Lidar Mirror Corner Radius for Drag Reduction

The patent applies curvature by rounding the corners of the mirror assembly with a radius of curvature of at least 0.1 mm. This curved geometry reduces aerodynamic drag by minimizing turbulence and vortex formation at the corners during high-speed rotation, thereby reducing energy loss while maintaining the required rotation speed for rapid environmental scanning.

The patent changes the geometric parameters of the mirror assembly by implementing rounded corners with specific radius values (at least 0.1 mm, optionally 0.1-1.0 mm, or up to 2.0 mm). This parameter modification optimizes the aerodynamic characteristics, reducing drag coefficients and allowing the system to maintain high rotation speeds with reduced energy consumption.

The patent implements rounded corners with a radius of curvature of at least 0.1 mm, which can be achieved through standard manufacturing processes such as CNC machining, molding, or polishing. This moderate level of curvature significantly reduces aerodynamic drag and dynamic pressure at high rotation speeds while remaining compatible with conventional manufacturing methods, thus maintaining ease of manufacture.

The patent specifies optimal parameter ranges for the corner radius (at least 0.1 mm, optionally 0.1-1.0 mm, or up to 2.0 mm) that balance manufacturing simplicity with aerodynamic performance. These parameter specifications allow manufacturers to achieve the desired drag reduction using standard production techniques without requiring complex or expensive manufacturing processes.