Detailed information about the 100 most recent patent applications.
| Application Number | Title | Filing Date | Disposal Date | Disposition | Time (months) | Office Actions | Restrictions | Interview | Appeal |
|---|---|---|---|---|---|---|---|---|---|
| 19141304 | TRANSMISSION SYSTEM | June 2025 | February 2026 | Allow | 8 | 0 | 0 | No | No |
| 19226668 | AIRCRAFT STRUCTURE | June 2025 | November 2025 | Allow | 6 | 0 | 0 | No | No |
| 19217117 | Stabilizers for Aerial Projectiles | May 2025 | December 2025 | Allow | 7 | 0 | 0 | No | No |
| 19121782 | FLAPPING DEVICE | April 2025 | January 2026 | Allow | 9 | 0 | 0 | No | No |
| 19110231 | PROPULSION SYSTEM FOR MULTICOPTERS AND RELATED AIRCRAFTS | March 2025 | March 2026 | Allow | 12 | 0 | 0 | Yes | No |
| 18552079 | PASSENGER TRANSPORT SYSTEM PROPELLED BY A SPACE LAUNCHER, HAVING A SEAT WITH VARIABLE INCLINATION BASED ON THE LOAD FACTOR | January 2025 | October 2025 | Allow | 25 | 0 | 0 | No | No |
| 19037788 | SATELLITE DISPENSING SYSTEM | January 2025 | September 2025 | Allow | 8 | 0 | 0 | No | No |
| 19033472 | Collapsible Fuel Cells for Aircraft | January 2025 | July 2025 | Allow | 6 | 0 | 0 | No | No |
| 19006885 | SYSTEM AND METHOD OF EJECTING A PAYLOAD FROM AN EXTRATERRESTRIAL SURFACE | December 2024 | June 2025 | Allow | 6 | 0 | 0 | No | No |
| 18978723 | RELIABLE SEPARATION OF A CLAMPED HDRM INTERFACE | December 2024 | June 2025 | Allow | 6 | 0 | 1 | No | No |
| 18976639 | DEVICE FOR ABSORBING ENERGY BY COMPRESSION, AIRCRAFT COMPRISING AT LEAST ONE SUCH DEVICE | December 2024 | June 2025 | Allow | 6 | 0 | 0 | No | No |
| 18867836 | AERODYNAMIC POD FOR AIRCRAFTS | November 2024 | June 2025 | Allow | 7 | 0 | 0 | No | No |
| 18930844 | ATMOSPHERIC RE-ENTRY VEHICLE WITH SKEWED BASE HEAT SHIELD | October 2024 | May 2025 | Allow | 7 | 0 | 0 | No | No |
| 18923918 | ARTIFICIAL SATELLITE AND ARTIFICIAL SATELLITE SYSTEM | October 2024 | May 2025 | Allow | 7 | 0 | 0 | No | No |
| 18855836 | DETERMINATION OF SPACECRAFT INERTIAL PROPERTIES | October 2024 | October 2025 | Allow | 12 | 0 | 0 | No | No |
| 18907917 | AIRCRAFT RUDDER PEDAL WITH MECHANICAL KINEMATIC CHAIN | October 2024 | June 2025 | Allow | 8 | 0 | 0 | No | No |
| 18905523 | AIRCRAFT COMPRISING AT LEAST ONE ENGINE ATTACHMENT SYSTEM THAT HAS REDUCED VERTICAL BULK | October 2024 | May 2025 | Allow | 7 | 0 | 0 | No | No |
| 18829462 | ELECTRICAL UMBILICAL SYSTEM FOR SPACE LAUNCH VEHICLE, USING ELECTROMAGNET | September 2024 | May 2025 | Allow | 8 | 0 | 0 | No | No |
| 18809177 | PROPULSOR ASSEMBLY POWERED BY A DUAL MOTOR SYSTEM | August 2024 | November 2025 | Abandon | 15 | 1 | 0 | No | No |
| 18807132 | Panels for use in a galley of an aircraft | August 2024 | January 2026 | Allow | 17 | 1 | 0 | Yes | No |
| 18776800 | AIRCRAFT TAKE-OFF AND LANDING DEVICE | July 2024 | April 2025 | Allow | 9 | 0 | 0 | No | No |
| 18728281 | ORBITAL DEPLOYMENT MODULE WITH A THREE-POINT SPACE PROPULSION SYSTEM | July 2024 | March 2025 | Allow | 9 | 0 | 0 | No | No |
| 18755692 | VTOL Aircraft Using Fixed Forward Canted Rotors With Forward-Facing Rotors | June 2024 | January 2026 | Allow | 19 | 0 | 0 | No | No |
| 18753030 | HELICOPTER ROTOR SYSTEM | June 2024 | June 2025 | Allow | 11 | 1 | 0 | No | No |
| 18747187 | VERTICAL TAKE-OFF AND LANDING AIRCRAFT | June 2024 | February 2026 | Allow | 20 | 0 | 0 | No | No |
| 18744822 | AIR DIRECTING ARRANGEMENT FOR CONTROLLING AIRFLOW AT AN OUTLET | June 2024 | January 2026 | Allow | 19 | 1 | 0 | No | No |
| 18744203 | MOVEABLE WING TIP ACTUATION SYSTEM | June 2024 | November 2025 | Allow | 17 | 1 | 0 | Yes | No |
| 18717204 | Airship with Self-Ballasting Airframe | June 2024 | January 2026 | Allow | 19 | 2 | 0 | No | No |
| 18732012 | ROTOR ASSEMBLY AND UNMANNED AERIAL VEHICLE HAVING THE SAME | June 2024 | March 2025 | Allow | 9 | 0 | 0 | No | No |
| 18664116 | SYSTEM AND METHOD FOR DIMPLED SPHERICAL STORAGE UNITS | May 2024 | April 2025 | Allow | 11 | 1 | 0 | No | No |
| 18663365 | SYSTEM AND METHOD FOR A STRATOSPHERIC AIRCRAFT | May 2024 | March 2025 | Allow | 10 | 0 | 0 | No | No |
| 18663355 | SYSTEM AND METHOD FOR A SPACECRAFT DOCKING STATION | May 2024 | May 2025 | Allow | 12 | 1 | 0 | No | No |
| 18661207 | COVER FOR A TRANSITION FROM A LINING TO A MONUMENT | May 2024 | October 2025 | Allow | 17 | 1 | 0 | No | No |
| 18657688 | TRAM SYSTEM AND METHODS FOR AUTONOMOUS TAKEOFF AND LANDING OF AIRCRAFT | May 2024 | December 2024 | Allow | 7 | 0 | 0 | No | No |
| 18654560 | MOVABLE WALL SECTION FOR REDUCED MOBILITY PASSENGER ACCESS | May 2024 | March 2025 | Allow | 10 | 0 | 0 | No | No |
| 18648328 | Rotor Deployment Mechanism For Vertical Take-Off And Landing Aircraft | April 2024 | December 2024 | Allow | 7 | 0 | 0 | No | No |
| 18705023 | ANTI-MISUSE SYSTEM, CONTROL SYSTEM, CHILD SAFETY SEAT, ANTI-MISUSE CONTROL METHOD AND METHOD FOR CONTROLLING CHILD SAFETY SEAT | April 2024 | February 2026 | Allow | 22 | 0 | 0 | No | No |
| 18645615 | COVER SYSTEM FOR WRAPPING A BACKREST FRAME | April 2024 | January 2026 | Allow | 21 | 0 | 0 | No | No |
| 18702297 | AIRCRAFT LANDING GEAR HAVING INTERLOCKED MALE AND FEMALE PARTS FOR TRANSMITTING MECHANICAL TORQUE | April 2024 | January 2025 | Allow | 9 | 0 | 0 | No | No |
| 18629943 | SENSOR-EQUIPPED SEAT | April 2024 | October 2025 | Allow | 18 | 0 | 0 | No | No |
| 18628323 | PAYLOAD CONTAINER FOR PARACHUTE DELIVERY SYSTEMS | April 2024 | August 2025 | Allow | 17 | 1 | 0 | No | No |
| 18616112 | Electric Vertical Take-Off And Landing Aircraft | March 2024 | August 2025 | Allow | 17 | 0 | 0 | No | No |
| 18695211 | CONVEYANCE SEAT | March 2024 | October 2025 | Allow | 19 | 0 | 0 | No | No |
| 18612132 | FLIGHT CONTROL OF LIFT PLUS CRUISE QUADCOPTER AIRCRAFT | March 2024 | June 2025 | Allow | 15 | 0 | 0 | No | No |
| 18610401 | CONTROL OF LIFT PLUS CRUISE QUADCOPTER AIRCRAFT | March 2024 | February 2026 | Abandon | 23 | 2 | 0 | No | No |
| 18593719 | Oblique Flying Wing Aircraft With Internal Ducting And Internal Propulsion | March 2024 | December 2024 | Allow | 10 | 0 | 0 | No | No |
| 18592141 | LIFT NACELLE | February 2024 | October 2024 | Allow | 7 | 0 | 0 | No | No |
| 18584242 | SPACE STRUCTURE CONTROL SYSTEM AND SPACE STRUCTURE CONTROL METHOD | February 2024 | January 2025 | Allow | 10 | 0 | 0 | No | No |
| 18444624 | Electric Vertical Take-Off And Landing Aircraft | February 2024 | September 2025 | Allow | 19 | 5 | 0 | No | No |
| 18416966 | SUPPORT ASSEMBLY FOR AN AIRCRAFT DOOR | January 2024 | January 2026 | Allow | 24 | 1 | 0 | No | No |
| 18413453 | Solar Sail for Orbital Maneuvers | January 2024 | November 2025 | Allow | 22 | 2 | 0 | No | No |
| 18576155 | SATELLITE WITH SPOT LIGHT MODE FOR EXTENDED DURATION TARGET IMAGING | January 2024 | May 2025 | Allow | 16 | 2 | 0 | No | No |
| 18575661 | METHOD FOR CONTROLLING THE ENERGY SET-UP OF A HYBRID PROPULSION SYSTEM | December 2023 | September 2025 | Allow | 21 | 1 | 0 | No | No |
| 18400150 | ICE PROTECTION SYSTEM HAVING MEMORY-BASED ICE REMOVAL ELEMENTS | December 2023 | February 2026 | Abandon | 26 | 2 | 0 | Yes | No |
| 18401316 | VTOL AIRCRAFT WITH DUAL PROPELLERS AND DIRECTIONAL CLUTCH | December 2023 | August 2025 | Allow | 20 | 2 | 0 | No | No |
| 18391266 | SYSTEMS AND METHODS FOR IMPROVED GEARBOXES FOR EVTOL AIRCRAFT | December 2023 | June 2024 | Allow | 6 | 0 | 0 | No | No |
| 18544463 | MAIN FRAME STRUCTURE HAVING BOX-SECTION BEARING BEAMS OF LAUNCH VEHICLE ENGINE | December 2023 | February 2024 | Allow | 2 | 0 | 0 | No | No |
| 18541910 | AEROSPACE VEHICLE SYSTEM AND METHOD OF OPERATION | December 2023 | November 2025 | Abandon | 23 | 1 | 0 | No | No |
| 18536837 | AERIAL VEHICLE WITH INDEPENDENT NAVIGATION IN SIX DEGREES OF FREEDOM | December 2023 | August 2025 | Allow | 21 | 1 | 0 | No | No |
| 18521655 | NACELLE DEVICE AND VTOL AIRCRAFT | November 2023 | November 2025 | Abandon | 23 | 1 | 0 | No | No |
| 18511258 | TORQUE TRANSMISSION DEVICE | November 2023 | March 2025 | Allow | 16 | 1 | 0 | No | No |
| 18511275 | CONTROL UNIT RESISTIVE AND LOCKING SYSTEM | November 2023 | December 2024 | Allow | 14 | 0 | 0 | Yes | No |
| 18561051 | AIR INLET FOR AN AIRCRAFT PROPULSION UNIT COMPRISING MOBILE MEMBERS FOR PROMOTING A THRUST REVERSAL PHASE, AND METHOD FOR USING SUCH AN AIR INLET | November 2023 | October 2024 | Allow | 11 | 0 | 0 | No | No |
| 18509696 | ROTORCRAFT WITH A NON-RETRACTABLE WHEEL-TYPE LANDING GEAR | November 2023 | March 2025 | Allow | 16 | 1 | 0 | No | No |
| 18560854 | LEADING-EDGE HIGH-LIFT DEVICE, WING, AND AIRCRAFT | November 2023 | March 2025 | Allow | 16 | 1 | 0 | No | No |
| 18388255 | FULLY AUTOMATED TOWING, ALIGNMENT AND HANGAR SYSTEM AND METHOD FOR OFFSHORE OPERATION HELICOPTER | November 2023 | January 2024 | Allow | 2 | 0 | 0 | No | No |
| 18496850 | Compound vertical takeoff and landing aircraft | October 2023 | June 2025 | Allow | 19 | 1 | 0 | No | No |
| 18383018 | Spacecraft with Retractable Solar Sails | October 2023 | December 2024 | Allow | 14 | 0 | 0 | No | No |
| 18379531 | ROW OF PASSENGER SEATS CONVERTIBLE TO A BED | October 2023 | March 2025 | Allow | 17 | 1 | 0 | No | No |
| 18554650 | ANNULAR AEROSPIKE NOZZLE WITH WIDELY-SPACED THRUST CHAMBERS, ENGINE INCLUDING THE ANNULAR AEROSPIKE NOZZLE, AND VEHICLE INCLUDING THE ENGINE | October 2023 | July 2024 | Allow | 9 | 0 | 0 | Yes | No |
| 18554587 | A NON-AXISYMMETRIC HEAT SHIELD, A NOZZLE DEFINED AT LEAST PARTIALLY BY THE HEAT SHIELD, AN ENGINE INCLUDING THE NOZZLE, AND A VEHICLE INCLUDING THE ENGINE | October 2023 | July 2024 | Allow | 9 | 0 | 0 | No | No |
| 18373276 | AIRCRAFT PORTION WITH A REDUCED DRAG | September 2023 | October 2024 | Allow | 12 | 0 | 0 | No | No |
| 18282846 | AN ADAPTABLE LATTICE STRUCTURE FOR MULTI-MISSION DRONES | September 2023 | January 2025 | Allow | 16 | 1 | 0 | No | No |
| 18243229 | LONG RANGE FREIGHTER AIRCRAFT | September 2023 | June 2024 | Allow | 10 | 2 | 0 | Yes | No |
| 18240914 | PROPULSOR ASSEMBLY POWERED BY A DUAL MOTOR SYSTEM | August 2023 | April 2024 | Allow | 7 | 0 | 0 | No | No |
| 18458594 | DUAL SPEED PLANETARY GEAR SYSTEM FOR CONVERTIBLE ENGINES | August 2023 | September 2024 | Allow | 12 | 0 | 0 | No | No |
| 18238487 | INTEGRATED WORKSTATION FOR AN IMMERSIVE EXPERIENCE AND VIDEO COMMUNICATIONS | August 2023 | November 2025 | Abandon | 27 | 1 | 0 | No | No |
| 18276051 | FLYING OBJECT COPING SYSTEM, DEFENSE INFORMATION INTEGRATION CENTER, COMMUNICATION ROUTE SEARCH DEVICE, AND FLIGHT PATH PREDICTION DEVICE | August 2023 | September 2024 | Allow | 13 | 0 | 0 | No | No |
| 18275404 | FLYING PATH PREDICTION METHOD, GROUND SYSTEM, FLYING OBJECT'S FLYING PATH MODEL, FLYING PATH PREDICTION DEVICE, FLYING OBJECT TRACKING SYSTEM, FLYING OBJECT COPING SYSTEM, UNIFIED DATA LIBRARY, SURVEILLANCE SATELLITE, AND SATELLITE CONSTELLATION | August 2023 | September 2024 | Allow | 14 | 0 | 0 | No | No |
| 18358406 | AIRCRAFT WALL ASSEMBLY | July 2023 | March 2025 | Allow | 20 | 1 | 0 | No | No |
| 18205842 | TRAM SYSTEM AND METHODS FOR AUTONOMOUS TAKEOFF AND LANDING OF AIRCRAFT | June 2023 | February 2024 | Allow | 8 | 0 | 0 | No | No |
| 18201944 | BLENDED WING BODY AIRCRAFT | May 2023 | February 2024 | Allow | 9 | 2 | 0 | Yes | No |
| 18321097 | LUGGAGE COMPARTMENT, CABIN COMPONENT ASSEMBLY AND AIRCRAFT | May 2023 | June 2024 | Allow | 13 | 0 | 0 | No | No |
| 18037887 | Cable Tilt Actuator for an Aircraft | May 2023 | November 2024 | Allow | 18 | 1 | 0 | Yes | No |
| 18320346 | LANDING GEAR ASSEMBLY | May 2023 | June 2024 | Allow | 13 | 0 | 0 | No | No |
| 18320406 | INDEPENDENT NON-SOLAR POWERED EXPLORATORY CRAFT FOR ORBITAL RENDEZVOUS AND POSITIONING FRAMEWORK | May 2023 | August 2025 | Allow | 27 | 0 | 0 | No | No |
| 18314757 | FUEL CELLS CONFIGURED TO DELIVER BI-POLAR HIGH VOLTAGE DC POWER | May 2023 | April 2024 | Allow | 11 | 0 | 0 | Yes | No |
| 18313112 | MONUMENT FIXTURES | May 2023 | September 2024 | Allow | 17 | 2 | 0 | Yes | No |
| 18141936 | Dual-state rotatable propulsion system | May 2023 | July 2024 | Allow | 14 | 0 | 0 | No | No |
| 18298973 | Aircraft-based Modular Door Panel Assembly | April 2023 | August 2024 | Allow | 16 | 0 | 0 | No | No |
| 18030797 | SYSTEM FOR PROVIDING PROTECTION FROM ICING USING A FUEL CELL | April 2023 | August 2024 | Allow | 17 | 0 | 0 | No | No |
| 18131771 | Collapsible Fuel Cells for Aircraft | April 2023 | December 2024 | Allow | 20 | 1 | 0 | No | No |
| 18295329 | HELICOPTER ROTOR SYSTEM | April 2023 | April 2024 | Allow | 12 | 0 | 0 | No | No |
| 18194738 | ENGINE ATTACHMENT SYSTEM FOR AIRCRAFT AND METHOD FOR ATTACHING AN ENGINE | April 2023 | June 2025 | Allow | 26 | 2 | 0 | Yes | No |
| 18189537 | SYSTEMS AND METHODS FOR ROUTING ELECTRICAL WIRING THROUGH AN AIRCRAFT STRUCTURE | March 2023 | August 2024 | Allow | 17 | 1 | 0 | Yes | No |
| 18122974 | SYSTEM INCLUDING STOWABLE TABLET HOLDER APPARATUS | March 2023 | June 2024 | Allow | 15 | 0 | 0 | No | No |
| 18183530 | DYNAMIC AXIAL PRELOADING WITH FLEXURE PLATE | March 2023 | March 2024 | Allow | 12 | 0 | 0 | No | No |
| 18118129 | AIRCRAFT RUDDER PEDAL WITH MECHANICAL KINEMATIC CHAIN | March 2023 | August 2024 | Allow | 17 | 0 | 0 | No | No |
| 18044177 | AIRCRAFT RADOME INCORPORATING A LIGHTNING PROTECTION SYSTEM, AND AIRCRAFT COMPRISING SUCH A RADOME | March 2023 | December 2024 | Allow | 22 | 1 | 0 | No | No |
| 18176219 | Thermal Control Systems and Methods for Spacecraft | February 2023 | August 2024 | Allow | 18 | 1 | 0 | No | No |
This analysis examines appeal outcomes and the strategic value of filing appeals for examiner XAVIER, VALENTINA.
With a 0.0% reversal rate, the PTAB affirms the examiner's rejections in the vast majority of cases. This reversal rate is in the bottom 25% across the USPTO, indicating that appeals face significant challenges here.
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, 33.3% 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 face challenges. Ensure your case has strong merit before committing to full Board review.
✓ Filing a Notice of Appeal is strategically valuable. The act of filing often prompts favorable reconsideration during the mandatory appeal conference.
Examiner XAVIER, VALENTINA works in Art Unit 3642 and has examined 399 patent applications in our dataset. With an allowance rate of 91.0%, this examiner allows applications at a higher rate than most examiners at the USPTO. Applications typically reach final disposition in approximately 29 months.
Examiner XAVIER, VALENTINA's allowance rate of 91.0% places them in the 75% percentile among all USPTO examiners. This examiner is more likely to allow applications than most examiners at the USPTO.
On average, applications examined by XAVIER, VALENTINA receive 0.99 office actions before reaching final disposition. This places the examiner in the 8% 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 XAVIER, VALENTINA is 29 months. This places the examiner in the 66% percentile for prosecution speed. Prosecution timelines are slightly faster than average with this examiner.
Conducting an examiner interview provides a +3.7% benefit to allowance rate for applications examined by XAVIER, VALENTINA. This interview benefit is in the 26% percentile among all examiners. Recommendation: Interviews provide a below-average benefit with this examiner.
When applicants file an RCE with this examiner, 32.3% of applications are subsequently allowed. This success rate is in the 68% 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 48.3% of cases where such amendments are filed. This entry rate is in the 73% 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, 75.0% result in withdrawal of the rejection or reopening of prosecution. This success rate is in the 61% 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 88.9% of appeals filed. This is in the 82% percentile among all examiners. Of these withdrawals, 50.0% occur early in the appeal process (after Notice of Appeal but before Appeal Brief). Strategic Insight: This examiner frequently reconsiders rejections during the appeal process compared to other examiners. Per MPEP § 1207.01, all appeals must go through a mandatory appeal conference. Filing a Notice of Appeal may prompt favorable reconsideration even before you file an Appeal Brief.
When applicants file petitions regarding this examiner's actions, 42.1% are granted (fully or in part). This grant rate is in the 34% 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 0.3% of allowed cases (in the 54% percentile). This examiner makes examiner's amendments more often than average to place applications in condition for allowance (MPEP § 1302.04).
Quayle Actions: This examiner issues Ex Parte Quayle actions in 0.0% of allowed cases (in the 38% 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.