EP 2109566 A2 20091021 - AIRCRAFT PROPELLER DRIVE, METHOD FOR DRIVING AN AIRCRAFT PROPELLER, USE OF A BEARING FOR AN AIRCRAFT PROPELLER DRIVE AND USE OF AN ELECTRIC MACHINE
Title (en)
AIRCRAFT PROPELLER DRIVE, METHOD FOR DRIVING AN AIRCRAFT PROPELLER, USE OF A BEARING FOR AN AIRCRAFT PROPELLER DRIVE AND USE OF AN ELECTRIC MACHINE
Title (de)
FLUGZEUGPROPELLERANTRIEB, VERFAHREN ZUM ANTREIBEN EINES FLUGZEUGPROPELLERS UND VERWENDUNG EINES LAGERS EINES FLUGZEUGPROPELLERANTRIEBS SOWIE VERWENDUNG EINER ELEKTROMASCHINE
Title (fr)
ENTRAÎNEMENT D'HÉLICE D'AVION, PROCÉDÉ D'ENTRAÎNEMENT D'UNE HÉLICE D'AVION, UTILISATION D'UN PALIER D'UN ENTRAÎNEMENT D'HÉLICE D'AVION ET UTILISATION D'UN MOTEUR ÉLECTRIQUE
Publication
Application
Priority
- DE 2008000036 W 20080114
- DE 102007002889 A 20070115
- DE 102007055336 A 20071119
Abstract (en)
[origin: WO2008086774A2] To improve the damping of vibrations in aircraft propeller drives, the invention discloses an aircraft propeller drive comprising a propeller, a motor and a drive train between the propeller and the motor. The drive train of said aircraft propeller drive has a torsional vibration damper.
IPC 8 full level
B64D 35/00 (2006.01)
CPC (source: EP US)
B64D 27/026 (2024.01 - EP); B64D 27/24 (2013.01 - EP US); B64D 35/00 (2013.01 - EP US); B64D 35/08 (2013.01 - EP US); F16F 15/134 (2013.01 - EP US); B64D 27/026 (2024.01 - US); Y02T 50/40 (2013.01 - EP US); Y02T 50/60 (2013.01 - EP US); Y10T 74/2132 (2015.01 - EP US)
Citation (search report)
See references of WO 2008086774A2
Designated contracting state (EPC)
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR
DOCDB simple family (publication)
WO 2008086774 A2 20080724; WO 2008086774 A3 20080918; WO 2008086774 A8 20081204; CN 101610949 A 20091223; DE 102007055336 A1 20080821; DE 112008000117 A5 20100506; EA 200900826 A1 20100430; EP 2109566 A2 20091021; US 2010038473 A1 20100218
DOCDB simple family (application)
DE 2008000036 W 20080114; CN 200880002312 A 20080114; DE 102007055336 A 20071119; DE 112008000117 T 20080114; EA 200900826 A 20080114; EP 08706739 A 20080114; US 44890008 A 20080114