A controllable and orderly inflation self-supporting solar sail structure

An inflatable deployment and self-supporting technology, applied in the aerospace field, can solve the problems of inability to deploy the solar sail surface and poor stability, and achieve the effects of uniform tension distribution, improved stable strength, and improved straightness.

Active Publication Date: 2016-05-11
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The existing technology cannot reliably and stably deploy the solar sail in orbit, and there is a problem of poor stability

Method used

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  • A controllable and orderly inflation self-supporting solar sail structure
  • A controllable and orderly inflation self-supporting solar sail structure
  • A controllable and orderly inflation self-supporting solar sail structure

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Embodiment Construction

[0031] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0032] It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other.

[0033] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments, but not as a limitation of the present invention.

[0034] like Figure 1 to Figure 9 As shown, a controllable and orderly inflation self-supporting solar sail str...

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Abstract

The invention relates to the field of spaceflight and discloses a controllably and orderly inflated self-supporting type solar sail structure. A sail surface approximately triangle-shaped and formed by three curves is adopted, the sail surface can be unfolded in orbit stably and orderly, and distribution gradient of internal plane stress forced on the sail surface after unfolding is reduced by 20%; a support ring with the inner diameter equal to a winding shaft is arranged at the position of rectangular vertice of the sail surface, and concentrated stress of the sail surface can be lowered; a circular opening enclosed by 4n (n is larger than or equal to 3, and n is an integer) sawteeth, and no relative movement between the vertice of the sail surface and the winding shaft can be guaranteed; four sets of inflated extension arms used for supporting the sail surface are unfolded, each set is formed by two extension arms, straightness of the inflated extension arms and rigidity of the inflated extension arms after being unfolded can be improved, the rigidity of the structure is two times of that of a structure with a single extension arm, and unfolding stability of the extension arms is improved.

Description

technical field [0001] The invention relates to the field of aerospace, in particular to a self-supporting solar sail structure that can be inflated and deployed in a controllable and orderly manner. Background technique [0002] After entering the 21st century, the field of deep space exploration has been paid more and more attention by human beings. As a new type of aircraft, the solar sail spacecraft can realize the accelerated motion of the aircraft without a propulsion system. The solar sail aircraft obtains flight power through the momentum exchange with the sun photons. And this propulsion resource is endless, and the propulsion sustaining force only depends on the life span of the solar sail film and the actuator and the distance from the light source. It has high research value in the field of deep space exploration. In order to provide enough propulsion for the spacecraft, the spacecraft needs a sufficiently large solar sail surface. The inflatable deployable so...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/44
Inventor 卫剑征马瑞强谭惠丰宋博林国昌田振辉刘宇飞
Owner HARBIN INST OF TECH
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