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2 499 751

(13)

(51)

IPC

B64G1/44(2006-01-01)

(21) (22)

Application

2012102656/11, 2012-01-25

(24)

Start date

2012-01-25

(22)

Actual filing date

2012-01-25

(45)

Published

2013-11-27

(72)

Inventor

Inin Igor' ViktorovichAfanas'Ev Anatolij Petrovich

(73)

Holder

Federal'Noe Gosudarstvennoe Unitarnoe Predprijatie Nauchno-Proizvodstvennyj Raketno-Kosmicheskij TsentrRossijskaja Federatsija, Ot Imeni Kotoroj Vystupaet Ministerstvo Oborony Rossijskoj Federatsii

SOLAR BATTERY STRUT Russian patent published in 2013 - IPC B64G1/44

Abstract RU 2499751 C2

FIELD: aircraft engineering.

SUBSTANCE: solar battery strut comprises two-link mechanism with common axle supporting torsion spring with cocking devices. One link is arranged at solar battery frame while another one is mounted at craft body. Spring-loaded rod to lock the link at end position is arranged at said link perpendicular to axis. Rocker is arranged at spring-loaded rod end to turn thereat. Antifriction bearings are rigidly secured at rod both ends to interact with cam taper grooves, said cams being rigidly mounted at the link opposite spring-loaded rod. Links of aforesaid mechanism have openings to link retainers threaded therein.

EFFECT: higher reliability, simplified installation of solar battery at craft body.

13 dwg

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RU 2 499 751 C2

Authors

Inin Igor' Viktorovich

Afanas'Ev Anatolij Petrovich

Dates

2013-11-27—Published

2012-01-25—Filed