SYSTEMS AND METHODS FOR VERTICAL TAKEOFF AND LANDING VEHICLE WITH STATOR STABILIZATION

SYSTEMS AND METHODS FOR VERTICAL TAKEOFF AND LANDING VEHICLE WITH STATOR STABILIZATION

A system can include a stator and a rotor. The system can include one or more components coupled with at least one of the stator or the rotor. The one or more components can mitigate or dampen a misalignment (e.g., displacement) between the stator and the rotor. The one or more components can includ...

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Bibliographische Detailangaben
Hauptverfasser: LEMBKE, Torbjörn, O'REGAN, Peter, ELVANDER, Josh, RANDALL, Roderick, CONCIA, Bernardo, RANDALL, Ian
Format: Patent
Sprache:eng ; fre
Schlagworte:
AEROPLANES
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
COSMONAUTICS
DYNAMO-ELECTRIC MACHINES
ELECTRICITY
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
GENERATION
HELICOPTERS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:A system can include a stator and a rotor. The system can include one or more components coupled with at least one of the stator or the rotor. The one or more components can mitigate or dampen a misalignment (e.g., displacement) between the stator and the rotor. The one or more components can include at least one component between the stator and a vehicle body. The one or more components can include one or more of a spring, a mass, a damper, or an elastomer. L'invention concerne un système pouvant comprendre un stator et un rotor. Le système peut comprendre un ou plusieurs composants couplés au stator et/ou au rotor. Le ou les composants peuvent atténuer ou amortir un désalignement (par exemple, un déplacement) entre le stator et le rotor. Le ou les composants peuvent comprendre au moins un composant entre le stator et un corps de véhicule. Le ou les composants peuvent comprendre un ou plusieurs éléments parmi un ressort, une masse, un amortisseur ou un élastomère.