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544results about How to "Reduce reflection loss" patented technology

Efficient solar energy thermal absorber based on optical-thermal absorbing cone structure

The invention relates to an efficient solar energy thermal absorber based on an optical-thermal absorbing cone structure. The efficient solar energy thermal absorber based on the optical-thermal absorbing cone structure comprises a sealing cover, an insulating tube sleeve, an airflow tube, a thermal absorbing body, a glass cover and a thermal absorbing fastening piece. The efficient solar energy thermal absorber is characterized in that the thermal absorbing body is in a truncated prism structure and each plane can be manufactured separately. Each plane is respectively an optical-thermal absorbing conic board, a plurality of sharp pyramids are distributed on a surface of each plane and each plane is made of a high thermal conductive porous material. The glass cover is in a circular truncated cone shape. A closed containing cavity is formed by the sealing cover, the thermal absorbing body and the glass cover. Air enters into the containing cavity through an air inlet of the sealing cover and is heated through each porous medium optical-thermal absorbing conic board so that solar energy is taken and finally flows out from an outlet end of the thermal absorber along the airflow tube. The efficient solar energy thermal absorber based on the optical-thermal absorbing cone structure has the advantages of solving the problems that an existing thermal absorber is low in thermal absorbing efficiency, difficult to process, large in loss in inner flow and the like, being used independently and in a combined mode through connectors, being mainly applicable to a solar energy thermoelectric conversion system and guaranteeing efficient operation of the system.
Owner:南京凌日星能源科技有限公司

Millimeter wave band broadband cylinder conformal 4*4 microstrip antenna as well as design method thereof

A millimeter wave band broad band column conformal 4*4 micro-band antenna and design method thereof relate to an antenna and design method thereof. For the purpose that the column conformal4 micro-band antenna for aviation, spaceflight, ship and surface car can stably work under frequency of 35GHz, the antenna is equipped with a sheet sticking layer(5), a first medium layer, a second medium layer, a middle floor(10) equipped with a H-shape groove(7), and a feeding network layer(6). The design method includes: designing a planar 4*4 micro-band antenna array with the H-shaped groove (7)in CST through coupling feeding micro-band antenna units by utilizing the H-shaped groove(7), drawing columns with different radius and different material, reducing column type carriers(2) with different thickness by utilizing ''substrate'' function, stretching the two medium layers, the feeding network layer(6), the middle floor(10) and the sheet sticking layer(5) to the column type carriers(2), fetching intersection of the two by utilizing ''intersect'' to conformally arrange the planar array on the column type carriers(2). The micro-band antenna for aviation, spaceflight, ship and surface car can stably work under frequency of 35GHz, and design method is simple.
Owner:HARBIN INST OF TECH

Coupling structure with silicon nanowire waveguide and fiber and manufacturing method thereof

The invention discloses a coupling structure with a silicon nanowire waveguide and a fiber and a manufacturing method thereof. The coupling structure comprises a first silicon dioxide waveguide beingan input waveguide, a tapered silicon dioxide waveguide, a second silicon dioxide waveguide, a silicon dioxide flat-panel structure, a tapered silicon waveguide, and a silicon output waveguide. One side of the tapered silicon dioxide waveguide is connected with the first silicon dioxide waveguide and the dimension of the cross section is reduced gradually along the light transmission direction; the second silicon dioxide waveguide is connected with the other side of the tapered silicon waveguide and the dimension of the cross section of the second silicon dioxide waveguide is smaller than thatof the first silicon dioxide waveguide; the silicon dioxide flat-panel structure is connected with the second silicon dioxide waveguide; the tapered silicon waveguide coated by the second silicon dioxide waveguide is arranged at a symmetric axis of the second silicon dioxide waveguide and has the cross section with the dimension extending gradually along the light transmission direction; and thesilicon output waveguide coated by the silicon dioxide flat-panel structure is arranged at a symmetric axis of the silicon dioxide flat-panel structure and is connected with the tapered silicon waveguide. The simple coupling structure is designed to be convenient and is manufactured easily with low cost; and large-scale production and application of the coupling structure can be realized easily.
Owner:INST OF SEMICONDUCTORS - CHINESE ACAD OF SCI
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