TURBOCOMPRESSOR FOR AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM

A bleed air system (65) for an aircraft includes a turbocompressor (62) including a turbine portion (76) coupled to drive a compressor portion (74). The compressor portion (74) includes a compressor inlet (100) and a compressor air discharge (102). The turbine portion (76) includes a turbine inlet (...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	FEULNER, Matthew R
Format:	Patent
Sprache:	eng ; fre ; 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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