Detailed information about the 100 most recent patent applications.
| Application Number | Title | Filing Date | Disposal Date | Disposition | Time (months) | Office Actions | Restrictions | Interview | Appeal |
|---|---|---|---|---|---|---|---|---|---|
| 19293888 | HYDROELECTRIC POWER GENERATION UTILIZING TIDAL FLOWS AND CORIOLIS FORCE | August 2025 | January 2026 | Allow | 6 | 0 | 0 | Yes | No |
| 19252967 | METHOD TO TIE COMPOSITE VANE PLATFORM AND AIRFOIL DESIGN DETAILS | June 2025 | January 2026 | Allow | 7 | 1 | 0 | No | No |
| 19242046 | TURBINE ENGINE WITH COMPOSITE AIRFOILS | June 2025 | December 2025 | Allow | 6 | 1 | 0 | No | No |
| 19227642 | TURBINE ENGINE WITH COMPOSITE AIRFOILS | June 2025 | August 2025 | Allow | 3 | 0 | 0 | Yes | No |
| 19227649 | TURBINE ENGINE WITH COMPOSITE AIRFOILS | June 2025 | December 2025 | Allow | 7 | 1 | 0 | No | No |
| 19214414 | TURBINE ENGINE WITH COMPOSITE AIRFOILS | May 2025 | November 2025 | Allow | 6 | 1 | 0 | No | No |
| 19214354 | TURBINE ENGINE WITH COMPOSITE AIRFOILS | May 2025 | October 2025 | Allow | 5 | 1 | 0 | No | No |
| 19128462 | FIBROUS TEXTURE FOR A CASING MADE OF COMPOSITE MATERIAL WITH REINFORCED FLANGES | May 2025 | November 2025 | Allow | 6 | 0 | 0 | Yes | No |
| 19186738 | COMPOSITE BLADE | April 2025 | December 2025 | Allow | 8 | 1 | 0 | No | No |
| 19170305 | SEAL ASSEMBLY FOR A ROTARY MACHINE | April 2025 | January 2026 | Allow | 10 | 2 | 0 | Yes | No |
| 19090318 | COMPRESSOR BLEED AIR COLLECTOR AND EXHAUST DUCTING FOR GAS TURBINE ENGINE SYSTEMS | March 2025 | November 2025 | Allow | 8 | 0 | 0 | Yes | No |
| 19089903 | POWER TURBINE BLADES IN GAS TURBINE ENGINES | March 2025 | September 2025 | Allow | 6 | 1 | 0 | No | No |
| 19072955 | IMPELLER WHEEL | March 2025 | September 2025 | Allow | 7 | 1 | 0 | No | No |
| 19067448 | High Capacity, Shallow Draft, Ocean-Borne Wind Turbine | February 2025 | November 2025 | Allow | 8 | 1 | 0 | No | No |
| 19034964 | VARIABLE PITCH AIRFOIL ASSEMBLY FOR A GAS TURBINE ENGINE | January 2025 | July 2025 | Allow | 5 | 0 | 1 | No | No |
| 19033762 | UMBRELLA CLAMPING FAN | January 2025 | September 2025 | Allow | 8 | 0 | 0 | Yes | No |
| 19014587 | CEILING FAN WITH BLADE HUB | January 2025 | January 2026 | Allow | 13 | 1 | 0 | No | No |
| 18877899 | TURBOMACHINE BLADING ASSEMBLY COMPRISING MEANS FOR LIMITING VIBRATION BETWEEN PLATFORMS | December 2024 | September 2025 | Allow | 9 | 0 | 0 | Yes | No |
| 18876240 | PITCH CHANGE MECHANISM WITH AN ACTUATOR SURROUNDING A FLUID TRANSFER BEARING | December 2024 | January 2026 | Allow | 13 | 1 | 0 | No | No |
| 18979662 | FAN | December 2024 | December 2025 | Allow | 12 | 1 | 0 | No | No |
| 18869635 | TURBOMACHINE BLADE, TURBOMACHINE AND METHOD FOR MANUFACTURING THE BLADE | November 2024 | October 2025 | Allow | 11 | 1 | 0 | No | No |
| 18929503 | PROPELLER GROUND STOP MECHANISM | October 2024 | May 2025 | Allow | 6 | 1 | 0 | Yes | No |
| 18860295 | PROPELLER BLADE OR AIRFOIL WITH WOUND COMPOSITE ROOT | October 2024 | June 2025 | Allow | 7 | 1 | 0 | No | No |
| 18829998 | PARTIAL SHEAR TUBE Y-WEAVE TRAILING EDGE FOR A CMC VANE AND METHOD THEREFOR | September 2024 | September 2025 | Allow | 13 | 1 | 0 | No | No |
| 18819149 | DUAL AIR SOURCE BEARING ASSEMBLY HOUSING FOR AN AIRCRAFT PROPULSION SYSTEM | August 2024 | October 2025 | Allow | 14 | 1 | 0 | No | No |
| 18840255 | AXIAL TURBOMACHINE COMPRESSOR WITH CONTROLLED RECIRCULATION BETWEEN THE INNER SHROUD AND THE ROTOR | August 2024 | November 2025 | Allow | 15 | 1 | 0 | No | No |
| 18806969 | TURBINE ENGINE WITH COMPOSITE AIRFOILS | August 2024 | February 2025 | Allow | 6 | 1 | 0 | No | No |
| 18807233 | TURBINE ENGINE WITH COMPOSITE AIRFOILS | August 2024 | January 2025 | Allow | 5 | 1 | 0 | No | No |
| 18807374 | TURBINE ENGINE WITH COMPSITE AIRFOILS | August 2024 | February 2025 | Allow | 6 | 1 | 0 | Yes | No |
| 18806835 | TURBINE ENGINE WITH COMPOSITE AIRFOILS | August 2024 | January 2025 | Allow | 5 | 1 | 0 | No | No |
| 18792695 | TURBINE ENGINE WITH COMPOSITE AIRFOILS | August 2024 | January 2025 | Allow | 6 | 1 | 0 | No | No |
| 18792941 | TURBINE ENGINE WITH COMPOSITE AIRFOILS | August 2024 | January 2025 | Allow | 6 | 1 | 0 | No | No |
| 18792952 | TURBINE ENGINE WITH COMPOSITE AIRFOILS | August 2024 | February 2025 | Allow | 7 | 1 | 0 | No | No |
| 18792961 | TURBINE ENGINE WITH COMPOSITE AIRFOILS | August 2024 | February 2025 | Allow | 6 | 1 | 0 | No | No |
| 18777644 | TURBINE ENGINE WITH COMPOSITE AIRFOILS | July 2024 | February 2025 | Allow | 7 | 1 | 0 | No | No |
| 18777725 | TURBINE ENGINE WITH COMPOSITE AIRFOILS | July 2024 | February 2025 | Allow | 7 | 1 | 0 | No | No |
| 18772879 | TIE SHAFT FOR ENGINE ROTATING ASSEMBLY | July 2024 | September 2025 | Allow | 14 | 1 | 0 | No | No |
| 18764770 | TURBINE ENGINE WITH COMPOSITE AIRFOILS | July 2024 | January 2025 | Allow | 7 | 1 | 0 | No | No |
| 18722026 | CMC MATERIALS WITH INTEGRATED THERMOCOUPLE | June 2024 | November 2024 | Allow | 5 | 0 | 0 | No | No |
| 18742456 | POWERED TURBO-EXPANDER COMBINING CENTRIFUGAL COMPRESSOR AND AN AXIAL FLOW TURBINE | June 2024 | August 2025 | Allow | 14 | 2 | 0 | Yes | No |
| 18741419 | TURBINE ENGINE WITH COMPOSITE AIRFOILS | June 2024 | February 2025 | Allow | 8 | 1 | 0 | No | No |
| 18739753 | PROPELLER | June 2024 | April 2025 | Abandon | 11 | 1 | 0 | Yes | No |
| 18717869 | METHOD FOR PRODUCING A BLADED COMPONENT FOR AN AIRCRAFT TURBINE ENGINE | June 2024 | December 2025 | Allow | 18 | 1 | 0 | No | No |
| 18736903 | METHOD FOR SIZING STUBS OPTIMIZED FOR ORBITAL WELDING OF BLADES ON A TURBOMACHINE ROTOR | June 2024 | March 2025 | Allow | 10 | 1 | 0 | No | No |
| 18735569 | SYSTEM AND METHOD FOR COMPENSATING FOR ROTOR IMBALANCE IN A WIND TURBINE | June 2024 | May 2025 | Allow | 11 | 0 | 0 | No | No |
| 18731485 | FAN AND ELECTRONIC DEVICE | June 2024 | October 2025 | Allow | 16 | 1 | 0 | No | No |
| 18655490 | PROTECTION SYSTEM | May 2024 | June 2025 | Allow | 14 | 1 | 1 | No | No |
| 18651545 | FAN WITH MULTILAYER FAN BLADES | April 2024 | August 2025 | Allow | 15 | 1 | 0 | No | No |
| 18648597 | RETAINING NUT WITH INTEGRATED OIL SCOOP | April 2024 | April 2025 | Allow | 12 | 0 | 0 | No | No |
| 18649081 | WHEELS INCLUDING A COATING LAYER AND METHODS FOR MAKING THE SAME | April 2024 | November 2025 | Allow | 19 | 3 | 1 | No | No |
| 18705827 | Coating for Aluminum Alloy Aerostructures | April 2024 | October 2025 | Allow | 18 | 1 | 1 | Yes | No |
| 18645037 | HANGING NECK FAN | April 2024 | February 2026 | Allow | 22 | 1 | 1 | No | No |
| 18640177 | METHOD FOR SIZING STUBS OPTIMIZED FOR ORBITAL WELDING OF BLADES ON A TURBOMACHINE ROTOR | April 2024 | March 2025 | Allow | 11 | 1 | 0 | No | No |
| 18701017 | BLADE FOR A LOW-NOISE INDUSTRIAL AXIAL FAN, INDUSTRIAL AXIAL FAN AND PROCESS FOR MANUFACTURING A BLADE OF AN INDUSTRIAL AXIAL FAN | April 2024 | July 2025 | Allow | 15 | 1 | 0 | No | No |
| 18632959 | WOVEN REINFORCING FIBER AIRFOIL STRUCTURE FOR A TURBINE ENGINE | April 2024 | October 2025 | Allow | 18 | 2 | 0 | No | No |
| 18631471 | METHOD OF MITIGATING ROTOR BOW IN A TURBINE ENGINE ROTOR | April 2024 | June 2025 | Allow | 14 | 1 | 1 | Yes | No |
| 18630268 | WIND TURBINE ROTOR BLADE WITH ACCESS WINDOW | April 2024 | December 2024 | Allow | 8 | 1 | 0 | No | No |
| 18622527 | METHOD FOR OPERATING A WIND TURBINE AND WIND TURBINE | March 2024 | March 2025 | Allow | 11 | 1 | 0 | No | No |
| 18694821 | METHOD FOR PREPARING A ROOT OF A TURBOMACHINE BLADE | March 2024 | May 2025 | Allow | 14 | 2 | 0 | Yes | No |
| 18610855 | METHOD AND SYSTEM OF FORMING A COMPOSITE AIRFOIL HAVING A SET OF PLIES | March 2024 | October 2025 | Allow | 19 | 1 | 0 | Yes | No |
| 18604004 | QUICK INSTALLATION CEILING FAN BLADES | March 2024 | August 2024 | Allow | 5 | 0 | 0 | No | No |
| 18597343 | BLOWER WHEEL ASSEMBLIES AND METHODS | March 2024 | April 2025 | Allow | 13 | 1 | 0 | No | No |
| 18594594 | TURBINE ENGINE WITH REDUCED CROSS FLOW AIRFOILS | March 2024 | June 2025 | Allow | 15 | 3 | 0 | Yes | No |
| 18688958 | AXIAL FAN MOTOR | March 2024 | February 2025 | Allow | 12 | 1 | 1 | No | No |
| 18592685 | CENTRIFUGAL FAN | March 2024 | July 2025 | Allow | 17 | 2 | 0 | No | No |
| 18687560 | PROPELLER FAN, BLOWER, AND AIR CONDITIONER | February 2024 | January 2025 | Allow | 10 | 0 | 0 | Yes | No |
| 18588423 | METHOD FOR MANUFACTURING A COMPOSITE BLADED DISK OR ROTOR | February 2024 | March 2025 | Allow | 13 | 0 | 0 | No | No |
| 18682902 | SEALING DEVICE AND FLOW MACHINE WITH THE SEALING DEVICE | February 2024 | September 2025 | Allow | 20 | 0 | 0 | Yes | No |
| 18681767 | METHOD OF CALIBRATING A REFERENCE OF A WIND TURBINE | February 2024 | March 2025 | Allow | 13 | 1 | 0 | Yes | No |
| 18434152 | DIFFUSER PIPE FOR AN AIRCRAFT PROPULSION SYSTEM | February 2024 | July 2025 | Allow | 18 | 2 | 0 | No | No |
| 18430341 | FAN IMPELLER STRUCTURE | February 2024 | March 2026 | Allow | 25 | 6 | 0 | Yes | No |
| 18418263 | HANDHELD FAN | January 2024 | July 2024 | Allow | 6 | 1 | 1 | No | No |
| 18414578 | AIRFOIL WITH VENTURI TUBE | January 2024 | February 2025 | Allow | 13 | 2 | 0 | No | No |
| 18399070 | METHOD FOR CONTROLLING A WIND POWER INSTALLATION | December 2023 | June 2025 | Allow | 17 | 1 | 0 | Yes | No |
| 18571688 | METHOD FOR BALANCING FAN VANES WITH TRAILING EDGE MACHINING | December 2023 | August 2024 | Allow | 8 | 0 | 0 | Yes | No |
| 18571015 | FIBROUS PREFORM WITH STIFFENERS FORMED BY UNIDIRECTIONAL YARN LAYERS | December 2023 | June 2024 | Allow | 6 | 0 | 0 | Yes | No |
| 18534154 | METHOD TO TIE COMPOSITE VANE PLATFORM AND AIRFOIL DESIGN DETAILS | December 2023 | April 2025 | Allow | 16 | 1 | 1 | No | No |
| 18524013 | METHOD OF CONTROLLING A WIND FARM USING A REINFORCEMENT LEARNING METHOD | November 2023 | January 2025 | Allow | 13 | 1 | 0 | No | No |
| 18525121 | COMPOSITE AIRFOIL | November 2023 | December 2025 | Allow | 24 | 1 | 0 | No | No |
| 18564494 | DIFFERENTIATED SHORTENING OF STRANDS OF THE FIBROUS REINFORCEMENT OF A FAN BLADE | November 2023 | November 2024 | Allow | 12 | 0 | 0 | No | No |
| 18513794 | METHOD OF MANUFACTURING CMC COMPONENT | November 2023 | April 2025 | Allow | 17 | 0 | 0 | No | No |
| 18514403 | BLOWER FAN | November 2023 | January 2025 | Allow | 14 | 1 | 0 | Yes | No |
| 18512681 | TRAVEL STOP FOR A TIP CLEARANCE CONTROL SYSTEM | November 2023 | March 2025 | Allow | 16 | 1 | 1 | No | No |
| 18504869 | PROPELLER GROUND STOP MECHANISM | November 2023 | August 2024 | Allow | 9 | 1 | 0 | Yes | No |
| 18502135 | CENTRIFUGAL COMPRESSOR AND TURBOCHARGER | November 2023 | August 2024 | Allow | 10 | 0 | 0 | Yes | No |
| 18500546 | AIR-TO-AIR HEAT EXCHANGER POTENTIAL IN GAS TURBINE ENGINES | November 2023 | April 2024 | Allow | 6 | 0 | 0 | No | No |
| 18496524 | POWER AMPLIFICATION, STORAGE AND REGENERATION SYSTEM AND METHOD USING TIDES, WAVES AND/OR WIND | October 2023 | February 2025 | Allow | 16 | 1 | 0 | No | No |
| 18491574 | ADDITIVELY MANUFACTURED PROTECTIVE COVER FOR GAS TURBINE COMPONENTS | October 2023 | July 2025 | Allow | 21 | 3 | 0 | Yes | No |
| 18480692 | CMC AIRFOIL WITH CIRCUMVENTING COOLING PASSAGE | October 2023 | January 2026 | Allow | 28 | 2 | 0 | Yes | Yes |
| 18480192 | AIRFOIL ASSEMBLY HAVING A COMPOSITE CORE | October 2023 | October 2025 | Allow | 24 | 4 | 0 | Yes | No |
| 18285122 | VANE COMPRISING A STRUCTURE MADE OF COMPOSITE MATERIAL, AND ASSOCIATED MANUFACTURING METHOD | September 2023 | July 2024 | Allow | 10 | 1 | 0 | Yes | No |
| 18552716 | TURBINE RING ASSEMBLY FOR A TURBOMACHINE | September 2023 | November 2024 | Allow | 14 | 2 | 0 | Yes | No |
| 18471922 | FAN FOR A LIGHTING DEVICE OF A MOTOR VEHICLE | September 2023 | June 2024 | Allow | 9 | 1 | 0 | No | No |
| 18549500 | CONTROL METHOD AND CONTROL DEVICE FOR WIND TURBINE | September 2023 | September 2024 | Allow | 12 | 2 | 0 | No | No |
| 18455293 | TILTED CMC VANE ARC SEGMENT | August 2023 | November 2024 | Allow | 14 | 3 | 0 | No | No |
| 18453564 | COMPOSITE COMPONENT HAVING AN ADDITIVELY PRINTED INNER PORTION | August 2023 | August 2025 | Allow | 23 | 2 | 1 | Yes | No |
| 18547099 | SYSTEM FOR CONTROLLING AERAULIC CONDITIONS ABOVE A LANDING OR DECK-LANDING ZONE | August 2023 | March 2026 | Allow | 31 | 1 | 0 | No | No |
| 18447980 | METHOD FOR EFFICIENT PART LOAD COMPRESSOR OPERATION | August 2023 | August 2025 | Allow | 24 | 2 | 1 | Yes | No |
| 18447831 | ROTOR BLADE SYSTEM FOR TURBINE ENGINES | August 2023 | May 2025 | Allow | 21 | 2 | 0 | Yes | No |
| 18229967 | ENGINE TRIM BALANCE SYSTEM | August 2023 | June 2024 | Allow | 10 | 1 | 0 | No | No |
This analysis examines appeal outcomes and the strategic value of filing appeals for examiner SEHN, MICHAEL L.
With a 30.4% reversal rate, the PTAB reverses the examiner's rejections in a meaningful percentage 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, 22.2% 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 SEHN, MICHAEL L works in Art Unit 3745 and has examined 553 patent applications in our dataset. With an allowance rate of 79.2%, this examiner has a below-average tendency to allow applications. Applications typically reach final disposition in approximately 37 months.
Examiner SEHN, MICHAEL L's allowance rate of 79.2% places them in the 48% percentile among all USPTO examiners. This examiner has a below-average tendency to allow applications.
On average, applications examined by SEHN, MICHAEL L receive 2.25 office actions before reaching final disposition. This places the examiner in the 63% percentile for office actions issued. This examiner issues a slightly above-average number of office actions.
The median time to disposition (half-life) for applications examined by SEHN, MICHAEL L is 37 months. This places the examiner in the 34% percentile for prosecution speed. Prosecution timelines are slightly slower than average with this examiner.
Conducting an examiner interview provides a +13.8% benefit to allowance rate for applications examined by SEHN, MICHAEL L. This interview benefit is in the 52% percentile among all examiners. Recommendation: Interviews provide an above-average benefit with this examiner and are worth considering.
When applicants file an RCE with this examiner, 23.7% of applications are subsequently allowed. This success rate is in the 33% 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 39.4% of cases where such amendments are filed. This entry rate is in the 60% percentile among all examiners. Strategic Recommendation: This examiner shows above-average receptiveness to after-final amendments. If your amendments clearly overcome the rejections and do not raise new issues, consider filing after-final amendments before resorting to an RCE.
When applicants request a pre-appeal conference (PAC) with this examiner, 88.9% result in withdrawal of the rejection or reopening of prosecution. This success rate is in the 67% percentile among all examiners. Strategic Recommendation: Pre-appeal conferences show above-average effectiveness with this examiner. If you have strong arguments, a PAC request may result in favorable reconsideration.
This examiner withdraws rejections or reopens prosecution in 59.6% of appeals filed. This is in the 34% percentile among all examiners. Of these withdrawals, 26.5% 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, 30.4% are granted (fully or in part). This grant rate is in the 18% percentile among all examiners. Strategic Note: Petitions are rarely granted regarding this examiner's actions compared to other examiners. Ensure you have a strong procedural basis before filing a petition, as the Technology Center Director typically upholds this examiner's decisions.
Examiner's Amendments: This examiner makes examiner's amendments in 0.0% of allowed cases (in the 44% 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 2.7% of allowed cases (in the 72% percentile). This examiner issues Quayle actions more often than average when claims are allowable but formal matters remain (MPEP § 714.14).
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.