EP 2152571 B1 20120222 - RUDDER PROPELLER DRIVE, AND RUDDER PROPELLER DRIVING METHOD
Title (en)
RUDDER PROPELLER DRIVE, AND RUDDER PROPELLER DRIVING METHOD
Title (de)
RUDERPROPELLERANTRIEB UND RUDERPROPELLERANTRIEBSVERFAHREN
Title (fr)
BLOC MOTEUR A HELICE DE GOUVERNAIL ET PROCEDE PERMETTANT SON FONCTIONNEMENT
Publication
Application
Priority
- DE 2008000903 W 20080530
- DE 202007007633 U 20070530
Abstract (en)
[origin: WO2008145114A2] The invention relates to a rudder propeller drive comprising a driving motor, the output shaft of which can be effectively connected to a shaft of a propeller by means of a drive train. The propeller shaft is accommodated in a rudder propeller housing that can be mounted outside a hull, while the propeller on the propeller shaft is located outside the rudder propeller housing. A lubricating and/or cooling device is provided for the propeller shaft and/or for drive train areas mounted in front of the propeller shaft. The drive train encompasses a hydrodynamic clutch or a hydrodynamic torque converter which is combined with or integrated into the lubricating and/or cooling device in such a way that the hydrodynamic clutch or the hydrodynamic torque converter and the lubricating and/or cooling device use a joint amount of functional fluid. The invention further relates to a rudder propeller driving method in which an output shaft of a driving motor is effectively connected to a shaft of a propeller by means of a drive train, said propeller shaft being accommodated in a rudder propeller housing located outside a hull. The propeller on the propeller shaft is located outside the rudder propeller housing. The propeller shaft and/or drive train areas mounted in front of the propeller shaft is/are lubricated and/or cooled using a functional fluid. The drive train encompasses a hydrodynamic clutch or a hydrodynamic torque converter to which functional fluid is fed that is part of the same amount of functional fluid used for lubricating and/or cooling the propeller shaft and/or drive train areas mounted in front of the propeller shaft.
IPC 8 full level
B63H 5/125 (2006.01); B63H 5/14 (2006.01); B63H 20/00 (2006.01); B63H 23/26 (2006.01); B63H 23/30 (2006.01); B63H 23/36 (2006.01)
CPC (source: EP US)
B63H 5/125 (2013.01 - EP US); B63H 5/14 (2013.01 - EP US); B63H 21/383 (2013.01 - EP US); B63H 21/386 (2013.01 - EP US); B63H 23/26 (2013.01 - EP US); B63H 23/30 (2013.01 - EP US); B63H 25/42 (2013.01 - EP US); B63H 2005/1256 (2013.01 - EP); B63H 2023/305 (2013.01 - EP US)
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 2008145114 A2 20081204; WO 2008145114 A3 20100218; AT E546352 T1 20120315; CA 2688370 A1 20081204; CN 101720296 A 20100602; CN 101720296 B 20120822; DE 112008002041 A5 20100429; EP 2152571 A2 20100217; EP 2152571 B1 20120222; ES 2382354 T3 20120607; JP 2010527838 A 20100819; JP 2014111448 A 20140619; JP 5720912 B2 20150520; KR 101546542 B1 20150821; KR 20100021572 A 20100225; RU 2009148815 A 20110710; US 2010190392 A1 20100729
DOCDB simple family (application)
DE 2008000903 W 20080530; AT 08758143 T 20080530; CA 2688370 A 20080530; CN 200880018193 A 20080530; DE 112008002041 T 20080530; EP 08758143 A 20080530; ES 08758143 T 20080530; JP 2010509672 A 20080530; JP 2014015836 A 20140130; KR 20097024393 A 20080530; RU 2009148815 A 20080530; US 60216608 A 20080530