INERTIAL MEASUREMENT MODULE, SHOCK ABSORPTION SYSTEM, AND UNMANNED AERIAL VEHICLE
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United States of America
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Issued Date -
Apr 10, 2025
app pub date -
Dec 18, 2024
filing date -
Dec 18, 2024
priority date (Note) -
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Abstract
Embodiments of the present invention are an inertial measurement module, includes a mount, a circuit board, an inertial measurement assembly, a thermally conductive member and a counterweight assembly. The circuit board is mounted to a surface of the mount. The inertial measurement assembly includes a thermal resistor and an inertial measurement unit. The thermally conductive member is configured to abut against the thermal resistor and the inertial measurement unit. The counterweight assembly is mounted to the surface of the mount. A first groove is arranged on an end surface of the counterweight assembly facing the mount. A receiving space is formed by the first groove and the end surface of the mount. The thermally conductive member and the inertial measurement assembly are both received in the receiving space. The thermally conductive member is arranged at a preset distance from a bottom of the first groove.
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