COOLED NOZZLE BLADE OF HIGH-PRESSURE TURBINE OF TURBOJET ENGINE WITH REPLACEABLE NOSE FOR BENCH TESTS

FIELD: aircraft engine construction.SUBSTANCE: invention relates to the field of aircraft engine construction, in particular to bench tests of a gas generator of an aircraft engine or a full-size aircraft engine; it is designed to measure parameters of working fluid behind a combustion chamber (at a...

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Bibliographische Detailangaben

Hauptverfasser:	Bazhin Sergei Vladimirovich, Shmyrin Aleksei Nikolaevich, Fadeev Sergei Ivanovich, Ponosova Natalia Vasilevna
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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