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Grivas
Demetrios Grivas, Toronto CA
| Patent application number | Description | Published |
|---|---|---|
| 20100025548 | Pipe Support Assembly - A pipe support assembly for supporting one or more pipes. According to an embodiment, the pipe support assembly comprises a main member having a saddle for holding a first pipe, a pipe holder attached to the main member and configured for holding a second pipe, and the main member includes an exterior surface for receiving a support strap for affixing to the structure. According to an embodiment, the first pipe comprises an insulated pipe with an outer insulation layer and the second pipe comprises an uninsulated pipe. According to another embodiment, the pipe support assembly includes a bottom mount for mounting the pipe support assembly to a structure. According to an embodiment, the mount comprises a bracket. According to another aspect, the mount comprises a base that is fastened to a structure. | 02-04-2010 |
Dimitrios Grivas, Chicago, IL US
| Patent application number | Description | Published |
|---|---|---|
| 20100186249 | NON-MARRING HIGH-PRECISION MARKING AND MEASURING TOOL - The invention is an tool for measuring and marking wall sheathing materials such as drywall, veneer, paneling, and various other wall sheathing materials. The tool provides rolling contact to protect finished surfaces and also maintains parallel positioning to maximize accuracy. | 07-29-2010 |
Nick J. Grivas, Crystal Lake, IL US
| Patent application number | Description | Published |
|---|---|---|
| 20110105198 | Method of Enabling A Remote Communications Device with A Telematics Functionality Module - Method of enabling a remote communications device ( | 05-05-2011 |
Nicolas Grivas, Dollard Des Ormeaux CA
| Patent application number | Description | Published |
|---|---|---|
| 20100236257 | GAS TURBINE COMBUSTOR EXIT DUCT AND HP VANE INTERFACE - An assembly for a gas turbine engine includes a combustor and a vane assembly disposed downstream thereof. A portion of an outer platform of the vane assembly defines an axial sliding joint connection with the combustor, and includes a plurality of depressions located in an outer circumferential surface thereof opposite the combustor. The depressions are disposed in regions of expected higher thermal growth about the circumference of the outer platform such that thermal growth of the entire outer platform is substantially uniform circumferentially therearound. | 09-23-2010 |
| 20110078902 | METHOD FOR CENTERING ENGINE STRUCTURES - A method for centering an engine structure such as a bearing housing is provided which may be used, for example, during assembly of a mid turbine frame or other engine case structure. In one aspect, the method includes using spacers with respective radial spokes which connect inner and outer portions of the case. In another aspect, centring may be provided by machining selected contacting surfaces of selected components. | 04-07-2011 |
| 20110081228 | INTERTURBINE VANE WITH MULTIPLE AIR CHAMBERS - A gas turbine engine has a mid turbine frame disposed between turbine rotor assemblies. The mid turbine frame includes hollow airfoils radially extending through an annular gas path duct. The airfoils each include a double-walled leading edge structure to define a front chamber separated from a rear chamber defined in the remaining space within the airfoil. | 04-07-2011 |