Issued Patents All Time
Showing 1–25 of 31 patents
| Patent # | Title | Co-Inventors | Date |
|---|---|---|---|
| 12372239 | Gaseous fuel nozzle for use in gas turbine engines | — | 2025-07-29 |
| 12092032 | Gas turbine engine hydrogen supply system and method | — | 2024-09-17 |
| 11988386 | Gas turbine engine injector module with thermally coupled fuel lines having respective outlets | Duane Peterson, Girish Kanakagiri, Jaydeep Basani, Nagaraja Rudrapatna, Paul Yankowich +2 more | 2024-05-21 |
| 11959401 | Deswirl system for gas turbine engine | Shakeel Nasir, Atul Verma, Jeffrey Krise, Doni Tapederi, Jacob Salai | 2024-04-16 |
| 11674686 | Coating occlusion resistant effusion cooling holes for gas turbine engine | Nagaraja Rudrapatna | 2023-06-13 |
| 11549437 | Combustor for gas turbine engine and method of manufacture | Hamdullah Ozogul, Atul Verma, Amy Kujala, Michael Wedig, Ryan Meyer +1 more | 2023-01-10 |
| 11519604 | Plug resistant effusion holes for gas turbine engine | Nagaraja Rudrapatna, Atul Verma, David Chou, Christopher Zollars | 2022-12-06 |
| 11306659 | Plug resistant effusion holes for gas turbine engine | Nagaraja Rudrapatna | 2022-04-19 |
| 11287133 | Axially staged rich quench lean combustion system | Sunil James | 2022-03-29 |
| 11085641 | Plug resistant effusion holes for gas turbine engine | Nagaraja Rudrapatna, Atul Verma, David Chou, Christopher Zollars | 2021-08-10 |
| 10895157 | Gas turbine engine components with air-cooling features, and related methods of manufacturing the same | Paul Yankowich | 2021-01-19 |
| 10816211 | Axially staged rich quench lean combustion system | Sunil James | 2020-10-27 |
| 10775044 | Gas turbine engine dual-wall hot section structure | Atul Verma, Sunil James, Hamdullah Ozogul, John Gintert | 2020-09-15 |
| 10166524 | Methane conversion apparatus and process using a supersonic flow reactor | Robert L. Bedard, Christopher Naunheimer, Gavin P. Towler, Laura E. Leonard, Gregory O. Woodcock +1 more | 2019-01-01 |
| 10101030 | Gas turbine engines with plug resistant effusion cooling holes | Eric Blumer | 2018-10-16 |
| 10029957 | Methane conversion apparatus and process using a supersonic flow reactor | Robert L. Bedard, Christopher Naunheimer, Gavin P. Towler, Laura E. Leonard, Gregory O. Woodcock +4 more | 2018-07-24 |
| 9656229 | Methane conversion apparatus and process using a supersonic flow reactor | Robert L. Bedard, Christopher Naunheimer, Gavin P. Towler, Laura E. Leonard, Gregory O. Woodcock +1 more | 2017-05-23 |
| 9410702 | Gas turbine engine combustors with effusion and impingement cooling and methods for manufacturing the same using additive manufacturing techniques | Dustin Michael Brandt, David Waldman, James Neumann, Art Payne | 2016-08-09 |
| 9400110 | Reverse-flow annular combustor for reduced emissions | Terrel Kuhn, Vinayender Kuchana, Veeraraghava Raju Hasti, Raymond Gage, Sunil James | 2016-07-26 |
| 9080770 | Reverse-flow annular combustor for reduced emissions | Veeraraghave Raju Hasti, Terrel Kuhn, Sunil James, Mario Scaini | 2015-07-14 |
| 8127554 | Quench jet arrangement for annular rich-quench-lean gas turbine combustors | Frank J. Zupanc | 2012-03-06 |
| 7926284 | Quench jet arrangement for annular rich-quench-lean gas turbine combustors | Frank J. Zupanc, Jurgen C. Schumacher | 2011-04-19 |
| 7905094 | Combustor systems with liners having improved cooling hole patterns | Paul Yankowich, Frank J. Zupanc, Ronald B. Pardington | 2011-03-15 |
| 7812282 | Methods of forming fan-shaped effusion holes in combustors | Terrel Kuhn, Sossity A. Flamand, Gregory O. Woodcock, Lowell Frye | 2010-10-12 |
| 7665306 | Heat shields for use in combustors | Thomas J. Bronson | 2010-02-23 |