Motzkus
Andreas Motzkus, Oppenheim DE
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20100064789 | MEASUREMENT MACHINE FOR THE UNIFORMITY OF VEHICLE TIRES - A measurement machine for uniformity serves for determining radial and lateral force fluctuations of vehicle tires ( | 03-18-2010 |
Ralf Motzkus, Berlin DE
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20100061864 | COATING OPTIMIZATIOH PROCESS USING A COUPON AND COMPONENT COMPRISING A COUPON - A method for optimizing the coating of a component using a coupon by introducing the coupon into a depression of the component, in which the geometry of the component is not altered as compared to a component without a coupon, is provided. A component having a depression into which a coupon is fastened is also provided. | 03-11-2010 |
20110117278 | Process for coating a component having partially closed holes and process for opening the holes - During the coating of a component including cooling-air holes, it is necessary, when remachining the coated cooling-air holes, to determine the correct alignment of the cooling-air row. A process is provided in that at least two cooling-air holes are kept clear by a masking material during the coating and the alignment of the cooling-air row is effected on the basis of these two unclosed cooling-air hole. | 05-19-2011 |
Thorsten Motzkus, Baden CH
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20090071167 | TURBOMACHINE, ESPECIALLY GAS TURBINE - A turbomachine with at least one combustion chamber and at least one turbine which lies downstream of it. The turbine has at least one support element and a lining element connected to the support element and formed as a heat shield. A gap sealed by means of a seal, is formed between the at least one combustion chamber and the turbine, an exchangeable insert is arranged in the gap on the end face on the support element and protects at least the support element against hot gases which penetrate into the gap, and against oxidation which is associated with it. | 03-19-2009 |
Thorsten Motzkus, Baden-Daettwil CH
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20090042154 | BURNER FOR A COMBUSTOR OF A TURBOGROUP - A burner for a combustor of a turbogroup is provided. The burner includes a burner body, an outlet flange, and a plenum which is exposed, or can be exposed, to admission of cooling medium. In order to improve the cooling of the outlet flange, a flow passage and a supply passage are formed. The flow passage and the supply passage are arranged so that the cooling medium from the plenum enters the flow passage, is transferred from the flow passage into the supply passage, and is discharged from the supply passage through holes into a burner interior. | 02-12-2009 |
Thorsten Motzkus, Birmenstore CH
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20110150635 | SEAL AND SEAL ARRANGEMENT FOR CONFINING LEAKAGE FLOWS BETWEEN ADJACENT COMPONENTS OF TURBO-MACHINES AND GAS TURBINES - A seal for stemming leakage flows between adjacent components ( | 06-23-2011 |
Thorsten Motzkus, Birmenstorf CH
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20110284669 | LANCE OF A GAS TURBINE BURNER - A lance of a gas turbine burner includes an inner duct having inner nozzles; an annular outer duct encircling the inner duct and having outer nozzles; and a spacer disposed between a terminal portion of the inner duct and a terminal portion of the outer duct, the spacer being fixed to both the inner duct and the outer duct. | 11-24-2011 |
Werner Motzkus, Stuttgart DE
Patent application number | Description | Published |
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20130322799 | TAPERED ROLLER BEARING WITH CAGE - A tapered roller bearing ( | 12-05-2013 |