Prosecution Insights
Prosecution Insights
Tech Center 3700 • Art Units: 3741
This examiner grants 59% of resolved cases
| App # | Title | Status | Assignee |
|---|---|---|---|
| 17916348 | PROPULSION SYSTEM FOR A NON-ROTARY-WING AIRCRAFT, AND ASSOCIATED AIRCRAFT | Non-Final OA | SAFRAN |
| 18538300 | OPEN ROTOR AIRCRAFT PROPULSION SYSTEM WITH ANTI-ICING SYSTEM | Final Rejection | RTX Corporation |
| 18121806 | SYSTEM AND METHOD FOR TESTING AIRCRAFT ENGINES | Non-Final OA | General Electric Company |
| 19292519 | SYSTEMS, METHODS, AND APPARATUS FOR FUEL SUPPLY AND INJECTION | Final Rejection | North American Wave Engine Corporation |
| 17659002 | FLIGHT VEHICLE | Final Rejection | TOYOTA JIDOSHA KABUSHIKI KAISHA |
| 18372646 | SYSTEM AND METHOD FOR USING AMMONIA AS A FUEL SOURCE FOR ENGINES | Non-Final OA | University of Central Florida Research Foundation, Inc. |
| 18455728 | AMMONIA COMBUSTOR | Non-Final OA | GE Infrastructure Technology LLC |
| 18281810 | ON-DEMAND HYDROGEN FOR POWER GENERATION | Non-Final OA | SIEMENS ENERGY GLOBAL GMBH & CO. KG |
| 18367262 | FUEL CONTAINMENT STRUCTURE FOR ENGINE FUEL DELIVERY SYSTEM | Final Rejection | Pratt & Whitney Canada Corp. |
| 18214248 | AIRCRAFT POWERPLANT WITH MULTIPLE INDEPENDENT FUEL SYSTEMS | Final Rejection | Pratt & Whitney Canada Corp. |
| 18361593 | THERMAL MANAGEMENT SYSTEM FOR AN ELECTRIC VEHICLE | Non-Final OA | Honeywell International Inc. |
| 18857011 | GAS TURBINE CONTROL DEVICE AND GAS TURBINE CONTROL METHOD | Non-Final OA | MITSUBISHI HEAVY INDUSTRIES, LTD. |
| 18998280 | IMPROVED PROPULSION ASSEMBLY FOR MULTI-ENGINE HYBRID AIRCRAFT | Non-Final OA | SAFRAN HELICOPTER ENGINES |
| 17864974 | Environmentally Friendly Aircraft | Final Rejection | EMBRAER S.A. |
| 18224920 | PROPORTIONAL CONTROL OF COOLING CIRCUIT OF FUEL NOZZLE | Non-Final OA | Collins Engine Nozzles, Inc. |
| 18261062 | BURNER | Non-Final OA | CROSSTOWN H2R AG |
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