Gijsbertus
Gijsbertus Beentjes, Harsefeld DE
Patent application number | Description | Published |
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20090159744 | System box for accommodating aircraft systems - A system box for accommodating aircraft systems, and for load transmission between an aircraft structure and a crew rest compartment. The system box comprises a first, a second and a third region, wherein the three regions differ from each other. The first region is adapted for attachment of the system box to the primary structure of the aircraft, wherein the second region is adapted for mechanical contact with a crew rest compartment for the aircrew. The mechanical contact in turn is adapted for load transmission between the aircraft structure and the crew rest compartment. Necessary aircraft systems are accommodated in the third region of the system box. | 06-25-2009 |
Gijsbertus De With, Valkenswaard NL
Patent application number | Description | Published |
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20090104347 | Hydrophobic Coating - Hydrophobic film or coating, comprising primary particles, secondary particles, adhering to the surface of the primary particles and having an average diameter that is smaller than the average diameter of the primary particles, and a hydrophobic layer covering at least partly the surface of the secondary particles and adhering to that surface, characterized in that the secondary particles are adhering to the surface of the primary particles by covalent chemical bonds. | 04-23-2009 |
20110156081 | POLYMERIC WAVELENGTH CONVERTING ELEMENTS - A wavelength converting element ( | 06-30-2011 |
Gijsbertus Oomens, Nussbaumen CH
Patent application number | Description | Published |
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20090064656 | METHOD FOR OPERATING A COMBINED-CYCLE POWER PLANT, AND COMBINED-CYCLE POWER PLANT USEFUL FOR CARRYING OUT THE METHOD - A method involved operating a combined-cycle power plant ( | 03-12-2009 |
20090249792 | OPERATION OF A GAS TURBINE - Provided is a control method for a gas turbine plant having a first and a second combustors in series, such that combustion gases produced in the first combustor flows into the second combustor. The second combustor having a fuel lance with internal partitions, for injecting at least one fuel and a gas having a mixture of inert gas and support air into the second combustor. The partitions enable the gas to carry, and/or veil, at least one of the fuels as the fuel exits the lance. A variable of the second combustor is measured and the inert gas to support air mixture varies in response to variations of the variable so as to at least partially compensate for the operational effects of the variable on the operation of the second combustor. | 10-08-2009 |
20120167546 | COMBINED-CYCLE POWER PLANT - A method involves operating a combined-cycle power plant ( | 07-05-2012 |