Prosecution Insights
Prosecution Insights
Tech Center 3700 • Art Units: 2834 3741 3746 3799
This examiner grants 64% of resolved cases
TAE JUN KIM is an examiner in Tech Center 3700, specifically assigned to Art Unit 2834. With 753 resolved cases, this examiner has a history of patent evaluations that provides a statistical basis for predicting prosecution outcomes. Practitioners can observe the application of examination standards based on this track record in Art Unit 2834.
The examiner maintains an allowance rate of 64.0 percent, which reflects the frequency of successful outcomes for applications reaching a final resolution. The path to grant involves a median days to allowance of 1333. This duration indicates the time applications typically spend in the system before reaching an allowance. Applicants should plan their patent strategies around this 1333-day timeline to manage expectations regarding patent term and commercialization schedules.
Engaging in interviews is a tactic to consider with this examiner, as evidenced by an interview lift of 25.7 percent. While the baseline allowance rate is 64.0 percent, the additional lift suggests that verbal communication helps resolve examiner concerns. Utilizing the 25.7 percent lift through interviewing can help navigate the median pendency and influence the probability of success for applications in Tech Center 3700.
| App # | Title | Status | Assignee |
|---|---|---|---|
| 18839134 | FUEL CONTROL SYSTEM | Final Rejection | Safran Aircraft Engines |
| 18697839 | OUTLET NOZZLE PROVIDED WITH CHEVRONS FOR AERONAUTICAL THRUSTER | Final Rejection | SAFRAN AIRCRAFT ENGINES |
| 18577131 | AERONAUTICAL THRUSTER | Non-Final OA | SAFRAN AIRCRAFT ENGINES |
| 17862806 | CONNECTING ROD FOR A TURBINE ENGINE NACELLE | Non-Final OA | SAFRAN NACELLES |
| 18436855 | ACOUSTICALLY TREATED THRUST REVERSER BULLNOSE FAIRING AND TORQUE BOX | Non-Final OA | The Boeing Company |
| 18732861 | CONTROL DEVICE, MOVING OBJECT, AND CONTROL METHOD | Non-Final OA | HONDA MOTOR CO., LTD. |
| 18807515 | ENGINE FUEL NOZZLE WITH COAXIAL FUEL AND AIR FLOWS | Non-Final OA | Pratt & Whitney Canada Corp. |
| 18654335 | PARTIAL-ADMISSION TURBINE ASSEMBLY FOR AN AIRCRAFT AND METHOD FOR CONTROLLING SAME | Non-Final OA | Pratt & Whitney Canada Corp. |
| 18241818 | HEATING COOKER, COMPUTER PROGRAM, AND HEATING COOKING METHOD | Non-Final OA | SHARP KABUSHIKI KAISHA |
| 19187633 | ROTATING DETONATION COMBUSTOR WITH DISCRETE DETONATION ANNULI | Non-Final OA | General Electric Company |
| 19169490 | REVERSE THRUST TURBOFAN ENGINE | Final Rejection | General Electric Company |
| 18800274 | VARIABLE FAN NOZZLE THRUST REVERSER ASSEMBLY | Non-Final OA | General Electric Company |
| 18672379 | ENGINE FOR AN AIRCRAFT | Final Rejection | General Electric Company |
| 18664933 | Turbine Engine Having a Damper | Non-Final OA | General Electric Company |
| 18615118 | GAS TURBINE ENGINE | Non-Final OA | General Electric Company |
| 18459542 | BATTERY WELDING SYSTEM FOR ASSEMBLING BATTERY PACK FOR ELECTRIC VEHICLE | Non-Final OA | Kia Corporation |
| 19228822 | FUEL SPRAY NOZZLES | Final Rejection | ROLLS-ROYCE plc |
| 18892678 | FUEL SPRAY NOZZLES | Final Rejection | ROLLS-ROYCE plc |
| 18764516 | GAS TURBINE ENGINE STARTING METHOD | Non-Final OA | ROLLS-ROYCE plc |
| 18741985 | GAS TURBINE ENGINE FUEL SYSTEM | Non-Final OA | Rolls-Royce plc |
| 18876358 | ELECTROSPRAY THRUSTER SELF-PRESERVATION | Final Rejection | The Regents of the University of Michigan |
| 18279800 | GAS-SHIELDED ARC WELDING METHOD, WELDED JOINT, AND WELDED JOINT PRODUCTION METHOD | Non-Final OA | JFE Steel Corporation |
| 18927563 | THERMAL MANAGEMENT SYSTEM FOR OPEN ROTOR AIRCRAFT PROPULSION SYSTEM | Non-Final OA | RTX Corporation |
| 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 |
| 18677242 | GAS TURBINE PLANT WITH AMMONIA DECOMPOSITION SYSTEM | Final Rejection | DOOSAN ENERBILITY CO., LTD. |
| 18616028 | Micro Gas Turbine Engine and Related Methods of Manufacture | Final Rejection | Purdue Research Foundation |
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