A
laser radar device used for aircraft carrying comprises a main
machine shell, an aircraft connecting base is arranged on the outer side of the main
machine shell, the main
machine shell comprises a main machine cover body and a main machine shell body, a
laser, an emergent light adjusting
assembly and a scanning
assembly are arranged in the main machine shell, the scanning
assembly comprises a rotatable
tower mirror, and the main machine cover body is provided with a transparent window mirror. The
laser emits pulse
laser beams, the angles of the pulse
laser beams are adjusted through the emergent light adjusting assembly and then reach the scanning assembly, and the
laser beams are reflected by the scanning assembly and then penetrate through the window mirror to reach the outside. The laser is reflected by a target, penetrates through the window mirror, reaches the
tower mirror, is reflected to the light gathering cover and is finally gathered to the light receiving plate; an L-shaped
air channel is arranged in the main machine shell, air enters from one end of the L-shaped
air channel, air exits from the other end of the L-shaped
air channel, and the problems that a traditional laser
radar structure is high in wind resistance, heavy in weight and unsmooth in heat dissipation are solved.