Open AccessIMPROVING THE DESIGN OF THERMAL TOOLS FOR ROCK FRACTURING
Author(s) -
Vitaly Povetkin,
Alfiya Nurmukhanova,
Amina Bukayeva,
Жаннур Бегендикова
Publication year - 2021
Publication title -
m. tynyšbaev atyndaġy k̦azak̦ kôlìk ža̋ne kommunikaciâlar akademiâsynyn̦ habaršysy/k̦azkka habaršysy
Language(s) - English
Resource type - Journals
eISSN - 2790-5802
pISSN - 1609-1817
DOI - 10.52167/1609-1817-2021-117-2-13-20
Subject(s) - nozzle , combustor , jet (fluid) , mechanics , gas burner , torch , mechanical engineering , combustion , thermal , shock wave , discharge coefficient , flow (mathematics) , detonation , coaxial , materials science , engineering , explosive material , chemistry , physics , thermodynamics , welding , organic chemistry
The article deals with the main parameters of the thermodynamic working device for rock destruction due to the implementation of a new method of fuel mixture combustion in shock waves initiated by a high-speed torch burner in gas-dynamic combustion intensifiers. A device for thermal destruction of rocks has been developed, which belongs to the mining industry and can be used for directed impact on rocks when they are destroyed by hot gas jets in mining, stone processing and construction industries. Also, installed coaxial to the nozzle, with increasing inside diameter, a cylindrical nozzle, with two cascades of ejection holes - the first cascade is made at a distance from the Laval nozzle, equal to the distance to complete expansion of the jet of the torch, then, the accelerating section of the nozzle and the new, formed by burning the unburned fuel, jet of the burner. It is found that the cross sectional area of the inner hole of the cylindrical nozzle, is made with an excess of the area of the critical cross section of the nozzle Laval burner 2.5-3 times, in which, because of the rapid expansion of the gas flow in the nozzle, there is turbulization, with the formation of a powerful zone of heating of the gas flow and the appearance of a standing detonation wave in it. The drilling angle of the ejection holes of the first stage is 45-50º to the axis of the nozzle, which serves for ejection of atmospheric air, the oxygen of which reacts with the surplus of combustible in the main jet of the burner and the formation of a more powerful jet.