TURBINE-ASSISTED CABIN AIR COMPRESSOR

An airplane is provided. The airplane includes a motor-driven compressor assembly (120). The motor-driven compressor assembly includes a shaft (216), a motor (212), a compressor (210), and a turbine (214) coupled to the compressor via the shaft. The motor provides a first power to the compressor via...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
1. Verfasser:	DeFrancesco, Gregory L
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	An airplane is provided. The airplane includes a motor-driven compressor assembly (120). The motor-driven compressor assembly includes a shaft (216), a motor (212), a compressor (210), and a turbine (214) coupled to the compressor via the shaft. The motor provides a first power to the compressor via the shaft. The turbine receives and expands a second medium to provide a second power to the compressor via the shaft. The compressor receives and compresses a first medium in accordance with the first power provided by the turbine and the second power provided by the motor.