An aircraft taxi system (100) includes a controllable voltage AC generator (103) configured to be connected to a power generation turbine shaft (102) and configured to convert rotational energy to electrical energy, wherein the controllable voltage AC generator (103) is configured to output a desired voltage irrespective of a change in a rotational speed of the power generation turbine shaft (102), an AC electric motor (105) configured to rotate at least one wheel of an aircraft landing gear, and an AC bus connecting the controllable voltage AC generator to each of the AC electric motor.
Systems utilizing a controllable voltage AC generator system
Systeme mit steuerbarem Spannungs-Wechselstromgeneratorsystem
Systèmes utilisant un système de générateur CA de tension contrôlable
2015-10-07
Patent
Electronic Resource
English
IPC: | B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / H02P CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS , Steuern oder Regeln von elektrischen Motoren, elektrischen Generatoren, dynamoelektrischen Umformern / B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung |
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