Memory alloy planet detection lander based on negative poisson ratio structure
A technology of memory alloy and negative Poisson's ratio, which is applied in the direction of the landing device of the spacecraft and the system for the return of the spacecraft to the Earth's atmosphere, etc. problems, to achieve the effect of being conducive to safe landing, enhancing the ability to resist shock and energy absorption, and strong landing buffer performance
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[0048] In order to better explain the present invention and facilitate understanding, the present invention will be described in detail below through specific embodiments in conjunction with the accompanying drawings.
[0049] refer to Figure 1 to Figure 7 , this embodiment provides a memory alloy planetary exploration lander based on a negative Poisson's ratio structure, including a lander body 9 and a buffer structure 1 .
[0050] The main body 9 of the lander is a cylindrical structure with a closed bottom, and its interior is used to accommodate payloads (including scientific instruments such as cameras and communication antennas).
[0051]The buffer structures 1 are connected to the side wall of the main body 9 of the lander at equal intervals in the circumferential direction.
[0052] The buffer structure 1 includes: a mechanical leg assembly 2 , a main shock absorber 5 and a foot pad 4 .
[0053] The mechanical leg assembly 2 includes a landing leg 21, which is a mem...
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