New hinge for solar panels
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Conceptual design and finite element method validation of a new
The proposed passive mechanism generates a lateral rotation motion based in an innovative anchor hinge design with a double torsional spring, to deploy the solar panels to a final position of 90° with respect to CubeSat''s body.
Design of an innovative active hinge for Self-deploying/folding
In this research, we propose a novel active hinge mechanism for solar panels, by which on one hand to realize the required deploying and folding movement actively, on the other hand to give a new way of active vibration control to
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With several hundred solar arrays in orbit, SpaceTech is a leading supplier of solar array systems for satellites. We are your one-stop solution for the full scope of solar arrays, from body-mounted panels, via single hinge deployable arrays to multi-hinge deployable solar array wings including deployment electronics & HDRM, solar array drive, mechanisms as well as photovoltaic
Design of an Innovative Active Hinge for Self-deploying/folding
This paper describes the design and optimization of a new type of active hinge, which has the potential application into solar panels for providing the panels with not only...
Conceptual design and finite element method validation of a new
The first time that a rotatory passive mechanism was used to deploy solar panels in CubeSats was in 2002 when Stanford University employed torsional springs and hinges to deploy solar panels in the QuakeSat project. 8,9 From that point, several missions have used deployable solar panels in very different configurations and with diverse deployment
Design and Optimization of a New Type of Active Hinge
This paper describes the design and optimization of a new type of active hinge, which has the potential application into solar panels for providing the panels with not only self-deploying/folding functions but also active vibration control capacity. The hinge was designed based on direct drive principle of interaction between
KR20140080705A
The present invention relates to a hinge for unfolding a solar panel and, more specifically, to a hinge for unfolding a solar panel capable of minimizing the impact generated when the...
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Smart tubular hinge with multi-environment adaptability for rapid
In this work, we developed a tubular hinge with dual-deformation deployability. For rapid deployment needs, the hinge can be deformed at room temperature and achieve quick elastic deployment within 0.3 s at room or low temperatures.
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Design and Optimization of a New Type of Active Hinge
This paper describes the design and optimization of a new type of active hinge, which has the potential application into solar panels for providing the panels with not only...
新型可展开式CubeSat太阳能电池板自锁铰链的概念设计和有限元
In this work, the design, analysis and manufacture of a deployment mechanism for CubeSat solar panels is shown. A finite element method analysis was carried out in a hinge with an integrated blocking system as well as a double torsion spring, which can be used on CubeSats.
(PDF) Conceptual design and finite element method
In this work, the design, analysis, and manufacture of a deployment mechanism for CubeSat solar panels is shown. A FEM analysis
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Design of an innovative active hinge for Self-deploying/folding
A novel passive vibration damping device is developed for the multi-panel sun-orientated deployable solar array that is lockable and located near the solar array root hinge to increase the structural damping without reducing the fundamental frequency.
Conceptual design and finite element method
The proposed passive mechanism generates a lateral rotation motion based in an innovative anchor hinge design with a double torsional spring, to deploy the solar panels to a final position of 90° with respect to CubeSat''s
(PDF) Conceptual design and finite element method validation of a new
In this work, the design, analysis, and manufacture of a deployment mechanism for CubeSat solar panels is shown. A FEM analysis was carried out in a hinge with an integrated blocking system...
Solar energy breakthrough could reduce need for solar farms
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6 FAQs about [New hinge for solar panels]
What is a solar hinge used for?
Due to the hinge's excellent deformation characteristics, it shows great promise for use in foldable and deployable structures such as solar wings, antennas, and solar sails. As illustrated in Fig. 5 a, hinges can be deployed on the upper and lower sides of a simulated solar panel, positioned vertically to negate the influence of gravity.
Can a solar panel hinge be deployed vertically?
As illustrated in Fig. 5 a, hinges can be deployed on the upper and lower sides of a simulated solar panel, positioned vertically to negate the influence of gravity. In this setup, the hinge only needs to overcome the friction at the connection points of the solar panels to deploy.
Can a solar sail hinge be used as a smart deformable hinge?
The hinge can achieve stable deployment of a simulated solar sail within 100 s at 40 W power. In the future, this dual-deformation design can be extended to more hinges, enabling their independent or combined use as smart deformable hinges, thereby expanding their applicability across various scenarios and environments.
How long should a solar sail hinge be?
It is worth noting that to increase the area of the deployed solar sail, both ends of the tubular hinge are extended to 17 cm. Since the positions and dimensions of the slits remain unchanged, the 17 cm long hinge retains excellent elastic deployment characteristics.
How do you remove a tubular hinge?
For the tubular hinge, heat it to the shaping temperature and maintain it for 10 min. After removal, quickly apply a small pressure to the middle of the hinge to facilitate folding and bending, use external force to secure both ends of the hinge, and cool to room temperature.
How much stress does a hinge have?
A maximum von-Misses stresses of 9.7 MPa in the active element of the main hinge, as well as of 46.721 MPa in the active element of the secondary hinge were obtained. These are shown in Figure 8 (a) and (b), respectively.
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