Zero-gravity compensation device for carbon fiber supporting rod type solar wing

The invention relates to a zero gravity compensation device for a carbon fiber support rod type solar wing, which is characterized by comprising a fixed lifting rope, a fixed device, a follow-up lifting rope and a follow-up device, one end of the fixed lifting rope is fixed on the fixed device, and...

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Hauptverfasser: HU YAHANG, ZANG ZIYI, XU QIANG, LI BINGHUI, AN CHANGHE, WANG GUOXING, CHENG ZE, ZANG XIAOKANG, DUAN PING
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creator HU YAHANG
ZANG ZIYI
XU QIANG
LI BINGHUI
AN CHANGHE
WANG GUOXING
CHENG ZE
ZANG XIAOKANG
DUAN PING
description The invention relates to a zero gravity compensation device for a carbon fiber support rod type solar wing, which is characterized by comprising a fixed lifting rope, a fixed device, a follow-up lifting rope and a follow-up device, one end of the fixed lifting rope is fixed on the fixed device, and the other end of the fixed lifting rope is fixed on a support rod connected with a solar wing simulation wall; one end of the follow-up lifting rope is fixed to the follow-up device, and the other end of the follow-up lifting rope is fixed to a supporting rod connected with the solar wing outer plate. The fixed device is mounted at a fixed position and comprises a position-adjustable lifting rope mounting point used for mounting a fixed lifting rope, and the lifting rope mounting point is alwayslocated on the axis of a root hinge, connected with the solar wing simulation wall, of the supporting rod; and the follow-up device can perform compound motion of circular motion and linear motion bytaking the plate hinge as
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subjects AIRCRAFT
AVIATION
COSMONAUTICS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
title Zero-gravity compensation device for carbon fiber supporting rod type solar wing
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