Reaction-jet turbine

A reaction-jet turbine has a rotor 1 in the form of a shaft 2 having at least one axial passage 3, and at least one gas dynamic supply device in the form of a supply pipe 17 positioned coaxially with the shaft in a spaced relation delta to the end thereof. At least one jet pipe 10 is cantilevered to...

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Bibliographische Detailangaben
Hauptverfasser:	SERGEI KONSTANTINOVICH KOROLEV, NIKOLAI DMITRIEVICH FEDORENKO, VLADIMIR PETROVICH ENA, VADIM VASILIEVICH SAYAPIN, PAVEL PAVOLICH PRIKHODCHENKO, VIKTOR IVANOVICH LITVINENKO, VLADIMIR VIKTOROVICH PSAREV, JURY LEONIDOVICH RUKHLOV, IRINA ALEXANDROVNA MAROCHKINA
Format:	Patent
Sprache:	eng
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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Beschreibung
Zusammenfassung:	A reaction-jet turbine has a rotor 1 in the form of a shaft 2 having at least one axial passage 3, and at least one gas dynamic supply device in the form of a supply pipe 17 positioned coaxially with the shaft in a spaced relation delta to the end thereof. At least one jet pipe 10 is cantilevered to the shaft 2 and has at the distal end thereof a thrust nozzle 12 communicating with an end inlet 5 of the axial passage 3 so as to form a continuous gas duct. The outlet portion of the supply pipe 17 is made in the form of a supply nozzle 19 having the minimum cross-sectional area thereof which is smaller than the minimum cross-sectional area of the thrust nozzle 12, the ratio between these areas being chosen to ensure a shock wave in the entry zone of the axial passage 3 of the shaft 2.