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Locker capable of achieving multi-module self-adaption and high precision of antenna

An adaptive, multi-module technology, applied in the field of satellite antennas, to achieve high-precision locking, ensure accuracy, and compensate for errors

Active Publication Date: 2019-03-29
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

Moreover, at present, the locker and related products that can realize multiple groups of antenna reflective surfaces to be locked simultaneously, compensate the error within a certain range and ensure the accuracy after locking are still blank.

Method used

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  • Locker capable of achieving multi-module self-adaption and high precision of antenna
  • Locker capable of achieving multi-module self-adaption and high precision of antenna
  • Locker capable of achieving multi-module self-adaption and high precision of antenna

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Embodiment Construction

[0026] The present invention will be further described below in conjunction with accompanying drawing.

[0027] The structure of the present invention is as figure 1 As shown, it includes a lock case 9 and a buckle 13 matched with the lock case.

[0028] The lock case 9 has a symmetrical structure, the top of the lock case 9 is provided with a lock case back cover 11, and the two sides are provided with a lock case side cover 1; A pressing block sliding groove 20 is provided, and a pressing block 12 is arranged in the pressing block sliding groove 20; a lock tongue sliding groove 18 is respectively arranged on both sides of the lock buckle inner groove 21, and a lock tongue sliding groove 18 is respectively provided with a lock Tongue sliding guide groove 19, first dead bolt 5 and second dead bolt 6, dead bolt sliding guide groove 19 guides the motion of first dead bolt 5; First dead bolt 5 sides have chute, second dead bolt 6 There is a slider on the side, and a stopper pro...

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PUM

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Abstract

In order to solve the problem that high-precision simultaneous locking cannot be achieved among satellite solid-plane antenna modules, the invention provides a locker which can achieve simultaneous locking of multiple sets of antenna reflecting surfaces, compensate for errors within a certain range and ensure the precision after locking, and achieves repeated folding, high-precision unfolding andlocking of a solid-plane reflecting surface antenna. Locking of the locker in the upper direction, the lower direction, the front direction, the rear direction, the left direction and the right direction is achieved by arranging a spring bolt divided into two parts and assembled together and the pressing block in the pressing block sliding groove in the spring bolt sliding groove, errors can be compensated within a certain range, the precision after locking is guaranteed, and high-precision locking between the two solid-surface reflector antennas is further achieved.

Description

technical field [0001] The invention relates to the technical field of satellite antennas, in particular to a multi-module self-adaptive high-precision locking device. Background technique [0002] With the development of satellite technology, more attention has been paid to the design requirements of multi-band, high precision and large capacity in the design of satellite antennas, and the design of satellite antennas has gradually become more complicated. However, due to the limitations of rocket carrying capacity, economy and other factors, the antenna structure needs to be light in weight and small in size. Based on the above contradictions, modular and expandable antenna technology has emerged and developed rapidly, and has become an important way to solve the needs of satellite antennas such as large aperture, high precision, and light weight. This requires the antenna to be in a folded state when launching, and to unfold after launching to the orbit. Therefore, the a...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H01Q15/16H01Q1/28F16B5/00
CPCF16B5/0004H01Q1/288H01Q15/162
Inventor 蔡友慧秦远田陈金宝马益王宸侯世涵杨全欧李波蒋松
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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