Open AccessCombustion-driven gas-dynamic CO2-laser on the basis of modern aviation engines
Author(s) -
А. С. Борейшо,
M. Yu. Vovk,
A D Edigarev,
И. А. Киселев,
V V Kulalaev,
A V Morozov,
Alexandr Orlov,
П. Г. Смирнов
Publication year - 2020
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1565/1/012021
Subject(s) - turbojet , airplane , aviation , gas turbines , combustion , aerospace engineering , nozzle , automotive engineering , laser , jet engine , propulsion , aeronautics , engineering , mechanical engineering , environmental science , physics , chemistry , organic chemistry , optics
Combination of combustion-driven gas-dynamic lasers with gas-turbine turbojet and turbo-shaft engines has been considered. Development of aviation technologies has been analyzed. Output performance of a laser taking air from modern helicopter and airplane engines taking into account ensuring exhaust of spent active medium into the ambient atmosphere has been determined. The application of penetration cooling of the laser nozzle bank blades has been evaluated.