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Abstract
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.
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Details
1 Baltic State Technical University «VOENMEH» named after D.F. Ustinov, 1, 1st Krasnoarmeyskaya st., Saint-Petersburg, Russia
2 Branch of PJSC «UEC-UMPO», Experimental design Bureau named after A. Lyulka, 13, Kasatkina st., Moscow, Russia
3 JSC «UEC Klimov», 11, Kantemirovskaya st., Saint-Petersburg, Russia
4 Laser Systems JSC, constr. 1, bld. 2, 28, Svyazi st., Strelna, Saint-Petersburg, Russia