Peloquin
Claude Peloquin, Gatineau CA
Patent application number | Description | Published |
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20140258921 | SYSTEM AND METHOD FOR ERGONOMIC PLACEMENT OF AN OBJECT OR CURSOR ON A COMPUTER DISPLAY - A method includes the steps of: providing a computer readable code configured to run on a local computer and configured to perform a process keep a reference point of an item in a substantially fixed position on a computer display while the item is being edited; running the computer readable code on the local computer; detecting by computer a user edit; recording by computer a position of the reference point of the item on the computer display and a value of a scroll bar; calculating by computer a new point of the reference point of the item and a new value of the scroll bar such that following the user edit, the reference of the item remains at the substantially fixed position on the computer display; and redrawing the item near the substantially fixed position on the computer display. A system to perform the method is also described. | 09-11-2014 |
20140258925 | SYSTEM AND METHOD FOR THE VISUALIZATION OF PROPERTIES OF OBJECTS - A method includes the steps of: providing a computer readable non-transitory storage medium including a computer readable code configured to run on a computer and to perform a process to visualize a property of objects of a computer drawing; providing a user input device communicatively coupled to the computer; displaying by the computer a list of the properties of the objects in the computer drawing; selecting by the user input device by a hover-over operation a selected property from the list of the properties; and indicating by the computer a marker on the computer drawing at one or more locations of an instance of the objects having the selected property. A system for visualization of a property of objects is also described. | 09-11-2014 |
Guy Peloquin, Jonquiere CA
Patent application number | Description | Published |
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20130168326 | FLOCCULENT ADDITION AND MIXING RATE FOR SEPARATING A SLURRY - The invention concerns a method for separating solid and liquor components of a process slurry comprising solid material entrained in a liquor, said method comprising: (a) a pre-treatment step of adding a flocculent to the process slurry and mixing the flocculent and the slurry by selecting a higher extent of mixing in an early stage of said step than in a later stage of said step, and (b) a solid/liquor separation step of allowing separation of solid material, including aggregates of solid material, and liquor of said process slurry to produce process outputs of a clarified liquor and solid material with some entrained liquor. The invention also concernes a method and an apparatus for adding a flocculent to a process slurry. | 07-04-2013 |
20130206707 | APPARATUS AND METHOD FOR REFINING A PROCESS LIQUOR BY GRAVITY SETTLING - An apparatus for refining a process liquor that includes solids, which apparatus includes a vessel having a base and a side wall that define an internal volume for containing the process liquor and for allowing gravity settling of the solids in the liquor, whereby to produce a refined liquor toward a top of the internal volume and a slurry toward a bottom of the internal volume, the apparatus further includes solids displacement elements disposed within the internal volume for directing settled solids and/or settling solids in the vicinity of the side wall or of the base toward a flow path of the slurry being extracted from the slurry outlet. A processing plant including the above refining apparatus and a method for refining a process liquor. | 08-15-2013 |
Patrick Peloquin, Varennes CA
Patent application number | Description | Published |
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20140219816 | HIGH PRESSURE TURBINE BLADE COOLING HOLE DISTRIBUTION - A turbine blade for a gas turbine engine with an airfoil portion defined by a perimeter wall surrounding at least one enclosure, the perimeter wall having a plurality of cooling holes defined therethrough and providing fluid communication between the at least one enclosure and a gaspath of the gas turbine engine. The plurality of cooling holes includes at least one row of holes selected from the group consisting of a first row, a second row, a third row and a fourth row, with the first, second, third and fourth rows of holes respectively including the holes numbered PA-1 to PA-10, PB-1 to PB-3, HA-1 to HA-9, and SA-1 to SA-8 located such that a central axis thereof extends through the respective point 1 and point 2 having a nominal location in accordance with the X, Y, Z Cartesian coordinate values set forth in Table 3. | 08-07-2014 |
20140219817 | HIGH PRESSURE TURBINE BLADE COOLING HOLE DISTRIBUTION - A turbine blade for a gas turbine engine with an airfoil portion defined by a perimeter wall surrounding at least one enclosure, the perimeter wall having a plurality of cooling holes defined therethrough and providing fluid communication between the at least one enclosure and a gaspath of the gas turbine engine. The plurality of cooling holes includes at least one row of holes selected from the group consisting of a first row, a second row, a third row and a fourth row, with the first, second, third and fourth rows of holes respectively including the holes numbered PA-1 to PA-10, PB-1 to PB-3, HA-1 to HA-9, and SA-1 to SA-8 located such that a central axis thereof extends through the respective point 1 and point 2 having a nominal location in accordance with the X, Y, Z Cartesian coordinate values set forth in Table 3. | 08-07-2014 |