Daeubler
Juergen Daeubler, Ummendorf DE
Patent application number | Description | Published |
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20110183987 | Stereoselective Synthesis of Bicyclic Heterocycles - The present invention relates to a process for the stereoselective preparation of compounds of formulae (1A) and (1B) | 07-28-2011 |
20120116080 | PROCESS FOR THE STEREOSELECTIVE PREPARATION OF BICYCLIC HETEROCYCLES - The present invention relates to a process for the stereoselective preparation of compounds of general formula (I) | 05-10-2012 |
20140135495 | STEREOSELECTIVE SYNTHESIS OF BICYCLIC HETEROCYCLES - The present invention relates to a process for the stereoselective preparation of compounds of formulae (1A) and (1B) | 05-15-2014 |
Manfred Daeubler, Dachau DE
Patent application number | Description | Published |
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20090214824 | Apparatus and method for coating a compressor housing - A running-in coating for a compressor housing is disclosed. The running-in coating has at least two layers where a first layer is dimensionally stable and at least one additional layer has run-in capability. | 08-27-2009 |
20110020560 | Method for Manufacturing a Run-In Coating - A method for the production of a run-in coating is provided, whereby a metallic run-in coating material is provided on a component on the stator side of a turbomachine, especially a gas turbine. According to an embodiment of the invention, the provided run-in coating undergoes a heat treatment for purposes of improving its run-in characteristics. | 01-27-2011 |
Manfred A. Daeubler, Dachau DE
Patent application number | Description | Published |
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20080282933 | Running-In Coating for Gas Turbines and Method for Production Thereof - A running-in coating for gas turbines and a method for production of a running-in coating are provided. The running-in coating serves to seal a radial gap between a housing ( | 11-20-2008 |
20090263239 | Ring structure with a metal design having a run-in lining - A ring structure with a metal design for a moving blade of axially flowed through compressor and turbine stages, particularly in gas turbine engines is provided. The ring structure includes a circular ring-shaped outer wall, a circular ring-shaped inner wall, which is located at a short radial distance from the moving blade tips, and includes a joining structure provided in the form of hollow chamber structure between the outer wall and the inner wall. The outer wall is provided in the form of a closed, mechanically stable housing wall of the compressor or turbine stage, and the joining structure provided in the form of hollow chamber structure is joined in a fixed manner to the outer wall and to the inner wall, for example, by soldering, diffusion welding or other joining techniques. The inner wall is provided in the form of a closed, mechanically stable structure, which serves as a run-in lining for the moving blade tips and which is made of a metal woven fabric and/or of a metal felt. | 10-22-2009 |
20100330271 | METHOD OF REPAIRING RUN-IN COATINGS - The present invention relates to a method of repairing intake coatings ( | 12-30-2010 |