Tech Center 3700 • Art Units: 3741
This examiner grants 64% of resolved cases
| App # | Title | Status | Assignee |
|---|---|---|---|
| 18279866 | LASER PROCESSING DEVICE | Non-Final OA | Panasonic Intellectual Property Management Co., Ltd. |
| 18821274 | SPILL RETURN FUEL NOZZLES FOR USAGE AS START NOZZLES | Non-Final OA | PRATT & WHITNEY CANADA CORP. |
| 18377180 | VARIABLE INLET GUARD FOR AN INLET OF AN AIRCRAFT ENGINE | Non-Final OA | Pratt & Whitney Canada Corp. |
| 18642208 | FUEL INJECTOR FOR A TURBINE ENGINE | Non-Final OA | General Electric Company |
| 18628126 | GAS TURBINE ENGINE BLEED SYSTEMS INCLUDING BLEED DISCHARGE EXHAUST DEVICES | Final Rejection | General Electric Company |
| 18623664 | GAS TURBINE ENGINE AND FUEL NOZZLE ASSEMBLY THEREFOR | Non-Final OA | GENERAL ELECTRIC COMPANY |
| 18450633 | COMBUSTOR MIXING ASSEMBLY | Non-Final OA | General Electric Company |
| 18239385 | LASER PROCESSING APPARATUS | Non-Final OA | SEIKO EPSON CORPORATION |
| 18851434 | GAS TURBINE CONTROL DEVICE, GAS TURBINE CONTROL METHOD, AND GAS TURBINE CONTROL PROGRAM | Non-Final OA | MITSUBISHI HEAVY INDUSTRIES, LTD. |
| 18578124 | GAS TURBINE COMBUSTOR AND GAS TURBINE | Non-Final OA | MITSUBISHI HEAVY INDUSTRIES, LTD. |
| 18458179 | HEATER CONTROL APPARATUS | Final Rejection | ISUZU MOTORS LIMITED |
| 17925406 | TURBOMACHINE EXHAUST CASE | Non-Final OA | SAFRAN AIRCRAFT ENGINES |
| 19133021 | IMPROVED HYBRID TURBOPROP ENGINE FOR AIRCRAFT | Non-Final OA | SAFRAN HELICOPTER ENGINES |
| 18721492 | AIRCRAFT TURBOMACHINE COMPRISING A DEVICE FOR INHIBITING THE ACCUMULATION OF COKE IN A DUCT | Non-Final OA | SAFRAN HELICOPTER ENGINES |
| 18965600 | SUPPLEMENTAL THRUST SYSTEM WITH ROTATING DETONATION COMBUSTOR | Non-Final OA | RTX Corporation |
| 18923015 | HYDROGEN ASSISTED COMBUSTION AND ENGINE COOLING | Final Rejection | RTX Corporation |
| 18496615 | ADDITIVE CLOCKED FUEL INJECTOR BOLT | Non-Final OA | RTX Corporation |
| 16844683 | COOLING SYSTEM FOR A GAS TURBINE ENGINE | Non-Final OA | RTX Corporation |
| 18399849 | COMBUSTOR WITH ADJUSTABLE AIR FLOW FOR AXIAL FUEL STAGE INJECTOR AND HEAD END FUEL NOZZLE ASSEMBLY | Final Rejection | GE Infrastructure Technology LLC |
| 18141586 | METHODS AND APPARATUSES FOR REDUCING ENGINE NOISE | Final Rejection | The Government of the United States of America, as represented by the Secretary of the Navy |
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