Detailed information about the 100 most recent patent applications.
| Application Number | Title | Filing Date | Disposal Date | Disposition | Time (months) | Office Actions | Restrictions | Interview | Appeal |
|---|---|---|---|---|---|---|---|---|---|
| 19285677 | GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES | July 2025 | January 2026 | Allow | 6 | 0 | 0 | No | No |
| 19234090 | GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES | June 2025 | January 2026 | Allow | 7 | 0 | 0 | Yes | No |
| 19208379 | Vane Assembly For Open Fan Engine | May 2025 | March 2026 | Allow | 10 | 1 | 0 | Yes | No |
| 19199194 | GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES | May 2025 | August 2025 | Allow | 4 | 0 | 0 | No | No |
| 19197884 | GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES | May 2025 | August 2025 | Allow | 3 | 0 | 0 | No | No |
| 19195004 | GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES | April 2025 | July 2025 | Allow | 3 | 0 | 0 | Yes | No |
| 19190284 | GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES | April 2025 | May 2025 | Allow | 1 | 0 | 0 | Yes | No |
| 19190507 | GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES | April 2025 | June 2025 | Allow | 1 | 0 | 0 | No | No |
| 19177403 | GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES | April 2025 | June 2025 | Allow | 2 | 0 | 0 | Yes | No |
| 19089683 | SUPER-COOLED ICE IMPACT PROTECTION FOR A GAS TURBINE ENGINE | March 2025 | November 2025 | Allow | 7 | 0 | 0 | Yes | No |
| 19050520 | GUIDE VANE ASSEMBLY WITH FIXED AND VARIABLE PITCH INLET GUIDE VANES | February 2025 | February 2026 | Allow | 12 | 2 | 1 | Yes | No |
| 18993567 | CLEANING SYSTEM USED FOR VEHICLES AND CAPABLE OF SUPPRESSING VIBRATIONS AND REDUCING NOISE | January 2025 | January 2026 | Allow | 12 | 0 | 0 | No | No |
| 18990445 | GAS TURBINE ENGINES WITH INLET GUIDE VANES | December 2024 | June 2025 | Allow | 6 | 1 | 1 | Yes | No |
| 18973853 | CONDUCTIVE AERODYNAMIC STATOR | December 2024 | June 2025 | Allow | 6 | 0 | 1 | No | No |
| 18952609 | SELF-STABILIZING TURBINE AND STEAM-DRIVEN TURBINE ASSEMBLY USING THE SAME | November 2024 | November 2025 | Allow | 12 | 1 | 1 | No | No |
| 18948970 | TRANSLATABLE GUIDE VANES FOR AIRCRAFT PROPULSION SYSTEM | November 2024 | July 2025 | Allow | 8 | 0 | 1 | Yes | No |
| 18942911 | AIRCRAFT ENGINE INCLUDING DIFFUSER SECURED TO A BEARING HOUSING | November 2024 | July 2025 | Allow | 8 | 1 | 0 | No | No |
| 18941701 | GAS TURBINE ENGINE STATOR VANE STAGE | November 2024 | September 2025 | Allow | 11 | 1 | 1 | No | No |
| 18934766 | IMPELLER ROTOR SEAL RUNNER WITH DIVERGENT GUIDE SURFACE | November 2024 | August 2025 | Allow | 10 | 1 | 0 | No | No |
| 18918102 | FAN STRUCTURE | October 2024 | May 2025 | Allow | 7 | 0 | 1 | No | No |
| 18914807 | BLOWER | October 2024 | July 2025 | Allow | 9 | 1 | 0 | Yes | No |
| 18855869 | STATOR PART HAVING A FIN, IN A TURBINE ENGINE | October 2024 | October 2025 | Allow | 12 | 0 | 0 | Yes | No |
| 18853894 | TANDEM STATOR | October 2024 | November 2025 | Allow | 13 | 0 | 0 | Yes | No |
| 18847771 | METHOD FOR MANUFACTURING A TURBOMACHINE BLADE | September 2024 | January 2026 | Allow | 16 | 1 | 0 | Yes | No |
| 18885163 | INNER RING SEGMENT, AXIALLY DIVIDED INNER RING AND VARIABLE VANE CASCADE FOR AN AIRCRAFT ENGINE | September 2024 | September 2025 | Allow | 12 | 1 | 1 | Yes | No |
| 18846841 | ROTOR BLADE, METHOD FOR MANUFACTURING A ROTOR BLADE AND A GAS TURBINE ENGINE | September 2024 | November 2025 | Allow | 14 | 1 | 0 | No | No |
| 18883095 | BLADING ASSEMBLY FOR A TURBOMACHINE AND TURBOMACHINE | September 2024 | July 2025 | Allow | 10 | 1 | 1 | Yes | No |
| 18846615 | MODULE FOR AN AIRCRAFT TURBINE ENGINE | September 2024 | March 2026 | Allow | 18 | 2 | 0 | No | No |
| 18825241 | SUPER-COOLED ICE IMPACT PROTECTION FOR A GAS TURBINE ENGINE | September 2024 | January 2025 | Allow | 4 | 0 | 0 | Yes | No |
| 18817380 | COLLAPSIBLE COVER FOR ENGINE INLET AND METHOD FOR COVERING ENGINE INLET | August 2024 | December 2025 | Allow | 16 | 2 | 0 | Yes | No |
| 18840981 | GAS TURBINE ENGINE BLADING COMPRISING A BLADE AND A PLATFORM WHICH HAS AN INTERNAL FLOW-INTAKE AND FLOW-EJECTION CANAL | August 2024 | February 2026 | Allow | 18 | 1 | 0 | No | No |
| 18840954 | TURBOMOLECULAR VACUUM PUMP AND ASSOCIATED METHOD | August 2024 | July 2025 | Allow | 11 | 0 | 0 | No | No |
| 18840399 | ROOT SECTION, WIND TURBINE BLADE AND METHODS FOR PRODUCING AND MODIFYING A ROOT PORTION OF A WIND TURBINE BLADE | August 2024 | July 2025 | Allow | 11 | 1 | 0 | No | No |
| 18782309 | CONTOUR WEAVES FOR INTERWOVEN VANES | July 2024 | May 2025 | Allow | 9 | 1 | 0 | Yes | No |
| 18730937 | GAS TURBINE NOZZLES WITH COOLING HOLES AND TURBINE | July 2024 | February 2025 | Allow | 7 | 0 | 0 | Yes | No |
| 18779702 | BLADE FOR A ROTOR ASSEMBLY OF A TURBINE ENGINE | July 2024 | July 2025 | Allow | 12 | 1 | 0 | No | No |
| 18730612 | SECONDARY FLOW GUIDE VANE OF A TURBOMACHINE AND TURBOMACHINE PROVIDED THEREWITH | July 2024 | April 2025 | Allow | 9 | 0 | 1 | Yes | No |
| 18767355 | METHOD FOR PRODUCING AN INJECTION MOLDED PART, INJECTION MOLD AND FAN IMPELLER | July 2024 | January 2025 | Allow | 6 | 0 | 0 | Yes | No |
| 18763783 | WIND TURBINE BLADE INTEGRATING A LIGHTNING PROTECTION SYSTEM | July 2024 | March 2025 | Allow | 8 | 0 | 1 | Yes | No |
| 18725605 | INDOOR UNIT AND AIR CONDITIONER | June 2024 | September 2025 | Allow | 15 | 1 | 0 | No | No |
| 18757064 | BLADE SPACER | June 2024 | July 2025 | Allow | 13 | 1 | 1 | Yes | No |
| 18755054 | TURBOFAN ENGINE HAVING ANGLED INLET PRE-SWIRL VANES | June 2024 | February 2025 | Allow | 8 | 0 | 1 | No | No |
| 18721937 | WIND TURBINE BLADE | June 2024 | May 2025 | Allow | 11 | 1 | 0 | No | No |
| 18721415 | TURBINE STATIC BLADE, FITTING STRUCTURE, AND GAS TURBINE | June 2024 | November 2025 | Allow | 17 | 2 | 1 | Yes | No |
| 18720918 | STATOR VANE COMPRISING A HEAT PIPE | June 2024 | April 2025 | Allow | 10 | 1 | 0 | Yes | No |
| 18744069 | GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES | June 2024 | January 2025 | Allow | 7 | 0 | 0 | No | No |
| 18734494 | GAS TURBINE ENGINE WITH SPLIT VARIABLE FAN EXIT GUIDE VANES AND AIRFLOW RADIAL TOTAL PRESSURE PROFILE RE-DISTRIBUTION | June 2024 | August 2025 | Allow | 15 | 2 | 0 | No | No |
| 18734531 | GAS TURBINE ENGINE WITH HYBRID FAN EXIT GUIDE VANES | June 2024 | January 2025 | Allow | 8 | 1 | 0 | No | No |
| 18734310 | GAS TURBINE ENGINE WITH VARIABLE FAN EXIT GUIDE VANES | June 2024 | January 2026 | Abandon | 20 | 3 | 0 | No | No |
| 18669669 | COMPRESSOR STATOR VANE AIRFOILS | May 2024 | March 2025 | Allow | 10 | 0 | 0 | No | No |
| 18657787 | FAN AND FAN BRACKET | May 2024 | October 2025 | Allow | 17 | 1 | 1 | No | No |
| 18656599 | ROTOR ASSEMBLY AND FLUID TRANSMISSION DEVICE HAVING THE SAME | May 2024 | December 2024 | Allow | 8 | 0 | 0 | No | No |
| 18653478 | VANE ASSEMBLIES WITH OVERLAPPING BAND COUPLINGS IN GAS TURBINE ENGINES | May 2024 | March 2025 | Allow | 11 | 1 | 1 | No | No |
| 18649376 | SEAL SYSTEM USING LAYERS OF SEAL SEGMENTS FORCED INTO SEALING ENGAGEMENT USING TENSION CABLE | April 2024 | April 2025 | Allow | 11 | 0 | 1 | Yes | No |
| 18701730 | DEVICE FOR ATTACHING MOTOR PROTECTOR AND ENCAPSULATED-TYPE ELECTRIC COMPRESSOR | April 2024 | September 2024 | Allow | 5 | 0 | 0 | No | No |
| 18634974 | AIR-FLOATING CENTRIFUGAL COMPRESSOR | April 2024 | January 2026 | Abandon | 21 | 1 | 1 | No | No |
| 18634206 | TURBOMACHINE LABYRINTH SEAL DESIGN FOR OXYGEN RICH PROCESS FLUIDS | April 2024 | June 2025 | Allow | 14 | 1 | 0 | Yes | No |
| 18634238 | METHOD OF USING A LABYRINTH SEAL FOR SEALING A TURBOMACHINE FOR OXYGEN RICH PROCESS FLUIDS | April 2024 | June 2025 | Allow | 14 | 1 | 0 | Yes | No |
| 18633432 | AIRFOIL WITH PROTECTIVE COATING | April 2024 | May 2025 | Allow | 13 | 1 | 0 | Yes | No |
| 18632282 | DOUBLE-LAYER BLADE CEILING FAN CAPABLE OF ADJUSTING ARRANGEMENT OF BLADES | April 2024 | September 2024 | Allow | 5 | 0 | 0 | No | No |
| 18628235 | TAILORING AIRCRAFT POWERPLANT SPLIT LINE WITH INFLATABLE BLADDER(S) | April 2024 | May 2025 | Allow | 13 | 0 | 1 | Yes | No |
| 18628322 | TURBINE VANE FOR A GAS TURBINE ENGINE | April 2024 | July 2025 | Allow | 16 | 2 | 1 | Yes | No |
| 18627026 | ROTOR BLADE SYSTEM OF TURBINE ENGINES | April 2024 | October 2024 | Allow | 7 | 0 | 1 | No | No |
| 18293904 | TURBOMACHINE COMPRISING AN OUTLET CONE INCORPORATING COMPONENTS COOLED BY CIRCULATION OF A COOLING FLOW | March 2024 | November 2025 | Allow | 22 | 1 | 2 | No | No |
| 18618081 | AIRFOIL FOR A TURBOFAN ENGINE | March 2024 | November 2024 | Allow | 8 | 0 | 1 | Yes | No |
| 18618349 | BLOWER | March 2024 | September 2024 | Allow | 6 | 0 | 0 | Yes | No |
| 18695477 | MODULE FOR AN AIRCRAFT TURBINE ENGINE | March 2024 | February 2025 | Allow | 11 | 0 | 0 | No | No |
| 18615610 | VARIABLE GUIDE VANE FOR AIRCRAFT PROPULSION SYSTEM | March 2024 | March 2025 | Allow | 11 | 0 | 1 | Yes | No |
| 18694555 | HIGH-PRESSURE GAS TURBINE FOR TURBOMACHINE AND TURBOMACHINE | March 2024 | September 2025 | Allow | 17 | 2 | 0 | Yes | No |
| 18692991 | CROSS FLOW FAN AND BLOWING DEVICE | March 2024 | November 2025 | Abandon | 20 | 0 | 1 | No | No |
| 18691222 | CROSS FLOW FAN | March 2024 | September 2024 | Allow | 6 | 0 | 0 | No | No |
| 18591666 | COOLING CIRCUIT FOR A STATOR VANE BRAZE JOINT | February 2024 | March 2025 | Allow | 13 | 1 | 1 | Yes | No |
| 18584300 | MODULAR TORQUE CONVERTER STATOR WITH CAMMED BLADES | February 2024 | October 2024 | Allow | 8 | 1 | 0 | Yes | No |
| 18583079 | REMOVABLE SHOULDER SCREW | February 2024 | January 2025 | Allow | 11 | 1 | 1 | Yes | No |
| 18441039 | TURBINE ENGINE WITH COMPOSITE AIRFOIL HAVING A NON-METALLIC LEADING EDGE PROTECTIVE WRAP | February 2024 | January 2025 | Allow | 11 | 1 | 1 | Yes | No |
| 18439495 | ADJUSTMENT SYSTEM FOR A COMPRESSOR | February 2024 | May 2025 | Abandon | 15 | 1 | 1 | No | No |
| 18438265 | COOLING NOZZLE VANES OF A TURBINE ENGINE | February 2024 | December 2024 | Allow | 10 | 0 | 0 | No | No |
| 18434951 | ACOUSTIC DAMPERS FOR LIFE SUPPORT SYSTEMS | February 2024 | January 2025 | Allow | 11 | 1 | 1 | No | No |
| 18294390 | PRESSURE BUSHING FOR A FLUID PUMP AND A PUMP INCLUDING THE PRESSURE BUSHING | February 2024 | August 2025 | Allow | 18 | 2 | 1 | Yes | No |
| 18428873 | GAS TURBINE ENGINE COMPONENT FORMED BY CMCS AND HAVING A COMPRESSED INSERT WITH TAPERED ENDS | January 2024 | June 2025 | Allow | 17 | 1 | 1 | No | No |
| 18395342 | MITIGATION OF ROTATING STALL IN TURBINE SECTION USING OUTER FLOW CONTROL VANES | December 2023 | December 2024 | Allow | 12 | 0 | 1 | No | No |
| 18390828 | DETACHABLE MOTOR ASSEMBLY AND COMMUNICATION MODULE | December 2023 | February 2026 | Allow | 26 | 0 | 0 | No | No |
| 18545092 | GAS TURBINE ENGINE VANE AND SPAR COMBINATION WITH VARIABLE AIR FLOW PATH | December 2023 | February 2025 | Allow | 14 | 1 | 1 | Yes | No |
| 18541606 | INTEGRATED CENTRIFUGAL COMPRESSOR DIFFUSER AND HIGH PRESSURE TURBINE VANE ASSEMBLY | December 2023 | July 2024 | Allow | 7 | 0 | 0 | No | No |
| 18569353 | UNDUCTED RECTIFIER FOR A TURBOMACHINE, TURBOMACHINE MODULE AND AIRCRAFT TURBOMACHINE | December 2023 | March 2025 | Allow | 15 | 2 | 0 | No | No |
| 18531953 | RADIAL TURBINE IMPELLER | December 2023 | August 2025 | Abandon | 21 | 2 | 1 | No | No |
| 18527567 | GUIDE VANE ASSEMBLY WITH FIXED AND VARIABLE PITCH INLET GUIDE VANES | December 2023 | October 2024 | Allow | 11 | 1 | 1 | Yes | No |
| 18524490 | SUPER-COOLED ICE IMPACT PROTECTION FOR A GAS TURBINE ENGINE | November 2023 | June 2024 | Allow | 6 | 0 | 0 | Yes | No |
| 18507032 | BLADES OF AN AXIAL TURBINE | November 2023 | February 2025 | Allow | 15 | 0 | 0 | No | No |
| 18288374 | MOORING RENEWABLE ENERGY SYSTEMS | October 2023 | January 2026 | Allow | 27 | 0 | 0 | Yes | No |
| 18379952 | INTERNAL ALUMINIDE COATING FOR VANES AND BLADES AND METHOD OF MANUFACTURE | October 2023 | December 2024 | Allow | 14 | 0 | 1 | Yes | No |
| 18480708 | TURBINE AIRFOIL HAVING COOLING HOLE ARRANGEMENT | October 2023 | February 2024 | Allow | 5 | 0 | 0 | No | No |
| 18477912 | BLADE OUTER AIR SEAL WITH RETAINER RING | September 2023 | September 2024 | Allow | 11 | 1 | 0 | No | No |
| 18476947 | WIND TURBINE ROTOR BLADE AND WIND TURBINE | September 2023 | March 2025 | Abandon | 17 | 1 | 0 | Yes | No |
| 18284315 | WIND FARM BLACK START | September 2023 | September 2024 | Allow | 11 | 0 | 0 | Yes | No |
| 18282460 | METHOD AND DEVICE OF CONTROLLING AN OPERATION OF A FLOATING WIND TURBINE | September 2023 | October 2025 | Allow | 25 | 2 | 1 | Yes | No |
| 18453093 | INTEGRAL STATOR VANE WELD SHIELD | August 2023 | November 2024 | Allow | 15 | 0 | 1 | Yes | No |
| 18546540 | SUCTION PIPE OF CENTRIFUGAL COMPRESSOR, CENTRIFUGAL COMPRESSOR WITH SUCTION PIPE, AND REFRIGERATOR | August 2023 | April 2025 | Abandon | 20 | 1 | 1 | No | No |
| 18230611 | VANE ASSEMBLY FOR OPEN FAN ENGINE | August 2023 | April 2024 | Allow | 8 | 0 | 0 | Yes | No |
| 18229336 | MODAL NOISE REDUCTION FOR GAS TURBINE ENGINE | August 2023 | February 2024 | Allow | 7 | 0 | 0 | Yes | No |
This analysis examines appeal outcomes and the strategic value of filing appeals for examiner DELRUE, BRIAN CHRISTOPHER.
With a 14.3% 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, 30.0% 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 DELRUE, BRIAN CHRISTOPHER works in Art Unit 3745 and has examined 378 patent applications in our dataset. With an allowance rate of 87.3%, this examiner has an above-average tendency to allow applications. Applications typically reach final disposition in approximately 27 months.
Examiner DELRUE, BRIAN CHRISTOPHER's allowance rate of 87.3% places them in the 66% percentile among all USPTO examiners. This examiner has an above-average tendency to allow applications.
On average, applications examined by DELRUE, BRIAN CHRISTOPHER receive 1.38 office actions before reaching final disposition. This places the examiner in the 21% percentile for office actions issued. This examiner issues significantly fewer office actions than most examiners.
The median time to disposition (half-life) for applications examined by DELRUE, BRIAN CHRISTOPHER is 27 months. This places the examiner in the 74% percentile for prosecution speed. Prosecution timelines are slightly faster than average with this examiner.
Conducting an examiner interview provides a +16.8% benefit to allowance rate for applications examined by DELRUE, BRIAN CHRISTOPHER. This interview benefit is in the 58% 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, 35.5% of applications are subsequently allowed. This success rate is in the 80% percentile among all examiners. Strategic Insight: RCEs are highly effective with this examiner compared to others. If you receive a final rejection, filing an RCE with substantive amendments or arguments has a strong likelihood of success.
This examiner enters after-final amendments leading to allowance in 38.5% of cases where such amendments are filed. This entry rate is in the 59% 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, 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 53.3% of appeals filed. This is in the 24% percentile among all examiners. Of these withdrawals, 12.5% 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, 66.7% are granted (fully or in part). This grant rate is in the 74% percentile among all examiners. Strategic Note: Petitions show above-average success regarding this examiner's actions. Petitionable matters include restriction requirements (MPEP § 1002.02(c)(2)) and various procedural issues.
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.