Prosecution Insights
Prosecution Insights
Tech Center 3700 • Art Units: 3741
This examiner grants 64% of resolved cases
Edwin G Kang works in Tech Center 3700 and Art Unit 3741, where he has handled 336 resolved cases. The data reveals an allowance rate pct of 64.0 and a median days to allowance of 1152. These 336 resolved cases establish a pattern of outcomes for applications in Art Unit 3741. The 64.0 percent allowance rate indicates the frequency of successful grants.
The interview lift pct of 67.8 shows that personal engagement provides a substantial increase in the probability of allowance. This 67.8 percent lift suggests that interviews are an exceptionally effective tool for resolving issues. Practitioners can use the 1152 days to allowance to plan for the duration of the prosecution. The 64.0 percent allowance rate and 1152 days to allowance are the key indicators for this examiner. The 336 resolved cases provide the basis for these observations.
| App # | Title | Status | Assignee |
|---|---|---|---|
| 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 |
| 18279866 | LASER PROCESSING DEVICE | Non-Final OA | Panasonic Intellectual Property Management Co., Ltd. |
| 18239385 | LASER PROCESSING APPARATUS | Non-Final OA | SEIKO EPSON CORPORATION |
| 18821274 | SPILL RETURN FUEL NOZZLES FOR USAGE AS START NOZZLES | Non-Final OA | PRATT & WHITNEY CANADA CORP. |
| 19122248 | PROPELLANT SUPPLY SYSTEM | Non-Final OA | Japan Aerospace Exploration Agency |
| 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 |
| 19144183 | TUBULAR BODY FOR COMBUSTOR, COMBUSTOR, AND GAS TURBINE | Non-Final OA | MITSUBISHI HEAVY INDUSTRIES, LTD. |
| 19128683 | OPERATION METHOD FOR GAS TURBINE | Non-Final OA | MITSUBISHI HEAVY INDUSTRIES, LTD. |
| 18458179 | HEATER CONTROL APPARATUS | Final Rejection | ISUZU MOTORS LIMITED |
| 18923015 | HYDROGEN ASSISTED COMBUSTION AND ENGINE COOLING | Non-Final OA | RTX Corporation |
| 18647646 | SIEVE RDE INJECTOR WITH VARIABLE PRESSURE DROP CAPABILITY | Non-Final OA | 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 |
| 19024486 | SYSTEMS, METHODS, AND APPARATUSES OF GAS TURBINE COOLING | Final Rejection | ConocoPhillips Company |
| 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 |
| 18114691 | FUEL INJECTOR AIR SWIRLER STRUCTURE WITH CANTED FLOW GUIDE SURFACE | Non-Final OA | Raytheon Technologies Corporation |
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