Detailed information about the 100 most recent patent applications.
| Application Number | Title | Filing Date | Disposal Date | Disposition | Time (months) | Office Actions | Restrictions | Interview | Appeal |
|---|---|---|---|---|---|---|---|---|---|
| 19061269 | COMBUSTOR ASSEMBLY FOR A GAS TURBINE ENGINE | February 2025 | October 2025 | Allow | 8 | 1 | 1 | No | No |
| 18999527 | SYSTEMS AND METHODS FOR CONTROLLING AN EXHAUST SYSTEM | December 2024 | September 2025 | Allow | 9 | 1 | 0 | Yes | No |
| 18970185 | AIRCRAFT, BLEED-AIR SYSTEMS FOR AIRCRAFT, AND METHODS OF PROVIDING THRUST TO AIRCRAFT | December 2024 | November 2025 | Allow | 11 | 2 | 1 | No | No |
| 18968296 | GAS TURBINE ENGINE INCLUDING A FUEL NOZZLE HAVING VORTEX GENERATORS | December 2024 | October 2025 | Allow | 11 | 1 | 1 | No | No |
| 18776600 | INJECTION NOZZLE AND COMBUSTION DEVICE | July 2024 | March 2026 | Abandon | 20 | 2 | 1 | Yes | No |
| 18772375 | COMBUSTOR ASSEMBLY WITH FASTENED COMBUSTOR LINER AND HEAD | July 2024 | November 2025 | Allow | 16 | 2 | 1 | Yes | No |
| 18772636 | PROPULSION ASSEMBLY FOR AN AIRCRAFT | July 2024 | March 2025 | Allow | 8 | 0 | 0 | No | No |
| 18760497 | COMBUSTOR PANEL WITH RAIL INTEGRATED PERIMETER STUDS | July 2024 | March 2025 | Allow | 8 | 1 | 1 | No | No |
| 18723678 | COMBUSTOR OF GAS TURBINE INCLUDING A FIXTURE THAT ATTACHES A LINER TO AN OUTER WALL HAVING A COOLING AIR PASSAGE | June 2024 | June 2025 | Allow | 12 | 1 | 0 | Yes | No |
| 18738326 | SYSTEMS AND METHODS OF GENERATING POWER USING A HYDROGEN FUEL SYSTEM | June 2024 | May 2025 | Allow | 11 | 2 | 0 | Yes | No |
| 18734786 | Turbine Engine Centerbody Generator | June 2024 | May 2025 | Allow | 11 | 1 | 1 | Yes | No |
| 18669683 | COMBUSTOR ASSEMBLY FOR A GAS TURBINE ENGINE | May 2024 | July 2025 | Abandon | 14 | 1 | 1 | No | No |
| 18664924 | TURBINE ENGINE HAVING A MULTICAVITY DAMPER | May 2024 | March 2025 | Allow | 10 | 1 | 1 | Yes | No |
| 18659359 | AXIAL FUEL STAGE INJECTOR WITH MULTIPLE MIXING CHAMBERS, AND COMBUSTOR AND GT SYSTEM INCLUDING SAME | May 2024 | January 2026 | Allow | 20 | 2 | 1 | Yes | No |
| 18659355 | AXIAL FUEL STAGE INJECTOR WITH AXIALLY ELONGATED MIXING CHAMBERS, AND COMBUSTOR AND GT SYSTEM INCLUDING SAME | May 2024 | February 2026 | Allow | 22 | 2 | 1 | Yes | No |
| 18652125 | COMBUSTOR APPARATUS | May 2024 | January 2026 | Abandon | 20 | 2 | 1 | No | No |
| 18633815 | POWER PLANT CYCLE USING RENEWABLE ENERGY FACILITATED BY A SUPERSONIC SHOCK WAVE COMPRESSOR APPARATUS | April 2024 | August 2024 | Allow | 4 | 0 | 0 | Yes | No |
| 18620134 | COMPACT SINGLE VARIABLE DISPLACEMENT PUMP FUEL SYSTEM WITH HIGH PRESSURE FUEL OIL COOLER BYPASS AND GAS GENERATOR FAULT | March 2024 | July 2025 | Allow | 15 | 2 | 1 | Yes | No |
| 18605020 | TURBOMACHINE FOR AN AIRCRAFT PROPULSION DRIVE | March 2024 | March 2025 | Abandon | 12 | 1 | 0 | No | No |
| 18583035 | CABLE AND TROLLEY SYSTEM FOR USE WITHIN AN IRRIGATION SPAN ASSEMBLY | February 2024 | February 2026 | Allow | 24 | 0 | 1 | Yes | No |
| 18581718 | AIRCRAFT PROPULSION UNIT COMPRISING AT LEAST ONE PRESSURE RELIEF DEVICE AND AIRCRAFT HAVING AT LEAST ONE SUCH PROPULSION UNIT | February 2024 | December 2025 | Allow | 21 | 1 | 1 | No | No |
| 18433518 | POWER PLANT CYCLE FOR A NEW RENEWABLE ENERGY OR OTHER HEAT SOURCE FACILITATED BY A SUPERSONIC SHOCK WAVE COMPRESSOR APPARATUS | February 2024 | August 2024 | Allow | 6 | 0 | 1 | Yes | No |
| 18429661 | INJECTOR WITH FAIRING AND ANNULAR PASSAGE FOR HYDROGEN-DRIVEN GAS TURBINE ENGINE | February 2024 | October 2025 | Allow | 20 | 2 | 0 | No | Yes |
| 18426506 | HYDROGEN-DRIVEN GAS TURBINE ENGINE WITH INJECTOR RING | January 2024 | February 2026 | Allow | 25 | 4 | 0 | No | No |
| 18425041 | TURBOMACHINE HAVING IMPROVED MIXING TUBE ELEMENTS | January 2024 | September 2025 | Abandon | 19 | 2 | 0 | No | No |
| 18291951 | COMBUSTOR FOR A GAS TURBINE ENGINE INCLUDING A COLLAR SURROUNDING A SECONDARY FUEL INJECTOR TO DEFINE UPSTREAM AND DOWNSTREAM PURGE PATHS | January 2024 | January 2026 | Allow | 24 | 3 | 0 | Yes | No |
| 18522482 | POWER PLANT CYCLE FOR A NEW RENEWABLE ENERGY OR OTHER HEAT SOURCE FACILITATED BY A SUPERSONIC SHOCK WAVE COMPRESSOR APPARATUS | November 2023 | July 2025 | Abandon | 20 | 1 | 0 | No | No |
| 18386508 | COOLING FUEL INJECTOR SYSTEM FOR AN ATTRITABLE ENGINE | November 2023 | July 2025 | Allow | 21 | 1 | 0 | No | No |
| 18376699 | GAS TURBINE ENGINE WITH ENTRAINED PARTICLE SEPARATORS | October 2023 | March 2026 | Allow | 29 | 3 | 1 | Yes | No |
| 18453506 | COMBUSTOR INCLUDING A STEAM INJECTOR OPERABLY INJECTING STEAM INTO A TRAPPED VORTEX CAVITY | August 2023 | June 2025 | Allow | 21 | 2 | 1 | Yes | No |
| 18235417 | TURBINE ENGINE TIP CLEARANCE CONTROL UTILIZING ELECTRIC MACHINE | August 2023 | February 2026 | Allow | 30 | 3 | 1 | No | No |
| 18360891 | MOTOR AND MOTOR CONTROLLER THERMAL MANAGEMENT FEATURES | July 2023 | April 2025 | Allow | 20 | 2 | 1 | Yes | No |
| 18360911 | EMERGENCY START OF A GAS TURBINE ENGINE | July 2023 | September 2025 | Allow | 26 | 3 | 1 | Yes | No |
| 18226975 | COMBUSTOR ASSEMBLY | July 2023 | December 2024 | Abandon | 17 | 1 | 1 | No | No |
| 18359178 | COMBUSTION SECTION WITH A PRIMARY COMBUSTOR AND A SET OF SECONDARY COMBUSTORS | July 2023 | April 2025 | Allow | 20 | 3 | 1 | Yes | No |
| 18339032 | ELECTRIC PROPULSION UNIT COMPRISING AT LEAST TWO INDEPENDENT SUPPORTS, AIRCRAFT COMPRISING AT LEAST ONE SUCH ELECTRIC PROPULSION UNIT | June 2023 | October 2025 | Abandon | 28 | 2 | 0 | Yes | No |
| 18326665 | TURBINE ENGINE INCLUDING A COMBUSTOR | May 2023 | August 2025 | Allow | 26 | 2 | 1 | Yes | No |
| 18326669 | TURBINE ENGINE INCLUDING A COMBUSTOR HAVING A TRAPPED VORTEX CAVITY DOWNSTREAM OF A COMBUSTION ZONE | May 2023 | February 2026 | Allow | 32 | 3 | 1 | Yes | No |
| 18251379 | MODULARITY OF AN AIRCRAFT TURBOMACHINE | May 2023 | February 2026 | Allow | 33 | 3 | 0 | No | No |
| 18113791 | VERTICAL JOINT COUPLING STRUCTURE OF CASING, AND GAS TURBINE HAVING SAME | February 2023 | September 2024 | Allow | 19 | 1 | 0 | No | No |
| 18171491 | BLOWER SYSTEM FOR BIDIRECTIONAL FLOW | February 2023 | June 2025 | Allow | 27 | 1 | 0 | Yes | No |
| 18103935 | AIRCRAFT HYBRID PROPULSION FAN DRIVE GEAR SYSTEM DC MOTORS AND GENERATORS | January 2023 | November 2024 | Allow | 22 | 1 | 1 | No | No |
| 18015788 | GAS TURBINE PLANT | January 2023 | April 2025 | Abandon | 27 | 2 | 0 | Yes | No |
| 18151721 | AIRCRAFT ENGINE EXHAUST MIXER | January 2023 | July 2024 | Abandon | 18 | 2 | 1 | No | No |
| 18149844 | REHEAT ASSEMBLY FOR GAS TURBINE ENGINE | January 2023 | May 2025 | Abandon | 28 | 4 | 1 | No | No |
| 18065984 | GAS TURBINE PROPULSION SYSTEM | December 2022 | December 2025 | Abandon | 36 | 2 | 0 | No | Yes |
| 17924324 | SYSTEM FOR PURGING A FUEL HAVING REACTIVE GAS | November 2022 | August 2025 | Abandon | 33 | 4 | 0 | No | No |
| 17919463 | SPARK PLUG FOR A SINGLE-PIECE COMBUSTION CHAMBER | October 2022 | July 2023 | Allow | 9 | 1 | 0 | Yes | No |
| 17933981 | HEAT TRANSFER DEVICE, TURBOMACHINE CASING AND RELATED STORAGE MEDIUM | September 2022 | July 2024 | Abandon | 22 | 2 | 0 | Yes | No |
| 17932319 | FUEL NOZZLE | September 2022 | August 2025 | Abandon | 35 | 4 | 0 | No | No |
| 17941537 | COMBUSTOR AND GAS TURBINE PROVIDED WITH SAME | September 2022 | December 2025 | Abandon | 39 | 4 | 0 | Yes | No |
| 17801376 | AIRCRAFT WING-PYLON CONNECTION | August 2022 | June 2025 | Allow | 34 | 2 | 1 | Yes | No |
| 17844989 | TURBOFAN COMPRISING A SERIES OF ROTARY BLADES FOR CLOSING OFF THE DUCT FOR THE SECONDARY STREAM | June 2022 | August 2023 | Allow | 14 | 1 | 0 | No | No |
| 17844280 | TURBOFAN HAVING A SET OF ROTATABLE BLADES FOR BLOCKING OFF THE DUCT FOR THE BYPASS FLOW | June 2022 | December 2022 | Allow | 6 | 0 | 0 | Yes | No |
| 17786084 | EXHAUST GAS PROCESSING EQUIPMENT AND GAS TURBINE PLANT | June 2022 | April 2025 | Allow | 34 | 2 | 0 | No | No |
| 17835524 | AIRCRAFT AND METHOD FOR PRE-COOLING AN ENVIRONMENTAL CONTROL SYSTEM | June 2022 | April 2025 | Abandon | 34 | 4 | 1 | No | No |
| 17804636 | VARIABLE MIXING NOZZLE DESIGN FOR JET NOISE REDUCTION | May 2022 | June 2024 | Abandon | 25 | 3 | 0 | No | No |
| 17664975 | COMBUSTOR WITH A VARIABLE PRIMARY ZONE COMBUSTION CHAMBER | May 2022 | May 2024 | Allow | 24 | 2 | 1 | No | No |
| 17779203 | ELECTRIC MODULE FOR AN AIRCRAFT TURBOMACHINE | May 2022 | November 2024 | Allow | 30 | 1 | 0 | Yes | No |
| 17663314 | PURGE SYSTEM FOR A HYDROGEN FUEL SYSTEM | May 2022 | July 2025 | Allow | 38 | 6 | 1 | Yes | No |
| 17734469 | A COMBUSTOR FOR A TURBINE ENGINE HAVING A FUEL-AIR MIXER INCLUDING A SET OF MIXING PASSAGES | May 2022 | September 2024 | Allow | 29 | 3 | 1 | Yes | No |
| 17689307 | COMBUSTOR FOR GAS TURBINE ENGINE INCLUDING A PLURALITY OF PROJECTIONS EXTENDING TOWARD A COMPRESSED AIR CHAMBER | March 2022 | July 2023 | Allow | 16 | 2 | 1 | Yes | No |
| 17650537 | REACTION AND DESIGN CONCEPT FOR ENGINES FOR CATALYTIC CONTROL / ERGETIC TRIGGERING (E.G. WITH METAL ADDITIVES) OF THE INTERNAL VELOCITY (ACCELERATION) AND EXIT VELOCITY WITH INFLUENCING OF TEMPERATURE AS WELL AS PRESSURE FOR IMPROVED 5 EFFICIENCY AND COMBUSTION CHAMBER ADAPTATION (TREIBER-CONCEPT) | February 2022 | January 2025 | Abandon | 35 | 0 | 1 | No | No |
| 17499083 | COMBUSTOR SWIRLER TO DOME ATTACHMENT | October 2021 | November 2024 | Allow | 37 | 6 | 0 | No | No |
| 17403081 | COMBUSTION CHAMBER COMPRISING AN ANNULAR TONGUE STRUCTURE OF A COMBUSTOR HEAD THAT ENGAGES A GROOVE PORTION OF CIRCUMFERENTIALY ARRANGED CASSETTE SEGMENTS | August 2021 | November 2023 | Abandon | 27 | 2 | 1 | No | No |
| 17393508 | TURBOFAN WITH OFFSET GAS GENERATOR AND AUXILIARY POWER CORE | August 2021 | July 2023 | Allow | 24 | 2 | 1 | No | No |
| 17376675 | AIRCRAFT HYBRID PROPULSION FAN DRIVE GEAR SYSTEM DC MOTORS AND GENERATORS | July 2021 | November 2022 | Allow | 16 | 1 | 1 | Yes | No |
| 17416956 | TURBOMACHINE COMBUSTION CHAMBER INCLUDING FLEXIBLE SEALED CONNECTIONS ALLOWING FOR MULTIDIRECTIONAL CLEARANCE | June 2021 | July 2023 | Abandon | 24 | 2 | 0 | Yes | No |
| 17340816 | COMBUSTOR FOR A GAS TURBINE ENGINE INCLUDING A LINER HAVING A LOOPED FEATURE | June 2021 | September 2023 | Allow | 27 | 3 | 1 | No | No |
| 17316126 | SCREW ROCKET NOZZLE | May 2021 | August 2023 | Abandon | 27 | 1 | 1 | No | No |
| 17198150 | VOLUTE TRAPPED VORTEX COMBUSTOR ASSEMBLY | March 2021 | October 2023 | Allow | 31 | 3 | 1 | Yes | No |
| 17166621 | FUEL INJECTION DEVICE FOR GAS TURBINE | February 2021 | June 2023 | Abandon | 28 | 2 | 0 | Yes | No |
| 17149266 | COMBUSTION CHAMBER WITH PARTICLE SEPARATOR | January 2021 | December 2022 | Allow | 23 | 2 | 0 | Yes | No |
| 17137526 | MITIGATING COMBUSTION DYNAMICS USING VARYING LIQUID FUEL CARTRIDGES | December 2020 | June 2025 | Abandon | 54 | 6 | 0 | No | No |
| 17256600 | TURBOMACHINE FOR AIRCRAFT COMPRISING A PLURALITY OF VARIABLE BYPASS VALVES AND CONTROL METHOD | December 2020 | September 2022 | Allow | 21 | 1 | 0 | No | No |
| 17120190 | Hybrid power generation equipment and control method thereof | December 2020 | April 2023 | Allow | 28 | 3 | 0 | No | No |
| 17110448 | THERMAL MANAGEMENT SYSTEM AND METHOD OF USING SAME | December 2020 | May 2023 | Abandon | 29 | 2 | 1 | No | No |
| 17096581 | GAS TURBINE ENGINE OPERATING POINT | November 2020 | November 2022 | Abandon | 24 | 1 | 0 | Yes | No |
| 17018580 | COMBUSTOR DILUTION HOLE ACTIVE HEAT TRANSFER CONTROL APPARATUS AND SYSTEM | September 2020 | April 2024 | Abandon | 43 | 3 | 1 | Yes | No |
| 17007060 | IMPINGEMENT COOLING APPARATUS FOR TURBOMACHINE | August 2020 | August 2023 | Allow | 35 | 3 | 0 | Yes | No |
| 17007089 | IMPINGEMENT COOLING APPARATUS SUPPORT STRUCTURE AND METHOD OF MANUFACTURE | August 2020 | September 2023 | Allow | 36 | 2 | 1 | No | No |
| 17004280 | HOT GAS PATH COMPONENT WITH METERING STRUCTURE INCLUDING CONVERGING-DIVERGING PASSAGE PORTIONS | August 2020 | June 2023 | Abandon | 33 | 2 | 1 | Yes | No |
| 16771060 | TUBULAR COMBUSTION CHAMBER WITH CERAMIC CLADDING | June 2020 | June 2024 | Abandon | 49 | 4 | 0 | Yes | No |
| 16893570 | VARYING THE BYPASS RATIO OF A TURBOFAN ENGINE | June 2020 | June 2023 | Abandon | 36 | 2 | 0 | Yes | No |
| 16892519 | LIMITING SPOOL SPEEDS IN A GAS TURBINE ENGINE | June 2020 | October 2023 | Abandon | 40 | 5 | 0 | Yes | No |
| 16892472 | REDUCING IDLE THRUST IN A PROPULSIVE GAS TURBINE | June 2020 | August 2023 | Abandon | 38 | 4 | 0 | Yes | No |
| 16890142 | CROSS FIRE TUBE INSTALLATION/REMOVAL METHODS AND APPARATUS | June 2020 | March 2026 | Allow | 60 | 4 | 0 | Yes | Yes |
| 16652074 | SUPERSONIC AIR INTAKE PASSAGE CAPABLE OF ACHIEVING SYNCHRONOUS ADJUSTMENT OF CAPTURING AREA AND THROAT AREA | May 2020 | November 2022 | Allow | 31 | 1 | 0 | Yes | No |
| 16845224 | TURBOFAN COMPRISING A SET OF ROTATABLE BLADES FOR BLOCKING OFF THE BYPASS FLOW DUCT | April 2020 | March 2022 | Allow | 23 | 0 | 0 | Yes | No |
| 16844596 | VANE SUPPORT SYSTEM | April 2020 | March 2025 | Allow | 59 | 2 | 1 | No | Yes |
| 16842915 | BURNER COOLING STRUCTURES | April 2020 | June 2023 | Allow | 38 | 3 | 0 | Yes | No |
| 16839923 | HYBRID PNEUMATIC AND ELECTRIC SECONDARY POWER INTEGRATED CABIN ENERGY SYSTEM FOR A PRESSURIZED VEHICLE | April 2020 | November 2022 | Abandon | 32 | 3 | 0 | Yes | No |
| 16825888 | PROCESS FOR REGULATING FLOWS IN OPERATION OF A POWER GENERATION PLANT | March 2020 | June 2023 | Abandon | 39 | 4 | 0 | No | Yes |
| 16825132 | FUEL INJECTOR FOR A TURBINE ENGINE | March 2020 | October 2022 | Abandon | 31 | 1 | 0 | No | No |
| 16825892 | PROCESS FOR CONTROLLING OXIDANT FLOWS IN OPERATION OF A POWER GENERATION PLANT | March 2020 | June 2023 | Abandon | 39 | 3 | 0 | No | Yes |
| 16803134 | MECHANICAL DEMAND FUEL PUMPING SYSTEM | February 2020 | November 2023 | Abandon | 45 | 4 | 1 | Yes | No |
| 16801379 | TEMPERATURE-MODULATED RECUPERATED GAS TURBINE ENGINE | February 2020 | April 2023 | Abandon | 38 | 2 | 1 | No | Yes |
| 16793773 | COMBUSTION CHAMBER ASSEMBLY WITH SHINGLE MEMBER AND BASE BODIES ALIGNED THEREWITH, EACH CARRYING A FASTENING ELEMENT, AND METHOD OF MANUFACTURING | February 2020 | April 2023 | Abandon | 38 | 2 | 1 | Yes | No |
| 16785787 | STACKABLE AIR SWIRLERS | February 2020 | March 2023 | Abandon | 37 | 1 | 0 | Yes | No |
| 16786475 | CMC CROSS-OVER TUBE | February 2020 | February 2022 | Allow | 24 | 3 | 1 | Yes | No |
This analysis examines appeal outcomes and the strategic value of filing appeals for examiner BURKE, THOMAS P.
With a 31.1% reversal rate, the PTAB reverses the examiner's rejections in a meaningful percentage of cases. This reversal rate is below the USPTO average, indicating that appeals face more challenges here than typical.
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, 26.2% of applications that filed an appeal were subsequently allowed. This appeal filing benefit rate is below the USPTO average, suggesting that filing an appeal has limited effectiveness in prompting favorable reconsideration.
⚠ Appeals to PTAB face challenges. Ensure your case has strong merit before committing to full Board review.
⚠ Filing a Notice of Appeal shows limited benefit. Consider other strategies like interviews or amendments before appealing.
Examiner BURKE, THOMAS P works in Art Unit 3741 and has examined 326 patent applications in our dataset. With an allowance rate of 39.0%, this examiner allows applications at a lower rate than most examiners at the USPTO. Applications typically reach final disposition in approximately 43 months.
Examiner BURKE, THOMAS P's allowance rate of 39.0% places them in the 7% percentile among all USPTO examiners. This examiner is less likely to allow applications than most examiners at the USPTO.
On average, applications examined by BURKE, THOMAS P receive 3.00 office actions before reaching final disposition. This places the examiner in the 87% percentile for office actions issued. This examiner issues more office actions than most examiners, which may indicate thorough examination or difficulty in reaching agreement with applicants.
The median time to disposition (half-life) for applications examined by BURKE, THOMAS P is 43 months. This places the examiner in the 17% percentile for prosecution speed. Applications take longer to reach final disposition with this examiner compared to most others.
Conducting an examiner interview provides a +23.4% benefit to allowance rate for applications examined by BURKE, THOMAS P. This interview benefit is in the 69% percentile among all examiners. Recommendation: Interviews provide an above-average benefit with this examiner and are worth considering.
When applicants file an RCE with this examiner, 11.4% of applications are subsequently allowed. This success rate is in the 6% percentile among all examiners. Strategic Insight: RCEs show lower effectiveness with this examiner compared to others. Consider whether a continuation application might be more strategic, especially if you need to add new matter or significantly broaden claims.
This examiner enters after-final amendments leading to allowance in 13.8% of cases where such amendments are filed. This entry rate is in the 14% percentile among all examiners. Strategic Recommendation: This examiner rarely enters after-final amendments compared to other examiners. You should generally plan to file an RCE or appeal rather than relying on after-final amendment entry. Per MPEP § 714.12, primary examiners have discretion in entering after-final amendments, and this examiner exercises that discretion conservatively.
When applicants request a pre-appeal conference (PAC) with this examiner, 0.0% result in withdrawal of the rejection or reopening of prosecution. This success rate is in the 21% percentile among all examiners. Note: Pre-appeal conferences show limited success with this examiner compared to others. While still worth considering, be prepared to proceed with a full appeal brief if the PAC does not result in favorable action.
This examiner withdraws rejections or reopens prosecution in 40.8% of appeals filed. This is in the 8% percentile among all examiners. Of these withdrawals, 12.9% occur early in the appeal process (after Notice of Appeal but before Appeal Brief). Strategic Insight: This examiner rarely withdraws rejections during the appeal process compared to other examiners. If you file an appeal, be prepared to fully prosecute it to a PTAB decision. Per MPEP § 1207, the examiner will prepare an Examiner's Answer maintaining the rejections.
When applicants file petitions regarding this examiner's actions, 0.0% are granted (fully or in part). This grant rate is in the 7% percentile among all examiners. Strategic Note: Petitions are rarely granted regarding this examiner's actions compared to other examiners. Ensure you have a strong procedural basis before filing a petition, as the Technology Center Director typically upholds this examiner's decisions.
Examiner's Amendments: This examiner makes examiner's amendments in 0.0% of allowed cases (in the 43% percentile). This examiner makes examiner's amendments less often than average. You may need to make most claim amendments yourself.
Quayle Actions: This examiner issues Ex Parte Quayle actions in 0.0% of allowed cases (in the 46% percentile). This examiner issues Quayle actions less often than average. Allowances may come directly without a separate action for formal matters.
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.