EP1519439B1 - Antenne satellite avec des éléments photovoltaiques pour l'alimentation électrique - Google Patents

Antenne satellite avec des éléments photovoltaiques pour l'alimentation électrique Download PDF

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Publication number
EP1519439B1
EP1519439B1 EP04020217A EP04020217A EP1519439B1 EP 1519439 B1 EP1519439 B1 EP 1519439B1 EP 04020217 A EP04020217 A EP 04020217A EP 04020217 A EP04020217 A EP 04020217A EP 1519439 B1 EP1519439 B1 EP 1519439B1
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EP
European Patent Office
Prior art keywords
antenna
satellite
angle
rotation
solar
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.)
Expired - Lifetime
Application number
EP04020217A
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German (de)
English (en)
Other versions
EP1519439A1 (fr
Inventor
Andreas Ten Haaft
Michael Ten Haaft
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ten Haaft GmbH
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ten Haaft GmbH
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Publication date
Application filed by ten Haaft GmbH filed Critical ten Haaft GmbH
Priority to PL04020217T priority Critical patent/PL1519439T3/pl
Priority to SI200430277T priority patent/SI1519439T1/sl
Publication of EP1519439A1 publication Critical patent/EP1519439A1/fr
Application granted granted Critical
Publication of EP1519439B1 publication Critical patent/EP1519439B1/fr
Anticipated expiration legal-status Critical
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    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/02—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
    • H01Q3/08—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying two co-ordinates of the orientation
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/12—Supports; Mounting means
    • H01Q1/125—Means for positioning
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/44—Details of, or arrangements associated with, antennas using equipment having another main function to serve additionally as an antenna, e.g. means for giving an antenna an aesthetic aspect
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q19/00—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
    • H01Q19/10—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces
    • H01Q19/12—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces wherein the surfaces are concave
    • H01Q19/13—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces wherein the surfaces are concave the primary radiating source being a single radiating element, e.g. a dipole, a slot, a waveguide termination

Definitions

  • FIG. 3 shows the embodiment according to the invention for adjusting the satellite antenna in the direction X-X such that the signal emitted by the geostationary satellite S strikes the reflector surface 10B in such a way that an optimization in the sense of maximizing the received signal occurs.
  • This first position P1 (satellite mode) is thus characterized by a particular value of the swivel angle ⁇ 1 about the horizontal axis H-H and the rotational angle ⁇ 1 about the vertical axis V-V.

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Aerials With Secondary Devices (AREA)
  • Details Of Aerials (AREA)

Claims (7)

  1. Antenne satellite (10) destinée à la réception de signaux de satellite, conformée en antenne plane ou parabolique, comportant un réflecteur (10B), des éléments photovoltaïques destinés à l'alimentation en courant, un dispositif de positionnement commandé par une unité de commande de sorte que l'antenne peut être réglée sur au moins une première position (P1) pour optimiser le signal de satellite et une deuxième position (P2) pour optimiser la puissance des éléments photovoltaïques, caractérisée en ce que les éléments photovoltaïques sont disposés en tant que module solaire (10A) au dos de l'antenne satellite (10), et le réflecteur (10B) est disposé à l'avant de l'antenne satellite (10), en ce que l'antenne (10) peut pivoter d'un angle de pivotement (β) autour d'un axe horizontal (H-H) au moyen d'un dispositif de positionnement, et en ce que cet angle de pivotement (β) est sensiblement de zéro degré dans une position de rangement dans laquelle le côté de l'antenne (10) qui comporte le réflecteur (10B) est rabattu vers le bas, et le module solaire (10A) pointe vers le haut pour générer du courant solaire en fonction de la position du soleil.
  2. Antenne selon la revendication 1, caractérisée en ce que le dispositif de positionnement contient un étrier (31) dont l'extrémité supérieure (31A) supporte l'antenne (10), et dont l'extrémité inférieure (31B) est reliée à un pied de façon à pouvoir pivoter de l'angle de pivotement (β) autour de l'axe horizontal (H-H).
  3. Antenne selon la revendication 2, caractérisée en ce que le pied est formé par une unité de rotation (32), avec un axe de rotation vertical (V-V) et un angle de rotation (α).
  4. Antenne selon la revendication 3, caractérisée en ce que la première position (P1) est formée par un premier angle de pivotement (β1) de l'étrier (31), nécessaire à la réception optimale du satellite, et par un premier angle de rotation (α1) de l'unité de rotation (32).
  5. Antenne selon la revendication 3, caractérisée en ce que la deuxième position (P2) est formée par un deuxième angle de pivotement (β2) de l'étrier (31), nécessaire à la réception maximale du rayonnement solaire, et par un deuxième angle de rotation (α2) de l'unité de rotation (32).
  6. Antenne selon la revendication 1, caractérisée en ce que l'unité de commande est associée à un récepteur de navigation dont les données de position permettent de prescrire au moins la première position (P1) du dispositif de positionnement, éventuellement avec compensation de l'angle d'erreur de polarisation linéaire.
  7. Antenne selon les revendications 5 et 6, caractérisée en ce que les données de polarisation du récepteur de navigation déterminent également la deuxième position (P2) destinée à l'alimentation solaire.
EP04020217A 2003-09-26 2004-08-26 Antenne satellite avec des éléments photovoltaiques pour l'alimentation électrique Expired - Lifetime EP1519439B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
PL04020217T PL1519439T3 (pl) 2003-09-26 2004-08-26 Antena satelitarna z elementami fotoelektrycznymi do zaopatrywania w energię
SI200430277T SI1519439T1 (sl) 2003-09-26 2004-08-26 Satelitska antena s fotovoltaiäśnimi elementi za oskrbo z energijo

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE20314930U DE20314930U1 (de) 2003-09-26 2003-09-26 Satellitenantenne mit Photovoltaik-Elementen zur Stromversorgung
DE20314930U 2003-09-26

Publications (2)

Publication Number Publication Date
EP1519439A1 EP1519439A1 (fr) 2005-03-30
EP1519439B1 true EP1519439B1 (fr) 2007-02-14

Family

ID=29762440

Family Applications (1)

Application Number Title Priority Date Filing Date
EP04020217A Expired - Lifetime EP1519439B1 (fr) 2003-09-26 2004-08-26 Antenne satellite avec des éléments photovoltaiques pour l'alimentation électrique

Country Status (10)

Country Link
US (1) US7102579B2 (fr)
EP (1) EP1519439B1 (fr)
AT (1) ATE354183T1 (fr)
AU (1) AU2004210546B2 (fr)
DE (2) DE20314930U1 (fr)
DK (1) DK1519439T3 (fr)
ES (1) ES2282770T3 (fr)
PL (1) PL1519439T3 (fr)
PT (1) PT1519439E (fr)
SI (1) SI1519439T1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007024231A1 (de) 2007-05-21 2008-11-27 Integrated Electronic Systems !Sys Consulting Gmbh Vorrichtung und Verfahren zum Empfang von Satellitensignalen
CN106129623A (zh) * 2016-07-26 2016-11-16 青田百凯通讯科技有限公司 自给自足智能型太阳能led炫彩卫星天线和调节方法

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0510096D0 (en) * 2005-05-18 2005-06-22 Sigma Wireless Technologies Lt Antenna assembly
WO2010065904A2 (fr) * 2008-12-05 2010-06-10 Gatekeeper Systems, Inc. Émetteur à énergie solaire
TWI495195B (zh) * 2009-08-04 2015-08-01 Ind Tech Res Inst 太陽能光電轉換裝置
US8599081B2 (en) * 2010-04-21 2013-12-03 City University Of Hong Kong Solar energy collection antennas
US8698681B2 (en) 2010-04-21 2014-04-15 City University Of Hong Kong Solar energy collection antennas
GB201402627D0 (en) 2014-02-14 2014-04-02 New Dawn Innovations Ltd Digital radio receiver system
GB2539193A (en) * 2015-06-05 2016-12-14 Avanti Communications Group Plc Satellite dish
US10536107B1 (en) * 2018-10-10 2020-01-14 Vector Launch Inc. Satellite modular power supply
CN110994175B (zh) * 2020-01-02 2020-08-11 诸暨市智盈智能技术服务部 一种可利用太阳能的家用卫星信号接收设备
CN116613522A (zh) * 2023-05-05 2023-08-18 德州众昌电子有限公司 一种具有发电功能的卫星天线成型方法

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US4974129A (en) * 1989-09-06 1990-11-27 Black & Decker, Inc. Automobile solar powered utility light
JPH11342731A (ja) * 1998-06-02 1999-12-14 Mitsubishi Heavy Ind Ltd 車両用空調装置
US6549793B1 (en) * 1999-03-22 2003-04-15 Ronald D. Baratono Combined rear view mirror and telephone
US20030169200A1 (en) * 2002-03-07 2003-09-11 Urban Marek W. Method and apparatus for automatically tracking the sun with an object

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US4266179A (en) * 1979-02-27 1981-05-05 Hamm Jr James E Solar energy concentration system
US4788555A (en) 1985-07-29 1988-11-29 Schultz Donald G Combined solar and signal receptor device
JPH02166807A (ja) * 1988-12-20 1990-06-27 Nec Corp 太陽電池付パラボラアンテナ
JPH05248709A (ja) * 1992-03-09 1993-09-24 Sony Corp パラボラアンテナ装置
DE4208101A1 (de) * 1992-03-13 1993-09-16 Thomson Brandt Gmbh Satellitenantenne oder richtantenne
US5528250A (en) * 1992-11-18 1996-06-18 Winegard Company Deployable satellite antenna for use on vehicles
DE4431779A1 (de) 1994-07-08 1996-01-18 Schultze Hans Georg Solarenergieversorgungs- und Signalempfangsanlage
JPH09153712A (ja) * 1995-11-30 1997-06-10 Matsushita Electric Works Ltd 追尾アンテナ装置
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JPH11342731A (ja) * 1998-06-02 1999-12-14 Mitsubishi Heavy Ind Ltd 車両用空調装置
US6549793B1 (en) * 1999-03-22 2003-04-15 Ronald D. Baratono Combined rear view mirror and telephone
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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007024231A1 (de) 2007-05-21 2008-11-27 Integrated Electronic Systems !Sys Consulting Gmbh Vorrichtung und Verfahren zum Empfang von Satellitensignalen
CN106129623A (zh) * 2016-07-26 2016-11-16 青田百凯通讯科技有限公司 自给自足智能型太阳能led炫彩卫星天线和调节方法

Also Published As

Publication number Publication date
DE20314930U1 (de) 2003-12-11
PT1519439E (pt) 2007-03-30
ATE354183T1 (de) 2007-03-15
US7102579B2 (en) 2006-09-05
DK1519439T3 (da) 2007-04-02
DE502004002889D1 (de) 2007-03-29
AU2004210546B2 (en) 2008-05-08
US20050068238A1 (en) 2005-03-31
EP1519439A1 (fr) 2005-03-30
ES2282770T3 (es) 2007-10-16
PL1519439T3 (pl) 2007-07-31
AU2004210546A1 (en) 2005-04-14
SI1519439T1 (sl) 2007-08-31

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