Prosecution Insights
Prosecution Insights
Tech Center 3700 • Art Units: 3741 3746 3799
This examiner grants 64% of resolved cases
| App # | Title | Status | Assignee |
|---|---|---|---|
| 18640938 | MONITORING FUEL PHASE IN AIRCRAFT POWERPLANT FUEL SYSTEM | Non-Final OA | RTX Corporation |
| 18422343 | INTERMEDIATE CASE FOR AIRCRAFT PROPULSION SYSTEM HOUSING | Final Rejection | RTX Corporation |
| 19187633 | ROTATING DETONATION COMBUSTOR WITH DISCRETE DETONATION ANNULI | Final Rejection | General Electric Company |
| 19169490 | REVERSE THRUST TURBOFAN ENGINE | Final Rejection | General Electric Company |
| 18672379 | ENGINE FOR AN AIRCRAFT | Final Rejection | General Electric Company |
| 18664933 | Turbine Engine Having a Damper | Final Rejection | General Electric Company |
| 18616028 | Micro Gas Turbine Engine and Related Methods of Manufacture | Final Rejection | Purdue Research Foundation |
| 18949542 | COMBUSTION EQUIPMENT FOR A GAS TURBINE ENGINE | Non-Final OA | ROLLS-ROYCE plc |
| 18892678 | FUEL SPRAY NOZZLES | Final Rejection | ROLLS-ROYCE plc |
| 18746600 | PROPULSION DEVICE WITH THRUST REVERSER LOCATING ARRANGEMENT | Non-Final OA | ROLLS-ROYCE plc |
| 18741985 | GAS TURBINE ENGINE FUEL SYSTEM | Non-Final OA | Rolls-Royce plc |
| 18631539 | CRYOGENIC FUELLED AIRCRAFT PROPULSION SYSTEM | Non-Final OA | Rolls-Royce plc |
| 18677242 | GAS TURBINE PLANT WITH AMMONIA DECOMPOSITION SYSTEM | Non-Final OA | DOOSAN ENERBILITY CO., LTD. |
| 18697839 | OUTLET NOZZLE PROVIDED WITH CHEVRONS FOR AERONAUTICAL THRUSTER | Non-Final OA | SAFRAN AIRCRAFT ENGINES |
| 18577131 | AERONAUTICAL THRUSTER | Final Rejection | SAFRAN AIRCRAFT ENGINES |
| 18876358 | ELECTROSPRAY THRUSTER SELF-PRESERVATION | Final Rejection | The Regents of the University of Michigan |
| 18807515 | ENGINE FUEL NOZZLE WITH COAXIAL FUEL AND AIR FLOWS | Final Rejection | Pratt & Whitney Canada Corp. |
| 18654335 | PARTIAL-ADMISSION TURBINE ASSEMBLY FOR AN AIRCRAFT AND METHOD FOR CONTROLLING SAME | Non-Final OA | Pratt & Whitney Canada Corp. |
| 18582136 | EXHAUST DUCT MOUNTING STRUCTURE FOR HYBRID AIRCRAFT POWERPLANT | Non-Final OA | Pratt & Whitney Canada Corp. |
| 18640054 | FUEL SYSTEMS FOR GAS TURBINE ENGINES | Non-Final OA | GE Avio S.r.l. |
| 18279643 | WELDING ELECTRODE AND SPOT-WELDING DEVICE | Non-Final OA | University Public Corporation Osaka |
| 18225796 | FLAT SPRAY FUEL INJECTORS | Non-Final OA | Collins Engine Nozzles, Inc. |
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