SE321561B - - Google Patents
Info
- Publication number
- SE321561B SE321561B SE1342366A SE1342366A SE321561B SE 321561 B SE321561 B SE 321561B SE 1342366 A SE1342366 A SE 1342366A SE 1342366 A SE1342366 A SE 1342366A SE 321561 B SE321561 B SE 321561B
- Authority
- SE
- Sweden
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
- B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
- B29D99/0021—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with plain or filled structures, e.g. cores, placed between two or more plates or sheets, e.g. in a matrix
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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
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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
- B29C70/34—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 and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
- B29C70/342—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 and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic pressure
-
- 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
- B29C70/34—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 and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
- B29C70/347—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 and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation combined with compressing after the winding of lay-ups having a non-circular cross-section, e.g. flat spiral windings
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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
- B29D24/00—Producing articles with hollow walls
- B29D24/002—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled
- B29D24/008—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having hollow ridges, ribs or cores
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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
- B29D99/0025—Producing blades or the like, e.g. blades for turbines, propellers, or wings
- B29D99/0028—Producing blades or the like, e.g. blades for turbines, propellers, or wings hollow blades
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/473—Constructional features
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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
- 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
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- 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
- B29L2031/3085—Wings
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/473—Constructional features
- B64C2027/4733—Rotor blades substantially made from particular materials
- B64C2027/4736—Rotor blades substantially made from particular materials from composite materials
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Aviation & Aerospace Engineering (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Moulding By Coating Moulds (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1965B0084009 DE1275279B (en) | 1965-10-06 | 1965-10-06 | Process for the production of a composite component from glass fiber reinforced plastic |
Publications (1)
Publication Number | Publication Date |
---|---|
SE321561B true SE321561B (en) | 1970-03-09 |
Family
ID=6982235
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE1342366A SE321561B (en) | 1965-10-06 | 1966-10-05 |
Country Status (4)
Country | Link |
---|---|
DE (1) | DE1275279B (en) |
FR (1) | FR1495841A (en) |
GB (1) | GB1166604A (en) |
SE (1) | SE321561B (en) |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2234130B1 (en) * | 1973-05-14 | 1976-04-30 | Kamov Nikolai | |
DE2529185C2 (en) * | 1975-07-01 | 1986-12-11 | Erich Dipl.-Volksw. 5300 Bonn Wintermantel | Component as a substructure element, reinforcement element or the like |
NO790234L (en) * | 1979-01-24 | 1980-07-25 | Torleif Omre | PROCEDURE FOR MANUFACTURING BEETS FOR LIGHTMASTERS AND SIMILAR |
FR2501578B1 (en) * | 1981-03-11 | 1987-09-04 | Desport Lucien | STRUCTURE OF A SANDWICH MATERIAL, METHOD AND MACHINE FOR MANUFACTURING SAID MATERIAL |
GB2119305A (en) * | 1982-04-26 | 1983-11-16 | M & G Trailers Ltd | Moulding hollow articles |
FR2555501A1 (en) * | 1983-11-28 | 1985-05-31 | Septem Sa | METHOD FOR MANUFACTURING HOLLOW RIGID STRUCTURES IN RESIN-IMPREGNATED FIBERS, DEVICE FOR IMPLEMENTING SAME AND STRUCTURE OBTAINED |
FR2565159B1 (en) * | 1984-05-30 | 1986-10-17 | Aerospatiale | METHOD FOR MANUFACTURING A PART OF A COMPLEX STRUCTURE BY FILAMENTARY WINDING AND A PART ARISING FROM THE PROCESS |
FR2748718B1 (en) * | 1985-10-09 | 1998-12-24 | Aerospatiale | REDUCED VULNERABILITY BLADE FOR ROTORS OF GIRAVIONS, AND MANUFACTURING METHOD THEREOF |
GB2190724B (en) * | 1986-04-16 | 1990-08-08 | Courtaulds Plc | Composite element |
GB2225742A (en) * | 1988-12-09 | 1990-06-13 | Westland Helicopters | Moulding a fibre reinforced composite, into a hollow structure comprising outer and inner skins connected by ribs |
DE3923416A1 (en) * | 1989-07-12 | 1991-01-24 | Mecron Med Prod Gmbh | METHOD FOR PRODUCING A BODY HAVING A HOLLOW PROFILE |
ITTO20070507A1 (en) | 2007-07-11 | 2009-01-12 | Alenia Aeronautica Spa | PROCESS OF MANUFACTURING OF A STRUCTURE OF A MONOLITHIC WING WITH AN INTEGRAL PROFILE |
FR2946009B1 (en) * | 2009-05-28 | 2011-07-08 | Lorraine De Construction Aeronautique 7274 Soc | COMPOSITE LANDSCAPE COMPOSITE PANEL FOR AN AIRCRAFT ELEMENT |
US8936216B2 (en) | 2009-05-28 | 2015-01-20 | Societe Lorraine De Construction Aeronautique | Composite structuring panel for the trailing edge of an aircraft element |
FR2954269B1 (en) * | 2009-12-18 | 2012-12-28 | Lorraine Construction Aeronautique | COMPOSITE LEAKING COMPOSITE PANEL FOR AIRCRAFT ELEMENT |
NL2013887B1 (en) | 2014-11-27 | 2016-09-23 | Fibercore Ip Bv | A method for forming a tubular semi-finished product made from fiber-reinforced plastics material. |
US10843416B2 (en) | 2015-05-11 | 2020-11-24 | Gulfstream Aerospace Corporation | Composite reinforcement structures and aircraft assemblies comprising composite reinforcement structures |
US10315366B2 (en) * | 2015-05-11 | 2019-06-11 | Gulfstream Aerospace Corporation | Apparatuses and methods for making reinforcement structures |
EP3219458B1 (en) | 2016-03-14 | 2019-05-08 | Airbus Operations, S.L. | Method and injection moulding tool for manufacturing a leading edge section with hybrid laminar flow control for an aircraft |
CN109016571B (en) * | 2018-07-11 | 2020-09-15 | 江苏新扬新材料股份有限公司 | Preparation method of airfoil |
US11046420B2 (en) * | 2019-10-23 | 2021-06-29 | The Boeing Company | Trailing edge flap having a waffle grid interior structure |
CN113002016B (en) * | 2021-02-27 | 2023-02-28 | 中复连众(哈密)复合材料有限公司 | Suction pouring forming method for web plate of megawatt wind power generation blade |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE483695A (en) * | 1945-09-19 | |||
BE511691A (en) * | 1951-03-20 | |||
AT229014B (en) * | 1957-10-05 | 1963-08-26 | Alfred Kepka | Process for the production of hollow bodies and hollow core for carrying out the process |
FR1216393A (en) * | 1957-11-21 | 1960-04-25 | Bristol Aircraft Ltd | Improvements in the manufacture of fiber-reinforced resin panels |
NL271641A (en) * | 1960-11-25 | |||
FR1354283A (en) * | 1963-01-25 | 1964-03-06 | Method of molding tubular parts, in particular masts and terminals, in synthetic resin |
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1965
- 1965-10-06 DE DE1965B0084009 patent/DE1275279B/en active Pending
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1966
- 1966-10-04 FR FR78718A patent/FR1495841A/en not_active Expired
- 1966-10-05 SE SE1342366A patent/SE321561B/xx unknown
- 1966-10-05 GB GB4446466A patent/GB1166604A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE1275279B (en) | 1968-08-14 |
FR1495841A (en) | 1967-09-22 |
GB1166604A (en) | 1969-10-08 |