Detailed information about the 100 most recent patent applications.
| Application Number | Title | Filing Date | Disposal Date | Disposition | Time (months) | Office Actions | Restrictions | Interview | Appeal |
|---|---|---|---|---|---|---|---|---|---|
| 18772636 | PROPULSION ASSEMBLY FOR AN AIRCRAFT | July 2024 | March 2025 | Allow | 8 | 0 | 0 | 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 |
| 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 |
| 18605020 | TURBOMACHINE FOR AN AIRCRAFT PROPULSION DRIVE | March 2024 | March 2025 | Abandon | 12 | 1 | 0 | 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 |
| 18453506 | COMBUSTOR INCLUDING A STEAM INJECTOR OPERABLY INJECTING STEAM INTO A TRAPPED VORTEX CAVITY | August 2023 | June 2025 | Allow | 21 | 2 | 1 | Yes | No |
| 18360891 | MOTOR AND MOTOR CONTROLLER THERMAL MANAGEMENT FEATURES | July 2023 | April 2025 | Allow | 20 | 2 | 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 |
| 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 |
| 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 |
| 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 |
| 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 |
| 16892472 | REDUCING IDLE THRUST IN A PROPULSIVE GAS TURBINE | June 2020 | August 2023 | Abandon | 38 | 4 | 0 | Yes | No |
| 16892519 | LIMITING SPOOL SPEEDS IN A GAS TURBINE ENGINE | June 2020 | October 2023 | Abandon | 40 | 5 | 0 | Yes | No |
| 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 |
| 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 |
| 16825888 | PROCESS FOR REGULATING FLOWS IN OPERATION OF A POWER GENERATION PLANT | March 2020 | June 2023 | Abandon | 39 | 4 | 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 |
| 16743077 | INTERNAL STRUCTURE OF A PRIMARY EXHAUST DUCT | January 2020 | October 2022 | Allow | 33 | 3 | 0 | Yes | No |
| 16719364 | AIRCRAFT ENGINE HAVING A BYPASS GAS PATH AND A BOOSTER GAS PATH AND METHOD OF OPERATION THEREOF | December 2019 | June 2023 | Abandon | 42 | 4 | 0 | Yes | No |
| 16719352 | AIRCRAFT ENGINE AND METHOD OF OPERATION THEREOF | December 2019 | July 2024 | Abandon | 54 | 4 | 1 | Yes | No |
| 16719341 | AIRCRAFT ENGINE AND METHOD OF OPERATION THEREOF | December 2019 | October 2023 | Abandon | 46 | 4 | 1 | No | No |
| 16705644 | BLUFF-BODY PILOTED HIGH-SHEAR INJECTOR AND METHOD OF USING SAME | December 2019 | February 2023 | Allow | 39 | 4 | 1 | Yes | No |
| 16613982 | HYBRID PROPULSIVE ARCHITECTURE FOR AN AIRCRAFT COMPRISING AN ENGINE WITH A REVERSIBLE ELECTRIC MACHINE MOUNTED ON TWO SHAFTS | November 2019 | March 2023 | Allow | 40 | 2 | 0 | Yes | No |
| 16682231 | LOW PRESSURE DIFFERENTIAL EJECTOR PUMP UTILIZING A LOBED, AXISYMMETRIC NOZZLE | November 2019 | November 2023 | Abandon | 48 | 6 | 0 | Yes | No |
| 16677826 | FLANGE BENDING SUPPORT | November 2019 | October 2022 | Abandon | 35 | 1 | 0 | No | No |
| 16599756 | COMBUSTOR FOR A GAS TURBINE ENGINE WITH CERAMIC MATRIX COMPOSITE SEALING ELEMENT | October 2019 | July 2022 | Allow | 33 | 3 | 1 | Yes | No |
| 16596129 | SYSTEM AND METHOD FOR OPERATING A MULTI-ENGINE ROTORCRAFT | October 2019 | June 2023 | Allow | 44 | 3 | 0 | Yes | No |
| 16593638 | SUPPORT STRUCTURE FOR A TURBINE VANE OF A GAS TURBINE ENGINE | October 2019 | May 2023 | Allow | 44 | 4 | 1 | Yes | No |
| 16579383 | HIGH TEMPERATURE GRADIENT GAS MIXER | September 2019 | August 2022 | Allow | 34 | 2 | 0 | Yes | No |
| 16575930 | GAS TURBINE COMBUSTOR | September 2019 | November 2021 | Allow | 26 | 1 | 1 | Yes | No |
| 16573200 | TURBINE ENGINE | September 2019 | September 2022 | Abandon | 36 | 1 | 1 | No | No |
| 16571396 | FLAMEOUT RISK MITIGATION IN ENGINES | September 2019 | March 2023 | Abandon | 42 | 4 | 0 | No | No |
| 16489193 | JET ENGINE WITH A RADIALLY VARIABLE WALL | August 2019 | October 2022 | Abandon | 37 | 2 | 0 | No | No |
| 16546368 | AIRCRAFT PROPULSION SYSTEM | August 2019 | September 2020 | Abandon | 13 | 0 | 0 | No | No |
| 16545281 | POWER SYSTEM FOR ROTARY WING AIRCRAFT | August 2019 | July 2022 | Abandon | 35 | 0 | 1 | No | No |
| 16543268 | FUEL NOZZLE, AND COMBUSTOR AND GAS TURBINE HAVING THE SAME | August 2019 | October 2021 | Allow | 26 | 2 | 0 | No | No |
| 16538544 | AERODYNAMIC GUIDE PLATE COLLAR FOR SWIRLER ASSEMBLY | August 2019 | February 2022 | Allow | 30 | 1 | 0 | Yes | No |
| 16526427 | DIFFUSER CASE HEATSHIELDS FOR GAS TURBINE ENGINES | July 2019 | August 2023 | Abandon | 49 | 6 | 0 | No | No |
| 16522463 | PROPULSION SYSTEM FOR AN AIRCRAFT AND METHOD OF MANUFACTURING A PROPULSION SYSTEM FOR AN AIRCRAFT | July 2019 | January 2022 | Abandon | 30 | 2 | 0 | No | No |
| 16451792 | GAS TURBINE ENGINE OUTLET GUIDE VANES | June 2019 | October 2022 | Abandon | 39 | 4 | 0 | No | No |
| 16448778 | COOLING FUEL INJECTOR SYSTEM FOR AN ATTRITABLE ENGINE | June 2019 | April 2024 | Abandon | 57 | 8 | 0 | Yes | No |
| 16433664 | AIRCRAFT ENGINE HAVING TWO GAS PATHS AND METHOD OF OPERATING SAME | June 2019 | October 2023 | Abandon | 52 | 6 | 0 | No | No |
| 16431245 | HYBRID GAS TURBOFAN POWERED SUB-IDLE DESCENT MODE | June 2019 | January 2025 | Abandon | 60 | 2 | 1 | Yes | Yes |
| 16398878 | GAS TURBINE ENGINE OPERATING POINT | April 2019 | March 2021 | Abandon | 22 | 2 | 1 | Yes | No |
| 16393185 | SCREW ROCKET NOZZLE | April 2019 | May 2022 | Abandon | 37 | 1 | 1 | No | No |
| 16391626 | AIR INTAKE SYSTEM | April 2019 | November 2021 | Allow | 31 | 3 | 0 | Yes | No |
| 16386169 | IN-SITU SOLID ROCKET MOTOR PROPELLANT GRAIN AGING USING LIQUID | April 2019 | April 2022 | Allow | 36 | 0 | 1 | Yes | No |
| 16361756 | ROCKETS EMBEDDED SCRAMJET NOZZLE (RESN) | March 2019 | March 2023 | Abandon | 48 | 3 | 0 | Yes | No |
| 16351405 | ROCKET TANK LIQUID LEVEL DETERMINATION, AND ASSOCIATED SYSTEMS AND METHODS | March 2019 | February 2025 | Allow | 60 | 3 | 0 | Yes | Yes |
| 16260543 | GAS TURBINE ENGINE COMBUSTOR WITH TAILORED TEMPERATURE PROFILE | January 2019 | June 2022 | Abandon | 41 | 4 | 0 | Yes | No |
| 16260606 | HYBRID FOSSIL FUEL AND SOLAR HEATED SUPERCRITICAL CARBON DIOXIDE POWER GENERATING SYSTEM AND METHOD | January 2019 | October 2021 | Abandon | 33 | 1 | 1 | No | No |
| 16213047 | CASING WITH INTEGRAL CAVITY | December 2018 | October 2023 | Abandon | 58 | 2 | 1 | No | Yes |
This analysis examines appeal outcomes and the strategic value of filing appeals for examiner BURKE, THOMAS P.
With a 26.2% reversal rate, the PTAB affirms the examiner's rejections in the vast majority 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, 22.4% 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 346 patent applications in our dataset. With an allowance rate of 40.2%, this examiner allows applications at a lower rate than most examiners at the USPTO. Applications typically reach final disposition in approximately 42 months.
Examiner BURKE, THOMAS P's allowance rate of 40.2% places them in the 4% 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 2.91 office actions before reaching final disposition. This places the examiner in the 94% 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 42 months. This places the examiner in the 5% percentile for prosecution speed. Applications take longer to reach final disposition with this examiner compared to most others.
Conducting an examiner interview provides a +24.9% benefit to allowance rate for applications examined by BURKE, THOMAS P. This interview benefit is in the 75% percentile among all examiners. Recommendation: Interviews are highly effective with this examiner and should be strongly considered as a prosecution strategy. Per MPEP § 713.10, interviews are available at any time before the Notice of Allowance is mailed or jurisdiction transfers to the PTAB.
When applicants file an RCE with this examiner, 12.3% of applications are subsequently allowed. This success rate is in the 3% 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 13.6% of cases where such amendments are filed. This entry rate is in the 8% 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 19% 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 40.0% of appeals filed. This is in the 5% percentile among all examiners. Of these withdrawals, 14.3% 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, 20.0% are granted (fully or in part). This grant rate is in the 11% 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 39% 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 40% 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.