POWER AND CHEMICAL ENGINEERING
The study examines short-diffuser adsorption filters designed to remove pollutants from vapor-gas mixtures. The design process of the flow path of such filters is considered, which includes the stages of determining the parameters of the adsorbent layer, modeling gas-dynamic processes using numerical methods in the ANSYS CFX program and analyzing the results. The numerical studies cover various options for backfilling the adsorbent, including layer profiling and the use of adsorbent with different porosity, which allows us to assess the impact of these factors on the aerodynamic resistance and overall efficiency of the filter. A design algorithm is also proposed that ensures optimal compliance between the adsorbent layer thickness and the local flow velocity, which helps to increase the protective action time of the filter and improve the quality of cleaning.
Among several typical energy storage methods, that flywheel energy storage has advantages such as high instantaneous power, high-performance and long service life, making it perfect secondary energy storage technology for traditional internal combustion engine vehicles. Although some progress has been made in the applied research of flywheel energy storage technology, there are no detailed studies at home and abroad that summarize its application in the vehicle applications. This paper searches the data on «flywheel energy storage», analyzes the research progress of flywheel energy storage in automotive industry, and analyzes the research progress of flywheel energy storage in vehicle applications. The search data show that flywheel energy storage technology for the vehicle applications has been studied for the last 20 years, although it is a niche research area. With respect to two typical flywheel hybrid systems, namely electric and mechanical drive, we have focused on the history of the study, research and validation of mechanical flywheel hybrid system in the automotive industry, as well as the structural characteristics of this system, the current state of research and future research trends.
AVIATION AND ROCKET-SPACE ENGINEERING
The paper presents a methodology for designing a small spacecraft to perform the tasks of technological processes in near-Earth space. When designing such a small spacecraft, it is assumed that it will be equipped with a microgravity platform to meet the requirements for micro-accelerations. The methodology is based on the principles of individuality, attainability and controllability. They guarantee the maximum possible consideration of the features of the gravity-sensitive process being implemented, including compliance with the requirements for limiting the micro-acceleration module in the working area of technological equipment and effective control of this implementation. The developed technique can be used in the design of a small spacecraft for technological purposes.
The research experimentally investigates the occurrence of technological elastic deformations of the central holes of gears of low technological rigidity (non-rigid gears) caused by their fixation in 3-cam self-centering cartridges. The authors present an experimental comparison of the attachment scheme by the involute with the scheme by the external diameter. Moreover, the graphs of distortion of the hole shape from roundness as a function of the torque applied to the wrench handle were plotted. The least squares method was used to confirm the assumed linear dependence of the graphs of hole shape distortion from roundness as a function of the tightening torque applied to the wrench handle. The authors compare the results obtained by the experiment with the obtained earlier using computer modeling, the adequacy of computer models and the reliability of the experimental results. Experimentally it was determined that at fixing by involute there is on 30,23 % less value of hole shape distortion from roundness in comparison with the scheme of fixing by external diameter. As a result, the scheme of fixing by involute with a gear of low technological rigidity is the best in terms of hole shape distortion from roundness in comparison with the scheme of fixing by external diameter.
The scientific novelty is to investigate the influence of clamping forces on the hole shape distortion of
a gear of small technological rigidity when fixed by its external diameter and involute in a 3-cam self-centring chuck. The resulting data allows scientifically justifying assignment of parameters of clamping devices in the production of gears of small technological stiffness used in aeronautical vehicles.
MATERIAL SCIENCE AND PROCESSING TECHNOLOGY
ISSN 2587-764X (Online)
















