PROCEDE ET DISPOSITIF DE REFROIDISSEMENT D'AUBES DE TURBINE

In one form of the present invention, turbine cooling air is modulated as a function of engine speed, altitude, and blade temperature.

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Bibliographische Detailangaben
1. Verfasser:	FREDERICK JOHN PINEO ET JOSE THOMAS ALVAREZ
Format:	Patent
Sprache:	fre
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:	In one form of the present invention, turbine cooling air is modulated as a function of engine speed, altitude, and blade temperature.