Development of an algorithm for calculating the energy concentration of infrared optical systems taking into account the charge flow effect in a photodetector array

2020 ◽  
Vol 87 (9) ◽  
pp. 506
Author(s):  
D. A. Drygin ◽  
A. B. Ostrun
2007 ◽  
Vol 130 (1) ◽  
Author(s):  
Akiba Segal ◽  
Michael Epstein

The “beam down” optics or “solar tower reflector” has been successfully used recently for testing in different projects at the Weizmann Institute of Science. There are currently sufficient data on this technology to evaluate its upscaling for commercial uses. The sizing of a tower reflector (TR) is directly linked to the layout of the heliostat field and the geometry of the ground secondary concentrator (compound parabolic concentrator (CPC)). It depends on its position relative to the aim point of the field, amount of spillage around it, and the allowable solar flux striking the TR. Its position influences the size of the image at the entrance plane of the ground CPC and the spillage around the CPC aperture. The spillage around the CPC is also directly related to the exit diameter of the CPC (equal to the entrance opening of the solar reactor, matching the CPC exit) and therefore linked to the input energy concentration, thermal losses, and working temperature in the reactor. Restrictions on the size of the exit of the CPC can influence the entire design of the optical system. This paper provides the correlations between the main design parameters and their sensitivity analysis. These correlations are based on edge-ray methodology, which provides a quick and sufficiently accurate means for preliminary evaluating large-scale beam down solar plants without the need for detailed design of the heliostat field and considering their errors. The size of the TR and the geometry of the CPC are correlated to the size of the reflective area of the heliostats field (and the power output). Thermal modeling of the TR has been performed, showing the maximum energy flux allowed on the reflector to avoid overheating, using natural cooling to the surrounding air. The current mirrors of the TR are limited to working temperatures of 120–130°C to achieve reasonable lifetime. This parameter must be considered when determining the TR position. A key issue discussed in this paper is the amount of spillage around the CPC entrance. To reduce the spillage losses, one needs to increase the size of the exit aperture (although there are practical limitations to this, e.g., due to the size of the reactor’s window). This, however, reduces the concentration and increases the thermal losses from the reactor and requires optimization work.


2019 ◽  
Vol 18 (2) ◽  
pp. 373-378
Author(s):  
Sergei Vassel ◽  
Natalia Vassel ◽  
Natalia Vertiy ◽  
Vladimir Kovalevskii

Author(s):  
J T Fourie

The attempts at improvement of electron optical systems to date, have largely been directed towards the design aspect of magnetic lenses and towards the establishment of ideal lens combinations. In the present work the emphasis has been placed on the utilization of a unique three-dimensional crystal objective aperture within a standard electron optical system with the aim to reduce the spherical aberration without introducing diffraction effects. A brief summary of this work together with a description of results obtained recently, will be given.The concept of utilizing a crystal as aperture in an electron optical system was introduced by Fourie who employed a {111} crystal foil as a collector aperture, by mounting the sample directly on top of the foil and in intimate contact with the foil. In the present work the sample was mounted on the bottom of the foil so that the crystal would function as an objective or probe forming aperture. The transmission function of such a crystal aperture depends on the thickness, t, and the orientation of the foil. The expression for calculating the transmission function was derived by Hashimoto, Howie and Whelan on the basis of the electron equivalent of the Borrmann anomalous absorption effect in crystals. In Fig. 1 the functions for a g220 diffraction vector and t = 0.53 and 1.0 μm are shown. Here n= Θ‒ΘB, where Θ is the angle between the incident ray and the (hkl) planes, and ΘB is the Bragg angle.


1988 ◽  
Vol 49 (C2) ◽  
pp. C2-343-C2-348
Author(s):  
L. A. LUGIATO ◽  
C. OLDANO ◽  
Kaige WANG ◽  
L. SANTIRANA ◽  
L. M. NARDUCCI ◽  
...  
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