Detailed information about the 100 most recent patent applications.
| Application Number | Title | Filing Date | Disposal Date | Disposition | Time (months) | Office Actions | Restrictions | Interview | Appeal |
|---|---|---|---|---|---|---|---|---|---|
| 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 |
| 18796453 | CMC COMBUSTOR DEFLECTOR | August 2024 | March 2025 | Allow | 7 | 0 | 1 | Yes | No |
| 18365299 | CONTAINMENT RING CAVITY PRESSURIZATION SYSTEM | August 2023 | May 2025 | Abandon | 21 | 3 | 0 | No | 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 |
| 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 |
| 18120835 | ASYMMETRIC INTRODUCTION OF STEAM INTO TURBINE ENGINE COMBUSTION CHAMBER | March 2023 | May 2025 | Allow | 26 | 3 | 1 | 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 |
| 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 |
| 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 |
| 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 |
| 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 |
| 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 |
| 17691781 | ENGINE FUEL NOZZLE AND SWIRLER | March 2022 | March 2025 | Allow | 36 | 5 | 1 | 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 |
| 17571661 | POWER SOURCE FOR AN AIRCRAFT | January 2022 | March 2025 | Abandon | 38 | 3 | 1 | Yes | No |
| 17571609 | INLEAKAGE MANAGEMENT APPARATUS | January 2022 | December 2024 | Allow | 35 | 4 | 0 | No | No |
| 17567990 | PROPULSION SYSTEM FUEL CELL CONTROL | January 2022 | March 2025 | Abandon | 38 | 2 | 0 | Yes | 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 |
| 17545283 | ELECTRICAL POWER SYSTEMS | December 2021 | July 2024 | Abandon | 31 | 2 | 1 | No | 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 |
| 17526340 | INTEGRAL SUPERSTRUCTURE FOR LOAD PATH OPTIMIZATION | November 2021 | January 2024 | Allow | 26 | 3 | 0 | Yes | No |
| 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 |
| 17331020 | AIRCRAFT ENGINE | May 2021 | March 2022 | Allow | 10 | 1 | 1 | Yes | No |
| 17330550 | HEAT EXCHANGE SYSTEM FOR AIRCRAFT ENGINE | May 2021 | April 2025 | Abandon | 46 | 6 | 0 | Yes | No |
| 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 |
| 17123479 | MASS FLOW METERING METHOD AND SYSTEM | December 2020 | March 2022 | Allow | 15 | 0 | 0 | Yes | No |
| 17108509 | GAS TURBINE ENGINE THAT FACILITATES TRANSFER OF ELECTRICAL POWER FROM ONE NETWORK TO ANOTHER NETWORK OPERATING AT A DIFFERENT VOLTAGE | December 2020 | February 2024 | Abandon | 39 | 4 | 0 | No | No |
| 17101460 | INJECTOR DEVICE AND METHOD FOR MANUFACTURING AN INJECTOR DEVICE | November 2020 | November 2023 | Abandon | 35 | 2 | 1 | Yes | No |
| 17094034 | Compact Airfoil Bleed-Air Re-circulation Heat Exchanger | November 2020 | June 2023 | Abandon | 32 | 2 | 1 | No | No |
| 17079906 | Aircraft Power Generation System | October 2020 | January 2024 | Abandon | 39 | 3 | 0 | No | No |
| 17050482 | EXTENDED GAS TURBINE PROCESS HAVING AN EXPANDER | October 2020 | September 2022 | Allow | 23 | 2 | 0 | Yes | No |
| 17061046 | TURBOSHAFT | October 2020 | August 2023 | Abandon | 35 | 4 | 0 | Yes | No |
| 17036999 | Gas Turbine Combustor and its Operating Method | September 2020 | May 2023 | Allow | 32 | 2 | 1 | Yes | No |
| 17002044 | ELECTRICAL SYSTEMS | August 2020 | April 2023 | Abandon | 31 | 3 | 0 | Yes | No |
| 16902308 | CMC Combustor Deflector | June 2020 | October 2021 | Allow | 16 | 0 | 0 | Yes | No |
| 16864349 | FUEL OXYGEN REDUCTION UNIT WITH BLEED DRIVEN BOOST IMPELLER | May 2020 | November 2024 | Abandon | 55 | 5 | 1 | No | No |
| 16848923 | EMBEDDED ELECTRIC MOTOR ASSEMBLY | April 2020 | April 2023 | Allow | 36 | 3 | 1 | Yes | No |
| 16837143 | AFTER-FAN SYSTEM FOR A GAS TURBINE ENGINE | April 2020 | January 2024 | Allow | 46 | 4 | 1 | Yes | No |
| 16641337 | TWIN-SPOOL TURBOJET ENGINE HAVING A LOW-PRESSURE SHAFT THRUST BEARING POSITIONED IN THE EXHAUST CASING | February 2020 | April 2025 | Abandon | 60 | 8 | 0 | Yes | No |
| 16786758 | ENGINE CONTROL DEVICE AND METHODS THEREOF | February 2020 | August 2022 | Allow | 30 | 3 | 1 | Yes | No |
| 16736322 | BOOSTER COMPRESSOR WITH SPEED CHANGE SYSTEM | January 2020 | December 2021 | Abandon | 23 | 2 | 0 | No | No |
| 16732774 | SYSTEMS AND METHODS FOR FUEL CELL AUXILIARY POWER IN SECONDARY FUEL APPLICATIONS | January 2020 | September 2023 | Abandon | 45 | 1 | 0 | Yes | No |
| 16732541 | LOW SPOOL POWER EXTRACTION VIA MULTIPLE GENERATORS | January 2020 | June 2025 | Abandon | 60 | 2 | 1 | No | Yes |
| 16625528 | ENGINE DEVICE AND METHOD FOR PROVIDING DRIVE POWER FOR AN ELECTRICAL DEVICE FOR PROVIDING ELECTRICAL ENERGY | December 2019 | August 2022 | Abandon | 32 | 1 | 0 | No | No |
| 16681292 | SYSTEMS AND METHODS FOR REMOVING HEAT FROM AIRCRAFT COMPONENTS | November 2019 | May 2023 | Allow | 42 | 2 | 1 | Yes | No |
| 16601146 | Combustion Chamber Of A Gas Turbine, Gas Turbine And Method For Operating The Same | October 2019 | January 2025 | Allow | 60 | 12 | 0 | Yes | No |
| 16530614 | SEAL ASSEMBLY | August 2019 | February 2023 | Abandon | 42 | 2 | 1 | No | No |
| 16513192 | GAS TURBINE ENGINE CORE ARRANGEMENT | July 2019 | October 2022 | Abandon | 40 | 5 | 0 | Yes | No |
| 16511135 | THERMALLY PROTECTED MOTOR/GENERATOR FOR GAS TURBINE ENGINE | July 2019 | December 2022 | Abandon | 41 | 2 | 0 | No | No |
| 16511284 | MODULATED COMBUSTOR BYPASS FOR HYBRID IDLE | July 2019 | March 2025 | Abandon | 60 | 6 | 1 | Yes | No |
| 16505343 | NOZZLE AND FUEL SYSTEM FOR OPERATION ON GAS WITH VARYING HEATING VALUE | July 2019 | August 2024 | Allow | 60 | 6 | 0 | Yes | No |
| 16471065 | METHOD FOR REGULATING A SUPPLY CIRCUIT | June 2019 | February 2022 | Allow | 32 | 1 | 0 | No | No |
| 16470223 | EXHAUST DUCT FOR A FOSSIL FUEL POWERED ENGINE COMPRISING A DILUTION SELECTIVE CATALYTIC REDUCTION SYSTEM | June 2019 | March 2023 | Allow | 45 | 4 | 0 | Yes | No |
| 16437387 | HYBRID ELECTRIC AIRCRAFT | June 2019 | October 2022 | Abandon | 40 | 3 | 0 | No | No |
| 16421760 | AIR COOLER FOR GAS TURBINE ENGINE | May 2019 | November 2021 | Allow | 30 | 1 | 0 | Yes | No |
| 16463157 | TURBO ENGINE, IN PARTICULAR TURBO GENERATOR AND EXCHANGER FOR SUCH TURBO ENGINE | May 2019 | August 2023 | Abandon | 51 | 4 | 0 | Yes | No |
| 16390315 | METHOD FOR REDUCING FUEL NOZZLE COKING IN A GAS TURBINE ENGINE | April 2019 | September 2021 | Allow | 28 | 2 | 0 | Yes | No |
| 16384270 | GAS TURBINE AUXILIARY POWER UNIT | April 2019 | January 2021 | Allow | 21 | 1 | 0 | Yes | No |
This analysis examines appeal outcomes and the strategic value of filing appeals for examiner LISOWSKI, JACEK.
With a 60.0% 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, 42.9% of applications that filed an appeal were subsequently allowed. This appeal filing benefit rate is above the USPTO average, suggesting that filing an appeal can be an effective strategy for prompting reconsideration.
✓ 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 185 patent applications in our dataset. With an allowance rate of 62.2%, this examiner allows applications at a lower rate than most examiners at the USPTO. Applications typically reach final disposition in approximately 36 months.
Examiner LISOWSKI, JACEK's allowance rate of 62.2% places them in the 15% 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 2.79 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 LISOWSKI, JACEK is 36 months. This places the examiner in the 18% percentile for prosecution speed. Applications take longer to reach final disposition with this examiner compared to most others.
Conducting an examiner interview provides a +44.0% 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, 24.7% 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 8.1% of cases where such amendments are filed. This entry rate is in the 4% 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, 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 61.5% of appeals filed. This is in the 34% percentile among all examiners. Of these withdrawals, 50.0% 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, 42.9% are granted (fully or in part). This grant rate is in the 45% 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 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.