Supply of air to an air-conditioning circuit of an aircraft cabin

Aircraft turboprop engine 110, comprising at least one low-pressure body 12 and one high-pressure body 14, the low-pressure body driving a thrust propeller by means of a gearbox 16, the turboprop engine further comprising means for supplying air to an air-conditioning circuit of an aircraft cabin. T...

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Bibliographische Detailangaben

Hauptverfasser:	Marc Missout, Julien Alexis Louis Ricordeau
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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