3results about How to "Affect image quality" patented technology

The utility model belongs to the technical field of optical equipment, and discloses a feeding and discharging device and a lens detecting and curing device, which comprise a detecting table, a measuring mechanism and a curing mechanism, an adjusting box is fixedly connected behind the top of the detecting table, a first gear is arranged in the adjusting box, and a first rotating shaft is fixedly connected in the first gear; a movable rod is fixedly connected to the front face of the first rotating shaft, a curing mechanism is arranged on the front face of the movable rod, a measuring mechanism is fixedly connected to the top of the curing mechanism, a supporting plate is fixedly connected to the top of the movable rod, and a first electric push rod is arranged on the left side of the supporting plate. The top and the bottom of the first electric push rod rotate respectively, vertical angle adjustment of the measuring mechanism and the curing mechanism is achieved, the phenomenon that distortion remarkably influences imaging quality and deviation is avoided, the phenomenon that the straightness error and the perpendicularity deviation of the two shafts are amplified due to the fact that the angles cannot be adjusted when the workbench moves is avoided, and then the detection precision is improved.

The low-inertia optical satellite configuration comprises a satellite body, a camera and a solar wing, the satellite body is of a hexagonal prism structure, the two axial end faces of the hexagonal prism structure are the ground facing face and the sky facing face respectively, the interior of the satellite body is divided into a platform cabin and a load cabin through a middle partition plate, and the platform cabin is arranged close to the sky facing face; the load cabin is arranged close to the ground; one part of the camera is mounted on a middle partition plate of the load cabin, and the other part of the camera extends out of the ground; the two opposite side faces of the satellite body are solar wing installation faces, solar wings are installed on the solar wing installation faces, and the solar wings are unfolded in the direction perpendicular to the central axis of the hexagonal prism structure after being unlocked and opened from the solar wing installation faces where the solar wings are located. According to the low-inertia optical satellite configuration, the camera is installed in the load cabin and half sinks in the satellite cabin, the solar wings of the satellite body are symmetrically arranged on the two opposite sides of the satellite body in a two-dimensional unfolding mode, and by means of the configuration, the rotational inertia of the satellite in orbit can be reduced.