Applicable to the lower end frame structure of the satellite bearing tube
A load-bearing cylinder and frame structure technology, which is applied to artificial satellites, space navigation equipment, space navigation aircraft, etc., can solve the problem of heavy weight of the lower end frame, and achieve a simple structure, low structural weight, and strong practicability Effect
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[0037] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will facilitate further understanding of the present invention in any form of techniques, but will not limit the invention in any form. It should be noted that several variations and improvements can also be made without departing from the concept of the present invention. These are all of the scope of protection of the present invention.
[0038] The present invention provides a lower frame structure suitable for use in satellite holders, such as figure 1 , figure 2 As shown, including the lower end frame and the carrier cylinder connection section 1, the lower end frame and the carrier connection section 2, and the connecting member; the carrier bobbin connection section 1 of the lower end frame and the lower end frame 1 is connected Parts, the present invention ensures the lower end frame and the carrier barrel connection section (1), the lower end box...
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