composite a parois non coplanaires, et piece composite comportant une telle armature. |
US6017048A (en) * | 1992-06-05 | 2000-01-25 | Fritschen; Thomas M. | Aero bicycle frame |
AT398064B (de) * | 1992-07-01 | 1994-09-26 | Hoac Austria Flugzeugwerk Wr N | Kunststoff-verbundprofil, insbesondere flügelholm für den flugzeugbau |
JPH0663378U (ja) * | 1993-02-12 | 1994-09-06 | セーラー万年筆株式会社 | 弁付筆記具 |
US5974760A (en) * | 1993-03-24 | 1999-11-02 | Tingley; Daniel A. | Wood I-beam with synthetic fiber reinforcement |
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US5639535A (en) * | 1996-06-06 | 1997-06-17 | The Boeing Company | Composite interleaving for composite interfaces |
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US6007894A (en) * | 1997-07-10 | 1999-12-28 | Mcdonnell Dougal Corporation | Quasi-isotropic composite isogrid structure and method of making same |
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US6272796B1 (en) | 1999-12-30 | 2001-08-14 | Harold E. Metzler | Mortise and tenon joint for post and beam I-beams composed of fiber reinforced pultruded polymer composite |
US6374570B1 (en) * | 2000-08-25 | 2002-04-23 | Lockheed Martin Corporation | Apparatus and method for joining dissimilar materials to form a structural support member |
ITPD20010064A1 (it) * | 2001-03-16 | 2002-09-16 | Vittorio Pareti | Struttura portante per la realizzazione di opere edili |
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US2410609A (en) * | 1943-07-17 | 1946-11-05 | Joseph S Pecker | Aircraft rotor wing construction |
US2572924A (en) * | 1948-07-07 | 1951-10-30 | Holoplast Ltd | Hollow plastic product and method of making the same |
GB1018289A (en) * | 1963-03-08 | 1966-01-26 | Gustav Krone | Elongated plastics sections |
FR2088413A1 (fr) * | 1970-05-08 | 1972-01-07 | Ibm | |
DE2334645A1 (de) * | 1973-07-07 | 1975-01-16 | Maschf Augsburg Nuernberg Ag | Stuetz- und biegetraeger |
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US2528049A (en) * | 1948-06-11 | 1950-10-31 | Holoplast Ltd | Acoustic panel |
US3673058A (en) * | 1969-04-07 | 1972-06-27 | Hexcel Corp | Honeycomb having laminates of unidirectional strands |
US3966013A (en) * | 1972-09-20 | 1976-06-29 | Hitco | Multi-ply woven article having acoustical elements between double plies |
JPS5117983A (en) * | 1974-08-05 | 1976-02-13 | Daicel Ltd | Furanjitsugiteno seizohohoto sonosochi |
JPS5125584A (en) * | 1974-08-28 | 1976-03-02 | Satsuki Kitani | Bojokyodobuzaito sonoseizohoho |
US3995081A (en) * | 1974-10-07 | 1976-11-30 | General Dynamics Corporation | Composite structural beams and method |
US4051289A (en) * | 1976-04-12 | 1977-09-27 | General Electric Company | Composite airfoil construction |
-
1976
- 1976-05-19 DE DE2622163A patent/DE2622163C3/de not_active Expired
-
1977
- 1977-05-12 US US05/796,414 patent/US4177306A/en not_active Expired - Lifetime
- 1977-05-12 GB GB20017/77A patent/GB1586184A/en not_active Expired
- 1977-05-17 IT IT2363077A patent/IT1076056B/it active
- 1977-05-17 FR FR7715147A patent/FR2396645A1/fr active Granted
- 1977-05-19 ES ES458963A patent/ES458963A1/es not_active Expired
- 1977-05-19 JP JP5714777A patent/JPS52140587A/ja active Granted
-
1983
- 1983-12-26 JP JP58244349A patent/JPS59176021A/ja active Pending
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US2410609A (en) * | 1943-07-17 | 1946-11-05 | Joseph S Pecker | Aircraft rotor wing construction |
US2572924A (en) * | 1948-07-07 | 1951-10-30 | Holoplast Ltd | Hollow plastic product and method of making the same |
GB1018289A (en) * | 1963-03-08 | 1966-01-26 | Gustav Krone | Elongated plastics sections |
FR2088413A1 (fr) * | 1970-05-08 | 1972-01-07 | Ibm | |
DE2334645A1 (de) * | 1973-07-07 | 1975-01-16 | Maschf Augsburg Nuernberg Ag | Stuetz- und biegetraeger |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2463055A1 (fr) * | 1979-08-09 | 1981-02-20 | Alkan R & Cie | Structure de mats d'accrochage de charges sous avion |
FR2514695A1 (fr) * | 1981-10-20 | 1983-04-22 | Aerospatiale | Demi-produit a base de fibres preimpregnees de resine polymerisable |
EP0077727A1 (fr) * | 1981-10-20 | 1983-04-27 | AEROSPATIALE Société Nationale Industrielle | Demi-produit à base de fibres préimprégnées de résine polymérisable |
EP0325221A1 (fr) * | 1988-01-19 | 1989-07-26 | Tene Yair | Structure en treillis |
Also Published As
Publication number | Publication date |
---|---|
FR2396645B1 (fr) | 1982-07-30 |
IT1076056B (it) | 1985-04-22 |
JPS6112781B2 (fr) | 1986-04-10 |
DE2622163B2 (de) | 1980-05-29 |
DE2622163A1 (de) | 1977-11-24 |
JPS59176021A (ja) | 1984-10-05 |
JPS52140587A (en) | 1977-11-24 |
GB1586184A (en) | 1981-03-18 |
ES458963A1 (es) | 1978-02-16 |
US4177306A (en) | 1979-12-04 |
DE2622163C3 (de) | 1983-05-26 |
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