Garth J.
Garth J. Vdovak, North Berwick, ME US
Patent application number | Description | Published |
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20160003161 | HEAT SHIELD MOUNT CONFIGURATION - An attachment interface assembly for a gas turbine engine has a component configured for attachment to an engine static structure. A fastener has a threaded body portion and an enlarged head portion. The threaded body portion is inserted through aligned holes in the component and engine static structure. A clip has a center opening that receives the threaded body portion such that the clip is positioned between the enlarged head portion and the component. | 01-07-2016 |
Garth J. Vdoviak, Jr., North Berwick, ME US
Patent application number | Description | Published |
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20140260321 | GAS TURBINE ENGINE STATIC STRUCTURE JOINT WITH UNDERCUTS - A gas turbine engine static structure has a joint that includes at least two flanges. The first flange includes a face extending axially proud between radially spaced apart undercuts. The second flange abuts the face. Fasteners secure the flanges to one another through the face. | 09-18-2014 |
20160032780 | Triple Flange Arrangement for a Gas Turbine Engine - A flange arrangement for a gas turbine engine includes a case flange between a forward flange and an aft flange. | 02-04-2016 |
Garth J. Vdoviak, Jr., Readfield, ME US
Patent application number | Description | Published |
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20160032771 | FLUID-COOLED SEAL ARRANGEMENT FOR A GAS TURBINE ENGINE - A component for a gas turbine engine includes a compartment housing that redirects oil from at least one passage in a rotational component onto a backside of a seal land. | 02-04-2016 |