Mechanism-type separation nut and joint unlocking mechanism of satellite and launch vehicle composed of mechanism-type separation nut
A separate nut and mechanism technology, which is applied in the aerospace field, can solve the problems of increased weight of power supply equipment, large satellite impact, and low reliability, and achieve the effects of avoiding superposition and amplification, small working impact, and high synchronization
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[0091] see figure 1 , the mechanism-type separation nut 1 of this embodiment includes the following components:
[0092] The central bearing rod 11 is a rod-shaped structure, and the upper end of the top is provided with an external hexagonal reaction moment loading interface; the middle section of the structure is a threaded section, which is connected to the satellite side structure through nuts; the lower section is an inner concave section, the upper side of the notch is a horizontal plane, and the lower side is The oblique cone surface has the function of guiding and positioning, and is used for the embedding of multi-lobes 12 to realize the limitation and connection;
[0093] Multi-petal 12, which is composed of four sub-petals cut by annular petals. The inner contour of the petals is consistent with the concave mating surface 1101 of the central bearing rod 11. The upper surface is a horizontal plane, and the lower surface is a conical surface. The structure is embedde...
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