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1. WO2012132690 - SPACECRAFT

Publication Number WO/2012/132690
Publication Date 04.10.2012
International Application No. PCT/JP2012/054628
International Filing Date 24.02.2012
IPC
B64G 1/44 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
1Cosmonautic vehicles
22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
42Arrangements or adaptations of power supply systems
44using radiation, e.g. deployable solar arrays
H01L 31/042 2006.01
HELECTRICITY
01BASIC ELECTRIC ELEMENTS
LSEMICONDUCTOR DEVICES; ELECTRIC SOLID STATE DEVICES NOT OTHERWISE PROVIDED FOR
31Semiconductor devices sensitive to infra-red radiation, light, electromagnetic radiation of shorter wavelength, or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
04adapted as photovoltaic conversion devices
042PV modules or arrays of single PV cells
CPC
B64G 1/44
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
1Cosmonautic vehicles
22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
42Arrangements or adaptations of power supply systems
44using radiation, e.g. deployable solar arrays
H01L 31/052
HELECTRICITY
01BASIC ELECTRIC ELEMENTS
LSEMICONDUCTOR DEVICES; ELECTRIC SOLID STATE DEVICES NOT OTHERWISE PROVIDED FOR
31Semiconductor devices sensitive to infra-red radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus peculiar to the manufacture or treatment thereof or of parts thereof; Details thereof
04adapted as photovoltaic [PV] conversion devices
052Cooling means directly associated or integrated with the PV cell, e.g. integrated Peltier elements for active cooling or heat sinks directly associated with the PV cells
H01L 31/0543
HELECTRICITY
01BASIC ELECTRIC ELEMENTS
LSEMICONDUCTOR DEVICES; ELECTRIC SOLID STATE DEVICES NOT OTHERWISE PROVIDED FOR
31Semiconductor devices sensitive to infra-red radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus peculiar to the manufacture or treatment thereof or of parts thereof; Details thereof
04adapted as photovoltaic [PV] conversion devices
054Optical elements directly associated or integrated with the PV cell, e.g. light-reflecting means or light-concentrating means
0543comprising light concentrating means of the refractive type, e.g. lenses
H01L 31/0547
HELECTRICITY
01BASIC ELECTRIC ELEMENTS
LSEMICONDUCTOR DEVICES; ELECTRIC SOLID STATE DEVICES NOT OTHERWISE PROVIDED FOR
31Semiconductor devices sensitive to infra-red radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus peculiar to the manufacture or treatment thereof or of parts thereof; Details thereof
04adapted as photovoltaic [PV] conversion devices
054Optical elements directly associated or integrated with the PV cell, e.g. light-reflecting means or light-concentrating means
0547comprising light concentrating means of the reflecting type, e.g. parabolic mirrors, concentrators using total internal reflection
H02S 20/30
HELECTRICITY
02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
SGENERATION OF ELECTRIC POWER BY CONVERSION OF INFRA-RED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
20Supporting structures for PV modules
30Supporting structures being movable or adjustable, e.g. for angle adjustment
Y02E 10/52
YSECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
10Energy generation through renewable energy sources
50Photovoltaic [PV] energy
52PV systems with concentrators
Applicants
  • 三菱重工業株式会社 MITSUBISHI HEAVY INDUSTRIES, LTD. [JP]/[JP] (AllExceptUS)
  • 黒田 能克 KURODA Yoshikatsu [JP]/[JP] (UsOnly)
  • 池淵 博 IKEBUCHI Hiroshi [JP]/[JP] (UsOnly)
  • 益川 一範 MASUKAWA Kazunori [JP]/[JP] (UsOnly)
Inventors
  • 黒田 能克 KURODA Yoshikatsu
  • 池淵 博 IKEBUCHI Hiroshi
  • 益川 一範 MASUKAWA Kazunori
Agents
  • 工藤 実 KUDOH Minoru
Priority Data
2011-07336629.03.2011JP
Publication Language Japanese (JA)
Filing Language Japanese (JA)
Designated States
Title
(EN) SPACECRAFT
(FR) ASTRONEF
(JA) 宇宙機
Abstract
(EN)
The present invention provides technology making it possible to reduce the cost of a spacecraft equipped with an on-board solar cell. The spacecraft is provided with a collector and a solar cell. The collector is disposed on the surface of the spacecraft body and collects incoming solar light inside the body. The solar cell is mounted inside the body and receives solar light collected by the collector.
(FR)
La présente invention concerne une technologie rendant possible de réduire le coût d'un astronef comportant une cellule solaire embarquée. L'astronef comporte un collecteur et une cellule solaire. Le collecteur est disposé sur la surface du corps d'astronef et collecte une lumière solaire entrante à l'intérieur du corps. La cellule solaire est montée à l'intérieur du corps et reçoit une lumière solaire collectée par le collecteur.
(JA)
 太陽電池を搭載する宇宙機のコストを削減することができる技術を提供する。宇宙機は、集光器と太陽電池とを備える。集光器は、宇宙機のボディの表面に配置され、入射する太陽光をボディの内部に集光する。太陽電池は、ボディの内部に搭載され、集光器によって集光された太陽光を受け取る。
Also published as
RU2013143835
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