Lead lag damper for helicopter rotor unit | Patent Publication Number 20130034442

US 20130034442 A1

Patent NumberUS 09114875 B2

Application Number13562405

Filled DateJul 31, 2012

Priority DateJul 31, 2012

Publication DateFeb 7, 2013

Original AssigneeAirbus

Current AssigneeAirbus Helicopters Deutschland Gmbh

Inventor/ApplicantsBernard Enenkl
Rupert Pfaller

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