DK200700628A - Fremgangsmåde og apparatur til fremstilling af blade - Google Patents
Fremgangsmåde og apparatur til fremstilling af blade Download PDFInfo
- Publication number
- DK200700628A DK200700628A DK200700628A DKPA200700628A DK200700628A DK 200700628 A DK200700628 A DK 200700628A DK 200700628 A DK200700628 A DK 200700628A DK PA200700628 A DKPA200700628 A DK PA200700628A DK 200700628 A DK200700628 A DK 200700628A
- Authority
- DK
- Denmark
- Prior art keywords
- component
- stacking
- layers
- stack
- fiber
- Prior art date
Links
Classifications
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- 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
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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
-
- 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
- B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
- B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
- B29C70/865—Incorporated in coherent impregnated reinforcing layers, e.g. by winding completely encapsulated
-
- 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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/04—Layered products comprising a layer of synthetic resin as impregnant, bonding, or embedding substance
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/06—Rotors
- F03D1/065—Rotors characterised by their construction elements
- F03D1/0675—Rotors characterised by their construction elements of the blades
-
- 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
- B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
-
- 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
- B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
- B29L2031/082—Blades, e.g. for helicopters
- B29L2031/085—Wind turbine blades
-
- 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
- B32B2603/00—Vanes, blades, propellers, rotors with blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2280/00—Materials; Properties thereof
- F05B2280/60—Properties or characteristics given to material by treatment or manufacturing
- F05B2280/6003—Composites; e.g. fibre-reinforced
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2253/00—Other material characteristics; Treatment of material
- F05C2253/04—Composite, e.g. fibre-reinforced
-
- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
-
- 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
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Composite Materials (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Wind Motors (AREA)
- Moulding By Coating Moulds (AREA)
Claims (10)
1. Fremgangsmåde (100) til fremstilling af et blad (24) ved at bruge en form med en facon svarende til en forudbestemt færdig facon af mindst en del af bladet, hvilken fremgangsmåde indbefatter stakning (102) af flere lag (32) af et materiale i formen, stakning (104) af mindst én komponent med stakken af de flere lag, hvor komponenten er et kompositmateriaie indbefattende en hærdet resin og mindst ét lag af fiber, og laminering (110) af stakken af de flere lag og komponenten.
2. Fremgangsmåde (100) ifølge krav 1, yderligere indbefattende fremstilling af komponenten ved indfletning af resinen med laget af fiber og hærdning af resinen før stakning (104) af komponenten.
3. Fremgangsmåde (100) ifølge krav 1, hvor laget af fiber er et første lag af fiber, og stakning af flere lag (32) af et materiale i formen indbefatter mindst én af: stakning af mindst ét andet lag af fiber i formen, og stakning af mindst ét lag af træ i formen.
4. Fremgangsmåde (100) ifølge krav 1, hvor stakning af mindst én komponent med stakken af de flere lag (32) indbefatter stakning (104) af komponenten mindst delvist mellem to tilgrænsende lag af de flere lag.
5. Fremgangsmåde (100) ifølge krav 1, hvor stakning af mindst én komponent med stakken af de flere lag (32) indbefatter stakning (106, 108) af mindst én af en bjælkebeklaedning (38, 40) og en støttekomponent til en rodsektion (26) med stakken af de flere lag.
6. Fremgangsmåde (100) ifølge krav 1, yderligere indbefattende forimprægnering af mindst ét lag af de flere lag (32) med resin før stakning af de flere lag i formen.
7. Fremgangsmåde (100) ifølge krav 1, hvor laminering indbefatter mindst én af indføring af resin ind i mindst ét lag af de flere lag (32), opvarmning af stakken af de flere lag og komponenten, og påføring af tryk på stakken af de flere lag og komponenten.
8. Fremgangsmåde (100) ifølge krav 1, hvor laminering (110) indbefatter laminering af stakken af de flere lag og komponenten ved at bruge en resinoverføringsstøbningsproces (resin transfer molding process) (RTM-proces).
9. Fremgangsmåde (100) til fremstilling af et blad (24) ved at bruge en form med en facon svarende til en forudbestemt færdig facon af mindst en del af bladet, hvilken fremgangsmåde indbefatter stakning (102) af flere lag (32) af et materiale i formen, stakning (104) af mindst én komponent med stakken af de flere lag, hvor komponenten indbefatter en facon, som svarer tii den forudbestemte færdige facon af mindst en del af bladet, og laminering (110) af stakken af de flere lag og komponenten.
10. Fremgangsmåde (200) til fremstilling af et blad (24) ved at bruge en filamentviklingsproces, hvilken fremgangsmåde indbefatter tilvejebringelse af en dorn med en facon svarende til en forudbestemt færdig facon af mindst en del af bladet, vikling (202) af fiber omkring dornen for at forme flere lag (32) af fiberen, positionering (204) af mindst én komponent tilgrænsende mindst ét lag af de flere lag af fiber, hvor komponenten indbefatter mindst ét af en facon, som svarer til den forudbestemte færdige facon af mindst en del af bladet og mindst ét lag af fiber, i hvilket en hærdet resin er indført, og laminering af de flere fiberlag og komponenten.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US41339106 | 2006-04-28 | ||
| US11/413,391 US20070251090A1 (en) | 2006-04-28 | 2006-04-28 | Methods and apparatus for fabricating blades |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| DK200700628A true DK200700628A (da) | 2007-10-29 |
| DK178536B1 DK178536B1 (da) | 2016-06-06 |
Family
ID=38542578
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DKPA200700628A DK178536B1 (da) | 2006-04-28 | 2007-04-27 | Fremgangsmåde til fremstilling af blade |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US20070251090A1 (da) |
| CN (1) | CN101062594B (da) |
| DE (1) | DE102007020338B4 (da) |
| DK (1) | DK178536B1 (da) |
Families Citing this family (57)
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| US7976282B2 (en) * | 2007-01-26 | 2011-07-12 | General Electric Company | Preform spar cap for a wind turbine rotor blade |
| DE602007007905D1 (de) * | 2007-05-07 | 2010-09-02 | Siemens Ag | Verfahren zur Herstellung eine Windturbinenschaufel |
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| GB0806666D0 (en) * | 2008-04-11 | 2008-05-14 | Bond Philip C | Windfarm radar clutter mitigation |
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| US5248242A (en) * | 1990-09-28 | 1993-09-28 | The Boeing Company | Aerodynamic rotor blade of composite material fabricated in one cure cycle |
| US5375324A (en) * | 1993-07-12 | 1994-12-27 | Flowind Corporation | Vertical axis wind turbine with pultruded blades |
| DE4335221C1 (de) * | 1993-10-15 | 1995-03-16 | Deutsche Forsch Luft Raumfahrt | Rotorblatt für Windkraftanlagen |
| US6183101B1 (en) * | 1995-02-03 | 2001-02-06 | Tseng-Lu Chien | Cover arrangement including an electro-luminescent element |
| FR2760681B1 (fr) * | 1997-03-12 | 1999-05-14 | Alternatives En | Procede de fabrication d'une piece de grandes dimensions en materiau composite et pale d'helice, en particulier d'eolienne, fabriquee selon ce procede |
| WO2003008800A1 (en) * | 2001-07-19 | 2003-01-30 | Neg Micon A/S | Wind turbine blade |
| US7048985B2 (en) | 2001-07-23 | 2006-05-23 | Vrac, Llc | Three-dimensional spacer fabric resin infusion media and reinforcing composite lamina |
| DK175718B1 (da) * | 2002-04-15 | 2005-02-07 | Ssp Technology As | Möllevinge |
| US7220930B2 (en) * | 2003-01-28 | 2007-05-22 | The Hoover Company | Floor care appliance with an electro luminescent switch panel |
| DE10336461A1 (de) | 2003-08-05 | 2005-03-03 | Aloys Wobben | Verfahren zur Herstellung eines Rotorblattes einer Windenergieanlage |
| DE10354106B4 (de) | 2003-11-19 | 2013-09-26 | Bayerische Motoren Werke Aktiengesellschaft | Verfahren zum Herstellen einer Faserverbundstruktur |
| US8047798B2 (en) * | 2005-02-03 | 2011-11-01 | Vestas Wind Systems A/S | Method of manufacturing a wind turbine blade shell member |
| AT510083A3 (de) | 2010-07-02 | 2012-03-15 | Hexcel Holding Gmbh | Faserverstärktes verbundformteil |
-
2006
- 2006-04-28 US US11/413,391 patent/US20070251090A1/en not_active Abandoned
-
2007
- 2007-04-27 DK DKPA200700628A patent/DK178536B1/da active
- 2007-04-28 CN CN2007101009499A patent/CN101062594B/zh active Active
- 2007-04-30 DE DE102007020338.3A patent/DE102007020338B4/de active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN101062594A (zh) | 2007-10-31 |
| DK178536B1 (da) | 2016-06-06 |
| DE102007020338B4 (de) | 2021-07-29 |
| CN101062594B (zh) | 2011-07-06 |
| US20070251090A1 (en) | 2007-11-01 |
| DE102007020338A1 (de) | 2007-10-31 |
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