USPTO Examiner LISOWSKI JACEK - Art Unit 3741

Recent Applications

Detailed information about the 100 most recent patent applications.

Application NumberTitleFiling DateDisposal DateDispositionTime (months)Office ActionsRestrictionsInterviewAppeal
19207845CLEARANCE PROBE ASSEMBLY USING REPLENISHABLE, CONTACTING ELONGATED CLEARANCE TIPMay 2025August 2025Allow300YesNo
18972209GEARBOX ASSEMBLY WITH LUBRICANT EXTRACTION VOLUME RATIODecember 2024September 2025Allow1011YesNo
18899997INTRODUCING STEAM WITH QUENCH AIR INTO TURBINE ENGINE COMBUSTORSeptember 2024January 2026Allow1611YesNo
18883610TURBINE ENGINE HAVING A PLURALITY OF LUBRICANT STRUTS, EACH DEFINING A LUBRICANT STRUT FLOWPATHSeptember 2024December 2025Allow1520YesNo
18844258A METHOD FOR THE COMBUSTION OF A FUEL GASSeptember 2024January 2026Abandon1610NoNo
18843154EJECTION CONE WITH AN ACOUSTIC CHAMBER FOR AN AIRCRAFT TURBINE ENGINEAugust 2024March 2026Allow1810NoNo
18796453CMC COMBUSTOR DEFLECTORAugust 2024March 2025Allow701YesNo
18836448HEATING TURBOMACHINE FOR A FUEL-CONDITIONING SYSTEM CONFIGURED TO SUPPLY AN AIRCRAFT TURBOSHAFT ENGINE WITH FUEL FROM A CRYOGENIC TANKAugust 2024June 2025Allow1000YesNo
18649607MONOLITHIC SUPERSTRUCTURE FOR GAS TURBINE ENGINESApril 2024March 2026Allow2330YesNo
18614885MAGNETIC FRAGRANCE CARDMarch 2024March 2026Allow2301NoNo
18431620BIFURCATION INTEGRATED ELECTRICAL SYSTEM FOR HYBRID AIRCRAFT PROPULSION SYSTEMFebruary 2024December 2025Allow2220NoNo
18546351CONSTRUCTING A TURBOMACHINERY INSTALLATION FOR ASSEMBLY ONSHORE AND INSTALLATION ON AN OFFSHORE PLATFORMAugust 2023March 2026Allow3110YesNo
18447525GAS TURBINE ENGINE WITH COMPOSITE AIRFOIL AND PREFORM COREAugust 2023November 2025Allow2831YesNo
18253081HYBRID PROPULSION TURBOPROP ENGINE COUPLED TO A PROPELLER AND AIRCRAFT COMPRISING SUCH A TURBOPROP ENGINEAugust 2023January 2026Allow3210YesNo
18365299CONTAINMENT RING CAVITY PRESSURIZATION SYSTEMAugust 2023May 2025Abandon2130NoNo
18358647COMBUSTION CHAMBER ASSEMBLY FOR OPERATION WITH LIQUID AND/OR GASEOUS FUEL, GAS TURBINE ASSEMBLY AND METHODJuly 2023August 2025Allow2511YesNo
18273432METHOD FOR CONTROLLING OPERATION MODES OF GAS TURBINE SYSTEMJuly 2023March 2025Allow2010YesNo
18251025FREE TURBINE TURBOMACHINE COMPRISING EQUIPMENT DRIVEN BY THE FREE TURBINEJuly 2023September 2024Allow1720YesNo
18337717OIL SYSTEMJune 2023October 2024Abandon1520NoNo
18257367PROPULSION UNIT FOR AN AIRCRAFT COMPRISING A SYSTEM FOR SEALING BETWEEN TWO AIR INTAKE PARTSJune 2023August 2025Allow2610NoNo
18204068AIRCRAFT POWER AND PROPULSION SYSTEMS COMPRISING PERMANENT MAGNET ELECTRICAL MACHINESMay 2023July 2025Allow2611YesNo
18251031FREE TURBINE TURBOGENERATOR COMPRISING A REVERSIBLE ELECTRICAL MACHINE COUPLED TO THE FREE TURBINEApril 2023August 2025Allow2860YesNo
18298952OVERALL AIRCRAFT SYSTEM DATA COLLECTOR FOR PROGNOSTICS AND HEALTH MANAGEMENTApril 2023January 2026Allow3420YesNo
18189483PROPULSION SYSTEMMarch 2023May 2024Abandon1420YesNo
18183989FUEL SYSTEM INCLUDING DRIVING TURBINEMarch 2023January 2025Allow2221YesNo
18121434INTRODUCING STEAM WITH QUENCH AIR INTO TURBINE ENGINE COMBUSTORMarch 2023May 2024Allow1411YesNo
18120821MODULATING FLUID FLOW WITHIN A TURBINE ENGINE USING STEAMMarch 2023October 2025Allow3121YesNo
18120835ASYMMETRIC INTRODUCTION OF STEAM INTO TURBINE ENGINE COMBUSTION CHAMBERMarch 2023May 2025Allow2631YesNo
18179045AIRCRAFT HYBRID ELECTRIC PROPULSION ARCHITECTURE ENABLING MODES OF OPERATIONMarch 2023February 2026Allow3520YesNo
18044056HYBRID TURBOMACHINE FOR AIRCRAFT WITH AN ACTIVE ACOUSTIC CONTROL SYSTEMMarch 2023March 2025Allow2430YesNo
18173992CONTROL DEVICE FOR POWER UNIT SYSTEMFebruary 2023August 2024Allow1820YesNo
18173371FUEL INJECTORFebruary 2023June 2025Abandon2821NoNo
18171092GAS TURBINE ENGINE WITH BLEED DIFFUSER BAFFLESFebruary 2023December 2025Allow3421YesYes
18102295RELIQUIFICATION OF BOIL OFF GAS AT AIRPORT GATEJanuary 2023October 2024Abandon2020NoNo
18158683ELECTRICAL SYSTEMS WITH DUAL-WOUND ROTARY ELECTRIC MACHINESJanuary 2023May 2025Allow2840YesNo
17988302HYDROGEN COMBUSTION CONTROL SYSTEM FOR A VEHICLE HAVING A TURBINE ENGINENovember 2022February 2026Allow3930YesNo
17921811TRANSITION PIECE, COMBUSTOR PROVIDED THEREWITH, GAS TURBINE, AND GAS TURBINE EQUIPMENTOctober 2022October 2024Abandon2420YesYes
17967345ELECTRIC MACHINE WITHIN A TURBINE ENGINEOctober 2022July 2024Allow2120YesNo
17966612ENGINE CONTROL DEVICE AND METHODS THEREOFOctober 2022May 2024Allow1920YesNo
17956921Turbine DeviceSeptember 2022October 2023Abandon1310NoNo
17951879STEAM INJECTED INTER-TURBINE BURNER ENGINESeptember 2022March 2026Allow4131YesYes
17950423ELECTRICAL POWER SYSTEM CONVERTER CONTROLSeptember 2022February 2025Allow2910NoNo
17902307GAS TURBINE ENGINE WITH INTEGRAL ACTUATION SYSTEMSeptember 2022August 2024Allow2421NoNo
17905318TURBINE ENGINE MODULE EQUIPPED WITH AN ELECTRIC MACHINE HAVING A ROTOR DRIVEN IN ROTATION VIA A MOTION TAKE-OFF MECHANISMAugust 2022November 2025Allow3940YesNo
17799029GAS TURBINE ENGINE HAVING A COMPRESSOR, COMBUSTOR AND TURBINE ALIGNED ALONG A ROTATING SHAFTAugust 2022March 2025Allow3130YesYes
17883809ELECTRIC COMPONENT FOR ELECTRIC POWER TRANSMISSION IN AN ELECTRIC SYSTEMAugust 2022August 2025Allow3610YesNo
17813761SYSTEM FOR LUBRICATING COMPONENTS OF A GAS TURBINE ENGINE INCLUDING A LUBRICANT BYPASS CONDUITJuly 2022February 2023Allow700NoNo
17846583DUAL FUEL PUMP SYSTEM FOR AN AIRCRAFTJune 2022March 2025Abandon3320NoNo
17738141AIRCRAFT FUEL PUMPING SYSTEMMay 2022March 2025Abandon3441NoNo
17774116Dual-Fuel Power System and Air Supply and Purging Method ThereofMay 2022May 2025Allow3620YesNo
17707334AIRCRAFT POWERPLANT(S) FOR AN AIRCRAFT WITH ELECTRIC MACHINE CONTROLLED PROPULSOR SPEEDMarch 2022December 2025Allow4541YesNo
17694713AIRCRAFT HAVING COOLING CIRCUITS INDEPENDENT OF EACH OTHERMarch 2022August 2025Allow4111YesNo
17692411TURBINE ENGINE WITH FUEL NOZZLE AND SWIRLER ASSEMBLYMarch 2022January 2026Abandon4661YesNo
17691781ENGINE FUEL NOZZLE AND SWIRLERMarch 2022March 2025Allow3651YesNo
17687832Method and Apparatus for Controlling Electrical Machines Operating with a Turbine EngineMarch 2022June 2025Allow4030YesNo
17686904FUEL NOZZLE AND SWIRLERMarch 2022June 2024Allow2831YesNo
17680751CMC COMBUSTOR DEFLECTORFebruary 2022May 2024Allow2721YesNo
17678176AIRCRAFT HAVING AN ENGINE AND A COOLING SYSTEM BASED ON DIHYDROGENFebruary 2022January 2025Abandon3540NoNo
17651743TURBO MACHINE COMBUSTOR ASSEMBLY HAVING SEPARABLE PORTIONS COUPLED AT A FITTED INTERFACEFebruary 2022August 2024Allow3021NoNo
17673426ENGINE COMPONENT ASSEMBLY WITH A COOLING APERTUREFebruary 2022December 2025Allow4620YesYes
17591412PNEUMATIC STARTER SUPPLEMENTAL LUBRICATION SYSTEMFebruary 2022November 2025Abandon4551NoNo
17571609INLEAKAGE MANAGEMENT APPARATUSJanuary 2022December 2024Allow3540NoNo
17571661POWER SOURCE FOR AN AIRCRAFTJanuary 2022March 2025Abandon3831YesNo
17567990PROPULSION SYSTEM FUEL CELL CONTROLJanuary 2022March 2025Abandon3820YesNo
17545283ELECTRICAL POWER SYSTEMSDecember 2021July 2024Abandon3121NoNo
17545771Zero-Emission Jet Engine Employing A Dual-Fuel Mix Of Ammonia And Hydrogen Using A WaveDecember 2021May 2023Allow1810YesNo
17545312ELECTRICAL POWER SYSTEMSDecember 2021September 2024Allow3321NoNo
17540570SYSTEM AND METHOD OF OPERATING MULTI-ENGINE SYSTEMDecember 2021May 2025Allow4130NoNo
17537546AIRCRAFT PROPULSION SYSTEM WITH REDUCED ROTATIONAL LOAD OF AN ENGINE SHAFTNovember 2021April 2025Allow4130YesNo
17533165GAS TURBINE SYSTEM THAT MITIGATES BATTERY ELECTRICITY CONSUMPTION DURING STARTING OR STOPPING OF A GAS TURBINE ENGINENovember 2021July 2025Allow4430YesNo
17526340INTEGRAL SUPERSTRUCTURE FOR LOAD PATH OPTIMIZATIONNovember 2021January 2024Allow2630YesNo
17517858METHOD FOR CONTROLLING A POWER PLANT OF A ROTORCRAFT COMPRISING AT LEAST TWO TURBOSHAFT ENGINESNovember 2021January 2026Allow5040YesYes
17608292TURBINE ENGINE SEPARATE FLOW MIXER WITH LOBESNovember 2021June 2024Allow3230YesNo
17499557PYROLYTIC CLEANING OF COMBUSTORSOctober 2021February 2024Abandon2830YesNo
17488696GAS TURBINE ENGINE EQUIPPED WITH A CONTROL SYSTEM FOR MANAGEMENT OF ROTOR MODES USING AN ELECTRIC MACHINESeptember 2021April 2025Allow4331YesNo
17477576PROPULSION SYSTEMSeptember 2021April 2024Abandon3120YesNo
17460617REMOVING NON-HOMOGENEOUS ICE FROM A FUEL SYSTEMAugust 2021March 2025Allow4331YesYes
17383120DUAL CYCLE INTERCOOLED ENGINE ARCHITECTURESJuly 2021February 2025Abandon4340NoNo
17362347GAS TURBINE ENGINE AND AIRCRAFT WITH A GAS TURBINE ENGINEJune 2021July 2023Abandon2420NoNo
17356825RADIAL EQUILIBRATED COMBUSTION NOZZLE ARRAYJune 2021December 2024Abandon4241YesNo
17304584IGNITION SYSTEM FOR POWER GENERATION ENGINEJune 2021January 2025Allow4331YesNo
17353023COMBUSTOR AND GAS TURBINE INCLUDING THE SAMEJune 2021February 2023Allow2021NoNo
17345626HYBRID ELECTRIC ENGINE POWER DISTRIBUTIONJune 2021November 2023Abandon3011NoNo
17340764COMBUSTOR FOR A GAS TURBINE ENGINEJune 2021May 2024Allow3521NoNo
17331989AIRCRAFT GAS TURBINE ENGINE WITH IMPROVED RESPONSE TO ROTOR UNBALANCEMay 2021April 2022Allow1011YesNo
17330550HEAT EXCHANGE SYSTEM FOR AIRCRAFT ENGINEMay 2021April 2025Abandon4660YesNo
17331020AIRCRAFT ENGINEMay 2021March 2022Allow1011YesNo
17326801System and Method for Regulating Velocity of Gases in a TurbomachineMay 2021January 2026Allow5640YesYes
17293999ELECTRIC POWER GENERATING APPARATUS FOR USE IN AIRCRAFTMay 2021April 2025Abandon4850YesYes
17314619FEATURE BASED COOLING USING IN WALL CONTOURED COOLING PASSAGEMay 2021April 2022Allow1100YesNo
17307780INTEGRATED FUEL CELL AND ENGINE COMBUSTOR ASSEMBLYMay 2021June 2024Allow3830YesNo
17244729FUEL MIXERApril 2021January 2025Allow4551NoNo
17223181EXTERNAL AUXILIARY POWER UNITApril 2021September 2023Abandon2911NoNo
17217659FLOW DIVIDER VALVES WITH TRANSIENT PRESSURE LIMITINGMarch 2021January 2023Allow2210NoNo
17211111TURBINE ENGINE SYSTEM EQUIPPED WITH A FUEL DEOXYGENATION SYSTEM AND TURBOELECTRIC POWER SYSTEMMarch 2021June 2024Abandon3940YesNo
17199244FUEL MIXERMarch 2021July 2023Allow2860YesNo
17160711GROUND OPERATIONS OF A HYBRID ELECTRIC PROPULSION SYSTEMJanuary 2021April 2023Abandon2611NoNo
17133303ACCESS HATCH FOR INTERNALLY MOUNTED TORCH IGNITORDecember 2020September 2022Allow2110YesNo
17130802SYSTEM FOR LUBRICATING COMPONENTS OF A GAS TURBINE ENGINE INCLUDING A LUBRICANT BYPASS CONDUITDecember 2020April 2022Allow1500YesNo
17125107AXIALLY ORIENTED INTERNALLY MOUNTED CONTINUOUS IGNITION DEVICE: REVERSE FLOW AXIAL ORIENTATIONDecember 2020March 2023Abandon2720NoNo

Appeals Overview

This analysis examines appeal outcomes and the strategic value of filing appeals for examiner LISOWSKI, JACEK.

Patent Trial and Appeal Board (PTAB) Decisions

Total PTAB Decisions
11
Examiner Affirmed
5
(45.5%)
Examiner Reversed
6
(54.5%)
Reversal Percentile
81.0%
Higher than average

What This Means

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.

Strategic Value of Filing an Appeal

Total Appeal Filings
18
Allowed After Appeal Filing
9
(50.0%)
Not Allowed After Appeal Filing
9
(50.0%)
Filing Benefit Percentile
83.6%
Higher than average

Understanding Appeal Filing Strategy

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.

Strategic Recommendations

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 - Prosecution Strategy Guide

Executive Summary

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.

Allowance Patterns

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.

Office Action Patterns

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.

Prosecution Timeline

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.

Interview Effectiveness

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.

Request for Continued Examination (RCE) Effectiveness

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.

After-Final Amendment Practice

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.

Pre-Appeal Conference Effectiveness

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.

Appeal Withdrawal and Reconsideration

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.

Petition Practice

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 Cooperation and Flexibility

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.

Prosecution Strategy Recommendations

Based on the statistical analysis of this examiner's prosecution patterns, here are tailored strategic recommendations:

  • Prepare for rigorous examination: With a below-average allowance rate, ensure your application has strong written description and enablement support. Consider filing a continuation if you need to add new matter.
  • Expect multiple rounds of prosecution: This examiner issues more office actions than average. Address potential issues proactively in your initial response and consider requesting an interview early in prosecution.
  • Prioritize examiner interviews: Interviews are highly effective with this examiner. Request an interview after the first office action to clarify issues and potentially expedite allowance.
  • Plan for RCE after final rejection: This examiner rarely enters after-final amendments. Budget for an RCE in your prosecution strategy if you receive a final rejection.

Relevant MPEP Sections for Prosecution Strategy

  • MPEP § 713.10: Examiner interviews - available before Notice of Allowance or transfer to PTAB
  • MPEP § 714.12: After-final amendments - may be entered "under justifiable circumstances"
  • MPEP § 1002.02(c): Petitionable matters to Technology Center Director
  • MPEP § 1004: Actions requiring primary examiner signature (allowances, final rejections, examiner's answers)
  • MPEP § 1207.01: Appeal conferences - mandatory for all appeals
  • MPEP § 1214.07: Reopening prosecution after appeal

Important Disclaimer

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.