GAS-TURBINE UNIT COOLING DEVICE

electrical engineering. SUBSTANCE: gas-turbine unit has fan assembly and annular header with holes facing turbine surface being cooled which accommodate variable rectangular-section nozzles whose outlet sections are made in the form of slits. EFFECT: reduced power requirement. 2 dwg

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Bibliographische Detailangaben
Hauptverfasser:	MITIN E.M, KARANDASHOV B.M, SOKOLOVSKIJ M.I, KISLITSYN G.F
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	electrical engineering. SUBSTANCE: gas-turbine unit has fan assembly and annular header with holes facing turbine surface being cooled which accommodate variable rectangular-section nozzles whose outlet sections are made in the form of slits. EFFECT: reduced power requirement. 2 dwg