GAS-TURBINE

A gas turbine has outer and the inner bodies, a shaft, a disc with working bodies installed on it, separate blades and a flow separator. Additionally it has floating unit installed on the shaft of the turbine and slide connected to the floating unit and installed in the channel of the flow separator...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	ZHEMANIUK PAVLO DMYTROVYCH, BOHUSLAIEV VIACHESLAV OLEKSANDROVYCH, DYKYI HRYHORII PETROVYCH, DOLMATOV DMYTRO ANATOLIIOVYCH, DOLMATOV ANATOLII IVANOVYCH, VOLKOV IHOR VOLODYMYROVYCH
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS 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 gas turbine has outer and the inner bodies, a shaft, a disc with working bodies installed on it, separate blades and a flow separator. Additionally it has floating unit installed on the shaft of the turbine and slide connected to the floating unit and installed in the channel of the flow separator with possibility of displacement according to the change of the position of the executive bodies with respect to the flow separator.