Prosecution Insights
Prosecution Insights
Tech Center 3700 • Art Units: 3665 3741
This examiner grants 86% of resolved cases
Examiner Craig Sang Kim is assigned to Art Unit 3665 in Tech Center 3700, where he has 787 resolved cases. The data shows an allowance rate of 86.3 percent. The median time to allowance for these cases is 1092 days, providing a benchmark for the duration of the prosecution process.
The interview lift for this examiner is 9.8 percent. This 9.8 percent lift indicates that direct communication provides an increase in the probability of allowance over the 86.3 percent base rate. Practitioners should factor this lift into their strategy when managing the 1092-day median pendency in Art Unit 3665.
With 787 resolved cases, the examiner's metrics are well-defined within Tech Center 3700. The 86.3 percent allowance rate is a primary indicator of success, while the 9.8 percent interview lift offers an additional avenue for resolution. These figures help set expectations for the 1092-day median pendency period.
| App # | Title | Status | Assignee |
|---|---|---|---|
| 19375390 | GAS TURBINE COMBUSTOR | Non-Final OA | Toyota Jidosha Kabushiki Kaisha |
| 19274016 | GAS TURBINE ENGINE HAVING A HEAT EXCHANGER LOCATED IN AN ANNULAR DUCT | Non-Final OA | General Electric Company |
| 19259284 | GAS TURBINE ENGINE HAVING A HEAT EXCHANGER LOCATED IN AN ANNULAR DUCT | Non-Final OA | General Electric Company |
| 19259177 | GAS TURBINE ENGINE HAVING A HEAT EXCHANGER LOCATED IN AN ANNULAR DUCT | Non-Final OA | General Electric Company |
| 19243886 | GAS TURBINE ENGINE HAVING A HEAT EXCHANGER LOCATED IN AN ANNULAR DUCT | Non-Final OA | General Electric Company |
| 19135606 | TRIPLE-FLOW AIRCRAFT TURBINE ENGINE | Non-Final OA | GENERAL ELECTRIC COMPANY |
| 19041520 | GAS TURBINE ENGINE HAVING A HEAT EXCHANGER LOCATED IN AN ANNULAR DUCT | Non-Final OA | General Electric Company |
| 18487413 | Closed-Loop Thermal Management System | Final Rejection | General Electric Company |
| 18952302 | FUEL SPRAY NOZZLE FOR A GAS TURBINE ENGINE | Non-Final OA | Rolls-Royce plc |
| 19145124 | PLANT AND METHOD FOR OPERATING PLANT | Non-Final OA | MITSUBISHI HEAVY INDUSTRIES, LTD. |
| 18292202 | SECUREMENT DEVICE, KIT, AND METHOD OF USING SECUREMENT DEVICE | Final Rejection | Solventum Intellectual Properties Company |
| 18403119 | CONNECTOR ASSEMBLY WITH DISLODGEMENT PREVENTION | Final Rejection | CareFusion 303, Inc. |
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