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An Active High Stiffness Locking Combination Mechanism for Flexible Solar Wings

A technology of locking mechanism and combined mechanism, which is applied in the field of aerospace, can solve the problems of low stiffness, unresolved high stiffness, etc.

Active Publication Date: 2020-10-23
SHANGHAI AEROSPACE SYST ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The traditional scheme adopts the configuration of male hinge and female hinge, which has disadvantages such as low rigidity
The flexible solar wing is a relatively cutting-edge space technology, and no related devices to solve its high-stiffness deployment and locking have been investigated at home and abroad.

Method used

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  • An Active High Stiffness Locking Combination Mechanism for Flexible Solar Wings
  • An Active High Stiffness Locking Combination Mechanism for Flexible Solar Wings
  • An Active High Stiffness Locking Combination Mechanism for Flexible Solar Wings

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Embodiment Construction

[0027] The embodiments of the present invention are described in detail below. This embodiment is implemented on the premise of the technical solution of the present invention, and detailed implementation methods and specific operating procedures are provided, but the protection scope of the present invention is not limited to the following implementation example.

[0028] Please refer to Figure 1-6 , an active high-rigidity locking combination mechanism for a flexible solar wing, comprising an upper case deployment locking mechanism 4 and a lower case deployment locking mechanism 3;

[0029] Such as Figure 4 As shown, the battery array assembly 2 includes an upper box 21 , a lower box 22 , and a battery board 23 pressed between the upper box 21 and the lower box 22 .

[0030] Such as Figure 5 As shown, the lower case unfolding locking mechanism 3 is an active mechanism, including a first support 31, a second support 32, and a driving mechanism 33; the driving mechanism ...

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Abstract

The invention discloses an active high-rigidity locking combined mechanism of a flexible solar wing. The active high-rigidity locking combined mechanism comprises lower box body unfolding and lockingmechanisms and upper box body unfolding and locking mechanisms, wherein the lower box body unfolding and locking mechanisms are arranged on the two sides of the stretching mechanism respectively, andthe two sides of each lower box body unfolding and locking mechanism are each provided with one upper box body unfolding and locking mechanism; the lower box body unfolding and locking mechanism rotating shaft and the upper box body unfolding and locking mechanism rotating shaft are arranged at coaxial positions; when the lower box body unfolding and locking mechanism is unfolded, the upper box body unfolding and locking mechanism is unfolded and then locked. After being unfolded in place, the active mechanism can continuously act to eliminate a mechanism gap so as to increase the locking height, and has the advantage of high locking rigidity; the passive hinge is driven by the active mechanism to be unfolded and locked, and has the advantages of being simple and reliable. And after the active mechanism drives the passive hinge to be unfolded and locked, the cell array assembly can be separated under the action of the stretching mechanism so as to be unfolded. The mechanism is simple and reliable in structure, high in mechanism robustness, high in locking rigidity and small in folding envelope.

Description

technical field [0001] The invention relates to the field of aerospace technology, and relates to a locking combination mechanism. Background technique [0002] In the field of aerospace technology, the power demand of aircraft is increasing day by day. Flexible solar wings are generally used in occasions with large power generation and large deployment areas. Their length and width are relatively large, and their deployment and locking rigidity is relatively high. Moreover, due to the constraints of the envelope of the rocket fairing, the flexible solar wing should be folded as far as possible. Possibly small. The traditional solution adopts the configuration of male hinge and female hinge, which has disadvantages such as low rigidity. The flexible solar wing is a relatively cutting-edge space technology, and no related device to solve its high-stiffness deployment and locking has been investigated at home and abroad. Contents of the invention [0003] Aiming at the pr...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/44B64G1/22
CPCB64G1/222B64G1/443
Inventor 霍杰程雷咸奎成袁伟王威倪啸枫付清山王治易
Owner SHANGHAI AEROSPACE SYST ENG INST
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