Detailed information about the 100 most recent patent applications.
| Application Number | Title | Filing Date | Disposal Date | Disposition | Time (months) | Office Actions | Restrictions | Interview | Appeal |
|---|---|---|---|---|---|---|---|---|---|
| 18805839 | COMBUSTOR AND GAS TURBINE | August 2024 | March 2026 | Allow | 19 | 2 | 0 | Yes | No |
| 18762161 | METHOD AND SYSTEM FOR COOLING OF ENGINE MOUNTED COMPONENTS | July 2024 | September 2025 | Allow | 15 | 1 | 1 | Yes | No |
| 18759149 | POWERPLANT FUEL SYSTEM UTILIZING AMMONIA | June 2024 | March 2026 | Allow | 20 | 2 | 1 | Yes | No |
| 18759194 | POWERPLANT FUEL SYSTEM UTILIZING AMMONIA | June 2024 | July 2025 | Allow | 13 | 1 | 1 | Yes | No |
| 18746729 | GAS TURBINE CONTROL DEVICE, GAS TURBINE CONTROL METHOD, AND STORAGE MEDIUM | June 2024 | November 2025 | Allow | 17 | 2 | 0 | Yes | No |
| 18680746 | CRYOGENIC FUEL DISTRIBUTION SYSTEMS INCLUDING HEAT EXCHANGERS AND RELATED METHODS | May 2024 | February 2026 | Allow | 20 | 2 | 1 | Yes | No |
| 18677375 | GAS TURBINE PLANT WITH AMMONIA DECOMPOSITION SYSTEM | May 2024 | November 2025 | Allow | 18 | 2 | 1 | Yes | No |
| 18419954 | FUEL SYSTEM WITH DUAL USE ELECTRIC PUMP | January 2024 | October 2025 | Abandon | 21 | 2 | 1 | No | No |
| 18393008 | AIRCRAFT WITH THERMAL ENERGY STORAGE SYSTEM | December 2023 | April 2025 | Allow | 16 | 1 | 1 | Yes | No |
| 18476579 | PROPULSION ASSEMBLY FOR AN AIRCRAFT | September 2023 | January 2026 | Abandon | 27 | 2 | 1 | No | No |
| 18466508 | BUILT-IN TEST OF ACTIVELY CONTROLLED FUEL NOZZLES | September 2023 | April 2025 | Allow | 19 | 1 | 0 | Yes | No |
| 18281879 | RUBBING POSITION IDENTIFICATION DEVICE AND RUBBING POSITION IDENTIFICATION METHOD FOR ROTATING MACHINE | September 2023 | June 2025 | Abandon | 21 | 0 | 1 | No | No |
| 18462144 | Purge System for Dual-Fuel Gas Turbine Engine | September 2023 | December 2025 | Allow | 27 | 2 | 1 | Yes | No |
| 18234336 | ROTATING DETONATION AUGMENTORS WITH FLOW RESTRICTION CONTROL FOR GAS TURBINE ENGINES | August 2023 | August 2025 | Abandon | 24 | 2 | 1 | Yes | No |
| 18365534 | HYDROGEN-EXHAUST GAS HEAT EXCHANGER OF A TURBOFAN ENGINE | August 2023 | August 2024 | Allow | 13 | 1 | 0 | Yes | No |
| 18224951 | ARCUATE FUEL GALLERY FOR TURBINE ENGINE FUEL NOZZLE | July 2023 | October 2025 | Allow | 27 | 2 | 1 | Yes | No |
| 18337531 | AIRCRAFT FUEL SYSTEM | June 2023 | September 2025 | Abandon | 27 | 4 | 0 | Yes | No |
| 18253791 | AIRCRAFT TURBINE ENGINE ASSEMBLY COMPRISING A PASSIVE VALVE FOR BY-PASSING A FUEL/OIL HEAT EXCHANGER | May 2023 | August 2024 | Allow | 15 | 1 | 0 | Yes | No |
| 18308968 | SHARED LOAD PATH BLADE OUTER AIR SEAL | April 2023 | September 2025 | Allow | 28 | 4 | 0 | Yes | No |
| 18302943 | METHOD OF OPTIMISING GAS TURBINE ENGINE COMBUSTION EQUIPMENT PERFORMANCE | April 2023 | April 2024 | Allow | 12 | 1 | 0 | No | No |
| 18110100 | FUEL INJECTOR PANELS HAVING MICROMIXERS | February 2023 | July 2025 | Allow | 29 | 2 | 0 | Yes | No |
| 18165813 | PERFORATED PLATE FUEL DISTRIBUTOR WITH SIMIPLIFIED SWIRLER | February 2023 | February 2026 | Abandon | 36 | 4 | 1 | No | No |
| 18104885 | COMBINED AIR SWIRLER AND FUEL DISTRIBUTOR | February 2023 | September 2025 | Abandon | 32 | 4 | 1 | No | No |
| 18162970 | ENGINE SYSTEM AND METHOD OF OPERATING THE SAME | February 2023 | February 2026 | Allow | 37 | 5 | 1 | Yes | No |
| 18161624 | COMBUSTOR NOZZLE FOR REDUCTION IN COMBUSTION VIBRATION, AND GAS TURBINE INCLUDING SAME | January 2023 | April 2025 | Abandon | 26 | 4 | 1 | Yes | No |
| 18161568 | COMBUSTOR NOZZLE AND GAS TURBINE INCLUDING THE SAME | January 2023 | January 2025 | Allow | 23 | 4 | 1 | Yes | No |
| 18154347 | NOZZLE ASSEMBLY WITH NOZZLE HEAD HAVING GUIDE ELEMENT | January 2023 | April 2025 | Allow | 27 | 4 | 0 | Yes | No |
| 17987191 | HYDROGEN GAS TURBINE | November 2022 | September 2025 | Abandon | 34 | 6 | 0 | No | No |
| 17980240 | MULTITUBE PILOT INJECTOR HAVING AN INSULATED MANIFOLD FOR A GAS TURBINE COMBUSTOR | November 2022 | August 2024 | Allow | 22 | 2 | 1 | Yes | No |
| 17980293 | MULTITUBE PILOT INJECTION INTO TRAPPED VORTICES IN A GAS TURBINE ENGINE | November 2022 | July 2024 | Allow | 20 | 1 | 1 | Yes | No |
| 17914694 | COMBUSTOR FOR GAS TURBINE AND GAS TURBINE | September 2022 | March 2025 | Abandon | 29 | 2 | 0 | No | No |
| 17940614 | IMPROVED GAS TURBINE ENGINE | September 2022 | July 2025 | Abandon | 34 | 4 | 1 | Yes | No |
| 17909408 | BURNER COMPONENT OF A BURNER, AND BURNER OF A GAS TURBINE HAVING A BURNER COMPONENT OF THIS TYPE | September 2022 | March 2024 | Allow | 19 | 2 | 0 | Yes | No |
| 17886802 | BURNER ASSEMBLY, GAS TURBINE COMBUSTOR, AND GAS TURBINE | August 2022 | December 2024 | Allow | 28 | 4 | 0 | Yes | No |
| 17877566 | METHODS FOR POWER TRANSFER IN CRYOGENIC FUEL APPLICATIONS | July 2022 | April 2025 | Allow | 32 | 4 | 0 | Yes | No |
| 17791737 | RESONATOR RING FOR COMBUSTION CHAMBER SYSTEMS | July 2022 | September 2025 | Abandon | 39 | 7 | 1 | No | No |
| 17853117 | METHOD OF CONTROLLING AN AIRCRAFT PROPULSION SYSTEM WITH A VARIABLE INLET GUIDE VANE, AND PROPULSION SYSTEM WITH A VARIABLE INLET GUIDE VANE SCHEDULING MANAGER | June 2022 | March 2025 | Abandon | 32 | 4 | 0 | Yes | No |
| 17747119 | Gas Turbine Combuster | May 2022 | July 2024 | Allow | 26 | 4 | 0 | Yes | No |
| 17730849 | BOTTOMING CYCLE WITH ISOLATED TURBO-GENERATORS | April 2022 | September 2025 | Abandon | 41 | 4 | 1 | No | No |
| 17730570 | HYDROGEN-EXHAUST GAS HEAT EXCHANGER OF A TURBOFAN ENGINE | April 2022 | April 2023 | Allow | 12 | 0 | 0 | No | No |
| 17725285 | Turbine Powered Electricity Generation | April 2022 | November 2023 | Abandon | 19 | 1 | 0 | No | No |
| 17655764 | COMBUSTOR HAVING MAIN BURNER AND DONUT-SHAPED SUB BURNER FOR USE IN COMBUSTION OF AMMONIA | March 2022 | August 2025 | Abandon | 41 | 6 | 1 | Yes | No |
| 17697285 | FUEL SUPPLY SYSTEM FOR A COMBUSTOR | March 2022 | June 2025 | Allow | 39 | 4 | 1 | Yes | No |
| 17696392 | METHOD FOR PROTECTING AN AIRCRAFT ENGINE ON SPIN-UP | March 2022 | January 2024 | Abandon | 22 | 3 | 1 | No | No |
| 17686800 | COMBUSTOR WITH DILUTION OPENINGS | March 2022 | July 2024 | Abandon | 28 | 2 | 1 | Yes | No |
| 17672946 | COMBUSTOR WITH RESONATOR | February 2022 | January 2025 | Abandon | 35 | 4 | 1 | No | No |
| 17670080 | HYDROGEN-OXYGEN FUELED POWERPLANT WITH WATER AND HEAT RECOVERY | February 2022 | January 2025 | Abandon | 35 | 5 | 1 | No | No |
| 17666594 | FUEL SUPPLY SYSTEM AND FUEL SUPPLY METHOD | February 2022 | June 2024 | Abandon | 29 | 2 | 1 | Yes | No |
| 17561964 | INJECTION NOZZLE, COMBUSTOR INCLUDING SAME NOZZLE, AND GAS TURBINE INCLUDING SAME COMBUSTOR | December 2021 | October 2023 | Allow | 21 | 2 | 1 | Yes | No |
| 17645115 | SYSTEM FOR PRODUCING DILUENT FOR A GAS TURBINE ENGINE | December 2021 | August 2024 | Allow | 32 | 4 | 1 | Yes | No |
| 17550083 | MICRO-MIXER MODULE AND COMBUSTOR HAVING THE SAME | December 2021 | June 2024 | Allow | 30 | 4 | 1 | Yes | No |
| 17550113 | FUEL NOZZLE, FUEL NOZZLE MODULE HAVING THE SAME, AND COMBUSTOR | December 2021 | February 2024 | Allow | 26 | 4 | 1 | Yes | No |
| 17542391 | MICROMIXER AND COMBUSTOR HAVING THE SAME | December 2021 | June 2024 | Allow | 30 | 4 | 1 | Yes | No |
| 17457441 | GAS TURBINE ENGINE INJECTOR MODULE WITH THERMALLY COUPLED FUEL LINES HAVING RESPECTIVE OUTLETS | December 2021 | January 2024 | Allow | 25 | 3 | 1 | Yes | No |
| 17540242 | MULTI-TUBE COMBUSTOR AND GAS TURBINE INCLUDING SAME | December 2021 | April 2023 | Allow | 17 | 3 | 0 | Yes | No |
| 17537355 | FLUID DELIVERY SYSTEM | November 2021 | July 2024 | Allow | 31 | 4 | 1 | Yes | No |
| 17535852 | FUEL NOZZLE WITH RESTRICTED CORE AIR PASSAGE | November 2021 | October 2023 | Abandon | 23 | 2 | 1 | No | No |
| 17531769 | COMBUSTOR NOZZLE, COMBUSTOR, AND GAS TURBINE INCLUDING SAME | November 2021 | January 2023 | Allow | 14 | 2 | 0 | Yes | No |
| 17512678 | COMBUSTOR NOZZLE, COMBUSTOR, AND GAS TURBINE INCLUDING THE SAME | October 2021 | July 2023 | Allow | 21 | 4 | 1 | Yes | No |
| 17510280 | MICRO-MIXER AND COMBUSTOR HAVING THE SAME | October 2021 | August 2023 | Allow | 22 | 3 | 1 | Yes | No |
| 17499517 | ADDITIVE SINGLE-PIECE BORE-COOLED COMBUSTOR DOME | October 2021 | October 2024 | Abandon | 36 | 4 | 0 | No | No |
| 17600737 | FUEL SUPPLY SYSTEM OF A TURBOMACHINE, WITH REGULATION OF THE FUEL FLOW | October 2021 | September 2024 | Abandon | 35 | 3 | 1 | Yes | No |
| 17491470 | AIRCRAFT WITH THERMAL ENERGY STORAGE SYSTEM | September 2021 | May 2024 | Abandon | 31 | 4 | 0 | Yes | No |
| 17487575 | HYDROGEN FUEL VAPORISER | September 2021 | February 2025 | Abandon | 40 | 4 | 1 | Yes | Yes |
| 17484579 | AIRCRAFT POWER PLANT WITH A TRANSMISSION TO DRIVE AN ELECTRICAL MACHINE | September 2021 | October 2025 | Abandon | 48 | 6 | 1 | No | No |
| 17476110 | FUEL INJECTION | September 2021 | December 2023 | Abandon | 27 | 4 | 1 | Yes | No |
| 17476174 | FUEL INJECTION | September 2021 | September 2023 | Allow | 24 | 3 | 0 | Yes | No |
| 17473072 | SYSTEM AND METHOD FOR DETERMINING HIGH OIL CONSUMPTION IN GAS TURBINE ENGINE | September 2021 | February 2024 | Allow | 29 | 5 | 0 | Yes | No |
| 17462932 | HEAT EXCHANGE SYSTEM USING COMPRESSOR AIR FOR FUEL PRE-HEATING | August 2021 | August 2025 | Abandon | 48 | 6 | 1 | No | No |
| 17434879 | COMBUSTOR AND GAS TURBINE | August 2021 | November 2024 | Allow | 39 | 3 | 1 | Yes | No |
| 17405372 | Combustor Fuel Nozzle Structure | August 2021 | March 2025 | Abandon | 43 | 5 | 0 | No | No |
| 17404726 | System and Methods for Recycling Hydrocarbon Waste Gas That is Generated During Cleaning of a Hydrocarbon Storage Tank | August 2021 | May 2024 | Abandon | 33 | 2 | 0 | Yes | Yes |
| 17373127 | METHOD OF MANAGING THERMAL ENERGY IN A PROPULSION SYSTEM | July 2021 | July 2024 | Abandon | 36 | 4 | 1 | No | No |
| 17367036 | PREMIXER ARRAY | July 2021 | December 2025 | Allow | 54 | 8 | 1 | Yes | Yes |
| 17419386 | BURNER, COMBUSTOR INCLUDING SAME, AND GAS TURBINE | June 2021 | February 2023 | Allow | 19 | 2 | 0 | Yes | No |
| 17359891 | HYBRID ELECTRIC MULTIPLE SHAFT CORE | June 2021 | July 2025 | Allow | 49 | 7 | 1 | Yes | No |
| 17357262 | COMBUSTOR ASSEMBLY FOR A GAS TURBINE ENGINE | June 2021 | July 2024 | Abandon | 36 | 5 | 1 | Yes | No |
| 17355689 | DILUTION AIR INLETS WITH NOTCHED TIP AND SLOTTED TAIL FOR COMBUSTOR | June 2021 | December 2023 | Allow | 29 | 3 | 1 | No | No |
| 17333631 | CORE DUCT ASSEMBLY | May 2021 | March 2023 | Allow | 22 | 2 | 0 | Yes | No |
| 17324009 | VARIABLE DISPLACEMENT METERING SYSTEM WITH MODE SELECTION | May 2021 | October 2023 | Abandon | 29 | 2 | 1 | Yes | No |
| 17320975 | TAPERED FUEL GALLERY FOR A FUEL NOZZLE | May 2021 | December 2022 | Allow | 19 | 1 | 1 | Yes | No |
| 17287457 | DEVICE FOR DE-ICING A TURBOMACHINE NOZZLE | April 2021 | April 2025 | Allow | 48 | 7 | 0 | Yes | No |
| 16976535 | COMBINED COOLING, HEATING AND POWER SYSTEM | November 2020 | November 2022 | Allow | 27 | 2 | 0 | Yes | No |
| 17071557 | Gas Turbine Combuster | October 2020 | April 2024 | Abandon | 42 | 4 | 1 | Yes | No |
| 17035954 | Gas Turbine Combustor | September 2020 | September 2023 | Abandon | 35 | 3 | 1 | No | No |
| 17041865 | SINGLE-SHAFT COMBINED CYCLE PLANT, TESTING METHOD FOR SINGLE-SHAFT COMBINED CYCLE PLANT, AND CONTROL DEVICE FOR SINGLE-SHAFT COMBINED CYCLE PLANT | September 2020 | December 2022 | Allow | 26 | 2 | 0 | Yes | No |
| 16884397 | MULTI-WALLED STRUCTURE FOR A GAS TURBINE ENGINE | May 2020 | November 2025 | Allow | 60 | 9 | 1 | Yes | No |
| 16880679 | SWIRLER WITH FUEL MANIFOLD, AND COMBUSTOR AND GAS TURBINE INCLUDING THE SAME | May 2020 | December 2023 | Allow | 43 | 5 | 1 | Yes | Yes |
| 16734925 | SYSTEMS AND METHODS FOR POWER TRANSFER IN CRYOGENIC FUEL APPLICATIONS | January 2020 | May 2022 | Allow | 28 | 0 | 0 | Yes | No |
| 16576099 | Flow Passages Formed in a Flame Tube for a Gas Turbine Combustor Chamber | September 2019 | December 2022 | Allow | 39 | 3 | 0 | Yes | No |
| 16552151 | TRAPPED VORTEX COMBUSTOR | August 2019 | March 2023 | Abandon | 43 | 0 | 1 | No | No |
| 16430872 | MAGNET ANTI-ICE SYSTEM | June 2019 | October 2025 | Allow | 60 | 4 | 0 | No | Yes |
| 16412535 | OIL RECOVERY SYSTEM | May 2019 | August 2022 | Abandon | 39 | 0 | 1 | No | No |
This analysis examines appeal outcomes and the strategic value of filing appeals for examiner LIU, JINGCHEN.
With a 33.3% reversal rate, the PTAB reverses the examiner's rejections in a meaningful percentage of cases. This reversal rate is above the USPTO average, indicating that appeals have better success 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, 40.0% 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 LIU, JINGCHEN works in Art Unit 3741 and has examined 45 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 31 months.
Examiner LIU, JINGCHEN's allowance rate of 62.2% places them in the 22% percentile among all USPTO examiners. This examiner is less likely to allow applications than most examiners at the USPTO.
On average, applications examined by LIU, JINGCHEN receive 3.58 office actions before reaching final disposition. This places the examiner in the 95% 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 LIU, JINGCHEN is 31 months. This places the examiner in the 57% percentile for prosecution speed. Prosecution timelines are slightly faster than average with this examiner.
Conducting an examiner interview provides a +58.3% benefit to allowance rate for applications examined by LIU, JINGCHEN. This interview benefit is in the 96% 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, 19.1% 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 8.3% 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 21% 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 21% percentile among all examiners. Of these withdrawals, 66.7% 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.
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.