DK2631468T3 - System og fremgangsmåde til luftbåren vindenergiproduktion - Google Patents

System og fremgangsmåde til luftbåren vindenergiproduktion Download PDF

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Publication number
DK2631468T3
DK2631468T3 DK12157057.6T DK12157057T DK2631468T3 DK 2631468 T3 DK2631468 T3 DK 2631468T3 DK 12157057 T DK12157057 T DK 12157057T DK 2631468 T3 DK2631468 T3 DK 2631468T3
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Denmark
Prior art keywords
glider
control means
tether
operating
flight
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DK12157057.6T
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English (en)
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Richard Dr Ruiterkamp
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Ampyx Power B V
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Publication of DK2631468T3 publication Critical patent/DK2631468T3/da

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C19/00—Aircraft control not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C31/00—Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
    • B64C31/02—Gliders, e.g. sailplanes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/60—Tethered aircraft
    • 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
    • F03D13/00—Assembly, mounting or commissioning of wind motors; Arrangements specially adapted for transporting wind motor components
    • F03D13/20—Arrangements for mounting or supporting wind motors; Masts or towers for wind motors
    • 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
    • F03D5/00—Other wind motors
    • 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
    • F03D5/00—Other wind motors
    • F03D5/02—Other wind motors the wind-engaging parts being attached to endless chains or the like
    • 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
    • F03D9/00—Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
    • F03D9/20—Wind motors characterised by the driven apparatus
    • F03D9/25—Wind motors characterised by the driven apparatus the apparatus being an electrical generator
    • F03D9/255—Wind motors characterised by the driven apparatus the apparatus being an electrical generator connected to electrical distribution networks; Arrangements therefor
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
    • H02G11/00—Arrangements of electric cables or lines between relatively-movable parts
    • H02G11/02—Arrangements of electric cables or lines between relatively-movable parts using take-up reel or drum
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/25—Fixed-wing aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/10—UAVs specially adapted for particular uses or applications for generating power to be supplied to a remote station, e.g. UAVs with solar panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00—UAVs characterised by their flight controls
    • B64U2201/20—Remote controls
    • B64U2201/202—Remote controls using tethers for connecting to ground station
    • 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
    • F05B2240/00—Components
    • F05B2240/90—Mounting on supporting structures or systems
    • F05B2240/92—Mounting on supporting structures or systems on an airbourne structure
    • 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
    • F05B2240/00—Components
    • F05B2240/90—Mounting on supporting structures or systems
    • F05B2240/92—Mounting on supporting structures or systems on an airbourne structure
    • F05B2240/921—Mounting on supporting structures or systems on an airbourne structure kept aloft due to aerodynamic effects
    • 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
    • F05B2240/00—Components
    • F05B2240/90—Mounting on supporting structures or systems
    • F05B2240/92—Mounting on supporting structures or systems on an airbourne structure
    • F05B2240/923—Mounting on supporting structures or systems on an airbourne structure which is a vehicle
    • 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
    • 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
    • Y02E10/728—Onshore wind turbines

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Remote Sensing (AREA)
  • Wind Motors (AREA)

Claims (14)

1. System til produktion af elektrisk strøm fra vind (50), omfattende et svævefly (10), der har et bæreplan (14), ombordværende styremidler med styreflader (20, 22, 24) til aerodynamisk udøvelse af torsionsmoment på svæveflyet for stigning, rulning og drejning af svæveflyet (10), når det er luftbåret, en flyvekontrolmiddel (64) til betjening af styremidlerne (20, 22, 24) og et forbindelsesmiddel til et tøjr (44), hvilket system yderligere omfatter en jordstation (40), der omfatter en spole (42) til tøjret (44), en roterende elektrisk maskine (46) forbundet med spolen (42) og et jordstationstyremiddel (66) til betjening af spolen (42) og den roterende elektriske maskine (46), og systemet omfatter yderligere et masterstyremiddel (62) til drift af systemet i mindst to alternative driftstilstande, hvori en første driftstilstand af systemet er tilvejebragt for produktion af elektrisk strøm med den roterende elektriske maskine (46) ved rotation af spolen (42) induceret ved af-spoling af tøjret (44) under brug af en løftekraft genereret ved udsættelse af det luftbårne svæveflys (10) bæreplan (14) for vind (50), og hvori en anden driftstilstand af systemet er tilvejebragt for systemgenoprettelse ved at drive spolen (42) med den roterende elektriske maskine (46), så tøjret (44) derved spoles ind på spolen (42).
2. System ifølge krav 1, kendetegnet ved, at flyvekontrolmidlet (64) tilvejebringer en første flyvekontroltilstand til automatisk flyvning og en anden flyvekontrol-tilstand til manuel betjening, især via en fjernstyringsenhed (68) med ledningsbundet eller trådløs forbindelse til flyvekontrolmidlet (64).
3. System ifølge krav 1 eller 2, kendetegnet ved, at systemet, især svæveflyet (10), yderligere omfatter en lufthastighedsføler (18) til bestemmelse af en lufthastighed af svæveflyet (10).
4. System ifølge ethvert af krav 1 til 3, kendetegnet ved, at svæveflyet (10) omfatter en styreenhed, der indbefatter både flyvekontrolmidlet (64) og masterstyremidlet (62).
5. System ifølge ethvert af krav 1 til 4, kendetegnet ved, at systemet, især jordstationen (40), yderligere omfatter en trækkraftføler (48) til bestemmelse af en trækkraft i tøjret (44).
6. System ifølge ethvert af krav 1 til 5, kendetegnet ved, at jordstationsstyremidlet (66) er udformet til at holde en forudbestemt måltrækkraft af tøjret (44), især under afspoling af tøjret (44).
7. System ifølge ethvert af krav 1 til 6, kendetegnet ved, at jordstationsstyremidlet (66) er udformet til at holde en forudbestemt målspolingshastighed, især under indspoling af tøjret (44).
8. System ifølge ethvert af krav 1 til 7, kendetegnet ved, at tøjret (44) omfatter en effekttransmissionsledning og/eller en datatransmissionsledning mellem svæveflyet (10) og jordstationen (40).
9. Fremgangsmåde til drift af et system til produktion af elektrisk strøm fra vind (50) ifølge ethvert af krav 1 til 8, hvilket system omfatter et svævefly (10) forbundet med et tøjr (44) og en jordstation (40) med en spole (42) til tøjret (44), hvori systemet betjenes skiftevist i en første driftstilstand til strømproduktion og en anden driftstilstand til systemgenoprettelse, hvori den første driftstilstand omfatter - styring af svæveflyet (10), så det følger et første flyvemønster (52) og derved genererer en løftekraft ved hjælp af et bæreplan (14) på svæveflyet (10), som er udsat for vind (50), - trækning i tøjret (44) ved hjælp af løftekraften og afspoling af tøjret (44), så der derved induceres en rotation af spolen (42), og - konvertering af spolens (42) rotation til elektrisk strøm, især ved hjælp af en roterende elektrisk maskine (46) forbundet med spolen (42), hvori den anden driftstilstand omfatter - styring af svæveflyet (10), så det følger et andet flyvemønster (54) for reduceret træk i tøjret (44), og - indspoling af tøjret (44) på spolen (42) ved at drive spolen, især ved hjælp af den roterende maskine (46) forbundet med spolen (42).
10. Fremgangsmåde ifølge krav 9, kendetegnet ved, at afspoling af tøjret (44) styres for at bevare en måltrækkraft i tøjret (44), som især er forudbestemt som en funktion af en lufthastighed af svæveflyet (10).
11. Fremgangsmåde ifølge krav 9 eller 10, kendetegnet ved, at indspolingen af tøjret (44) styres for at bevare en målspolehastighed, som især er forudbestemt som en funktion af en lufthastighed af svæveflyet (10).
12. Svævefly (10) til et system ifølge ethvert af krav 1 til 8, omfattende et bæreplan (14) til generering af en løftekraft ved udsættelse af bæreplanet (14) for vind (50), ombordværende styremidler med styreflader (20, 22, 24) til aerodynamisk udøvelse af torsionsmoment på svæveflyet til stigning, rulning og drejning af svæveflyet (10), når det er luftbåret, en flyvekontrolmiddel (64) til betjening af styremidlerne (20, 22, 24) og et forbindelsesmiddel til et tøjr (44), hvori svæveflyet (10) omfatter en ombordværende styreenhed, der indbefatter flyvekontrol-midlet (64) og et masterstyremiddel (62) til betjening af systemet i mindst to alternative driftstilstande.
13.
Anvendelse af et svævefly (10) til produktion af elektrisk strøm fra vind (50) ved hjælp af et system ifølge ethvert af krav 1 til 8 og/eller ved udøvelse af en fremgangsmåde ifølge ethvert af krav 10 til 12, hvilket svævefly (10) omfatter et bæreplan (14) til generering af en løftekraft ved udsættelse af bæreplanet (14) for vind (50), ombordværende styremidler med styreflader (20, 22, 24) til aerodynamisk udøvelse af torsionsmoment på svæveflyet til stigning, rulning og drejning af svæveflyet (10), når det er luftbåret, en flyvekontrolmiddel (64) til betjening af styremidlerne (20, 22, 24) og et forbindelsesmiddel til et tøjr (44), hvori svæveflyet (10) især er et svævefly ifølge krav 12.
DK12157057.6T 2012-02-27 2012-02-27 System og fremgangsmåde til luftbåren vindenergiproduktion DK2631468T3 (da)

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EP12157057.6A EP2631468B1 (en) 2012-02-27 2012-02-27 System and method for airborne wind energy production

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DK2631468T3 true DK2631468T3 (da) 2016-12-12

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US (2) US20140361122A1 (da)
EP (1) EP2631468B1 (da)
JP (1) JP6215849B2 (da)
AR (1) AR090093A1 (da)
AU (4) AU2013225398A1 (da)
CA (1) CA2864682C (da)
DK (1) DK2631468T3 (da)
ES (1) ES2605421T3 (da)
PL (1) PL2631468T3 (da)
PT (1) PT2631468T (da)
WO (1) WO2013127499A1 (da)

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Publication number Publication date
EP2631468A1 (en) 2013-08-28
US11358716B2 (en) 2022-06-14
AU2019271968A1 (en) 2019-12-19
AU2013225398A1 (en) 2014-09-18
CA2864682C (en) 2019-08-27
AU2018201966A1 (en) 2018-04-12
US20140361122A1 (en) 2014-12-11
JP6215849B2 (ja) 2017-10-18
AR090093A1 (es) 2014-10-15
JP2015514893A (ja) 2015-05-21
CA2864682A1 (en) 2013-09-06
PT2631468T (pt) 2016-12-02
PL2631468T3 (pl) 2017-07-31
ES2605421T3 (es) 2017-03-14
WO2013127499A1 (en) 2013-09-06
US20210047033A1 (en) 2021-02-18
AU2021273556A1 (en) 2021-12-16
EP2631468B1 (en) 2016-09-07

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