Inventor
Atul Kohli
Inventor
Tolland, CT, US
Overview
Patents· 31 as inventor
Public. Assignee & technology derived from the patent record. Each patent links to its LexDana page.
F01Dprimary
F01DNon-positive displacement machines or engines, e.g. steam turbines28%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants26%
Y02TClimate change mitigation technologies related to transportation17%
F23RGenerating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers12%
Y10TTechnical subjects covered by former us classification7%
F02CGas-turbine plants5%
B22CFoundry moulding3%
B23HWorking of metal by the action of a high concentration of electric current on a workpiece using an electrode which takes the place of a tool1%
F16BDevices for fastening or securing constructional elements or machine parts together, e.g. nails, bolts, circlips, clamps, clips or wedges1%
PatentTitleYear
11,078,793Gas turbine engine airfoil with large thickness properties202110,947,854Internal cooling cavity with trip strips202110,731,474Airfoil with varying wall thickness202010,711,618Turbine component with tip film cooling and method of cooling202010,690,346Washer for combustor assembly202010,670,275Cooling configurations for combustor attachment features202010,619,489Airfoil having end wall contoured pedestals202010,605,094Internal cooling cavity with trip strips202010,577,947Baffle insert for a gas turbine engine component202010,494,939Air shredder insert201910,458,252Cooling passages for a gas path component of a gas turbine engine201910,422,233Baffle insert for a gas turbine engine component and component with baffle insert201910,337,334Gas turbine engine component with a baffle insert201910,301,964Baffle with flow augmentation feature201910,280,841Baffle insert for a gas turbine engine component and method of cooling20199,482,100'Multi-lobed cooling hole'20169,273,560'Gas turbine engine component with multi-lobed cooling hole'20169,022,737'Airfoil including trench with contoured surface'20158,955,576'Cast features for a turbine engine airfoil'20158,763,402'Multi-lobed cooling hole and method of manufacture'20148,733,111'Cooling hole with asymmetric diffuser'20148,695,683'Cast features for a turbine engine airfoil'20148,689,568'Cooling hole with thermo-mechanical fatigue resistance'20148,683,813'Multi-lobed cooling hole and method of manufacture'20148,584,470'Tri-lobed cooling hole and method of manufacture'20138,105,030'Cooled airfoils and gas turbine engine systems involving such airfoils'20127,980,819'Cast features for a turbine engine airfoil'20117,883,320'Article having diffuser holes and method of making same'20117,845,907'Blade cooling passage for a turbine engine'20106,932,572'Film cooled article with improved temperature tolerance'20056,547,524'Film cooled article with improved temperature tolerance'2003Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
2003–2021Patents assigned to UNITED TECHNOLOGIES CORP (30)· patent assignee history
2003–2005Based in Vernon, CT, US· patent location history
2010–2021Based in Tolland, CT, US· patent location history
2012–2016Patents assigned to KOHLI ATUL (9)· patent assignee history
2013–2016Patents assigned to ZELESKY MARK F (6)· patent assignee history
2014–2016Patents assigned to GLEINER MATTHEW S (5)· patent assignee history
2020–2021Patents assigned to RAYTHEON TECH CORP (6)· patent assignee history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| UNITED TECHNOLOGIES CORP | 30 | 2003–2021 |
| KOHLI ATULself | 9 | 2012–2016 |
| RAYTHEON TECH CORP | 6 | 2020–2021 |
| ZELESKY MARK F | 6 | 2013–2016 |
| GLEINER MATTHEW S | 5 | 2014–2016 |
Locations
| Location | Patents | Span |
|---|---|---|
| Tolland, CT, US | 29 | 2010–2021 |
| Vernon, CT, US | 2 | 2003–2005 |