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A kind of antenna bracket and spacecraft

A technology for antenna brackets and spacecraft, which is applied to antennas, antenna supports/mounting devices, antenna components, etc., and can solve problems such as antenna load vibration shock amplification

Active Publication Date: 2021-06-15
BEIJING INST OF RADIO MEASUREMENT
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, due to the height of the mounting bracket, the actual vibration and impact of the antenna load may be amplified

Method used

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  • A kind of antenna bracket and spacecraft
  • A kind of antenna bracket and spacecraft
  • A kind of antenna bracket and spacecraft

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Embodiment Construction

[0027] In order to have a clearer understanding of the above objects, features and advantages of the present invention, the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments. It should be noted that, in the case of no conflict, the embodiments of the present application and the features in the embodiments can be combined with each other.

[0028] In the following description, many specific details are set forth in order to fully understand the present invention. However, the present invention can also be implemented in other ways different from those described here. Therefore, the protection scope of the present invention is not limited by the specific details disclosed below. EXAMPLE LIMITATIONS.

[0029] Refer below Figure 1 to Figure 3 Some embodiments according to the invention are described.

[0030] Such as Figure 1 to Figure 3 As shown, the embodiment of the first aspect of the present...

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Abstract

The present invention provides an antenna support and a spacecraft. The antenna support includes: a support body and at least one sealed compartment. The support body at least partially passes through each compartment and is filled with a viscous fluid. The antenna support provided by the present invention is based on the principle of tuning liquid damping, and the support, the compartment and the viscous fluid form a shock-absorbing buffer device. During the launch phase of the spacecraft, the vibration and impact of the spacecraft are transmitted to the bottom of the frame, causing the viscous fluid in the compartment to slosh, generating dynamic lateral pressure on the frame, and reducing the acceleration response at the top of the frame; At the same time, the vibration of the viscous fluid can effectively absorb and consume the vibration energy of the support, so as to achieve the effect of shock absorption and buffering, reduce the acceleration response of the antenna load in the launch section of the spacecraft, and improve the adaptability and reliability of the antenna load and the support body .

Description

technical field [0001] The invention relates to the technical field of aerospace equipment, in particular to an antenna bracket and a spacecraft. Background technique [0002] The low-orbit broadband communication satellite communication load usually has a reflector antenna load of the mechanical scanning working system. In order to avoid rotation interference, antenna loads such as antenna loads and servo shafts need to be fixedly connected to the star through mounting brackets, and the shaft is supported to a certain height from the star. The mounting bracket plays the role of bearing mechanical loads such as vibration and impact of the antenna load in the transmitting section. [0003] The mounting bracket is generally formed by precision machining through an aluminum alloy thick plate. The bottom is the mounting interface with the star, and the upper part is the mounting interface with the antenna load. [0004] In the prior art, the antenna load mounting bracket has a...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H01Q1/12H01Q1/22F16F15/023B64G1/66
CPCB64G1/66F16F15/023H01Q1/1242H01Q1/22
Inventor 周红华李全贺
Owner BEIJING INST OF RADIO MEASUREMENT