Detailed information about the 100 most recent patent applications.
| Application Number | Title | Filing Date | Disposal Date | Disposition | Time (months) | Office Actions | Restrictions | Interview | Appeal |
|---|---|---|---|---|---|---|---|---|---|
| 19255078 | AIRFOIL-MOUNTED ACOUSTIC RESONATOR ARRAY FOR GAS TURBINE ENGINE COMPONENT | June 2025 | March 2026 | Allow | 8 | 1 | 1 | Yes | No |
| 19239186 | TEST BLADE FOR GAS TURBINE ENGINE AND METHOD OF MAKING | June 2025 | February 2026 | Allow | 8 | 1 | 0 | No | No |
| 19215171 | Mixing Utensil | May 2025 | December 2025 | Allow | 7 | 1 | 1 | Yes | No |
| 19201295 | SEALING ARRANGEMENT FOR A TURBOMACHINE, SEAL CARRIER ELEMENT FOR THE SEALING ARRANGEMENT, GUIDE BLADE ELEMENT, AND TURBOMACHINE | May 2025 | December 2025 | Allow | 7 | 1 | 1 | No | No |
| 19084572 | AIR MOVING DEVICES, AERODYNAMIC ROTOR, AND METHODS | March 2025 | December 2025 | Allow | 9 | 1 | 1 | Yes | No |
| 19082910 | FLUID FLOW DISTRIBUTOR FOR VAPOR PHASE COATING OF TURBINE COMPONENTS | March 2025 | October 2025 | Allow | 7 | 0 | 0 | Yes | No |
| 19044230 | GAS TURBINE ENGINE ROTOR BLADE GEOMETRY AND METHOD FOR SELECTING SAME | February 2025 | November 2025 | Allow | 9 | 1 | 0 | No | No |
| 19021666 | UNDUCTED AIRFOIL ASSEMBLY | January 2025 | October 2025 | Allow | 9 | 1 | 1 | Yes | No |
| 18878775 | AIR GUIDE RING AND AXIAL FLOW FAN COMPRISING SAME | December 2024 | March 2026 | Allow | 14 | 1 | 0 | Yes | No |
| 18872664 | METHOD FOR CONTROLLING OF A PUMP UNIT AND A PUMP UNIT FOR PUMPING LIQUID OR SUSPENSION | December 2024 | February 2026 | Allow | 14 | 1 | 0 | Yes | No |
| 18926574 | AIRCRAFT ENGINE HAVING A SCROLL CASE AND A TURBINE SUPPORT CASE SECURED TOGETHER | October 2024 | November 2025 | Allow | 12 | 1 | 0 | No | No |
| 18859818 | PROPELLER BLADE OR AIRFOIL WITH HOLLOW COMPOSITE ROOT | October 2024 | August 2025 | Allow | 10 | 1 | 1 | Yes | No |
| 18857316 | WIND TURBINE BLADE AND METHOD FOR MANUFACTURING A WIND TURBINE BLADE | October 2024 | December 2025 | Allow | 14 | 1 | 0 | Yes | No |
| 18891746 | AIR MOVING DEVICES, AERODYNAMIC ROTOR, AND METHODS | September 2024 | December 2025 | Allow | 15 | 1 | 1 | Yes | No |
| 18813053 | TURBINE COMPONENT FOR GAS TURBINE ENGINE | August 2024 | August 2025 | Allow | 12 | 0 | 1 | No | No |
| 18810890 | CENTRIFUGAL FAN | August 2024 | December 2025 | Allow | 16 | 1 | 1 | Yes | No |
| 18806936 | INTEGRATED AIR CYCLE MACHINE FOR AN ENVIRONMENTAL CONTROL SYSTEM OF AN AIRCRAFT | August 2024 | October 2025 | Allow | 14 | 1 | 1 | No | No |
| 18805478 | Masking System | August 2024 | January 2026 | Allow | 18 | 1 | 1 | No | No |
| 18765490 | FAN LOAD TENSION STRUCTURAL GUIDE VANE WITH BYPASS COOLING CAVITIES | July 2024 | August 2025 | Allow | 13 | 2 | 1 | Yes | No |
| 18753294 | MILL SPINDLE FAN | June 2024 | August 2025 | Allow | 14 | 2 | 1 | Yes | No |
| 18752669 | OIL-LUBRICATED VACUUM PUMP WITH IMPROVED OIL SEALING | June 2024 | December 2025 | Allow | 18 | 1 | 0 | No | No |
| 18750076 | DUAL-WALLED COMPONENTS FOR A GAS TURBINE ENGINE | June 2024 | October 2025 | Allow | 16 | 2 | 1 | Yes | No |
| 18749190 | SLIP BASED RADIAL BEARING SUPPORT | June 2024 | October 2025 | Allow | 15 | 1 | 1 | No | No |
| 18721922 | MODULAR WIND TURBINE BLADE | June 2024 | November 2025 | Allow | 17 | 1 | 0 | No | No |
| 18715603 | AUXILIARY ARM FOR A TURBOMACHINE EXHAUST CASING | June 2024 | October 2025 | Allow | 17 | 1 | 0 | Yes | No |
| 18731044 | Compact Blade Pitch Mechanism And Aircraft Using Same | May 2024 | September 2025 | Allow | 16 | 1 | 1 | Yes | No |
| 18731058 | PASSIVE NOISE DISSIPATOR FOR LAPTOP COOLING FANS | May 2024 | October 2025 | Allow | 17 | 2 | 1 | Yes | No |
| 18678000 | GAS TURBINE ENGINE | May 2024 | August 2025 | Allow | 15 | 1 | 1 | Yes | No |
| 18678281 | TURBINE ENGINE INCLUDING A VANE SUPPORT AND A VANE | May 2024 | August 2025 | Allow | 14 | 2 | 1 | Yes | No |
| 18678876 | TURBINE SHROUD ASSEMBLIES WITH STRIP SEALS | May 2024 | June 2025 | Allow | 12 | 1 | 1 | No | No |
| 18675388 | COMPRESSOR ROTOR BLADE AIRFOILS | May 2024 | September 2024 | Allow | 4 | 0 | 0 | No | No |
| 18673618 | TURBOCHARGER BEARING HOUSING | May 2024 | September 2025 | Allow | 16 | 2 | 1 | Yes | No |
| 18661272 | SRV OPEN ROTOR WITH CORE INLET FORWARD OF ROTOR | May 2024 | July 2025 | Allow | 14 | 2 | 1 | Yes | No |
| 18657373 | AXIAL EXPANDABLE EXHAUST DUCT | May 2024 | January 2025 | Allow | 8 | 1 | 0 | No | No |
| 18655692 | Lowering Ceiling Fan Device | May 2024 | September 2025 | Allow | 16 | 2 | 1 | Yes | No |
| 18655958 | FLANGE WITH STRESS ATTENTUATION FEATURE | May 2024 | August 2025 | Allow | 15 | 2 | 1 | No | No |
| 18654134 | ENGINE COMPONENT | May 2024 | May 2025 | Allow | 12 | 2 | 1 | Yes | No |
| 18653052 | COMPOSITE AIRFOIL ASSEMBLY HAVING A COMPOSITE AIRFOIL AND SPAR | May 2024 | June 2025 | Allow | 14 | 2 | 1 | Yes | No |
| 18652338 | TURBOMACHINE WITH TURBINE SECTION HAVING INTEGRATED FLUID SEPARATOR | May 2024 | March 2025 | Allow | 11 | 1 | 1 | No | No |
| 18651631 | RADIAL TURBINE ROTOR WITH ADDITIVE LAYER MANUFACTURED COMPONENTS | April 2024 | December 2025 | Abandon | 20 | 2 | 1 | Yes | No |
| 18646941 | AFT MOUNTED PUSHER FAN FOR GAS TURBINE ENGINE | April 2024 | September 2025 | Allow | 16 | 2 | 1 | Yes | No |
| 18643284 | ANGULARLY POSITIONED MARINE PROPELLER COMBINATION AND A METHOD OF OPERATING A MARINE PROPELLER COMBINATION | April 2024 | August 2025 | Allow | 16 | 2 | 1 | Yes | No |
| 18638440 | MULTI-STAGE PARTIAL ADMISSION AXIAL TURBINE | April 2024 | August 2025 | Allow | 16 | 1 | 0 | No | No |
| 18638410 | CONNECTION COMPONENT AND FAN | April 2024 | March 2025 | Allow | 11 | 2 | 1 | No | No |
| 18636837 | ANNULUS FILLER FOR A GAS TURBINE ENGINE | April 2024 | August 2025 | Allow | 16 | 1 | 0 | Yes | No |
| 18636729 | ENERGY CONVERSION DEVICE, ASSOCIATED SYSTEMS AND METHODS | April 2024 | November 2025 | Allow | 19 | 1 | 1 | No | No |
| 18635858 | AERODYNAMICALLY MISTUNED AIRFOILS FOR UNSTEADY LOSS REDUCTION | April 2024 | April 2025 | Allow | 12 | 1 | 1 | Yes | No |
| 18632841 | LEADING EDGE PLATING ON LOW PRESSURE COMPRESSOR VANE FOR WEIGHT AND STRENGTH OPTIMIZATION | April 2024 | November 2025 | Allow | 20 | 3 | 1 | Yes | No |
| 18619014 | FLUID FLOW DISTRIBUTOR FOR VAPOR PHASE COATING OF TURBINE COMPONENTS | March 2024 | December 2024 | Allow | 9 | 1 | 1 | Yes | No |
| 18692557 | TURBINE ENGINE ELEMENT COMPRISING AT LEAST ONE BLADE OBTAINED BY ADDITIVE MANUFACTURING | March 2024 | March 2026 | Allow | 24 | 2 | 1 | Yes | No |
| 18600604 | SEGMENTED VARIABLE FAN OUTLET GUIDE VANE WITH PASS THROUGH ACTUATION MECHANISMS | March 2024 | July 2025 | Allow | 17 | 2 | 1 | Yes | No |
| 18594658 | SYSTEMS AND METHODS FOR SENSORS ON CIRCUMFERENTIAL INTERIOR SURFACE OF TURBOMACHINE CASING | March 2024 | November 2024 | Allow | 8 | 1 | 0 | No | No |
| 18687378 | DAMPING DEVICE FOR A ROTOR WHEEL OF AN AIRCRAFT TURBINE ENGINE, ROTOR WHEEL FOR AN AIRCRAFT TURBINE ENGINE, TURBINE ENGINE FOR AN AIRCRAFT, AND METHOD FOR MANUFACTURING A DAMPING DEVICE | February 2024 | October 2025 | Allow | 19 | 1 | 1 | Yes | No |
| 18588230 | DUST-COLLECTING DEVICE FOR FAN BLADES | February 2024 | October 2024 | Allow | 7 | 1 | 0 | Yes | No |
| 18686496 | Splash Ring | February 2024 | September 2025 | Abandon | 18 | 1 | 1 | No | No |
| 18586012 | COVER PLATE CONNECTIONS FOR A HOLLOW FAN BLADE | February 2024 | October 2025 | Allow | 19 | 3 | 1 | Yes | No |
| 18583544 | AIRCRAFT ENGINE IMPELLER WITH EXDUCER SHROUD FORWARD SWEEP | February 2024 | December 2025 | Allow | 22 | 3 | 1 | Yes | No |
| 18581641 | AXIALLY ADJUSTABLE INSERTED RING WITHIN PACKING RING AND METHOD OF USING SAME | February 2024 | April 2025 | Allow | 14 | 2 | 1 | Yes | No |
| 18581225 | PARTITION DAMPER SEAL CONFIGURATIONS FOR SEGMENTED INTERNAL COOLING HARDWARE | February 2024 | October 2024 | Allow | 8 | 1 | 0 | Yes | No |
| 18684371 | STATOR PART OF A TURBOMACHINE COMPRISING A BLADE AND A FIN DEFINING BETWEEN THEM A DECREASING SURFACE FROM UPSTREAM TO DOWNSTREAM IN THE GAS FLOW DIRECTION | February 2024 | January 2025 | Allow | 11 | 2 | 0 | Yes | No |
| 18683579 | METHODS OF SEMI-PERMANENTLY ATTACHING COMPONENTS ON A WIND TURBINE ROTOR BLADE | February 2024 | August 2025 | Allow | 18 | 1 | 1 | Yes | No |
| 18434049 | VANE WITH SEAL | February 2024 | May 2025 | Allow | 15 | 1 | 1 | No | No |
| 18681111 | LIQUID-FEED-TYPE GAS COMPRESSOR | February 2024 | May 2025 | Allow | 16 | 1 | 1 | No | No |
| 18430130 | AIRFOIL-MOUNTED ACOUSTIC RESONATOR ARRAY FOR GAS TURBINE ENGINE COMPONENT | February 2024 | March 2025 | Allow | 14 | 2 | 1 | Yes | No |
| 18424383 | GAS TURBINE ENGINE ROTOR BLADE GEOMETRY AND METHOD FOR SELECTING SAME | January 2024 | September 2024 | Allow | 8 | 0 | 1 | Yes | No |
| 18408739 | FLOW BODY FOR A GAS TURBINE, GAS TURBINE, METHOD FOR MANUFACTURING A FLOW BODY FOR A GAS TURBINE, AND METHOD FOR REPAIRING A FLOW BODY OF A GAS TURBINE | January 2024 | April 2025 | Allow | 15 | 1 | 1 | Yes | No |
| 18408722 | BLISK | January 2024 | October 2024 | Allow | 9 | 1 | 1 | Yes | No |
| 18572095 | FAN FOR HANDHELD BLOWER | December 2023 | March 2025 | Allow | 15 | 2 | 0 | No | No |
| 18541234 | AERONAUTICAL PROPULSION SYSTEM | December 2023 | May 2025 | Allow | 17 | 1 | 1 | Yes | No |
| 18541060 | AERONAUTICAL PROPULSION SYSTEM | December 2023 | July 2024 | Allow | 7 | 1 | 1 | Yes | No |
| 18571100 | SHEAR WEB FOR A WIND TURBINE BLADE AND METHOD OF MAKING SAME | December 2023 | April 2025 | Allow | 16 | 1 | 1 | Yes | No |
| 18570342 | SYSTEM FOR CHANGING THE PITCH OF THE BLADES OF A TURBOMACHINE PROPELLER | December 2023 | December 2024 | Allow | 12 | 2 | 0 | No | No |
| 18536428 | COMPONENT FOR A TURBINE ENGINE WITH A COOLING HOLE | December 2023 | January 2025 | Allow | 14 | 2 | 1 | Yes | No |
| 18530937 | Rotor Blade with Frangible Spar for a Gas Turbine Engine | December 2023 | March 2026 | Allow | 27 | 1 | 1 | No | No |
| 18565112 | COOLING A WIND TURBINE | November 2023 | March 2026 | Allow | 27 | 3 | 1 | Yes | No |
| 18511237 | ADDITIVE MANUFACTURED SEAL ROTOR; AND METHOD | November 2023 | November 2024 | Allow | 12 | 2 | 0 | No | No |
| 18560043 | WING STRUCTURE AND WING STRUCTURE MANUFACTURING METHOD | November 2023 | September 2025 | Allow | 22 | 2 | 1 | Yes | No |
| 18497452 | COMPRESSOR ROTOR BLADE AIRFOILS | October 2023 | November 2024 | Allow | 12 | 0 | 0 | Yes | No |
| 18496251 | FAN BLADE FOR A GAS TURBINE ENGINE | October 2023 | September 2024 | Allow | 11 | 1 | 1 | No | No |
| 18383506 | Morphing Airfoil | October 2023 | September 2024 | Allow | 11 | 2 | 0 | Yes | No |
| 18381062 | AIRCRAFT POWER SYSTEM MODULE WITH INTEGRAL LUBRICANT RESERVOIR | October 2023 | February 2025 | Allow | 16 | 2 | 0 | Yes | No |
| 18381066 | LUBRICATION SYSTEM FOR AIRCRAFT POWERPLANT AND CLUTCH SYSTEM | October 2023 | May 2025 | Allow | 19 | 3 | 1 | No | No |
| 18377397 | BEARING ASSEMBLY FOR A GAS TURBINE ENGINE | October 2023 | December 2024 | Allow | 15 | 1 | 0 | No | No |
| 18552853 | Device for sealing and reinjecting a bypass flow for a turbine nozzle | September 2023 | April 2025 | Allow | 18 | 2 | 0 | No | No |
| 18550414 | IMPELLER ASSEMBLY AND MIXING APPARATUS | September 2023 | February 2025 | Allow | 17 | 1 | 0 | No | No |
| 18462425 | PROPELLER CONTROL MECHANISM | September 2023 | November 2023 | Allow | 2 | 1 | 1 | No | No |
| 18463013 | THRUST GENERATING DEVICE | September 2023 | April 2025 | Allow | 19 | 1 | 1 | No | No |
| 18238491 | Rotor Structure for Fluid Kinetic Power Generation Turbine | August 2023 | September 2025 | Abandon | 24 | 2 | 1 | No | No |
| 18452246 | FAN BLADE OR VANE WITH IMPROVED BIRD IMPACT CAPABILITY | August 2023 | March 2025 | Allow | 19 | 2 | 0 | Yes | No |
| 18231561 | ROTOR ASSEMBLY FOR GAS TURBINE ENGINES WITH REPLACEABLE BALANCE WEIGHT BANDS | August 2023 | September 2024 | Allow | 13 | 1 | 1 | No | No |
| 18446078 | FAN BLADE OR VANE WITH IMPROVED BIRD IMPACT CAPABILITY | August 2023 | April 2025 | Allow | 20 | 2 | 0 | Yes | No |
| 18354714 | INTEGRALLY BLADED ROTOR WITH INCREASED RIM BENDING STIFFNESS | July 2023 | October 2024 | Allow | 15 | 1 | 0 | Yes | No |
| 18348452 | COMPOSITE AIRFOIL ASSEMBLY FOR A TURBINE ENGINE | July 2023 | January 2025 | Allow | 18 | 1 | 1 | Yes | No |
| 18345018 | UNDUCTED AIRFOIL ASSEMBLY | June 2023 | October 2024 | Allow | 15 | 2 | 1 | No | No |
| 18215308 | ADVANCED THERMALLY CONDUCTIVE LIGHTWEIGHT ELASTOMERIC SEAL | June 2023 | August 2024 | Allow | 13 | 1 | 1 | No | No |
| 18337533 | TURBINE BLADE SQUEALER TIP WALL WITH CHAMFERED SURFACE | June 2023 | September 2024 | Allow | 15 | 3 | 0 | Yes | No |
| 18208684 | NON-CIRCULAR STRESS REDUCING CROSSOVER | June 2023 | February 2024 | Allow | 8 | 1 | 1 | Yes | No |
| 18207749 | ROTARY WING AIR VEHICLE | June 2023 | October 2024 | Allow | 17 | 1 | 0 | Yes | No |
| 18200220 | ADDITIVELY MANUFACTURED RADIAL TURBINE ROTOR WITH COOLING MANIFOLDS | May 2023 | January 2024 | Allow | 8 | 1 | 0 | Yes | No |
| 18316656 | VARIABLE PITCH FAN OF A GAS TURBINE ENGINE | May 2023 | June 2024 | Allow | 13 | 1 | 1 | Yes | No |
This analysis examines appeal outcomes and the strategic value of filing appeals for examiner ZAMORA ALVAREZ, ERIC J.
With a 37.5% 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, 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.
✓ 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 ZAMORA ALVAREZ, ERIC J works in Art Unit 3745 and has examined 403 patent applications in our dataset. With an allowance rate of 86.6%, this examiner has an above-average tendency to allow applications. Applications typically reach final disposition in approximately 29 months.
Examiner ZAMORA ALVAREZ, ERIC J's allowance rate of 86.6% places them in the 65% percentile among all USPTO examiners. This examiner has an above-average tendency to allow applications.
On average, applications examined by ZAMORA ALVAREZ, ERIC J receive 1.77 office actions before reaching final disposition. This places the examiner in the 39% percentile for office actions issued. This examiner issues fewer office actions than average, which may indicate efficient prosecution or a more lenient examination style.
The median time to disposition (half-life) for applications examined by ZAMORA ALVAREZ, ERIC J is 29 months. This places the examiner in the 67% percentile for prosecution speed. Prosecution timelines are slightly faster than average with this examiner.
Conducting an examiner interview provides a +28.3% benefit to allowance rate for applications examined by ZAMORA ALVAREZ, ERIC J. This interview benefit is in the 76% 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, 31.4% of applications are subsequently allowed. This success rate is in the 64% percentile among all examiners. Strategic Insight: RCEs show above-average effectiveness with this examiner. Consider whether your amendments or new arguments are strong enough to warrant an RCE versus filing a continuation.
This examiner enters after-final amendments leading to allowance in 49.2% of cases where such amendments are filed. This entry rate is in the 74% 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 22% 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 63.6% of appeals filed. This is in the 43% percentile among all examiners. 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, 46.7% are granted (fully or in part). This grant rate is in the 41% 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 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 1.7% of allowed cases (in the 66% 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.