Detailed information about the 100 most recent patent applications.
| Application Number | Title | Filing Date | Disposal Date | Disposition | Time (months) | Office Actions | Restrictions | Interview | Appeal |
|---|---|---|---|---|---|---|---|---|---|
| 18726915 | THRUST REVERSER COMPRISING FIXED CASCADES AND A SEALING MEMBRANE | July 2024 | April 2025 | Allow | 9 | 0 | 0 | No | No |
| 18672887 | ELECTRICALLY STARTING A GAS TURBINE ENGINE | May 2024 | May 2025 | Allow | 11 | 0 | 0 | No | No |
| 18400324 | ANTI-BACK-TRANSFER INTAKE STRUCTURE FOR ROTATING DETONATION COMBUSTION CHAMBER | December 2023 | November 2024 | Abandon | 10 | 1 | 0 | No | No |
| 18377032 | Pulse Detonation Wave Generator | October 2023 | May 2025 | Abandon | 19 | 1 | 1 | No | No |
| 18037161 | GAS TURBINE INLET COOLING FOR CONSTANT POWER OUTPUT | May 2023 | February 2025 | Allow | 21 | 1 | 1 | Yes | No |
| 18033700 | METHOD FOR CREATING MAXIMUM OUTPUT IN GAS TURBINE, METHOD FOR CREATING OUTPUT FOR CONTROLLING GAS TURBINE, METHOD FOR CONTROLLING GAS TURBINE, DEVICE FOR EXECUTING SAID METHODS, AND PROGRAM FOR CAUSING COMPUTER TO EXECUTE SAID METHODS | April 2023 | September 2024 | Allow | 17 | 0 | 0 | No | No |
| 18299102 | REVERSE THRUST TURBOFAN ENGINE | April 2023 | December 2024 | Allow | 20 | 2 | 1 | Yes | No |
| 18044958 | COOLING SYSTEM OF A COMPARTMENT OF PIECES OF EQUIPMENT IN A NACELLE OF AN AIRCRAFT PROPELLING ASSEMBLY | March 2023 | August 2024 | Allow | 17 | 0 | 0 | Yes | No |
| 18170604 | RAM-AIR DUCT SYSTEM | February 2023 | February 2025 | Allow | 24 | 3 | 0 | Yes | No |
| 18158093 | LOCK SYSTEM FOR A THRUST REVERSER | January 2023 | April 2025 | Allow | 27 | 3 | 1 | Yes | No |
| 18065143 | AMMONIA BASED HYDROGEN POWERED COMBINED PROPULSION SYSTEM | December 2022 | June 2024 | Allow | 18 | 1 | 1 | Yes | No |
| 18065137 | PROPULSION SYSTEM USING RAMJET BLEED AIR FOR GAS TURBINE COMBUSTION | December 2022 | February 2025 | Allow | 26 | 3 | 1 | Yes | No |
| 18057269 | COMBUSTOR NOZZLE, COMBUSTOR, AND GAS TURBINE INCLUDING SAME | November 2022 | March 2025 | Allow | 27 | 4 | 0 | Yes | No |
| 18057517 | COMBUSTOR NOZZLE, COMBUSTOR, AND GAS TURBINE INCLUDING SAME | November 2022 | May 2024 | Allow | 18 | 2 | 0 | Yes | No |
| 18048214 | GAS TURBINE | October 2022 | June 2025 | Abandon | 31 | 4 | 1 | Yes | No |
| 17902149 | SYSTEM INCLUDING CAVITATION IMPELLER AND TURBINE | September 2022 | December 2024 | Abandon | 28 | 4 | 1 | Yes | No |
| 17799347 | ASSEMBLING STRUCTURE OF COMPRESSOR OF GAS TURBINE ENGINE | August 2022 | March 2024 | Allow | 20 | 1 | 0 | Yes | No |
| 17798795 | METHOD AND SYSTEM FOR CONTROLLING A THRUST REVERSER OF AN AIRCRAFT | August 2022 | November 2024 | Allow | 28 | 3 | 1 | Yes | No |
| 17878468 | THRUST REVERSER CASCADE WITH OFFSET VANE LEADING EDGES | August 2022 | June 2025 | Allow | 34 | 5 | 0 | No | No |
| 17812573 | ENGINE FOR AN AIRCRAFT | July 2022 | October 2024 | Abandon | 27 | 4 | 0 | No | No |
| 17810624 | ADAPTOR FOR A FUEL SYSTEM OF AN AIRCRAFT ENGINE | July 2022 | November 2024 | Allow | 28 | 2 | 1 | No | No |
| 17855905 | COMBUSTOR ASSEMBLY FOR A TURBINE ENGINE | July 2022 | February 2024 | Abandon | 19 | 2 | 0 | No | No |
| 17848036 | ANTI-BACK-TRANSFER INTAKE STRUCTURE FOR ROTATING DETONATION COMBUSTION CHAMBER | June 2022 | July 2024 | Abandon | 24 | 4 | 0 | No | No |
| 17734370 | VARIABLE CYCLE JET ENGINE | May 2022 | August 2024 | Abandon | 28 | 4 | 0 | No | No |
| 17492587 | PROPULSION CONCEPT COMBINING CONVENTIONAL ROCKET ENGINES AND AIR-BREATHING ENGINES (HEBER CONCEPT) | April 2022 | November 2024 | Abandon | 37 | 0 | 1 | No | No |
| 17656459 | ADAPTED PROCESS CONCEPT AND PERFORMANCE CONCEPT FOR ENGINES (E.G. ROCKETS), AIR-BREATHING PROPULSION SYSTEMS (E.G. SUBSONIC RAMJETS, RAMJETS, ROCKET RAMJETS), TURBOPUMPS OR NOZZLES (E.G. BELL NOZZLES, AEROSPIKES) | March 2022 | June 2024 | Abandon | 27 | 1 | 0 | No | No |
| 17694479 | Variable Area Fan Nozzle Actuation System | March 2022 | June 2025 | Allow | 39 | 5 | 1 | No | No |
| 17687873 | BIMODAL COMBUSTION SYSTEM | March 2022 | April 2025 | Abandon | 37 | 4 | 0 | No | No |
| 17640112 | THRUST REVERSER COMPRISING PRIMARY LATCHES OFFSET WITH RESPECT TO A PLANE OF SYMMETRY OF THE MOVABLE HOOD | March 2022 | March 2025 | Allow | 37 | 4 | 0 | Yes | No |
| 17640111 | THRUST REVERSER COMPRISING A SINGLE ACTUATOR FOR CONTROLLING A MOBILE COWLING | March 2022 | February 2024 | Allow | 24 | 2 | 0 | Yes | No |
| 17666244 | POSITION SENSOR FOR AIRCRAFT NACELLE THRUST REVERSER DOOR | February 2022 | July 2024 | Allow | 29 | 2 | 0 | Yes | No |
| 17632761 | THRUST REVERSER COMPRISING AT LEAST ONE INITIATOR TO INITIATE THE CLOSING OF A MOBILE EXTERNAL STRUCTURE OF THIS REVERSER | February 2022 | June 2025 | Abandon | 40 | 4 | 0 | Yes | No |
| 17632755 | AIRCRAFT THRUST REVERSER COMPRISING A BRAKING MECHANISM FOR SLOWING A MOBILE COWL IN THE EVENT OF OVERTRAVEL | February 2022 | January 2024 | Allow | 23 | 3 | 0 | Yes | No |
| 17582408 | ROTATING DETONATION ENGINE | January 2022 | March 2024 | Abandon | 26 | 2 | 1 | No | No |
| 17626637 | CONSTANT VOLUME TURBOMACHINE COMBUSTION CHAMBER | January 2022 | September 2024 | Allow | 32 | 3 | 0 | No | No |
| 17596864 | CONSTANT-VOLUME COMBUSTION SYSTEM WITH SYNCHRONIZED INJECTION | December 2021 | August 2024 | Allow | 32 | 4 | 0 | Yes | No |
| 17617373 | METHOD OF CONTROLLING DEFLAGRATION COMBUSTION PROCESS IN PISTONLESS COMBUSTOR | December 2021 | October 2024 | Allow | 35 | 3 | 0 | Yes | No |
| 17536480 | AIRCRAFT PROPULSION UNIT | November 2021 | April 2025 | Allow | 40 | 4 | 1 | Yes | No |
| 17610580 | DOOR FOR THRUST REVERSER OF AN AIRCRAFT PROPULSION ASSEMBLY, COMPRISING A FLEXIBLE BAFFLE | November 2021 | April 2024 | Allow | 30 | 2 | 0 | Yes | No |
| 17601043 | PROCESS FOR USING AN AIR INPUT OF A TURBOREACTOR NACELLE COMPRISING AN AIR INPUT LIP WHICH COMPRISES A PORTION WHICH CAN BE MOVED TO PROMOTE A THRUST INVERSION PHASE | October 2021 | September 2024 | Allow | 36 | 2 | 0 | No | No |
| 17340533 | THRUST REVERSER PROVIDED WITH A LIGHTWEIGHT THRUST REVERSER FLAP | June 2021 | November 2024 | Allow | 41 | 3 | 0 | Yes | No |
| 17195131 | TURBINE ENGINE ASSEMBLY INCLUDING A ROTATING DETONATION COMBUSTOR | March 2021 | April 2024 | Allow | 38 | 3 | 1 | Yes | No |
| 17072620 | VORTEX THRUSTER SYSTEM INCLUDING CATALYST BED WITH SCREEN ASSEMBLY | October 2020 | June 2024 | Abandon | 44 | 4 | 0 | Yes | No |
| 17004586 | VARIABLE GEOMETRY ROTATING DETONATION COMBUSTOR | August 2020 | February 2024 | Abandon | 42 | 4 | 0 | No | No |
| 16795990 | ROTATING INTERNAL COMBUSTION ENGINE | February 2020 | April 2025 | Allow | 60 | 4 | 1 | No | No |
| 16750939 | SYSTEMS AND METHODS FOR AIR-BREATHING WAVE ENGINES FOR THRUST PRODUCTION | January 2020 | April 2022 | Allow | 27 | 1 | 0 | No | No |
| 16696910 | COMBINED CYCLE FLIGHT PROPULSION SYSTEMS | November 2019 | September 2022 | Abandon | 33 | 1 | 1 | No | No |
| 16695472 | EFFICIENT JET | November 2019 | June 2020 | Allow | 7 | 1 | 0 | Yes | No |
| 16686702 | ROTATING DETONATION COMBUSTOR AND SYSTEM | November 2019 | October 2024 | Allow | 59 | 7 | 2 | Yes | No |
| 16686495 | ROTATING DETONATION COMBUSTOR | November 2019 | November 2024 | Allow | 60 | 6 | 1 | Yes | No |
| 16497979 | AUTO-DRIVEN PLASMA ACTUATOR FOR TRANSITION FROM DEFLAGRATION TO DETONATION COMBUSTION REGIME AND METHOD | September 2019 | June 2022 | Allow | 33 | 3 | 0 | No | Yes |
| 16582561 | MAGNETIC SQUEEZE FILM DAMPER SYSTEM FOR A GAS TURBINE ENGINE | September 2019 | May 2022 | Abandon | 32 | 1 | 1 | Yes | No |
| 16470822 | Ram-jet and turbo-jet detonation engine | July 2019 | March 2022 | Abandon | 33 | 1 | 0 | No | No |
| 16456870 | SUPERSONIC AIRCRAFT TURBOFAN | June 2019 | May 2021 | Allow | 22 | 1 | 0 | Yes | No |
| 16455295 | PULSE COMBUSTOR PERFORMANCE IMPROVEMENT WITH AIRSPEED | June 2019 | March 2022 | Abandon | 33 | 2 | 0 | No | No |
| 16468996 | SCRAMJET ENGINE | June 2019 | September 2021 | Allow | 28 | 2 | 0 | No | No |
| 16336624 | FLOW DEFLECTOR FOR A DISCHARGE VALVE SYSTEM, DISCHARGE VALVE SYSTEM AND TURBOMACHINE COMPRISING SUCH A DISCHARGE VALVE SYSTEM | March 2019 | March 2021 | Allow | 23 | 1 | 0 | No | No |
| 16363144 | SYSTEM AND METHOD FOR GENERATING ELECTRIC ENERGY | March 2019 | March 2021 | Abandon | 24 | 1 | 0 | No | No |
| 16269513 | FUEL DETONATION COMBUSTION PULSE DEVICE | February 2019 | August 2021 | Abandon | 31 | 2 | 0 | No | No |
| 16267473 | ROTATING DETONATION COMBUSTOR WITH DISCRETE DETONATION ANNULI | February 2019 | January 2025 | Allow | 60 | 6 | 1 | Yes | No |
| 16236018 | MODULATED TURBINE COOLING SYSTEM | December 2018 | March 2021 | Abandon | 27 | 1 | 0 | Yes | No |
| 16229093 | COMBUSTION EQUIPMENT | December 2018 | September 2021 | Allow | 33 | 2 | 0 | Yes | No |
| 16227237 | TURBOJET EQUIPPED WITH A DOUBLE-ACTION ACTUATOR, WHICH CAN BE USED TO CONTROL REVERSE THRUST | December 2018 | May 2021 | Allow | 29 | 2 | 0 | Yes | No |
| 16203829 | AIRCRAFT JET ENGINE COMPRISING MEANS FOR VARYING ITS OUTPUT SURFACE AREA | November 2018 | January 2021 | Abandon | 25 | 1 | 0 | No | No |
| 16203335 | ROTATING DETONATION COMBUSTOR WITH OFFSET INLET | November 2018 | February 2022 | Allow | 38 | 2 | 1 | No | No |
| 16097732 | ANNULAR COMBUSTION CHAMBER WITH CONTINUOUS DETONATION WAVE | October 2018 | September 2021 | Abandon | 34 | 2 | 0 | Yes | No |
| 16169645 | FUEL STAGING FOR ROTATING DETONATION COMBUSTOR | October 2018 | April 2021 | Allow | 30 | 1 | 1 | No | No |
| 16142337 | REVERSE-FLOW CORE GAS TURBINE ENGINE WITH A PULSE DETONATION SYSTEM | September 2018 | September 2021 | Abandon | 36 | 2 | 1 | No | No |
| 16055313 | RAMJET ENGINE WITH ROTATING DETONATION COMBUSTION SYSTEM AND METHOD FOR OPERATION | August 2018 | February 2022 | Allow | 42 | 2 | 1 | No | No |
| 16034321 | TURBINE BLADE, TURBINE INCLUDING SAME TURBINE BLADE, AND GAS TURBINE INCLUDING SAME TURBINE | July 2018 | August 2020 | Allow | 25 | 1 | 0 | Yes | No |
| 15992513 | Combustion System Deflection Mitigation Structure | May 2018 | August 2020 | Abandon | 27 | 1 | 0 | No | No |
| 15992380 | BACKFLOW PREVENTION SYSTEM FOR A GAS TURBINE ENGINE | May 2018 | December 2020 | Abandon | 31 | 2 | 0 | Yes | No |
| 15992416 | EXHAUST ASSEMBLY WITH VORTEX GENERATOR | May 2018 | May 2021 | Abandon | 35 | 2 | 1 | Yes | No |
| 15992364 | SYSTEM AND METHOD FOR USE OF INTERCOOLER COOLED FLUID AS BEARING PRESSURIZATION FLUID SOURCE | May 2018 | January 2025 | Allow | 60 | 5 | 1 | Yes | Yes |
| 15985737 | COOLING SYSTEM FOR A TURBINE ENGINE | May 2018 | November 2020 | Allow | 30 | 1 | 0 | No | No |
| 15984206 | COMBINED CYCLE POWER PLANT SYSTEM ARRANGEMENTS | May 2018 | October 2021 | Abandon | 41 | 2 | 2 | No | No |
| 15979217 | ENGINE FOR AN AIRCRAFT | May 2018 | March 2022 | Allow | 46 | 3 | 1 | Yes | No |
| 15977639 | PROTECTIVE BAFFLES FOR GAS TURBINE NOISE ATTENUATION SYSTEM | May 2018 | January 2021 | Abandon | 32 | 2 | 0 | No | No |
| 15975895 | FLUID MANIFOLD FOR GAS TURBINE ENGINE AND METHOD FOR DELIVERING FUEL TO A COMBUSTOR USING SAME | May 2018 | May 2020 | Allow | 24 | 1 | 1 | No | No |
| 15974870 | FLAMESHEET DIFFUSION CARTRIDGE | May 2018 | March 2020 | Allow | 22 | 1 | 0 | No | No |
| 15904892 | Engine With Rotating Detonation Combustion System | February 2018 | May 2024 | Abandon | 60 | 6 | 1 | No | No |
| 15904868 | Engine With Rotating Detonation Combustion System | February 2018 | June 2022 | Allow | 52 | 4 | 1 | Yes | No |
| 15904991 | Engine With Rotating Detonation Combustion System | February 2018 | June 2022 | Allow | 51 | 4 | 1 | No | No |
| 15904918 | Engine With Rotating Detonation Combustion System | February 2018 | January 2022 | Allow | 46 | 3 | 1 | No | No |
| 15882463 | HIGH-MACH VEHICLE COOLING | January 2018 | March 2020 | Allow | 26 | 1 | 0 | Yes | No |
| 15860804 | Combustor Assembly for a Turbine Engine | January 2018 | May 2022 | Abandon | 52 | 4 | 1 | No | No |
| 15860835 | Combustor Assembly for a Turbine Engine | January 2018 | May 2022 | Abandon | 52 | 4 | 1 | No | No |
| 15860820 | Combustor Assembly for a Turbine Engine | January 2018 | March 2022 | Allow | 51 | 3 | 1 | Yes | No |
| 15795894 | MULTI-CAN ANNULAR ROTATING DETONATION COMBUSTOR | October 2017 | June 2021 | Allow | 44 | 3 | 1 | Yes | No |
| 15711742 | CAVITY STABILIZED DETONATION COMBUSTOR ASSEMBLY OF A ROTATING DETONATION ENGINE | September 2017 | December 2020 | Abandon | 39 | 2 | 0 | No | No |
| 15710020 | SYSTEMS, APPARATUSES AND METHODS FOR IMPROVED ROTATING DETONATION ENGINES | September 2017 | March 2021 | Abandon | 42 | 1 | 1 | No | No |
| 15705954 | TURBINE ENGINE ASSEMBLY INCLUDING A ROTATING DETONATION COMBUSTOR | September 2017 | December 2020 | Allow | 39 | 2 | 1 | No | No |
| 15551419 | CONSTANT-VOLUME COMBUSTION SYSTEM FOR A TURBINE ENGINE OF AN AIRCRAFT ENGINE | August 2017 | January 2022 | Abandon | 53 | 3 | 1 | No | No |
| 15673056 | SWIRL REDUCING GAS TURBINE ENGINE RECUPERATOR | August 2017 | June 2021 | Abandon | 46 | 3 | 0 | No | No |
| 15549584 | TURBINE ENGINE AIR GUIDE ASSEMBLY WITH IMPROVED AERODYNAMIC PERFORMANCE | August 2017 | June 2021 | Allow | 47 | 3 | 0 | Yes | No |
| 15545992 | CONSTANT-VOLUME COMBUSTION MODULE FOR A TURBINE ENGINE | July 2017 | January 2020 | Allow | 30 | 2 | 0 | No | No |
| 15545287 | CONSTANT-VOLUME COMBUSTON MODULE FOR A TURBINE ENGINE, COMPRISING COMMUNICATION-BASED IGNITION | July 2017 | September 2020 | Abandon | 38 | 2 | 0 | Yes | No |
| 15649093 | CONTINUOUS DETONATION GAS TURBINE ENGINE | July 2017 | June 2020 | Abandon | 35 | 2 | 0 | Yes | No |
| 15641760 | ENGINE, ROTARY DEVICE, POWER GENERATOR, POWER GENERATION SYSTEM, AND METHODS OF MAKING AND USING THE SAME | July 2017 | September 2021 | Abandon | 50 | 7 | 2 | Yes | No |
| 15618495 | ANNULAR THROATS ROTATING DETONATION COMBUSTOR | June 2017 | March 2021 | Abandon | 45 | 2 | 1 | No | No |
This analysis examines appeal outcomes and the strategic value of filing appeals for examiner KIM, TAE JUN.
With a 20.0% 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, 25.0% 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 KIM, TAE JUN works in Art Unit 3799 and has examined 131 patent applications in our dataset. With an allowance rate of 50.4%, this examiner allows applications at a lower rate than most examiners at the USPTO. Applications typically reach final disposition in approximately 37 months.
Examiner KIM, TAE JUN's allowance rate of 50.4% places them in the 8% percentile among all USPTO examiners. This examiner is less likely to allow applications than most examiners at the USPTO.
On average, applications examined by KIM, TAE JUN receive 2.80 office actions before reaching final disposition. This places the examiner in the 92% 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 KIM, TAE JUN is 37 months. This places the examiner in the 16% percentile for prosecution speed. Applications take longer to reach final disposition with this examiner compared to most others.
Conducting an examiner interview provides a +25.2% benefit to allowance rate for applications examined by KIM, TAE JUN. 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, 22.2% of applications are subsequently allowed. This success rate is in the 19% 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 5.2% of cases where such amendments are filed. This entry rate is in the 2% 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 22% 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 50.0% of appeals filed. This is in the 16% percentile among all examiners. Of these withdrawals, 20.0% 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, 58.8% are granted (fully or in part). This grant rate is in the 75% 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 45% 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 12.1% of allowed cases (in the 89% 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.