Kühlluft-Übertragungsvorrichtung

An inducer 44 comprising vanes 76 (Fig. 3) receives pressurized cooling air 36 from the engine compressor and directs it in a substantially tangential direction to a radial flow impeller 46 formed by radial passageways (58, Fig. 4) defined between walls 52,54. An air seal 48,50, is provided. Cooling...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	BERTKE, JAMES HERMAN, CINCINNATI, OHIO, US, CORSMEIER, ROBERT JAMES, CINCINNATI, OHIO, US, REIGEL, JAMES ROBERT, CINCINNATI, OHIO, US, LENAHAN, DEAN THOMAS, CINCINNATI, OHIO, US
Format:	Patent
Sprache:	ger
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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