RU2011134378A - SOLAR BATTERY - Google Patents

SOLAR BATTERY Download PDF

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Publication number
RU2011134378A
RU2011134378A RU2011134378/06A RU2011134378A RU2011134378A RU 2011134378 A RU2011134378 A RU 2011134378A RU 2011134378/06 A RU2011134378/06 A RU 2011134378/06A RU 2011134378 A RU2011134378 A RU 2011134378A RU 2011134378 A RU2011134378 A RU 2011134378A
Authority
RU
Russia
Prior art keywords
torsion bars
brackets
torsion
solar battery
axis
Prior art date
Application number
RU2011134378/06A
Other languages
Russian (ru)
Other versions
RU2485026C2 (en
Inventor
Игорь Викторович Инин
Анатолий Петрович Афанасьев
Владимир Михайлович Городецкий
Original Assignee
Федеральное Государственное Унитарное Предприятие "Государственный научно-производственный ракетно-космический центр "ЦСКБ-Прогресс" (ФГУП "ГНПРКЦ "ЦСКБ-Прогресс")
Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации
Priority date (The priority date 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 date listed.)
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Publication date
Application filed by Федеральное Государственное Унитарное Предприятие "Государственный научно-производственный ракетно-космический центр "ЦСКБ-Прогресс" (ФГУП "ГНПРКЦ "ЦСКБ-Прогресс"), Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации filed Critical Федеральное Государственное Унитарное Предприятие "Государственный научно-производственный ракетно-космический центр "ЦСКБ-Прогресс" (ФГУП "ГНПРКЦ "ЦСКБ-Прогресс")
Priority to RU2011134378/06A priority Critical patent/RU2485026C2/en
Publication of RU2011134378A publication Critical patent/RU2011134378A/en
Application granted granted Critical
Publication of RU2485026C2 publication Critical patent/RU2485026C2/en

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Classifications

    • 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
    • Y02E10/40—Solar thermal energy, e.g. solar towers

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  • Photovoltaic Devices (AREA)
  • Hinges (AREA)

Abstract

Солнечная батарея, содержащая раму, верхние и нижние створки, попарно связанные между собой шарнирами, на оси которых закреплены торсионы, на других концах которых установлены кронштейны, в которых размещены механизмы взведения торсионов, отличающаяся тем, что кронштейны закреплены на торсионах с возможностью вращения и установлены в исходном положении симметрично оси торсионов, причем один из кронштейнов закреплен на верхней створке, а другой на нижней, расположение которых обеспечивает механизмами взведения закручивание торсионов только в одну сторону.A solar battery containing a frame, upper and lower leaves, pairwise interconnected by hinges, on the axis of which are mounted torsion bars, at the other ends of which brackets are mounted, in which torsion cocking mechanisms are located, characterized in that the brackets are rotatably mounted on the torsion bars and installed in the initial position, it is symmetrical to the axis of the torsion bars, with one of the brackets mounted on the upper leaf and the other on the lower one, the arrangement of which ensures the torsion bars twist t only one way.

Claims (1)

Солнечная батарея, содержащая раму, верхние и нижние створки, попарно связанные между собой шарнирами, на оси которых закреплены торсионы, на других концах которых установлены кронштейны, в которых размещены механизмы взведения торсионов, отличающаяся тем, что кронштейны закреплены на торсионах с возможностью вращения и установлены в исходном положении симметрично оси торсионов, причем один из кронштейнов закреплен на верхней створке, а другой на нижней, расположение которых обеспечивает механизмами взведения закручивание торсионов только в одну сторону. A solar battery containing a frame, upper and lower leaves, pairwise interconnected by hinges, on the axis of which are mounted torsion bars, at the other ends of which brackets are mounted, in which torsion cocking mechanisms are located, characterized in that the brackets are rotatably mounted on the torsion bars and installed in the initial position, it is symmetrical to the axis of the torsion bars, with one of the brackets mounted on the upper leaf and the other on the lower one, the arrangement of which ensures the torsion bars twist t only one way.
RU2011134378/06A 2011-08-16 2011-08-16 Solar cell battery RU2485026C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2011134378/06A RU2485026C2 (en) 2011-08-16 2011-08-16 Solar cell battery

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2011134378/06A RU2485026C2 (en) 2011-08-16 2011-08-16 Solar cell battery

Publications (2)

Publication Number Publication Date
RU2011134378A true RU2011134378A (en) 2013-02-27
RU2485026C2 RU2485026C2 (en) 2013-06-20

Family

ID=48786590

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2011134378/06A RU2485026C2 (en) 2011-08-16 2011-08-16 Solar cell battery

Country Status (1)

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RU (1) RU2485026C2 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2167793C2 (en) * 1998-06-17 2001-05-27 Государственный научно-производственный ракетно-космический центр "ЦСКБ-Прогресс" Spacecraft solar battery
RU2214949C1 (en) * 2002-06-18 2003-10-27 Государственный научно-производственный ракетно-космический центр "ЦСКБ-Прогресс" Spacecraft solar battery
RU2309875C1 (en) * 2006-02-20 2007-11-10 Закрытое акционерное общество "ТехКом" Method of forming frameless centrifugal structure (versions) and device for realization of this method
KR101008062B1 (en) * 2008-08-20 2011-01-13 한국항공우주연구원 Satellite solar array deployment motion analysis using the fluorescent targets

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RU2485026C2 (en) 2013-06-20

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Effective date: 20150623

PD4A Correction of name of patent owner