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32results about How to "High lightweight" patented technology

Space remote sensor support frame made of carbon fiber composite

The invention relates to a space remote sensor support frame made of carbon fiber composite, comprising a horizontal lifting ring, a remote sensor support frame body and a vertical lifting ring. The remote sensor support frame body is formed into a three-dimensional grid-like structure by a closed shell, internally peripherally radiating reinforcing ribs and axially parallel reinforcing ribs. Theshape of the inner side wall of the shell corresponds to the shape of a space remote sensor; the outer side wall of the shell comprises an circular-arc shaped plate, a left vertical plate, a right vertical plate, a front plate, a rear plate and a bottom plate; the left vertical plate is connected with the bottom plate through a left horizontal plate and a left inclined plate; the right vertical plate is connected with the bottom plate through a right horizontal plate and a right inclined plate; the space remote sensor is fixedly connected with a round flange of the remote sensor support framebody; and the horizontal lifting ring and the vertical lifting ring are connected with the remote sensor support frame body through pre-buried components. The space remote sensor support frame made of carbon fiber composite has a light weight, high structural strength and high lightweight rate and can be applied to the space remote sensing field and the rocket, aviation and machinery industries.
Owner:CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI

Design method of large caliber optics telescope four way structure and obtained four way structure

The invention discloses a design method of a large caliber optics telescope four way structure and the obtained four way structure, relates to the machinery industry photoelectric instrument field, and solves the problems that an existing design method of an existing four way structure is long in product design period and the existing four way structure is low in structure lightweight rate. The design method of the large caliber optics telescope four way structure includes steps: building a four way structure initialization geometric model of the large caliber optics telescope four way structure, using a finite element method to build a finite element simulation model of the large caliber optics telescope four way structure in dispersion mode, using four way material distribution as an optimization design variable and setting reduction of the weight of the existing four way structure as an optimization objective under an optimization constraint condition which meets displacement deformation, using a topological optimization method to perform weight reduction optimization on the finite element simulation model, performing distribution design on a shell plate, an inner rib plate and an inner circle plate and confirming the initial thicknesses of the shell plate, the inner rib plate and the inner circle plate, using the initial thicknesses of the shell plate, the inner rib plate and the inner circle plate as another optimization design variable to perform the weight reduction optimization twice, and performing rigidity performance analysis verification to obtain the lightweight four way structure which meets performance constraint. The maximum deformation value of the obtained four way structure is 0.0698mm, and less than the maximum design deformation value 0.08mm, and the weight of the obtained four way structure is reduced from 122.217t to 13.776t, and furthermore the lightweight rate of the obtained four way structure reaches 89%.
Owner:CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI

Light space camera main force-bearing device with focusing function

A light space camera main force-bearing device with a focusing function belongs to the technical field of space optical remote sensing. The problem that the requirements for the quality and assembly of parts are high and the envelope size and quality of effective loads are increased due to the fact that a focusing mechanism needs to be independently designed to achieve camera focusing in the priorart is solved. A main force-bearing back plate is coaxially and fixedly connected to the bottom end of a lower circular ring structure. A primary mirror of a camera is arranged on the main force-bearing back plate, and a secondary mirror of the camera is arranged on an upper circular ring structure. The linear expansion coefficient characteristic of the material of a main force-bearing truss andthe linear expansion coefficient characteristic of the material of the main force-bearing back plate are matched. Heat conducting films are respectively adhered to the outer wall of the lower circularring structure and each truss rod, and a thermistor and a plurality of heating sheets are adhered to each heat conducting film. Through cooperative use of the heating sheets, the thermistors and theheat conducting films and through the main force-bearing truss and the main force-bearing back plate with matched material linear expansion coefficients, camera focusing is realized.
Owner:CHANGGUANG SATELLITE TECH CO LTD

A light-weight space camera main bearing device with focusing function

The utility model relates to a light space camera main force bearing device with a focusing function, which belongs to the technical field of space optical remote sensing. The invention solves the problems in the prior art that the focusing mechanism needs to be separately designed to realize the camera focusing, which leads to higher requirements on the quality and assembly of the parts, and meanwhile increases the envelope size and quality of the payload. The main load-bearing backplane is coaxially fixed at the bottom of the lower ring structure, the primary mirror of the camera is installed on the main load-bearing backplane, the secondary mirror of the camera is installed on the upper ring structure, the material of the main load-bearing truss and the main The characteristics of the linear expansion coefficient of the load-bearing backboard material match, and the outer wall of the lower ring structure and each truss rod are respectively pasted with a heat-conducting film, and each heat-conducting film is pasted with a thermistor and several heating sheets. Through the combined use of heaters, thermistors, and heat-conducting films, combined with the main load-bearing truss and main load-bearing back plate with matching material linear expansion coefficients, the camera focus is realized.
Owner:CHANGGUANG SATELLITE TECH CO LTD

Lightweight reflector structure based on additive manufacturing technology

PendingCN114252944AWarranty Strength RequirementsOvercome the problem of not being able to processMirrorsMountingsManufacturing technologyEngineering
The invention provides a lightweight reflecting mirror structure based on an additive manufacturing technology, which belongs to the technical field of optical manufacturing and comprises a mirror surface, a lightweight supporting structure for supporting the mirror surface, an outer frame for mounting and fixing the mirror surface and a back plate, the lightweight supporting structure is positioned in a space surrounded by the mirror surface, the outer frame and the back plate, and consists of a plurality of truss groups which are uniformly arranged on the back plate; the lightweight supporting structure is prepared by adopting an additive manufacturing technology. According to the light-weight reflecting mirror structure based on the additive manufacturing technology, the mirror body is designed in a back plate closed mode, internal truss design is adopted for light weight, the machining means is additive manufacturing, and truss structures commonly used in additive manufacturing and constructional engineering are introduced into the light-weight reflecting mirror, so that the strength requirement of the mirror body is met, and the service life of the light-weight reflecting mirror structure is prolonged. And the lightweight rate is further improved, and the problem that machining cannot be conducted through a traditional material reduction machining means is solved.
Owner:CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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