Detailed information about the 100 most recent patent applications.
| Application Number | Title | Filing Date | Disposal Date | Disposition | Time (months) | Office Actions | Restrictions | Interview | Appeal |
|---|---|---|---|---|---|---|---|---|---|
| 19207845 | CLEARANCE PROBE ASSEMBLY USING REPLENISHABLE, CONTACTING ELONGATED CLEARANCE TIP | May 2025 | August 2025 | Allow | 3 | 0 | 0 | Yes | No |
| 18972209 | GEARBOX ASSEMBLY WITH LUBRICANT EXTRACTION VOLUME RATIO | December 2024 | September 2025 | Allow | 10 | 1 | 1 | Yes | No |
| 18899997 | INTRODUCING STEAM WITH QUENCH AIR INTO TURBINE ENGINE COMBUSTOR | September 2024 | January 2026 | Allow | 16 | 1 | 1 | Yes | No |
| 18883610 | TURBINE ENGINE HAVING A PLURALITY OF LUBRICANT STRUTS, EACH DEFINING A LUBRICANT STRUT FLOWPATH | September 2024 | December 2025 | Allow | 15 | 2 | 0 | Yes | No |
| 18844258 | A METHOD FOR THE COMBUSTION OF A FUEL GAS | September 2024 | January 2026 | Abandon | 16 | 1 | 0 | No | No |
| 18843154 | EJECTION CONE WITH AN ACOUSTIC CHAMBER FOR AN AIRCRAFT TURBINE ENGINE | August 2024 | March 2026 | Allow | 18 | 1 | 0 | No | No |
| 18796453 | CMC COMBUSTOR DEFLECTOR | August 2024 | March 2025 | Allow | 7 | 0 | 1 | Yes | No |
| 18836448 | HEATING TURBOMACHINE FOR A FUEL-CONDITIONING SYSTEM CONFIGURED TO SUPPLY AN AIRCRAFT TURBOSHAFT ENGINE WITH FUEL FROM A CRYOGENIC TANK | August 2024 | June 2025 | Allow | 10 | 0 | 0 | Yes | No |
| 18649607 | MONOLITHIC SUPERSTRUCTURE FOR GAS TURBINE ENGINES | April 2024 | March 2026 | Allow | 23 | 3 | 0 | Yes | No |
| 18614885 | MAGNETIC FRAGRANCE CARD | March 2024 | March 2026 | Allow | 23 | 0 | 1 | No | No |
| 18431620 | BIFURCATION INTEGRATED ELECTRICAL SYSTEM FOR HYBRID AIRCRAFT PROPULSION SYSTEM | February 2024 | December 2025 | Allow | 22 | 2 | 0 | No | No |
| 18546351 | CONSTRUCTING A TURBOMACHINERY INSTALLATION FOR ASSEMBLY ONSHORE AND INSTALLATION ON AN OFFSHORE PLATFORM | August 2023 | March 2026 | Allow | 31 | 1 | 0 | Yes | No |
| 18447525 | GAS TURBINE ENGINE WITH COMPOSITE AIRFOIL AND PREFORM CORE | August 2023 | November 2025 | Allow | 28 | 3 | 1 | Yes | No |
| 18253081 | HYBRID PROPULSION TURBOPROP ENGINE COUPLED TO A PROPELLER AND AIRCRAFT COMPRISING SUCH A TURBOPROP ENGINE | August 2023 | January 2026 | Allow | 32 | 1 | 0 | Yes | No |
| 18365299 | CONTAINMENT RING CAVITY PRESSURIZATION SYSTEM | August 2023 | May 2025 | Abandon | 21 | 3 | 0 | No | No |
| 18358647 | COMBUSTION CHAMBER ASSEMBLY FOR OPERATION WITH LIQUID AND/OR GASEOUS FUEL, GAS TURBINE ASSEMBLY AND METHOD | July 2023 | August 2025 | Allow | 25 | 1 | 1 | Yes | No |
| 18273432 | METHOD FOR CONTROLLING OPERATION MODES OF GAS TURBINE SYSTEM | July 2023 | March 2025 | Allow | 20 | 1 | 0 | Yes | No |
| 18251025 | FREE TURBINE TURBOMACHINE COMPRISING EQUIPMENT DRIVEN BY THE FREE TURBINE | July 2023 | September 2024 | Allow | 17 | 2 | 0 | Yes | No |
| 18337717 | OIL SYSTEM | June 2023 | October 2024 | Abandon | 15 | 2 | 0 | No | No |
| 18257367 | PROPULSION UNIT FOR AN AIRCRAFT COMPRISING A SYSTEM FOR SEALING BETWEEN TWO AIR INTAKE PARTS | June 2023 | August 2025 | Allow | 26 | 1 | 0 | No | No |
| 18204068 | AIRCRAFT POWER AND PROPULSION SYSTEMS COMPRISING PERMANENT MAGNET ELECTRICAL MACHINES | May 2023 | July 2025 | Allow | 26 | 1 | 1 | Yes | No |
| 18251031 | FREE TURBINE TURBOGENERATOR COMPRISING A REVERSIBLE ELECTRICAL MACHINE COUPLED TO THE FREE TURBINE | April 2023 | August 2025 | Allow | 28 | 6 | 0 | Yes | No |
| 18298952 | OVERALL AIRCRAFT SYSTEM DATA COLLECTOR FOR PROGNOSTICS AND HEALTH MANAGEMENT | April 2023 | January 2026 | Allow | 34 | 2 | 0 | Yes | No |
| 18189483 | PROPULSION SYSTEM | March 2023 | May 2024 | Abandon | 14 | 2 | 0 | Yes | No |
| 18183989 | FUEL SYSTEM INCLUDING DRIVING TURBINE | March 2023 | January 2025 | Allow | 22 | 2 | 1 | Yes | No |
| 18121434 | INTRODUCING STEAM WITH QUENCH AIR INTO TURBINE ENGINE COMBUSTOR | March 2023 | May 2024 | Allow | 14 | 1 | 1 | Yes | No |
| 18120821 | MODULATING FLUID FLOW WITHIN A TURBINE ENGINE USING STEAM | March 2023 | October 2025 | Allow | 31 | 2 | 1 | Yes | No |
| 18120835 | ASYMMETRIC INTRODUCTION OF STEAM INTO TURBINE ENGINE COMBUSTION CHAMBER | March 2023 | May 2025 | Allow | 26 | 3 | 1 | Yes | No |
| 18179045 | AIRCRAFT HYBRID ELECTRIC PROPULSION ARCHITECTURE ENABLING MODES OF OPERATION | March 2023 | February 2026 | Allow | 35 | 2 | 0 | Yes | No |
| 18044056 | HYBRID TURBOMACHINE FOR AIRCRAFT WITH AN ACTIVE ACOUSTIC CONTROL SYSTEM | March 2023 | March 2025 | Allow | 24 | 3 | 0 | Yes | No |
| 18173992 | CONTROL DEVICE FOR POWER UNIT SYSTEM | February 2023 | August 2024 | Allow | 18 | 2 | 0 | Yes | No |
| 18173371 | FUEL INJECTOR | February 2023 | June 2025 | Abandon | 28 | 2 | 1 | No | No |
| 18171092 | GAS TURBINE ENGINE WITH BLEED DIFFUSER BAFFLES | February 2023 | December 2025 | Allow | 34 | 2 | 1 | Yes | Yes |
| 18102295 | RELIQUIFICATION OF BOIL OFF GAS AT AIRPORT GATE | January 2023 | October 2024 | Abandon | 20 | 2 | 0 | No | No |
| 18158683 | ELECTRICAL SYSTEMS WITH DUAL-WOUND ROTARY ELECTRIC MACHINES | January 2023 | May 2025 | Allow | 28 | 4 | 0 | Yes | No |
| 17988302 | HYDROGEN COMBUSTION CONTROL SYSTEM FOR A VEHICLE HAVING A TURBINE ENGINE | November 2022 | February 2026 | Allow | 39 | 3 | 0 | Yes | No |
| 17921811 | TRANSITION PIECE, COMBUSTOR PROVIDED THEREWITH, GAS TURBINE, AND GAS TURBINE EQUIPMENT | October 2022 | October 2024 | Abandon | 24 | 2 | 0 | Yes | Yes |
| 17967345 | ELECTRIC MACHINE WITHIN A TURBINE ENGINE | October 2022 | July 2024 | Allow | 21 | 2 | 0 | Yes | No |
| 17966612 | ENGINE CONTROL DEVICE AND METHODS THEREOF | October 2022 | May 2024 | Allow | 19 | 2 | 0 | Yes | No |
| 17956921 | Turbine Device | September 2022 | October 2023 | Abandon | 13 | 1 | 0 | No | No |
| 17951879 | STEAM INJECTED INTER-TURBINE BURNER ENGINE | September 2022 | March 2026 | Allow | 41 | 3 | 1 | Yes | Yes |
| 17950423 | ELECTRICAL POWER SYSTEM CONVERTER CONTROL | September 2022 | February 2025 | Allow | 29 | 1 | 0 | No | No |
| 17902307 | GAS TURBINE ENGINE WITH INTEGRAL ACTUATION SYSTEM | September 2022 | August 2024 | Allow | 24 | 2 | 1 | No | No |
| 17905318 | TURBINE ENGINE MODULE EQUIPPED WITH AN ELECTRIC MACHINE HAVING A ROTOR DRIVEN IN ROTATION VIA A MOTION TAKE-OFF MECHANISM | August 2022 | November 2025 | Allow | 39 | 4 | 0 | Yes | No |
| 17799029 | GAS TURBINE ENGINE HAVING A COMPRESSOR, COMBUSTOR AND TURBINE ALIGNED ALONG A ROTATING SHAFT | August 2022 | March 2025 | Allow | 31 | 3 | 0 | Yes | Yes |
| 17883809 | ELECTRIC COMPONENT FOR ELECTRIC POWER TRANSMISSION IN AN ELECTRIC SYSTEM | August 2022 | August 2025 | Allow | 36 | 1 | 0 | Yes | No |
| 17813761 | SYSTEM FOR LUBRICATING COMPONENTS OF A GAS TURBINE ENGINE INCLUDING A LUBRICANT BYPASS CONDUIT | July 2022 | February 2023 | Allow | 7 | 0 | 0 | No | No |
| 17846583 | DUAL FUEL PUMP SYSTEM FOR AN AIRCRAFT | June 2022 | March 2025 | Abandon | 33 | 2 | 0 | No | No |
| 17738141 | AIRCRAFT FUEL PUMPING SYSTEM | May 2022 | March 2025 | Abandon | 34 | 4 | 1 | No | No |
| 17774116 | Dual-Fuel Power System and Air Supply and Purging Method Thereof | May 2022 | May 2025 | Allow | 36 | 2 | 0 | Yes | No |
| 17707334 | AIRCRAFT POWERPLANT(S) FOR AN AIRCRAFT WITH ELECTRIC MACHINE CONTROLLED PROPULSOR SPEED | March 2022 | December 2025 | Allow | 45 | 4 | 1 | Yes | No |
| 17694713 | AIRCRAFT HAVING COOLING CIRCUITS INDEPENDENT OF EACH OTHER | March 2022 | August 2025 | Allow | 41 | 1 | 1 | Yes | No |
| 17692411 | TURBINE ENGINE WITH FUEL NOZZLE AND SWIRLER ASSEMBLY | March 2022 | January 2026 | Abandon | 46 | 6 | 1 | Yes | No |
| 17691781 | ENGINE FUEL NOZZLE AND SWIRLER | March 2022 | March 2025 | Allow | 36 | 5 | 1 | Yes | No |
| 17687832 | Method and Apparatus for Controlling Electrical Machines Operating with a Turbine Engine | March 2022 | June 2025 | Allow | 40 | 3 | 0 | Yes | No |
| 17686904 | FUEL NOZZLE AND SWIRLER | March 2022 | June 2024 | Allow | 28 | 3 | 1 | Yes | No |
| 17680751 | CMC COMBUSTOR DEFLECTOR | February 2022 | May 2024 | Allow | 27 | 2 | 1 | Yes | No |
| 17678176 | AIRCRAFT HAVING AN ENGINE AND A COOLING SYSTEM BASED ON DIHYDROGEN | February 2022 | January 2025 | Abandon | 35 | 4 | 0 | No | No |
| 17651743 | TURBO MACHINE COMBUSTOR ASSEMBLY HAVING SEPARABLE PORTIONS COUPLED AT A FITTED INTERFACE | February 2022 | August 2024 | Allow | 30 | 2 | 1 | No | No |
| 17673426 | ENGINE COMPONENT ASSEMBLY WITH A COOLING APERTURE | February 2022 | December 2025 | Allow | 46 | 2 | 0 | Yes | Yes |
| 17591412 | PNEUMATIC STARTER SUPPLEMENTAL LUBRICATION SYSTEM | February 2022 | November 2025 | Abandon | 45 | 5 | 1 | No | No |
| 17571609 | INLEAKAGE MANAGEMENT APPARATUS | January 2022 | December 2024 | Allow | 35 | 4 | 0 | No | No |
| 17571661 | POWER SOURCE FOR AN AIRCRAFT | January 2022 | March 2025 | Abandon | 38 | 3 | 1 | Yes | No |
| 17567990 | PROPULSION SYSTEM FUEL CELL CONTROL | January 2022 | March 2025 | Abandon | 38 | 2 | 0 | Yes | No |
| 17545283 | ELECTRICAL POWER SYSTEMS | December 2021 | July 2024 | Abandon | 31 | 2 | 1 | No | No |
| 17545771 | Zero-Emission Jet Engine Employing A Dual-Fuel Mix Of Ammonia And Hydrogen Using A Wave | December 2021 | May 2023 | Allow | 18 | 1 | 0 | Yes | No |
| 17545312 | ELECTRICAL POWER SYSTEMS | December 2021 | September 2024 | Allow | 33 | 2 | 1 | No | No |
| 17540570 | SYSTEM AND METHOD OF OPERATING MULTI-ENGINE SYSTEM | December 2021 | May 2025 | Allow | 41 | 3 | 0 | No | No |
| 17537546 | AIRCRAFT PROPULSION SYSTEM WITH REDUCED ROTATIONAL LOAD OF AN ENGINE SHAFT | November 2021 | April 2025 | Allow | 41 | 3 | 0 | Yes | No |
| 17533165 | GAS TURBINE SYSTEM THAT MITIGATES BATTERY ELECTRICITY CONSUMPTION DURING STARTING OR STOPPING OF A GAS TURBINE ENGINE | November 2021 | July 2025 | Allow | 44 | 3 | 0 | Yes | No |
| 17526340 | INTEGRAL SUPERSTRUCTURE FOR LOAD PATH OPTIMIZATION | November 2021 | January 2024 | Allow | 26 | 3 | 0 | Yes | No |
| 17517858 | METHOD FOR CONTROLLING A POWER PLANT OF A ROTORCRAFT COMPRISING AT LEAST TWO TURBOSHAFT ENGINES | November 2021 | January 2026 | Allow | 50 | 4 | 0 | Yes | Yes |
| 17608292 | TURBINE ENGINE SEPARATE FLOW MIXER WITH LOBES | November 2021 | June 2024 | Allow | 32 | 3 | 0 | Yes | No |
| 17499557 | PYROLYTIC CLEANING OF COMBUSTORS | October 2021 | February 2024 | Abandon | 28 | 3 | 0 | Yes | No |
| 17488696 | GAS TURBINE ENGINE EQUIPPED WITH A CONTROL SYSTEM FOR MANAGEMENT OF ROTOR MODES USING AN ELECTRIC MACHINE | September 2021 | April 2025 | Allow | 43 | 3 | 1 | Yes | No |
| 17477576 | PROPULSION SYSTEM | September 2021 | April 2024 | Abandon | 31 | 2 | 0 | Yes | No |
| 17460617 | REMOVING NON-HOMOGENEOUS ICE FROM A FUEL SYSTEM | August 2021 | March 2025 | Allow | 43 | 3 | 1 | Yes | Yes |
| 17383120 | DUAL CYCLE INTERCOOLED ENGINE ARCHITECTURES | July 2021 | February 2025 | Abandon | 43 | 4 | 0 | No | No |
| 17362347 | GAS TURBINE ENGINE AND AIRCRAFT WITH A GAS TURBINE ENGINE | June 2021 | July 2023 | Abandon | 24 | 2 | 0 | No | No |
| 17356825 | RADIAL EQUILIBRATED COMBUSTION NOZZLE ARRAY | June 2021 | December 2024 | Abandon | 42 | 4 | 1 | Yes | No |
| 17304584 | IGNITION SYSTEM FOR POWER GENERATION ENGINE | June 2021 | January 2025 | Allow | 43 | 3 | 1 | Yes | No |
| 17353023 | COMBUSTOR AND GAS TURBINE INCLUDING THE SAME | June 2021 | February 2023 | Allow | 20 | 2 | 1 | No | No |
| 17345626 | HYBRID ELECTRIC ENGINE POWER DISTRIBUTION | June 2021 | November 2023 | Abandon | 30 | 1 | 1 | No | No |
| 17340764 | COMBUSTOR FOR A GAS TURBINE ENGINE | June 2021 | May 2024 | Allow | 35 | 2 | 1 | No | No |
| 17331989 | AIRCRAFT GAS TURBINE ENGINE WITH IMPROVED RESPONSE TO ROTOR UNBALANCE | May 2021 | April 2022 | Allow | 10 | 1 | 1 | Yes | No |
| 17330550 | HEAT EXCHANGE SYSTEM FOR AIRCRAFT ENGINE | May 2021 | April 2025 | Abandon | 46 | 6 | 0 | Yes | No |
| 17331020 | AIRCRAFT ENGINE | May 2021 | March 2022 | Allow | 10 | 1 | 1 | Yes | No |
| 17326801 | System and Method for Regulating Velocity of Gases in a Turbomachine | May 2021 | January 2026 | Allow | 56 | 4 | 0 | Yes | Yes |
| 17293999 | ELECTRIC POWER GENERATING APPARATUS FOR USE IN AIRCRAFT | May 2021 | April 2025 | Abandon | 48 | 5 | 0 | Yes | Yes |
| 17314619 | FEATURE BASED COOLING USING IN WALL CONTOURED COOLING PASSAGE | May 2021 | April 2022 | Allow | 11 | 0 | 0 | Yes | No |
| 17307780 | INTEGRATED FUEL CELL AND ENGINE COMBUSTOR ASSEMBLY | May 2021 | June 2024 | Allow | 38 | 3 | 0 | Yes | No |
| 17244729 | FUEL MIXER | April 2021 | January 2025 | Allow | 45 | 5 | 1 | No | No |
| 17223181 | EXTERNAL AUXILIARY POWER UNIT | April 2021 | September 2023 | Abandon | 29 | 1 | 1 | No | No |
| 17217659 | FLOW DIVIDER VALVES WITH TRANSIENT PRESSURE LIMITING | March 2021 | January 2023 | Allow | 22 | 1 | 0 | No | No |
| 17211111 | TURBINE ENGINE SYSTEM EQUIPPED WITH A FUEL DEOXYGENATION SYSTEM AND TURBOELECTRIC POWER SYSTEM | March 2021 | June 2024 | Abandon | 39 | 4 | 0 | Yes | No |
| 17199244 | FUEL MIXER | March 2021 | July 2023 | Allow | 28 | 6 | 0 | Yes | No |
| 17160711 | GROUND OPERATIONS OF A HYBRID ELECTRIC PROPULSION SYSTEM | January 2021 | April 2023 | Abandon | 26 | 1 | 1 | No | No |
| 17133303 | ACCESS HATCH FOR INTERNALLY MOUNTED TORCH IGNITOR | December 2020 | September 2022 | Allow | 21 | 1 | 0 | Yes | No |
| 17130802 | SYSTEM FOR LUBRICATING COMPONENTS OF A GAS TURBINE ENGINE INCLUDING A LUBRICANT BYPASS CONDUIT | December 2020 | April 2022 | Allow | 15 | 0 | 0 | Yes | No |
| 17125107 | AXIALLY ORIENTED INTERNALLY MOUNTED CONTINUOUS IGNITION DEVICE: REVERSE FLOW AXIAL ORIENTATION | December 2020 | March 2023 | Abandon | 27 | 2 | 0 | No | No |
This analysis examines appeal outcomes and the strategic value of filing appeals for examiner LISOWSKI, JACEK.
With a 54.5% 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, 50.0% 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 LISOWSKI, JACEK works in Art Unit 3741 and has examined 162 patent applications in our dataset. With an allowance rate of 63.0%, this examiner allows applications at a lower rate than most examiners at the USPTO. Applications typically reach final disposition in approximately 39 months.
Examiner LISOWSKI, JACEK's allowance rate of 63.0% places them in the 23% percentile among all USPTO examiners. This examiner is less likely to allow applications than most examiners at the USPTO.
On average, applications examined by LISOWSKI, JACEK receive 2.98 office actions before reaching final disposition. This places the examiner in the 86% 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 LISOWSKI, JACEK is 39 months. This places the examiner in the 28% percentile for prosecution speed. Prosecution timelines are slightly slower than average with this examiner.
Conducting an examiner interview provides a +46.7% benefit to allowance rate for applications examined by LISOWSKI, JACEK. This interview benefit is in the 91% 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, 22.0% of applications are subsequently allowed. This success rate is in the 27% percentile among all examiners. Strategic Insight: RCEs show below-average effectiveness with this examiner. Carefully evaluate whether an RCE or continuation is the better strategy.
This examiner enters after-final amendments leading to allowance in 9.4% of cases where such amendments are filed. This entry rate is in the 9% 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, 44.4% result in withdrawal of the rejection or reopening of prosecution. This success rate is in the 41% 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 52.2% of appeals filed. This is in the 23% percentile among all examiners. Of these withdrawals, 25.0% 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, 75.0% are granted (fully or in part). This grant rate is in the 81% percentile among all examiners. Strategic Note: Petitions are frequently granted regarding this examiner's actions compared to other examiners. Per MPEP § 1002.02(c), various examiner actions are petitionable to the Technology Center Director, including prematureness of final rejection, refusal to enter amendments, and requirement for information. If you believe an examiner action is improper, consider filing a petition.
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 47% 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.