A 2D full air floating deployment hanging device for ground simulation of solar wing panels
A ground simulation and hanging device technology, applied in the field of solar wing hanging, can solve the problem of inability to solve the high-precision requirements of solar wing panels, and achieve the effects of low production cost, simple and compact structure, and prevention of additional influences
Active Publication Date: 2018-12-14
浙江海宁经编产业园区开发有限公司
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Problems solved by technology
[0007] The purpose of the present invention is to solve the problem that the existing hanging device cannot meet the high-precision requirements in the hanging process of the solar wing, and the quality of the follower parts is relatively large, and the additional influence of friction and inertial force is insufficient, and a solar wing is provided. The slab ground simulates the two-dimensional full air floatation deployment hanging device, which can effectively avoid the additional influence of friction and inertial force, and is suitable for hanging solar panels
Method used
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Embodiment Construction
[0023] The present invention will be further described below in conjunction with accompanying drawing:
[0024] Such as Figure 1-7As shown in the figure, a two-dimensional full air-floating hanging device for ground simulation of a solar wing panel includes a short beam frame 2, a short beam slider 1, a short beam air bearing seat 3, a side air cushion 4, an adjusting bolt 5, and a suspension screw seat 6 and hanging rope 7; the two ends of the short beam frame 2 are respectively connected to two long straight slide rails arranged in parallel through the air bearing slider, and the short beam frame 2 is connected to the two long straight slide rails by the air bearing slider at both ends. Moving along a straight line, the middle part of the short beam frame 2 is provided with a first square through hole 18. The first square through hole 18 divides the top of the short beam frame 2 into two horizontal support planes 16 on the left and right. The short beam frame 2 The upper e...
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The invention discloses a two-dimensional full airfioatation unfolding hanging device for the ground-based simulation of a solar wing plate. The device comprises a short beam frame, a short beam slider, a short beam airfioatation base, side air cushions, adjusting bolts, a suspension screw seat and a hanging rope. The bottom of the short beam slider is V-shaped, the short beam airfioatation base is supported on the short beam frame, a V-shaped groove matched with the short beam slider is formed in the upper part of the short beam airfioatation base, a second square through hole is formed in the middle of the short beam airfioatation base, first airfioatation holes are formed in the two sides of the V-shaped groove on the two sides of the second square through hole, and second airfioatation holes are formed in the positions, in contact with the two horizontal support planes of the short beam frame, of the undersurface of the short beam airfioatation base. According to the device, the weight is decreased on the basis of guaranteeing the rigidity to the maximum, and thus the additional impact generated by the inertial force of follow-up components is avoided; and airfioatation is adopted for supporting between the short beam frame and a long straight guide track, and airfioatation is adopted for supporting between the short beam airfioatation base and the short beam frame, so that the influence of friction force on the whole hanging device is minimized.
Description
technical field [0001] The invention relates to the field of solar wing suspension, and more specifically, relates to a ground simulation two-dimensional full-air floating deployment suspension device for a solar wing panel. Background technique [0002] The solar wing is the energy source of the satellite. The solar panel is a device that collects solar energy. It is usually used to supply energy for satellites and spacecraft, and can also be used to install on the top of environmentally friendly cars. The solar wing is the energy source of the satellite. When the satellite is launched, the solar wing is in a folded state. After the star rocket is separated, it is opened and the direction is constantly adjusted during the flight of the satellite, so that the solar cells are aligned with the sun to provide energy for the entire star. The solar wing monitoring camera can capture the deployment process and working status of the solar wing, and judge whether the solar wing is...
Claims
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IPC IPC(8): B64G7/00
CPCB64G7/00
Inventor 谢毅
Owner 浙江海宁经编产业园区开发有限公司