DEVICE FOR COOLING ROTOR BLADES OF GAS TURBINE

FIELD: transport engineering; aircraft engines. SUBSTANCE: disk 2 is provided with ring manifold 7 with pipes 8 according to number of passages 3 in disk 2. Manifold 7 has chamber 9 open on side of disk 2. Injectors 6 are oriented towards chamber 9 and pipes 8 are oriented towards passages 3. Inject...

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Bibliographische Detailangaben

Hauptverfasser:	Iskakov K.M, Shatalov Ju.S, Ryzhov A.A, Gepshtejn F.S, Skiba V.V
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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