Detailed information about the 100 most recent patent applications.
| Application Number | Title | Filing Date | Disposal Date | Disposition | Time (months) | Office Actions | Restrictions | Interview | Appeal |
|---|---|---|---|---|---|---|---|---|---|
| 19005225 | COMBINED CYCLE POWER GENERATION FACILITY | December 2024 | June 2025 | Allow | 6 | 0 | 0 | No | No |
| 18947604 | COMBUSTOR NOZZLE, COMBUSTOR, AND GAS TURBINE INCLUDING SAME | November 2024 | April 2025 | Allow | 5 | 0 | 0 | No | No |
| 18894458 | MULTI-STAGE MICRO-DECOMPOSITION SWIRL BURNER WITH AN AMMONIA-DOPED FUEL AND LOW NOX CONTROL METHOD | September 2024 | November 2024 | Allow | 2 | 0 | 0 | No | No |
| 18793126 | CRYOGENIC FUEL SEMI-CLOSED INJECTION COOLED BOTTOMING CYCLE | August 2024 | March 2025 | Allow | 8 | 0 | 0 | No | No |
| 18834516 | A FUEL NOZZLE FOR A GAS TURBINE, COMBUSTOR INCLUDING THE FUEL NOZZLE, AND GAS TURBINE | July 2024 | June 2025 | Allow | 11 | 1 | 0 | Yes | No |
| 18767604 | THERMAL IMPACT OF GAS STORAGE | July 2024 | March 2025 | Allow | 8 | 0 | 0 | No | No |
| 18727215 | CONTROL METHOD FOR GAS TURBINE COMBUSTOR AND CONTROL DEVICE FOR GAS TURBINE COMBUSTOR | July 2024 | June 2025 | Allow | 12 | 1 | 0 | No | No |
| 18760805 | COMBINED HEAT AND POWER SYSTEM USING AND PRODUCING CO2 AND METHOD OF OPERATION | July 2024 | June 2025 | Allow | 12 | 1 | 0 | No | No |
| 18735712 | DUAL CYCLE INTERCOOLED HYDROGEN ENGINE ARCHITECTURE | June 2024 | June 2025 | Allow | 12 | 1 | 0 | No | No |
| 18734201 | SYSTEM AND METHOD FOR BLENDING MULTIPLE FUELS | June 2024 | March 2025 | Allow | 9 | 1 | 0 | No | No |
| 18716550 | FUEL DISTRIBUTION ASSEMBLY FOR A TURBOMACHINE | June 2024 | February 2025 | Allow | 9 | 0 | 0 | No | No |
| 18731709 | LIQUID ROCKET ENGINE INJECTOR WITH VARIABLE FLOW AREA | June 2024 | March 2025 | Allow | 9 | 1 | 0 | No | No |
| 18710368 | HEAT ENGINE SYSTEM COMPRISING A RESERVOIR FOR RECEIVING AND SUPPLYING A WORKING FLUID FROM AND TO A COMPRESSOR VIA A BLEED VALVE AND AN INTAKE VALVE | May 2024 | January 2025 | Allow | 8 | 1 | 0 | Yes | No |
| 18665376 | GAS TURBINE PLANT WITH AMMONIA DECOMPOSITION SYSTEM | May 2024 | November 2024 | Allow | 6 | 0 | 0 | No | No |
| 18662660 | DUAL FUEL GAS TURBINE COMBUSTION CHAMBER MODULE HAVING AN ANNULAR COMBUSTION CHAMBER | May 2024 | June 2025 | Allow | 13 | 1 | 0 | No | No |
| 18657325 | HIGH BANDWIDTH CONTROL OF TURBOFAN/TURBOPROP THRUST RESPONSE USING EMBEDDED ELECTRIC MACHINES | May 2024 | March 2025 | Allow | 10 | 1 | 0 | No | No |
| 18652159 | AN IMPROVED COMBUSTOR APPARATUS | May 2024 | March 2025 | Allow | 11 | 1 | 0 | No | No |
| 18652134 | COMBUSTOR APPARATUS | May 2024 | September 2024 | Allow | 4 | 0 | 0 | No | No |
| 18638783 | INLET CONDITIONING SYSTEMS AND METHODS FOR A TURBOMACHINE | April 2024 | October 2024 | Allow | 6 | 0 | 0 | No | No |
| 18633110 | FUEL INJECTOR MANIFOLD HAVING A VARIABLE FUEL FLOW SYSTEM FOR A TURBINE ENGINE | April 2024 | February 2025 | Allow | 11 | 1 | 0 | No | No |
| 18626811 | FUEL NOZZLE FOR HYDROGEN-BASED FUEL OPERATION | April 2024 | March 2025 | Allow | 11 | 1 | 0 | No | No |
| 18626818 | FUEL NOZZLE FOR HYDROGEN-BASED FUEL OPERATION | April 2024 | September 2024 | Allow | 5 | 0 | 0 | No | No |
| 18626821 | FUEL NOZZLE FOR HYDROGEN-BASED FUEL OPERATION | April 2024 | January 2025 | Allow | 9 | 0 | 0 | No | No |
| 18610437 | COOLING STRUCTURE FOR RADIAL TURBINE | March 2024 | February 2025 | Allow | 11 | 1 | 0 | Yes | No |
| 18609726 | DUAL-MODE RAMJET ENGINE WITH VARIABLE FUEL INJECTION | March 2024 | September 2024 | Allow | 6 | 0 | 0 | No | No |
| 18608525 | COMBUSTION SYSTEM WITH DUAL FUEL CAPABILITY | March 2024 | December 2024 | Allow | 9 | 1 | 0 | No | No |
| 18601912 | CLUSTER OF SWIRLED MINI-MIXERS FOR FUEL-STAGED, AXIALLY STAGED COMBUSTION | March 2024 | December 2024 | Allow | 9 | 1 | 0 | No | No |
| 18433160 | REUSABLE UPPER STAGE ROCKET WITH AEROSPIKE ENGINE | February 2024 | March 2025 | Allow | 13 | 1 | 0 | No | No |
| 18433223 | SYSTEM AND METHOD HAVING MULTI-FLUID INJECTORS FOR ISOTHERMAL EXPANSION IN TURBINE STAGE OF GAS TURBINE ENGINE | February 2024 | September 2024 | Allow | 8 | 1 | 0 | No | No |
| 18423649 | INJECTOR WITH DISC FOR HYDROGEN-DRIVEN GAS TURBINE ENGINE | January 2024 | October 2024 | Allow | 8 | 0 | 0 | No | No |
| 18421471 | GAS TURBINE ENGINE COMPRISING FUEL-OIL HEAT EXCHANGERS FLUIDLY CONNECTED TO FUEL SPRAY NOZZLES | January 2024 | March 2025 | Allow | 14 | 1 | 0 | No | No |
| 18579841 | A DEVICE TO PRODUCE HIGHER PRESSURE AND TEMPERATURE IN A GAS | January 2024 | September 2024 | Allow | 8 | 0 | 0 | No | No |
| 18409690 | GAS TURBINE FUEL NOZZLE HAVING AN INNER AIR PASSAGE AND PLURAL OUTER FUEL PASSAGES | January 2024 | September 2024 | Allow | 9 | 1 | 0 | No | No |
| 18577686 | THERMALLY INTEGRATED AMMONIA FUELLED ENGINE | January 2024 | February 2025 | Abandon | 14 | 1 | 0 | No | No |
| 18401572 | METHOD OF OPERATING GAS TURBINE COMBUSTOR WITH MULTIPLE FUEL STAGES | December 2023 | March 2025 | Allow | 15 | 2 | 0 | Yes | No |
| 18394407 | TURBINE ENGINE HAVING A COMBUSTION SECTION WITH A FUEL NOZZLE ASSEMBLY | December 2023 | October 2024 | Allow | 10 | 0 | 0 | No | No |
| 18571617 | INDUSTRIAL PREMIXED GAS COMBUSTOR USING INTERNAL EXHAUST GAS RECIRCULATION AND OPERATING METHOD THEREOF | December 2023 | June 2025 | Allow | 18 | 1 | 0 | No | No |
| 18541041 | CENTRAL STAGED COMBUSTION CHAMBER WITH SELF-EXCITED SWEEPING OSCILLATING FUEL INJECTION NOZZLES | December 2023 | September 2024 | Allow | 9 | 1 | 0 | No | No |
| 18529360 | METHOD OF OPERATING A GAS TURBINE COMBUSTOR COMPRISING INJECTING A DILUENT INTO THE PRIMARY AND SECONDARY COMBUSTION ZONES | December 2023 | September 2024 | Allow | 10 | 1 | 0 | No | No |
| 18507877 | SEQUENTIAL COMBUSTION GAS TURBINE ENGINE INCLUDING A STEAM SYSTEM FOR INJECTING STEAM TO EACH COMBUSTOR | November 2023 | April 2025 | Allow | 17 | 2 | 0 | Yes | No |
| 18488217 | METHOD OF STARTING A GAS TURBINE ENGINE | October 2023 | September 2024 | Allow | 11 | 0 | 1 | No | No |
| 18484827 | DRIVE SYSTEM FOR AN AIRCRAFT, AIRCRAFT HAVING A DRIVE SYSTEM AND METHOD FOR OPERATING AN AIRCRAFT | October 2023 | February 2025 | Allow | 17 | 2 | 0 | Yes | No |
| 18482949 | FUEL-AIR MIXING ASSEMBLY IN A TURBINE ENGINE | October 2023 | June 2024 | Allow | 9 | 0 | 0 | No | No |
| 18377776 | FUEL NOZZLE HAVING INNER AND OUTER MIXING CHAMBERS FED WITH FUEL VIA FIRST AND SECOND HOLE PATTERNS | October 2023 | December 2024 | Allow | 14 | 1 | 0 | No | No |
| 18479992 | GAS TURBINE COMBUSTION SYSTEM HAVING AN AMMONIA AUTOTHERMAL CRACKING DEVICE | October 2023 | November 2024 | Allow | 14 | 1 | 0 | No | No |
| 18372796 | INJECTION MANIFOLD WITH TESLA VALVES FOR ROTATING DETONATION ENGINES | September 2023 | August 2024 | Allow | 11 | 1 | 0 | No | No |
| 18473246 | GAS TURBINE COMBUSTOR INJECTOR ASSEMBLY COMPRISING AN AIR SUPPLY UNIT HAVING AN INCLINED SURFACE RELATIVE TO AN INCLINED INJECTION PIPE | September 2023 | September 2024 | Allow | 12 | 1 | 0 | No | No |
| 18472568 | METHOD FOR DETECTING AND ANNUNCIATING GAS TURBINE ENGINE COMPRESSOR STALL | September 2023 | July 2024 | Allow | 9 | 0 | 0 | No | No |
| 18464565 | GAS TURBINE COMBUSTOR STRUCTURE | September 2023 | June 2024 | Allow | 9 | 0 | 0 | No | No |
| 18463016 | COMBUSTION DEVICE COMPRISING PLURAL SWIRLING BLADES AND GAS TURBINE SYSTEM HAVING THE SAME | September 2023 | September 2024 | Allow | 13 | 1 | 0 | No | No |
| 18460078 | COMBUSTOR SWIRLER WITH VANES INCORPORATING OPEN AREA | September 2023 | October 2024 | Allow | 14 | 2 | 0 | No | No |
| 18240655 | GAS TURBINE ENGINE EXHAUST DIFFUSER HAVING MULTIPLE INCLINED SURFACES AT DIFFERENT ANGLES | August 2023 | August 2024 | Allow | 12 | 2 | 0 | No | No |
| 18238792 | CONTROLLABLE FUEL NOZZLE VALVES WITH REDUNDANCY | August 2023 | July 2024 | Allow | 11 | 1 | 0 | No | No |
| 18452958 | GAS TURBINE COMBUSTOR FUEL NOZZLE ASSEMBLY AND COMBUSTOR LINER HAVING DILUTION HOLES IN ARRANGEMENTS | August 2023 | September 2024 | Allow | 13 | 1 | 0 | No | No |
| 18234340 | ROTATING DETONATION AUGMENTORS WITH ADJUSTABLE THROATS FOR GAS TURBINE ENGINES | August 2023 | April 2024 | Allow | 8 | 0 | 0 | No | No |
| 18229319 | Hydrogen Injection For Enhanced Combustion Stability In Gas Turbine Systems | August 2023 | April 2024 | Allow | 9 | 0 | 0 | No | No |
| 18224869 | PROPORTIONAL RESTRICTION OF A SECONDARY CIRCUIT OF A FUEL INJECTOR | July 2023 | November 2024 | Allow | 16 | 2 | 0 | Yes | No |
| 18224843 | PROPORTIONAL RESTRICTION OF FUEL NOZZLE WITH AN AUXILIARY CIRCUIT | July 2023 | November 2024 | Allow | 16 | 1 | 0 | Yes | No |
| 18353424 | CONNECTING APPARATUS FOR THE FLOW CONNECTION BETWEEN A FUEL FEED LINE SYSTEM AND A NOZZLE APPARATUS, NOZZLE APPARATUS AND GAS TURBINE ARRANGEMENT | July 2023 | September 2024 | Allow | 14 | 1 | 0 | No | No |
| 18353405 | NOZZLE DEVICE FOR FEEDING AT LEAST ONE GASEOUS FUEL AND ONE LIQUID FUEL, SET, SUPPLY LINE SYSTEM, AND GAS TURBINE ASSEMBLY | July 2023 | July 2024 | Abandon | 12 | 1 | 0 | No | No |
| 18272178 | BURNER WITH TWO-LAYER VORTEX COUNTERCURRENT FLOW | July 2023 | March 2025 | Allow | 20 | 1 | 0 | No | No |
| 18261185 | FUEL SYSTEM AND METHOD FOR SUPPLYING A COMBUSTION CHAMBER IN AN AIRCRAFT TURBOSHAFT ENGINE WITH FUEL | July 2023 | August 2024 | Allow | 13 | 0 | 0 | Yes | No |
| 18350205 | FUEL NOZZLE AND SWIRLER | July 2023 | May 2024 | Allow | 10 | 1 | 0 | No | No |
| 18218683 | CANTILEVER STATOR VANE WITH DAMPER | July 2023 | March 2024 | Allow | 8 | 0 | 0 | No | No |
| 18347705 | MANIFOLD ASSEMBLY AND ANTI-ICE SYSTEM FOR GAS TURBINE ENGINE | July 2023 | May 2024 | Allow | 10 | 1 | 0 | No | No |
| 18345002 | COMPOSITE AIRFOIL ASSEMBLY FOR A TURBINE ENGINE | June 2023 | March 2024 | Allow | 8 | 0 | 0 | No | No |
| 18213571 | TURBULENCE GENERATOR MIXER FOR ROTATING DETONATION ENGINE | June 2023 | January 2025 | Allow | 18 | 2 | 1 | No | No |
| 18211624 | GAS TURBINE OPERATING CONDITIONS | June 2023 | November 2023 | Allow | 5 | 0 | 1 | No | No |
| 18206851 | GAS TURBINE CONTROL METHOD, STORAGE MEDIUM STORING GAS TURBINE CONTROL PROGRAM, GAS TURBINE CONTROL DEVICE, AND GAS TURBINE FACILITY | June 2023 | April 2024 | Allow | 10 | 0 | 0 | No | No |
| 18203973 | COMBINED HEAT AND POWER SYSTEM USING AND PRODUCING CO2 AND METHOD OF OPERATION | May 2023 | March 2024 | Allow | 10 | 0 | 0 | No | No |
| 18320682 | GAS TURBINE FUEL MIXER COMPRISING A PLURALITY OF MINI TUBES FOR GENERATING A FUEL-AIR MIXTURE | May 2023 | June 2024 | Allow | 13 | 1 | 0 | No | No |
| 18197558 | PRESSURE CONTROL FOR BIFURCATED FLOW OF A TURBINE ENGINE | May 2023 | July 2024 | Allow | 14 | 2 | 0 | Yes | No |
| 18317545 | HYDROGEN STEAM INJECTED AND INTER-COOLED TURBINE ENGINE | May 2023 | May 2024 | Allow | 12 | 0 | 1 | No | No |
| 18252079 | TURBOJET ENGINE REAR PART COMPRISING A NOZZLE HAVING FLAPS COMPRISING LEVERS THAT ARE MOVABLE BY MEANS OF UPSTREAM AND DOWNSTREAM BEARING WALLS | May 2023 | February 2024 | Allow | 9 | 0 | 0 | No | No |
| 18313137 | LIQUID ROCKET ENGINE INJECTOR WITH VARIABLE FLOW AREA | May 2023 | February 2024 | Allow | 10 | 1 | 0 | No | No |
| 18251798 | FASTENING OF AN EXHAUST CONE IN A TURBOMACHINE NOZZLE | May 2023 | January 2024 | Allow | 9 | 0 | 0 | No | No |
| 18251617 | COMBUSTOR INCLUDING HEAT EXCHANGE STRUCTURE AND ROCKET COMPRISING SAME | May 2023 | April 2024 | Allow | 12 | 1 | 0 | No | No |
| 18034686 | RESONATOR RING, METHOD AND BASKET | April 2023 | May 2024 | Allow | 12 | 3 | 0 | No | No |
| 18032937 | COMBUSTION ADJUSTMENT METHOD AND COMBUSTION CONTROL DEVICE OF GAS TURBINE | April 2023 | April 2024 | Allow | 12 | 1 | 0 | No | No |
| 18031917 | AERONAUTICAL PROPULSION SYSTEM WITH IMPROVED PROPULSIVE EFFICIENCY | April 2023 | December 2023 | Allow | 8 | 0 | 0 | No | No |
| 18248800 | METHOD FOR CONTROLLING MIXING RATIO BY THERMAL ACTION IN THE PROPELLANT TANKS OF SPACE SYSTEMS | April 2023 | June 2024 | Allow | 14 | 1 | 0 | No | No |
| 18248665 | FUEL SUPPLY CIRCUIT FOR A COMBUSTION CHAMBER OF A TURBOMACHINE | April 2023 | October 2023 | Allow | 7 | 0 | 0 | No | No |
| 18248666 | DEVICE FOR DISTRIBUTING FUEL FLOWS FOR A FUEL SUPPLY CIRCUIT OF A TURBOMACHINE COMBUSTION CHAMBER | April 2023 | April 2024 | Allow | 12 | 2 | 0 | No | No |
| 18129646 | BOOSTING GAS TURBINE ENGINE POWER WITH FLUID MOTOR | March 2023 | June 2024 | Allow | 14 | 2 | 0 | No | No |
| 18192144 | DUAL PROPELLANT MICROWAVE ELECTROTHERMAL PROPULSION SYSTEMS | March 2023 | June 2024 | Allow | 14 | 0 | 0 | No | No |
| 18245406 | ELECTRICAL CONNECTION OF AN ELECTRICAL MACHINE IN AN AIRCRAFT TURBINE ENGINE | March 2023 | August 2024 | Allow | 17 | 1 | 0 | No | No |
| 18121436 | FUEL INJECTOR ASSEMBLY FOR GAS TURBINE ENGINE WITH FUEL, AIR AND STEAM INJECTION | March 2023 | March 2024 | Allow | 12 | 1 | 0 | No | No |
| 18168912 | GAS TURBINE FUEL SPRAY NOZZLE HAVING ENHANCED SYPHOIC PURGE FUEL GALLERY | February 2023 | December 2024 | Allow | 22 | 1 | 0 | No | No |
| 18020177 | PERFORMANCE EVALUATION METHOD, OPERATION CONTROL METHOD, PERFORMANCE EVALUATION DEVICE, AND PROGRAM | February 2023 | December 2024 | Allow | 22 | 1 | 0 | No | No |
| 18007082 | CIRCUIT FOR SUPPLYING FUEL TO AN AERONAUTICAL CRYOGENIC TURBOMACHINE AND ASSOCIATED METHOD | January 2023 | June 2023 | Allow | 5 | 0 | 0 | No | No |
| 18097696 | Multi-Nozzle Fuel Injection Method for Gas Turbine | January 2023 | December 2023 | Allow | 10 | 2 | 0 | No | No |
| 18016024 | JET ENGINE FOR AIRCRAFT | January 2023 | October 2023 | Allow | 9 | 0 | 0 | No | No |
| 18092099 | SYSTEM AND METHOD HAVING MULTI-FLUID INJECTORS FOR ISOTHERMAL EXPANSION IN TURBINE STAGE OF GAS TURBINE ENGINE | December 2022 | October 2023 | Allow | 9 | 0 | 0 | No | No |
| 18090152 | DUAL CYCLE INTERCOOLED HYDROGEN ENGINE ARCHITECTURE | December 2022 | March 2024 | Allow | 14 | 1 | 0 | No | No |
| 18147208 | METHODS OF OPERATING A TURBOMACHINE COMBUSTOR ON HYDROGEN | December 2022 | February 2024 | Allow | 14 | 2 | 0 | No | No |
| 18081949 | COMBUSTOR HAVING THERMALLY COMPLIANT BUNDLED TUBE FUEL NOZZLE | December 2022 | October 2023 | Allow | 10 | 0 | 0 | No | No |
| 18061611 | DETONATION ROCKET ENGINE COMPRISING AN AEROSPIKE NOZZLE AND CENTRING ELEMENTS WITH COOLING CHANNELS | December 2022 | July 2023 | Allow | 8 | 0 | 0 | No | No |
| 17999832 | INSTALLATION FOR SUPPLYING CRYOGENIC FUEL TO THE COMBUSTION CHAMBER OF A TURBINE ENGINE | November 2022 | October 2023 | Allow | 11 | 0 | 0 | No | No |
| 17993574 | TANGENTIAL PRESSURE ATOMIZING TIP WITHOUT FEED CHAMBER | November 2022 | May 2024 | Allow | 18 | 1 | 1 | No | No |
| 17923588 | PILOT CONE COOLING | November 2022 | December 2023 | Allow | 14 | 1 | 0 | No | No |
This analysis examines appeal outcomes and the strategic value of filing appeals for examiner RODRIGUEZ, WILLIAM H.
With a 57.1% reversal rate, the PTAB has reversed the examiner's rejections more often than affirming them. This reversal rate is in the top 25% across the USPTO, indicating that appeals are more successful here than in most other areas.
Filing a Notice of Appeal can sometimes lead to allowance even before the appeal is fully briefed or decided by the PTAB. This occurs when the examiner or their supervisor reconsiders the rejection during the mandatory appeal conference (MPEP § 1207.01) after the appeal is filed.
In this dataset, 53.3% of applications that filed an appeal were subsequently allowed. This appeal filing benefit rate is in the top 25% across the USPTO, indicating that filing appeals is particularly effective here. The act of filing often prompts favorable reconsideration during the mandatory appeal conference.
✓ Appeals to PTAB show good success rates. If you have a strong case on the merits, consider fully prosecuting the appeal to a Board decision.
✓ Filing a Notice of Appeal is strategically valuable. The act of filing often prompts favorable reconsideration during the mandatory appeal conference.
Examiner RODRIGUEZ, WILLIAM H works in Art Unit 3741 and has examined 836 patent applications in our dataset. With an allowance rate of 90.4%, this examiner has an above-average tendency to allow applications. Applications typically reach final disposition in approximately 33 months.
Examiner RODRIGUEZ, WILLIAM H's allowance rate of 90.4% places them in the 72% percentile among all USPTO examiners. This examiner has an above-average tendency to allow applications.
On average, applications examined by RODRIGUEZ, WILLIAM H receive 1.32 office actions before reaching final disposition. This places the examiner in the 26% percentile for office actions issued. This examiner issues fewer office actions than average, which may indicate efficient prosecution or a more lenient examination style.
The median time to disposition (half-life) for applications examined by RODRIGUEZ, WILLIAM H is 33 months. This places the examiner in the 29% percentile for prosecution speed. Prosecution timelines are slightly slower than average with this examiner.
Conducting an examiner interview provides a +5.7% benefit to allowance rate for applications examined by RODRIGUEZ, WILLIAM H. This interview benefit is in the 32% percentile among all examiners. Recommendation: Interviews provide a below-average benefit with this examiner.
When applicants file an RCE with this examiner, 36.5% of applications are subsequently allowed. This success rate is in the 79% percentile among all examiners. Strategic Insight: RCEs are highly effective with this examiner compared to others. If you receive a final rejection, filing an RCE with substantive amendments or arguments has a strong likelihood of success.
This examiner enters after-final amendments leading to allowance in 61.8% of cases where such amendments are filed. This entry rate is in the 84% percentile among all examiners. Strategic Recommendation: This examiner is highly receptive to after-final amendments compared to other examiners. Per MPEP § 714.12, after-final amendments may be entered "under justifiable circumstances." Consider filing after-final amendments with a clear showing of allowability rather than immediately filing an RCE, as this examiner frequently enters such amendments.
When applicants request a pre-appeal conference (PAC) with this examiner, 50.0% result in withdrawal of the rejection or reopening of prosecution. This success rate is in the 43% percentile among all examiners. Note: Pre-appeal conferences show below-average success with this examiner. Consider whether your arguments are strong enough to warrant a PAC request.
This examiner withdraws rejections or reopens prosecution in 65.0% of appeals filed. This is in the 40% percentile among all examiners. Of these withdrawals, 38.5% occur early in the appeal process (after Notice of Appeal but before Appeal Brief). Strategic Insight: This examiner shows below-average willingness to reconsider rejections during appeals. Be prepared to fully prosecute appeals if filed.
When applicants file petitions regarding this examiner's actions, 39.3% are granted (fully or in part). This grant rate is in the 37% percentile among all examiners. Strategic Note: Petitions show below-average success regarding this examiner's actions. Ensure you have a strong procedural basis before filing.
Examiner's Amendments: This examiner makes examiner's amendments in 3.2% of allowed cases (in the 84% percentile). Per MPEP § 1302.04, examiner's amendments are used to place applications in condition for allowance when only minor changes are needed. This examiner frequently uses this tool compared to other examiners, indicating a cooperative approach to getting applications allowed. Strategic Insight: If you are close to allowance but minor claim amendments are needed, this examiner may be willing to make an examiner's amendment rather than requiring another round of prosecution.
Quayle Actions: This examiner issues Ex Parte Quayle actions in 6.9% of allowed cases (in the 83% percentile). Per MPEP § 714.14, a Quayle action indicates that all claims are allowable but formal matters remain. This examiner frequently uses Quayle actions compared to other examiners, which is a positive indicator that once substantive issues are resolved, allowance follows quickly.
Based on the statistical analysis of this examiner's prosecution patterns, here are tailored strategic recommendations:
Not Legal Advice: The information provided in this report is for informational purposes only and does not constitute legal advice. You should consult with a qualified patent attorney or agent for advice specific to your situation.
No Guarantees: We do not provide any guarantees as to the accuracy, completeness, or timeliness of the statistics presented above. Patent prosecution statistics are derived from publicly available USPTO data and are subject to data quality limitations, processing errors, and changes in USPTO practices over time.
Limitation of Liability: Under no circumstances will IronCrow AI be liable for any outcome, decision, or action resulting from your reliance on the statistics, analysis, or recommendations presented in this report. Past prosecution patterns do not guarantee future results.
Use at Your Own Risk: While we strive to provide accurate and useful prosecution statistics, you should independently verify any information that is material to your prosecution strategy and use your professional judgment in all patent prosecution matters.