FIELD: engines and pumps.
SUBSTANCE: gas turbine engine with a pulsed operation comprises symmetrically disposed combustion chambers with entrance and exit windows over them adjacent to the rotor disk end. The rotor disk is formed circumferentially opposite to open windows of chambers with a dull side, cavity with turbine blades, purge window and the message channel, there are through windows in the disk, and from the opposite side, exhaust pipes are adjacent thereto.
EFFECT: increased reliability.
3 dwg
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