Innocent
Joseph Innocent, Ellicott City, MD US
Patent application number | Description | Published |
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20100285945 | MITIGATION OF SECONDARY PHASE FORMATION DURING WASTE VITRIFICATION - A method for vitrification of high level waste to reduce the formation of persistent secondary phases comprising the steps of providing a high level waste for vitrification; providing a glass frit additive for mixing with said high level waste; redistributing selected constituents of said glass frit for mixing separately as raw chemicals with said high level waste; and, feeding said high level waste, said glass frit additive, and the redistributed glass frit constituents to a melter for vitrification of said high level waste so that formation of secondary phases is suppressed. | 11-11-2010 |
Manuel Innocent, Wezemaal BE
Patent application number | Description | Published |
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20110227134 | PIXEL SENSING CIRCUIT - Systems and methods of pixel sensing circuits. In accordance with a first embodiment of the present invention, a pixel sensing circuit includes a floating diffusion functionally coupled to and surrounded by a ring transfer gate. The ring transfer gate is functionally coupled to and surrounded by a photo diode. The photo diode may be surrounded by a region of poly silicon. The disclosed structure provides radiation hardening and low light performance. | 09-22-2011 |
Manuel H. Innocent, Wezemaal BE
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20130140441 | IMAGE SENSOR PIXEL AND METHOD - In accordance with an embodiment, a 4T pixel includes a first switch having a control terminal and first and second current carrying terminals and an amplifier having an input terminal and an output terminal. A second switch is coupled between the first switch and the amplifier. | 06-06-2013 |
Simon Innocent, Toulouse FR
Patent application number | Description | Published |
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20100253692 | DISPLAY SYSTEM FOR AVIONIC AND NON-AVIONIC APPLICATIONS - The present invention relates to a display device for a glass cockpit of an aircraft, intended to provide video streams to a plurality of viewing screens of said glass cockpit, said aircraft being partitioned into a secured area, a so-called avionic world (AW), and a non-secured area, a so-called open world (OW), said system comprising at least one first port intended to receive first data to be displayed from a system ( | 10-07-2010 |