DK3027893T3 - En vindmøllevinge med fæstningslinje ved siden af en sandwichpanel i vingen - Google Patents

En vindmøllevinge med fæstningslinje ved siden af en sandwichpanel i vingen Download PDF

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Publication number
DK3027893T3
DK3027893T3 DK14750703.2T DK14750703T DK3027893T3 DK 3027893 T3 DK3027893 T3 DK 3027893T3 DK 14750703 T DK14750703 T DK 14750703T DK 3027893 T3 DK3027893 T3 DK 3027893T3
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Denmark
Prior art keywords
blade
wind turbine
structural
sandwich panel
trailing edge
Prior art date
Application number
DK14750703.2T
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English (en)
Inventor
Jesper Hasselbalch Garm
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Lm Wp Patent Holding As
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Publication of DK3027893T3 publication Critical patent/DK3027893T3/da

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Classifications

    • 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
    • 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
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
    • B29C66/128—Stepped joint cross-sections
    • B29C66/1282—Stepped joint cross-sections comprising at least one overlap joint-segment
    • B29C66/12821—Stepped joint cross-sections comprising at least one overlap joint-segment comprising at least two overlap joint-segments
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
    • B29C66/128—Stepped joint cross-sections
    • B29C66/1286—Stepped joint cross-sections comprising at least one bevelled joint-segment
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/20—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
    • B29C66/23—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being multiple and parallel or being in the form of tessellations
    • B29C66/232—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being multiple and parallel or being in the form of tessellations said joint lines being multiple and parallel, i.e. the joint being formed by several parallel joint lines
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
    • B29C66/54—Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721—Fibre-reinforced materials
    • 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
    • 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
    • F05B2260/00—Function
    • F05B2260/30—Retaining components in desired mutual position
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Wind Motors (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)

Claims (12)

1. En vindmøllevinge (10) dannet af en tryksidevingeskal (24) og en sugesidevingeskal (26), der er forbundne til dannelse af et vingelegeme med en bæreplansprofil med en forkant (18) og en bagkant (20), hvor vingen (10) omfatter i det mindste en sandwichpanelkonstruktion i nævnte vingeskaller (24; 26), hvor en kerne (46) er anbragt mellem et indre skinlag og et ydre skinlag i nævnte vingeskaller (24; 26), hvor den i det mindste ene sandwichpanelkonstruktion omfatter en kerne (46) med en tilspidset endedel (86), fortrinsvist placeret ved bagkanten af kernen (46), hvor en strukturel fæstningslinje (80) er placeret ved siden af den i det mindste ene sandwichpanelkonstruktion for at forbinde en del af tryksidevingeskallen (24) og en del af sugesidevingeskallen (26), hvor den strukturelle fæstningslinje (80) er placeret i afstand fra vindmøllevingens (10) forkant (18) og bagkant (20), hvor den i det mindste ene sandwichpanelkonstruktion er placeret for at tilvejebringe parallelle fæstningsflader mellem tryksidevingeskallen (24) og sugesidevingeskallen (26), hvor den strukturelle fæstningslinje (80) er placeret mellem de parallelle fæstningsflader (80), og hvor den strukturelle fæstningslinje (80) er placeret ved kernens (46) tilspidsede endedel (86) af den i det mindste en sandwichpanel.
2. Vindmøllevingen ifølge krav 1, hvor den strukturelle fæstningslinje (80) er placeret mellem et par sandwichkonstruktionpaneler for at forbinde tryksidevingeskallen (24) til sugesidevingeskallen (26).
3. Vindmøllevingen ifølge krav 1 eller krav 2, hvor vingen (10) omfatter i det mindste en bagkantssandwichpanelkonstruktion i nævnte vingeskaller (24; 26), hvor en kerne (46) er anbragt mellem et indre skinlag og et ydre skinlag i nævnte vingeskaller (24; 26), hvor den i det mindste ene sandwichpanelkonstruktion er placeret ved vindmøllevingens (10) bagkantside, hvor en strukturel bagkantsfæstningslinje er placeret ved siden af den i det mindste ene bagkantssandwichpanelkonstruktion for at forbinde tryksidevingeskallen (24) og sugesidevingeskallen (26), hvor den strukturelle bagkantsfæstningslinje er placeret i afstand fra den faktiske bagkant af vindmøllevingen.
4. Vindmøllevingen ifølge krav 3, hvor tryksidevingeskallen (24) omfatter en trykside-bagkantssandwichpanelkonstruktion og sugesidevingeskallen (26) omfatter en sugeside-bagkantssandwichpanelkonstruktion, og hvor den strukturelle bagkantsfæstningslinje er placeret mellem i det mindste en del af trykside- og sugeside-bagkantssandwichpanelkonstruktionerne.
5. Vindmøllevingen ifølge ethvert af de foregående krav, hvor vindmøllevingen omfatter en ikke-strukturel tætningsmiddel tilvejebrag ved vingen faktiske bagkant mellem overforhindanden liggende bagkantsdele af tryk- og sugesideskallerne (24; 26).
6. Vindmøllevingen ifølge krav 5, hvor det ikke-strukturelle forseglingsmiddel omfatter et polyuretan-baseret klæbemiddel.
7. Vindmøllevingen ifølge ethvert af de foregående krav, hvor vindmøllevingen omfatter et reflekterende legeme eller markør tilvejbragt ved siden af den strukturelle fæstninglinje (80), så det reflekterende legeme eller markør er placeret til at måle tykkelsen af fæstningslinjen (80) ved hjælp af en ikke-invasiv testprocedure, eksempelvis en magnetisk baseret scanteknik.
8. Et vindenergianlæg med i det mindste en vindmøllevinge ifølge ethvert af kravene 1-7.
9. En fremgangsmåde til fremstilling af en del til en vindmøllevinge (10), omfattende: tilvejebringelse af en første vingekomponent (24) med en sandwichplanelkonstruktion i den første vingekomponent (24), hvor en kerne (46) er anbragt mellem et indre skinlag og et ydre skinlag i vingekomponenten (24), hvor kernen har en tilspidset endedel (86), tilvejebringelse af en anden vingekomponent (26), forsyning af et strukturel klæbemiddel (80) til i det mindste en af den første og den anden vingekomponent (24; 26); sammenføjning af den første og den anden vingekomponent (24; 26), så det strukturelle klæbemiddel (80) er placeret ved siden af i det mindste en del af sandwichpanelkonstruktionen i den første vingekomponent (24), hvor det strukturelle klæbemiddel (80) er placeret ved siden af kernens (46) tilspidsede endedel (86) af den i det mindste ene sandwichpanelkonstruktion; og hærdning af det strukturelle fæstningsmiddel (80) for at danne en del af en vindmøllevinge (10), hvor det hærdede klæbemiddel danner en strukturel fæstningslinje (80) placeret ved siden af den i det mindste ene sandwichpanelkonstruktion for at forbinde den første vingekomponent (24) og den anden vingekomponent (26), hvor den strukturelle fæstningslinje (80) er placeret i afstand fra vindmøllevingens (10) forkant (18) og bagkant (20), og hvor sandwichpanelkonstruktionen er arrangeret til tilvejebringelse af parallelle fæstningsflader mellem den første vingekomponent (24) og den anden vingekomponent (26), hvor den strukturelle fæstningslinje (80) er placeret mellem de parallelle fæstningsflader.
10. Fremgangsmåden ifølge krav 9, hvor fremgangsmåden omfatter trinnet til tilvejebringelse af en anden vingekomponent med en sandwichpanelkonstruktion i den anden vingekomponent, hvor en kerne (46) er anbragt mellem et indre skinlag og et ydre skinlag i den anden vingekomponent, og hvor det strukturelle klæbemiddel forsynes til i det mindste en af den første og den anden vingekomponent ved siden af i det mindste en del af sandwichpanelkonstruktionen.
11. Fremgangsmåden ifølge krav 9 eller krav 10, hvor trinnet til sammenføjning omfatter sammenføjning af den første og den anden vingekomponent, så det strukturelle klæbemiddel er placeret mellem i det mindste en del af den første og den anden vingekomponenters sandwichpanelkonstruktioner.
12. Fremgangsmåden ifølge ethvert af kravene 9-11, hvor den første og den anden vingekomponent omfatter vindmøllevingeskaller (24; 26).
DK14750703.2T 2013-07-30 2014-07-23 En vindmøllevinge med fæstningslinje ved siden af en sandwichpanel i vingen DK3027893T3 (da)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP13178448 2013-07-30
PCT/EP2014/065851 WO2015014692A1 (en) 2013-07-30 2014-07-23 A wind turbine blade having a bond line adjacent a sandwich panel of the blade

Publications (1)

Publication Number Publication Date
DK3027893T3 true DK3027893T3 (da) 2018-01-08

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Country Status (10)

Country Link
US (1) US9739260B2 (da)
EP (1) EP3027893B1 (da)
CN (1) CN105431630B (da)
BR (1) BR112016001551B1 (da)
CA (1) CA2919083C (da)
DK (1) DK3027893T3 (da)
ES (1) ES2652673T3 (da)
MX (1) MX365406B (da)
PL (1) PL3027893T3 (da)
WO (1) WO2015014692A1 (da)

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Also Published As

Publication number Publication date
MX2016000656A (es) 2017-02-15
ES2652673T3 (es) 2018-02-05
EP3027893A1 (en) 2016-06-08
US20160168997A1 (en) 2016-06-16
EP3027893B1 (en) 2017-09-20
CA2919083A1 (en) 2015-02-05
CA2919083C (en) 2018-07-31
US9739260B2 (en) 2017-08-22
WO2015014692A1 (en) 2015-02-05
BR112016001551A2 (da) 2017-07-25
MX365406B (es) 2019-05-31
CN105431630B (zh) 2018-06-22
PL3027893T3 (pl) 2018-02-28
BR112016001551B1 (pt) 2022-11-29
CN105431630A (zh) 2016-03-23

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