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Denzler

Eduard Denzler, Elgg CH

Patent application numberDescriptionPublished
20090162207Method For The Manufacture Of An Erosion Protection Layer And A Component With Said Erosion Protection Layer - In accordance with the invention a method for the manufacture of an erosion protection layer on a metallic substrate is proposed in which a material is welded onto the metallic substrate (06-25-2009

Michael Denzler, Regensburg DE

Patent application numberDescriptionPublished
20080197314Fuel Injector With a Housing, and Method For Finishing and Labeling the Housing - A fuel injector has a housing for an actuator (08-21-2008
20100102138PIEZOELECTRIC COMPONENT COMPRISING A SECURITY LAYER AND AN INFILTRATION BARRIER AND A METHOD FOR THE PRODUCTION THEREOF - A piezoelectric component with a monolithic stack, has electrode layers and piezoceramic layers arranged alternately one on top of the other, the piezoceramic layers have a piezoceramic, and having at least one porous security layer arranged in the stack for the formation of a crack if mechanical overload of the stack should occur. The piezoelectric component has an infiltration barrier arranged between the security layer and a lateral surface section of the stack for suppressing the penetration of a foreign substance into the security layer. The piezoelectric component can be as a piezoactuator for controlling a valve, particularly a valve of an internal combustion engine.04-29-2010

Rainer Denzler, Baienfurt DE

Patent application numberDescriptionPublished
20100241327METHOD FOR DETERMINING THE AXIAL WEAR AND THE COUNTERFORCE GRADIENT IN A MULTIPLE DISK SWITCHING ELEMENT - A method of detecting axial wear and a counterforce gradient of a multiple disc switching element (09-23-2010

Roland Denzler, Weisslingen CH

Patent application numberDescriptionPublished
20090214914Plant with High-Temperature Fuel Cells and Clamping Device for a Cell Stack - The plant (08-27-2009

Susanne Denzler, Meckenbeuren DE

Patent application numberDescriptionPublished
20080283672Drive system for a variable camber aircraft wing - The present invention relates to a drive system for a variable camber aircraft wing having position variable front flaps and/or rear flaps, having drive shafts, which are arranged such that that the flaps undergo a change of position in operation of the drive shafts, and having one or more drive units in driving connection with the drive shafts, wherein at least one switchable coupling is provided via which the drive shafts of two flaps of an aircraft wing can be coupled to one another.11-20-2008