High-precision multi-joint locking surface antenna auxiliary deployment mechanism

A deployment mechanism and high-precision technology, applied in the field of satellite antennas, can solve the problem of inability to achieve simultaneous flipping and precise docking of multiple groups of antenna reflecting surface sub-modules, and achieve the effects of high positional accuracy, control of flipping angle, and precise flipping angle.

Active Publication Date: 2020-07-17
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

[0004] Aiming at the technical problem that the auxiliary deployment mechanism in the prior art cannot realize the simultaneous flipping and precise docking of multiple groups of antenna reflection surface sub-modules, and in order to fill this blank field, the present invention discloses a high-precision multi-joint locking surface antenna Auxiliary unfolding mechanism, the invention can assist the simultaneous flipping of multiple antenna modules to ensure the next step of antenna module docking and unfolding operations

Method used

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  • High-precision multi-joint locking surface antenna auxiliary deployment mechanism
  • High-precision multi-joint locking surface antenna auxiliary deployment mechanism
  • High-precision multi-joint locking surface antenna auxiliary deployment mechanism

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Embodiment Construction

[0039] In order to make the objectives, technical solutions and effects of the present invention clearer and clearer, the following examples are given to further illustrate the present invention in detail. It should be pointed out that the specific implementation described here is only used to explain the present invention, but not to limit the present invention.

[0040] Such as Figure 1~5 As shown, the structure of the present invention includes: a turning module I, a rotating connection module II, and a fixed module III. The turning module I and the fixed module III contain a wedge telescopic mechanism; the wedge telescopic mechanism is as Picture 9 As shown, the shown wedge telescopic mechanism includes an upper cover 15, a guide block 16, an upper guide groove 18, a lower guide groove 22, a wedge pressing rod 17, a wedge 19, an integral rod 20, a connecting block 24, and a spring mandrel 25, spring 26, ring 29.

[0041] The rotating connection module II includes a large mo...

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Abstract

The invention discloses a high-precision multi-butt-joint-locking-plane antenna auxiliary unfolding mechanism, and belongs to the technical field of satellite antennas. The mechanism comprises an overturning module I, a rotation connection module II and a fixing module III, the module I and the module III comprise wedge telescoping mechanisms, the rotation connection module II comprises a large motor, a transmission shaft fixedly combined with a motor shaft of the large motor, and a first installation plate and a second installation plate supporting connection of the large motor and the transmission shaft, and the overturning module I and the rotation connection module II are separately connected with the transmission shaft. By employing the mechanism, the whole process of antenna unfolding is reversible, when an antenna needs to be withdrawn, wedges of the auxiliary mechanism can perform accurate butt joint with a reflection plane and are then vertically overturned to an original position, the antenna reflection plane with greater length can be carried in a segmented manner, a fixing effect is achieved during folding of the reflection plane, and the problem of simultaneous and accurate overturning of multiple groups of reflection planes is solved.

Description

Technical field [0001] The invention relates to the technical field of satellite antennas, in particular to a multi-module, self-adaptive, high-precision auxiliary deployment mechanism of a satellite solid surface antenna. Background technique [0002] With the development of satellite technology, the design of satellite antennas pays more attention to the design requirements of multiple frequency bands, high precision, and large capacity. Therefore, the design of satellite antennas gradually becomes more complicated. However, due to the limitations of rocket carrying capacity and economy, the antenna structure is required to be light and small. Based on the above contradictions, modular and expandable antenna technology emerged and developed rapidly. It has become an important way to solve the needs of satellite antennas such as large-diameter, high-precision, and lightweight. This requires the antenna to be folded when launching. Because the satellite reflecting surface area i...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H01Q1/08H01Q1/12
CPCH01Q1/08H01Q1/12
Inventor 杨全欧秦远田陈金宝王宸蔡友慧候世涵李波蒋松
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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