Prosecution Insights
Prosecution Insights
Tech Center 3700 • Art Units: 3745
This examiner grants 62% of resolved cases
Justin A. Pruitt is an examiner in Tech Center 3700 and Art Unit 3745, where he has 270 resolved cases. His allowance rate is 61.9%, and the median days to allowance is 1125. These metrics suggest that a majority of applications are granted. Practitioners should consider the 1125-day median when planning their strategy for the 270 cases in this examiner's portfolio.
The data reveals an interview lift of 15.4%. This positive lift indicates that conducting an interview is an effective tactic for increasing the 61.9% baseline allowance rate. Given the 1125-day median pendency, the 15.4% lift offers a clear path for practitioners to improve their chances of success. In Art Unit 3745, leveraging the 15.4% lift can be a key factor in navigating the 270 resolved cases and achieving a favorable outcome.
| App # | Title | Status | Assignee |
|---|---|---|---|
| 19165449 | HYDROSTATIC ANNULAR SEAL | Non-Final OA | SAFRAN AIRCRAFT ENGINES |
| 18402471 | CONDITIONING APPARATUS | Final Rejection | Samsung Electronics Co., Ltd. |
| 18795485 | System to Selectively Transfer Power of a Turbine Engine | Non-Final OA | The Boeing Company |
| 19012497 | APPARATUS TO REDUCE VIBRATION OF SEAL SEGMENTS FOR A GAS TURBINE ENGINE | Non-Final OA | General Electric Company |
| 18467387 | AEROFOIL FOR A GAS TURBINE ENGINE | Non-Final OA | ROLLS-ROYCE plc |
| 19471028 | A ROTOR, A POWER-GENERATION TURBOMACHINE COMPRISING SAID ROTOR, AND A THERMODYNAMIC CIRCUIT USING SAID TURBOMACHINE | Non-Final OA | Nuovo Pignone Tecnologie - S.r.l. |
| 18464792 | PROXIMITY MEASUREMENT BETWEEN SEAL ELEMENTS OF A GAS TURBINE ENGINE | Final Rejection | RTX Corporation |
| 19334190 | CLEARANCE FLOW CONTROL FOR MIXED-FLOW FAN | Non-Final OA | Carrier Corporation |
| 18851710 | GAS TURBINE ENGINE WITH TURBINE VANE CARRIER COOLING FLOW PATH | Final Rejection | Siemens Energy Global GmbH & Co. KG |
| 18408763 | FLOW BODY FOR A GAS TURBINE, GAS TURBINE, METHOD FOR MANUFACTURING A FLOW BODY FOR A GAS TURBINE, AND METHOD FOR REPAIRING A FLOW BODY OF A GAS TURBINE | Final Rejection | DOOSAN ENERBILITY CO., LTD. |
| 18408342 | METHOD FOR MANUFACTURING A BLADE FOR A GAS TURBINE, TURBINE BLADE, AND GAS TURBINE | Final Rejection | DOOSAN ENERBILITY CO., LTD. |
| 18401306 | APPARATUS AND METHOD FOR CONTROLLING SUBSTRATE POLISH EDGE UNIFORMITY | Final Rejection | Applied Materials, Inc. |
| 18558530 | A ROTOR BLADE FOR A WIND TURBINE, A WIND TURBINE, AND A METHOD FOR MANUFACTURING THE ROTOR BLADE | Final Rejection | LM WIND POWER A/S |
| 18402261 | BRUSH HEAD FOR FACIAL SKIN CLEANING | Final Rejection | KAO CORPORATION |
| 16796227 | ROTOR BLADE AND METHOD FOR FORMING A ROTOR BLADE | Non-Final OA | United Technologies Corporation |
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