BLADE FOR GAS TURBINE, IMPLEMENTATION OF TURBINE BLADE AND PROCEDURE FOR TURBINE BLADE COOLING

FIELD: power engineering. ^ SUBSTANCE: gas turbine blade is made with wall of blade positioned on suction side and with wall of blade converging to it in area of back edge and positioned from pressure side. The blade wall positioned on the suction side consists of a neck of the back edge projecting...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: LERNER KRISTIAN, BAL'DAUF SHTEFAN, KHENDLER MIKHEL
Format: Patent
Sprache:eng ; rus
Schlagworte:
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