Prosecution Insights
Prosecution Insights
Tech Center 3700 • Art Units: 3741
This examiner grants 58% of resolved cases
| App # | Title | Status | Assignee |
|---|---|---|---|
| 19474295 | PROPULSION SYSTEM ARCHITECTURE COMPRISING AN UNDUCTED FAN AND A DUCTED FAN | Non-Final OA | Safran Aircraft Engines |
| 19476476 | PROPELLER OF AN AIRCRAFT TURBINE ENGINE AND METHOD FOR DE-ICING SAME | Non-Final OA | SAFRAN NACELLES |
| 17916348 | PROPULSION SYSTEM FOR A NON-ROTARY-WING AIRCRAFT, AND ASSOCIATED AIRCRAFT | Final Rejection | SAFRAN |
| 18998280 | IMPROVED PROPULSION ASSEMBLY FOR MULTI-ENGINE HYBRID AIRCRAFT | Final Rejection | SAFRAN HELICOPTER ENGINES |
| 18218470 | FAIL-OPERATIONAL VTOL AIRCRAFT | Non-Final OA | Archer Aviation Inc. |
| 18189458 | CONTROL DEVICE FOR AIRCRAFT | Non-Final OA | HONDA MOTOR CO., LTD. |
| 18186222 | TEMPERATURE CONTROL SYSTEM AND TEMPERATURE CONTROL METHOD AND AIRCRAFT | Non-Final OA | HONDA MOTOR CO.,LTD. |
| 18121810 | METHOD AND APPARATUS FOR THRUST DETERMINATION IN AN AIRCRAFT ENGINE | Non-Final OA | General Electric Company |
| 18121806 | SYSTEM AND METHOD FOR TESTING AIRCRAFT ENGINES | Final Rejection | General Electric Company |
| 18174806 | GAS TURBINE ENGINE SYSTEM | Non-Final OA | ROLLS-ROYCE plc |
| 18857011 | GAS TURBINE CONTROL DEVICE AND GAS TURBINE CONTROL METHOD | Final Rejection | MITSUBISHI HEAVY INDUSTRIES, LTD. |
| 18455728 | AMMONIA COMBUSTOR | Final Rejection | GE Infrastructure Technology LLC |
| 18361593 | THERMAL MANAGEMENT SYSTEM FOR AN ELECTRIC VEHICLE | Final Rejection | Honeywell International Inc. |
| 18372646 | SYSTEM AND METHOD FOR USING AMMONIA AS A FUEL SOURCE FOR ENGINES | Final Rejection | University of Central Florida Research Foundation, Inc. |
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