Dejulio
Emil Dejulio, Columbus, IN US
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20140246183 | MICROCHANNEL HEAT EXCHANGER AND METHODS OF MANUFACTURE - An apparatus includes a first flow panel and a second flow panel. The first flow panel includes a first flow portion and a second flow portion. The first flow portion defines a flow passageway within which a gas can flow in a first direction. The second flow portion defines a set of microchannels in fluid communication with the flow passageway and within which the gas can flow in a second direction, where the second direction is nonparallel to the first direction. The first flow panel is coupled to the second flow panel to define a heat transfer passageway within which a heat transfer medium can be conveyed in a third direction, where the third direction is opposite the first direction. In such embodiments, the heat transfer passageway is fluidically isolated from the flow passageway and the set of microchannels by a thermally conductive side wall. | 09-04-2014 |
Emil R. Dejulio, Columbus, IN US
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20090288388 | Gas turbine exhaust - An exhaust device is disclosed that includes a duct that turns an exhaust flow from a gas turbine engine from a first direction to a second direction. A diverter cup is disposed within the duct and serves to split the exhaust flow into two streams as well as introduce cooling air through an ejector pump at the downstream end of the diverter cup. A splitter is disposed downstream of the diverter cup and serves to split the cooling air into two streams which are thereafter mixed with the split exhaust flow. A diffuser is created in the exhaust device between the duct and the splitter. Various cooling slots are also provided in the duct. | 11-26-2009 |
20110299065 | SYSTEM AND METHOD FOR MEASURING RADIANT ENERGY IN GAS TURBINE ENGINES, COMPONENTS AND RIGS - One embodiment of the present invention is a unique system for measuring radiant energy in gas turbine engines, gas turbine engine components and gas turbine engine/component rigs. Another embodiment is a unique method for measuring radiant energy in gas turbine engines, gas turbine engine components and gas turbine engine/component rigs. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for measuring radiant energy. Further embodiments, forms, features, aspects, benefits, and advantages of the present application shall become apparent from the description and figures provided herewith. | 12-08-2011 |
James Dejulio, Venice, CA US
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20100121650 | SYSTEM AND METHOD FOR CONTENT DEVELOPMENT - Media content is developed using a competition model and supporting computerized systems. Multiple competition phases may be held to generate content throughout the creative process from idea to completed project. Prizes are awarded to the competitors that create winning submissions and the reuse of submissions. | 05-13-2010 |
Kelvin Ray Dejulio, Parker, CO US
Patent application number | Description | Published |
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20090294446 | Cover Apparatus - Broadly, the present invention is of a cover apparatus for a container with an interior and having an open end defined by a sidewall edge portion. The cover apparatus includes an annular element with structure to removably engage the sidewall edge portion. Further included in the cover apparatus is a separable disc that is rotationally removably engaged to the annular element, the disc is sized and configured to allow for one-way axial movement relative to the annular element, such that the disc and the annular element substantially enclose the container interior. | 12-03-2009 |