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Knepper
Angela Knepper, Cheltenham GB
| Patent application number | Description | Published |
|---|---|---|
| 20120025016 | AIRCRAFT PROPELLER - A propeller for an aircraft is disclosed. The propeller has an odd number of unequally circumferentially spaced blades. The propeller may be provided as part of a contra-rotating propeller arrangement and/or aft of a pylon on an aircraft. The propeller has been found to reduce noise levels and to be efficient. | 02-02-2012 |
Jean-Claude Knepper, Ingeldorf LU
| Patent application number | Description | Published |
|---|---|---|
| 20120136110 | PREPARATION OF RUBBER CONTAINING SILICA AND CARBON BLACK REINFORCEMENT, RUBBER COMPOSITION AND TIRE WITH COMPONENT - The invention relates to preparation of a rubber composition containing silica and carbon black reinforcement, the resultant rubber composition and tire with component comprised of such rubber composition. | 05-31-2012 |
Kerstin Knepper, Kundl / Tirol AT
| Patent application number | Description | Published |
|---|---|---|
| 20110009629 | PREPARATION OF MORPHOLINE DERIVATIVES - This invention relates to processes and intermediates for the stereoselective morpholine derivatives. The invention in particular allows the stereoselective preparation of the drugs aprepitant and fosaprepitant. | 01-13-2011 |
Kerstin Knepper, Woergl AT
| Patent application number | Description | Published |
|---|---|---|
| 20100010239 | Process for the Production of Prostaglandins and Prostaglandin Analogs - The present invention relates to an improved process for the production of prostaglandins and prostaglandin analogs. In particular, this invention relates to the production of prostaglandins of the PGF | 01-14-2010 |
Markus Knepper, Waltenhofen/oberdorf DE
| Patent application number | Description | Published |
|---|---|---|
| 20080202484 | Ignition coil for an internal combustion engine - An ignition coil for an internal combustion engine has a core, which is provided with a plastic extrusion coat on its periphery. The core is concentrically surrounded by a secondary coil and a primary coil. The plastic extrusion coat of the core is used as a coil shell for the secondary coil so that it is possible to dispense with a separate secondary coil shell. The ignition coil therefore has an especially compact design. | 08-28-2008 |
| 20090220297 | Apparatus for attaching an electrical device to a housing - The apparatus simplifies release of the locking connections. The second housing section of the electrical device is designed rotationally asymmetrically in such a way that when rotated about the longitudinal axis, the electrical device at one particular side wall of the second housing section causes the at least one locking connection to open. | 09-03-2009 |
Peter Knepper, Ganderkesee DE
| Patent application number | Description | Published |
|---|---|---|
| 20100038409 | Joining Method For Joining Components - A method is provided for connecting components particularly in the field of aerospace wherein a first component is connected to a second component, comprising the following steps: arranging at least one nano- or microstructured material between the first and the second component, initiating an exothermic reaction of the nano- or microstructured material for connecting both components with each other. | 02-18-2010 |
| 20110091709 | METHOD FOR COATING A FIBER COMPOSITE COMPONENT FOR AN AIRCRAFT OR SPACECRAFT AND FIBER COMPOSITE COMPONENT PRODUCED BY SAID METHOD - In a method for coating a fibre composite component for an aircraft or spacecraft, a surface layer of the fibre composite component, which surface layer has spacing from the fibres introduced in the fibre composite component for the protection thereof, is pretreated, at least in portions to form a primer coat; at least one functional coat is then applied to the formed primer coat. A corresponding fibre composite component comprises at least one functional coat which is applied to a primer coat. | 04-21-2011 |
| 20110256414 | METHOD FOR COATING A FIBER COMPOSITE COMPONENT FOR AN AIRCRAFT OR SPACECRAFT AND FIBER COMPOSITE COMPONENT PRODUCED BY SAID METHOD - In a method for coating a fibre composite component for an aircraft or spacecraft, a surface layer of the fibre composite component, which surface layer has spacing from the fibres introduced in the fibre composite component for the protection thereof, is pretreated, at least in portions to form a primer coat; at least one functional coat is then applied to the formed primer coat. A corresponding fibre composite component comprises at least one functional coat which is applied to a primer coat. | 10-20-2011 |