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35 results about "Foldscope" patented technology

A Foldscope is an optical microscope that can be assembled from simple components, including a sheet of paper and a lens. It was developed by Manu Prakash and designed to cost less than US$1 to build. It is part of the "frugal science" movement which aims to make cheap and easy tools available for scientific use in the developing world.

Projection device for changing imaging effect through light refraction

The invention relates to the technical field of projection equipment. The invention further discloses a projection device for changing the imaging effect through light refraction. The device comprisesa shell, a telescopic rod is movably connected to the surface of the shell, a folding mirror is movably connected to the surface of the telescopic rod, a flexible screen is fixedly connected to the surface of the folding mirror, a toothed plate is movably connected to the interior of the shell, an extrusion plate is movably connected to the surface of the toothed plate, an elastic cover is movably connected to the surface of the extrusion plate, and a compression spring is movably connected to the interior of the elastic cover. If the range of the video projected at the moment is too small, the extrusion plate can be pushed to move towards two sides, and the extrusion plate meshes the toothed plate to push the shell to rotate away, and drives the folding mirror to rotate to the state shown in the figure 8. When the folding mirror is unfolded, the spring rod pushes the lamp source to move in the direction close to the folding mirror. In the moving process, it is known that the maximumprojection picture is enlarged from the maximum projection picture, and therefore the effect of changing the shape of the convex lens and the focal length to enlarge the projection picture is achieved.
Owner:杭州新五板全息科技有限公司

Long-focal-length large-view-field miniaturized active athermalization optical system

PendingCN113805325AHigh resolutionWide temperature range operationOptical elementsImaging lensOptic system
The invention discloses a long-focal-length large-view-field miniaturized active athermalization optical system which comprises a Cassegrain reflection primary mirror, a reflection secondary mirror, a field lens, a collimating mirror, a first folding mirror, a second folding mirror, a first imaging mirror group, a third folding mirror, a second imaging mirror group, a fourth folding mirror, an imaging lens and a detector focal plane. The Cassegrain reflection primary mirror and the reflection secondary mirror form a Cassegrain imaging system, the field lens is arranged between the Cassegrain reflection primary mirror and the reflection secondary mirror, and the field lens is used for compressing the field angle of the collimating mirror and correcting the field curvature of the imaging system; and the collimating lens, the first folding lens, the second folding lens, the first imaging lens group, the third folding lens, the second imaging lens group, the fourth folding lens, the imaging lens and the detector focal plane are sequentially connected through light paths. The system can work in a wide temperature range, the cost of the system is reduced, meanwhile, the space structure of the system is optimized through the turning mirror, and miniaturization is achieved.
Owner:AEROSPACE SCI & IND MICROELECTRONICS SYST INST CO LTD

Optical turbulence sensor and method for combining multi-aperture glitter and differential image motion

The invention discloses an optical turbulence sensor and a method for combining multi-aperture glitter and differential image motion. The optical turbulence sensor consists of a Febry lens, an exit pupil splitting mirror component, a CCD (charge coupled device) image sensor and a computer, and is characterized in that the Febry lens is used for matching an entrance pupil of a small telescope, so that the exit pupil is positioned on the exit pupil splitting mirror component; a combination focus of the Febry lens and the small telescope is positioned at a field diaphragm; an openable reflecting mirror, the field diaphragm with a through hole at the center, and the exit pupil splitting mirror component U1 are sequentially mounted on the same optical axis behind the Febry lens; a grid partitioning board and a field eye lens are arranged on a reflecting optical axis of the openable reflecting mirror; a folding mirror and the CCD image sensor are sequentially arranged on a reflected light path of the exit pupil splitting mirror component; the output end of the CCD image sensor is connected with the computer. Field installation and field adjustment of a system are facilitated; optical and mechanical structures are greatly simplified; influence from external vibration is avoided, so that the field installation and the field adjustment are facilitated and the reliability is greatly improved.
Owner:NANJING INST OF ASTRONOMICAL OPTICS & TECH NAT ASTRONOMICAL OBSE

Optical remote sensor using structural deformation amount to compensate misalignment rate of optical system

The invention discloses an optical remote sensor using structural deformation amount to compensate the misalignment rate of an optical system. The optical remote sensor using the structural deformation amount to compensate the misalignment rate of the optical system includes a primary mirror, a secondary mirror, a folding mirror, a beam splitter, a triple mirror, a main bearing frame and an elastic supporting rod; the main bearing frame includes a front mounting surface and a rear mounting surface back to the front mounting surface; the primary mirror is elastically mounted on the front mounting surface; the secondary mirror is elastically connected to one end of the supporting rod and opposite to the primary mirror in a spaced manner; the end of the supporting rod away from the secondarymirror is connected to the front mounting surface; the folding mirror and the beam splitter are mounted on the rear mounting surface; and the triple mirror is mounted on the rear mounting surface andopposite to the beam splitter in a spaced manner. By means of the optical remote sensor using the structural deformation amount to compensate the misalignment rate of the optical system, the primary mirror and the secondary mirror deviate from the theoretical position by the deformation amount under the action of gravity, so that the best pose of the primary mirror and the secondary mirror is adjusted under the gravity of the ground; after the space remote sensor launches into orbit and gravity deformation rebound release occurs, the position relationship between the primary mirror and the secondary mirror can still maintain the position relationship during adjustment, and the image quality of the space remote sensor is not affected.
Owner:CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI

Bearing cylinder type main supporting structure of large off-axis three-mirror space remote sensing camera

The invention discloses a bearing cylinder type main supporting structure of a large off-axis three-mirror space remote sensing camera. The invention relates to the technical field of space optical remote sensing, and solves the problems of low support rigidity and overlarge size envelope of a camera mirror assembly caused by large length-width ratio and large mass of main, third and folding mirrors of a camera due to the characteristics of long focal length and wide field of view of an optical system in the prior art, and the structure comprises a front frame, a rear frame, a main bearing cylinder, a truss rod assembly and a reinforcing rib assembly, the main bearing cylinder is connected with the front frame and the rear frame through screws. The truss rod assembly comprises two truss rods which are symmetrically arranged, the upper end of each truss rod is in positioning connection with the front frame, and the lower end of each truss rod is in positioning connection with the rear frame; the lower end of the reinforcing rib assembly is connected with the main bearing cylinder and the upper end of the reinforcing rib assembly is connected with the front frame through titanium alloy joints; the front frame, the force bearing cylinder, the rear frame and the truss rod joints are all in a plane assembly form, so that the assembly difficulty is greatly reduced, and meanwhile, theproduction period and the manufacturing cost are greatly reduced.
Owner:CHANGGUANG SATELLITE TECH CO LTD

Load-bearing cylinder main support structure of large off-axis three-mirror space remote sensing camera

The main bearing structure of the large-scale off-axis three-mirror space remote sensing camera involves the field of space optical remote sensing technology. It solves the problem of large aspect ratios of the main, third and folding mirrors of the camera due to the characteristics of the long focal length and wide field of view of the existing optical system. Due to the large mass, the supporting rigidity of the camera mirror assembly is low and the size envelope is too large, including the front frame, the rear frame, the main load-bearing cylinder, the truss rod assembly and the rib assembly; the main load-bearing cylinder and the front frame and the rear frame All are connected by screws; the truss rod assembly includes two symmetrically arranged truss rods, the upper end of each truss rod is positioned and connected with the front frame, and the lower end of each truss rod is positioned and connected with the rear frame; And the upper end of the rib assembly is connected with the front frame by a titanium alloy joint; the joints of the front frame, the load-bearing tube, the rear frame and the truss rod of the present invention are all in the form of plane assembly, which greatly reduces the difficulty of assembly, and at the same time greatly reduces the production cycle and manufacturing cost.
Owner:CHANGGUANG SATELLITE TECH CO LTD

Physical experiment table device for optical teaching

The invention discloses a physical experiment table device for optical teaching, which comprises a device main body, a supporting plate and an internal groove, the supporting plate is fixedly connected above the device main body, the internal groove is fixedly connected inside the lower part of the supporting plate, device table legs are fixedly connected to two sides of the bottom of the device main body, and supporting rods are fixedly connected to two sides of the top of the supporting plate. The top of the supporting rod is fixedly connected with an experiment plate, the two sides of the experiment plate are fixedly connected with adjusting plates, the middle of one side of each adjusting plate is fixedly connected with an experiment transverse plate, the top of each experiment transverse plate is fixedly connected with an experiment vertical plate, the interior of each experiment vertical plate is fixedly connected with an adjusting groove, and the front face of the lower portion of each adjusting groove is fixedly connected with an anti-skid layer. The anti-skid layer can well prevent devices from being collided to cause falling of articles, a folding mirror surface can be unfolded, then a light source is reflected through the mirror surface, teaching is better carried out, a bottom pad is soft in texture, friction force between device table legs and the ground can be increased, the physical experiment table device is better stabilized, and the physical experiment table device is prevented from moving easily.
Owner:EASTERN GANSU UNIVERSITY

Optical Remote Sensor Using Structural Deformation to Compensate Optical System Misalignment

An optical remote sensor that uses structural deformation to compensate for the misalignment of an optical system, including a primary mirror, a secondary mirror, a folding mirror, a beam splitter, three mirrors, a main load-bearing frame and an elastic support rod; the main load-bearing frame includes a front mounting surface and the rear mounting surface opposite to the front mounting surface; the primary mirror is elastically installed on the front mounting surface, the secondary mirror is elastically connected to one end of the support rod and is opposite to the primary mirror, and the end of the support rod away from the secondary mirror is connected to the front mounting surface connection; the folding mirror and the beam splitter are installed on the rear installation surface; the three mirrors are installed on the rear installation surface and are opposite to the beam splitter at intervals. The invention makes the primary mirror and the secondary mirror deviate from the theoretical position through the deformation amount under the action of gravity, so that the optimal pose of the primary mirror and the secondary mirror installed under the action of gravity on the ground will be deformed by gravity after the space remote sensor is launched into orbit When the rebound is released, the positional relationship between the primary mirror and the secondary mirror can still maintain the positional relationship during assembly and adjustment, and the imaging quality of the space remote sensor will not be affected.
Owner:CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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