An undercarriage unit is provided. The undercarriage unit comprises: a rotatable wheel; at least one electromagnet for releasably coupling the undercarriage unit to the aircraft; a switch for selectively activating and deactivating the at least one electromagnet; and a controller arranged to actuate the switch. An aircraft having the undercarriage unit is also provided.
AIRCRAFT UNDERCARRIAGE
2024-02-22
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
British Library Conference Proceedings | 1997
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