EXHAUST EDUCTOR COOLING SYSTEM

A method and apparatus for cooling the heat generated by a gas turbine engin e mounted in a compartment is provided. The apparatus comprises a novel eductor (60) that incorporates a mixer nozzl e (70) to entrain sufficient air flow through the com- partment to provide all the necessary cooling. The...

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Bibliographische Detailangaben
Hauptverfasser:	KENZLER, KURT T, DAVIS, THOMAS W, SHEORAN, YOGENDRA Y, SCHMITTENBERG, MARC, LYON, CRAIG A, ROYALTY, CHARLES M
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS
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