Microsatellite assembly device, parallel assembly equipment, and assembly method
A technology for assembling devices and micro-satellites, applied in the field of micro-satellites, can solve the problems of poor specialization, inability to meet the requirements of micro-satellites in batches, rapid and low-cost assembly, and inability to meet the needs of micro-satellites
Active Publication Date: 2021-03-02
HARBIN INST OF TECH
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Problems solved by technology
However, the traditional custom-based single-satellite assembly mode can no longer meet the needs of mass, fast, and low-cost assembly of microsatellites
In the field of satellite assembly, the current assembly system of microsatellites follows the assembly system of large satellites, which has low efficiency and poor specialization, and cannot meet the assembly requirements of microsatellites, especially mass-produced microsatellites
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[0033] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the drawings in the embodiments of the present invention.
[0034] Generally, a microsatellite may include a plurality of compartments, each compartment may be in a prism shape such as a square prism, a hexagonal prism, and each compartment may be composed of multiple parts. Among the parts constituting the compartment, the main load-bearing beams corresponding to the edges of the above-mentioned quadrangular or hexagonal prisms are hollow, in other words, the main load-bearing beams include through holes extending along their longitudinal axes. When multiple compartments are stacked together, the through holes of the main bearing beams of different compartments are also stacked together to form a channel, so that the connecting rods of the compartments can pass through the formed channel.
[0035] see Figure 1 to Figure 3 , the embo...
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The embodiment of the present invention discloses a microsatellite assembly device, parallel assembly equipment and assembly method. The device includes a base, and the base has a plurality of first series of holes, and each set of first series of holes starts near the center of the base. Beginning to arrange toward the edge of the base; a plurality of stop rods suitable for assembling a plurality of parts into cabin sections; a plurality of stop guide rails suitable for assembling a plurality of cabin sections into the tiny satellite; wherein, the Each of the plurality of limit rods or each of the plurality of limit rails can be fixed to the base through a different hole in the first series of holes to adjust the plurality of limit stops. The distance between each of the bars or each of the plurality of limit guide rails relative to the center of the base, so that the plurality of limit rods or the plurality of limit guide rails are adapted to the Dimensions of tiny satellites.
Description
technical field [0001] The invention relates to the field of microsatellites, in particular to a microsatellite assembly device, parallel assembly equipment and assembly method. Background technique [0002] Micro-satellites with low cost, large-scale cluster applications, and rapid emergency response will usher in a peak application in the next few years. However, the traditional custom-based single-satellite assembly mode can no longer meet the needs of mass, fast, and low-cost assembly of micro-satellites. In the field of satellite assembly, the current assembly system of microsatellites follows the assembly system of large satellites, which has low efficiency and poor specialization, and cannot meet the assembly requirements of microsatellites, especially mass-produced microsatellites. Therefore, it is necessary to develop a specialized final assembly platform for mass microsatellite assembly, and form a specialized final assembly method that meets the needs of mass mic...
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IPC IPC(8): B23P21/00
CPCB23P21/004
Inventor 王峰刘源曹喜滨张冀鹞郭金生孔宪仁王震
Owner HARBIN INST OF TECH