Detailed information about the 100 most recent patent applications.
| Application Number | Title | Filing Date | Disposal Date | Disposition | Time (months) | Office Actions | Restrictions | Interview | Appeal |
|---|---|---|---|---|---|---|---|---|---|
| 19091000 | POWER SUPPLY SYSTEM, MOVING OBJECT, AND CONTROL METHOD OF POWER SUPPLY SYSTEM | March 2025 | February 2026 | Allow | 10 | 0 | 0 | No | No |
| 19079138 | ADDITIVE MANUFACTURED INTEGRAL FASTENING SYSTEM FOR MISSION ADAPTABLE UNMANNED AERIAL VEHICLES | March 2025 | August 2025 | Allow | 5 | 1 | 0 | No | No |
| 19072348 | JOINT ASSEMBLY IN AN AIRCRAFT STRUCTURE | March 2025 | January 2026 | Allow | 11 | 1 | 0 | No | No |
| 19070709 | AIRCRAFT CONTROL SYSTEM AND METHOD | March 2025 | November 2025 | Allow | 8 | 1 | 0 | No | No |
| 19071178 | WING FOR AN AIRCRAFT | March 2025 | January 2026 | Allow | 10 | 1 | 0 | No | No |
| 19064551 | ELECTRIC AIRCRAFT | February 2025 | March 2026 | Allow | 12 | 1 | 0 | No | No |
| 19062885 | AUTOMATED DETERMINATION OF COST OWNERSHIP OF SPACE DEBRIS | February 2025 | March 2026 | Allow | 13 | 2 | 0 | No | No |
| 19061304 | AIRCRAFT AIR INLET COMPRISING AT LEAST A MAIN DE-ICING SYSTEM AND AT LEAST ONE SECONDARY DE-ICING SYSTEM POSITIONED AT A SPLICE PLATE | February 2025 | December 2025 | Allow | 10 | 1 | 0 | No | No |
| 19057341 | MECHANICAL ARCHITECTURE FOR DISTRIBUTED FLAP ACTUATION SYSTEM | February 2025 | December 2025 | Allow | 10 | 1 | 0 | No | No |
| 19042938 | Actuation assembly for a trailing edge flap of an aircraft wing | January 2025 | March 2026 | Allow | 14 | 1 | 0 | No | No |
| 19040768 | ELECTRIC TILTROTOR AIRCRAFT | January 2025 | November 2025 | Allow | 10 | 1 | 0 | No | No |
| 19037907 | WING ASSEMBLIES AND AIRCRAFT WITH GAP-ADJUSTMENT ASSEMBLIES FOR SLATS | January 2025 | August 2025 | Allow | 6 | 0 | 0 | No | No |
| 19032968 | SHEAR PIN LATCH RECEPTACLE ASSEMBLY FOR AIRCRAFT DOORS | January 2025 | August 2025 | Allow | 6 | 0 | 0 | No | No |
| 19016563 | AIRCRAFT HYBRID MOTIVE POWER SOURCE SYSTEM AND METHOD FOR CONTROLLING SAME | January 2025 | November 2025 | Allow | 10 | 1 | 0 | No | No |
| 18987937 | AIRCRAFT WING WITH A WING TIP DEVICE | December 2024 | November 2025 | Allow | 10 | 1 | 0 | No | No |
| 18983819 | REDUCING EDDY CURRENT PROPAGATION IN ELECTRIC DEVICE HOUSING | December 2024 | October 2025 | Allow | 10 | 1 | 0 | No | No |
| 18975286 | INDEPENDENTLY MODULATED FUEL CELL COMPRESSORS | December 2024 | March 2026 | Abandon | 15 | 2 | 0 | No | No |
| 18974246 | Aircraft Inceptor Trim Apparatus | December 2024 | November 2025 | Allow | 11 | 1 | 0 | No | No |
| 18969781 | AIRCRAFT WITH ELECTRICALLY POWERED ENGINE ACCESSORIES | December 2024 | November 2025 | Allow | 11 | 1 | 0 | No | No |
| 18967908 | DRIVE SYSTEM FOR A LIFT CONTROL DEVICE OF AN AIRCRAFT, AIRCRAFT WING AND AIRCRAFT | December 2024 | October 2025 | Allow | 10 | 1 | 0 | No | No |
| 18962386 | RIB MOUNTING FLANGES FOR AN UNMANNED AERIAL VEHICLE | November 2024 | September 2025 | Allow | 10 | 1 | 0 | No | No |
| 18962243 | VTOL Aircraft for Network System | November 2024 | December 2025 | Allow | 13 | 1 | 0 | No | No |
| 18862468 | ELECTRIC AIRCRAFT | November 2024 | February 2026 | Abandon | 16 | 1 | 0 | No | No |
| 18924577 | DEVICE AND METHOD FOR GENERATING FLUTTER ON AT LEAST A PART OF AN AIRCRAFT | October 2024 | June 2025 | Allow | 8 | 0 | 0 | No | No |
| 18918235 | ELECTRIC PROPULSION SYSTEM FOR A FLIGHT VEHICLE | October 2024 | July 2025 | Allow | 8 | 0 | 0 | No | No |
| 18913529 | Hydrofoil Equipped Seaglider Takeoff | October 2024 | November 2025 | Allow | 13 | 1 | 0 | Yes | No |
| 18909392 | Vertical Take-Off and Landing Aircraft and Methods of Taking-Off, Landing, High Speed Flight, and Aircraft Control | October 2024 | October 2025 | Allow | 12 | 1 | 0 | No | No |
| 18906638 | FLIGHT VEHICLE AND MAAS PROVISION METHOD | October 2024 | July 2025 | Allow | 9 | 1 | 0 | No | No |
| 18892105 | DRAG REDUCTION FIN DEPLOYMENT MECHANISM | September 2024 | October 2025 | Allow | 13 | 1 | 0 | No | No |
| 18889012 | COMPUTER-IMPLEMENTED METHOD FOR REDUCING TIRE WEAR ON AN AIRCRAFT | September 2024 | November 2025 | Allow | 14 | 1 | 0 | No | No |
| 18830730 | SIDESTICK CONTROL APPARATUS | September 2024 | September 2025 | Allow | 12 | 1 | 0 | No | No |
| 18824571 | Hybrid Propulsion For Airborne Craft | September 2024 | June 2025 | Allow | 9 | 0 | 0 | No | No |
| 18822911 | Aircraft Control System | September 2024 | July 2025 | Allow | 10 | 1 | 0 | No | No |
| 18820617 | METHOD OF REDUCING AERODYNAMIC LOADS ON AN AIRCRAFT LOCATED ON THE GROUND | August 2024 | January 2026 | Allow | 16 | 2 | 0 | No | No |
| 18816476 | MONITORING SYSTEM FOR MONITORING A HYBRID POWER PLANT OF A ROTORCRAFT, ASSOCIATED ROTORCRAFT AND METHOD | August 2024 | October 2025 | Allow | 13 | 1 | 0 | No | No |
| 18814297 | SYSTEMS AND METHODS FOR OIL MAINTENANCE AND DISTRIBUTION IN ELECTRIC ENGINES FOR EVTOL AIRCRAFT | August 2024 | February 2026 | Allow | 18 | 0 | 0 | Yes | No |
| 18802403 | SYSTEM AND METHOD FOR AUTOMATED FLIGHT CORRECTION IN AN ELECTRIC AIRCRAFT | August 2024 | December 2025 | Abandon | 16 | 1 | 0 | No | No |
| 18764970 | WING FOR AN AIRCRAFT | July 2024 | August 2025 | Allow | 14 | 1 | 0 | No | No |
| 18760211 | Multi-engine assembly and installation method for electric aircraft propulsion | July 2024 | December 2025 | Allow | 17 | 1 | 0 | No | No |
| 18759054 | CONTROL ASSEMBLY FOR AIRCRAFT PROPULSION SYSTEMS | June 2024 | July 2025 | Allow | 13 | 0 | 0 | No | No |
| 18745279 | COUNTERBALANCED RETRACT ACTUATOR FOR LANDING GEAR | June 2024 | August 2025 | Allow | 14 | 1 | 0 | Yes | No |
| 18712172 | ELECTRIC FAN AND ELECTRIC AIRCRAFT | May 2024 | April 2025 | Allow | 11 | 0 | 0 | No | No |
| 18660437 | AIRCRAFT CONTROL SYSTEMS AND METHODS USING SLIDING MODE CONTROL AND FEEDBACK LINEARIZATION | May 2024 | April 2025 | Allow | 11 | 0 | 0 | No | No |
| 18647813 | TAILORED STRUCTURAL ACTUATION SYSTEM | April 2024 | April 2025 | Allow | 11 | 0 | 0 | No | No |
| 18646091 | SEAL | April 2024 | July 2025 | Allow | 15 | 1 | 0 | No | No |
| 18642497 | REMOTE ACTUATION SYSTEMS AND RELATED SIX-PHASE MOTOR CONTROL METHODS | April 2024 | July 2025 | Allow | 15 | 1 | 0 | No | No |
| 18701755 | Hybrid flying device | April 2024 | July 2025 | Allow | 15 | 1 | 0 | No | No |
| 18629363 | SEAT ASSEMBLY, CLIP, AND METHOD OF MANUFACTURE | April 2024 | February 2026 | Allow | 23 | 1 | 0 | No | No |
| 18623590 | ELECTRIC SLIDE RAIL SYSTEMS AND METHODS | April 2024 | February 2026 | Allow | 23 | 1 | 0 | No | No |
| 18622924 | EASY-TO-TRANSPORT CHAIR | March 2024 | March 2026 | Allow | 24 | 2 | 0 | No | No |
| 18697237 | ELEMENT FOR COVERING A SEAT SUPPORT ELEMENT | March 2024 | February 2026 | Allow | 23 | 1 | 0 | No | No |
| 18612462 | FLY-BY-WIRE SYSTEM WITH FCC-INTEGRATED SERVO ACTUATORS | March 2024 | September 2025 | Allow | 18 | 1 | 0 | No | No |
| 18607424 | Three-Dimensional Extension Linkage For Aircraft | March 2024 | March 2025 | Allow | 12 | 0 | 0 | No | No |
| 18602607 | COMPONENT FOR AIRCRAFT INTERIORS | March 2024 | February 2026 | Allow | 23 | 1 | 0 | No | No |
| 18594762 | PROPULSION SYSTEM WITH CONCENTRIC ROCKET MOTOR AND ELECTRIC MOTOR | March 2024 | July 2025 | Allow | 16 | 0 | 0 | No | No |
| 18584306 | VEHICLE SEAT LONGITUDINAL ADJUSTMENT ASSEMBLY | February 2024 | October 2025 | Allow | 20 | 0 | 0 | No | No |
| 18439070 | HYBRID AIRCRAFT POWER PLANT | February 2024 | May 2025 | Allow | 15 | 1 | 0 | No | No |
| 18429869 | COMPOSITE BEAM FOR AIRCRAFT SEAT FRAME | February 2024 | February 2026 | Allow | 24 | 1 | 0 | No | No |
| 18294537 | SYSTEMS AND METHODS FOR AIRCRAFT TAIL STRIKE PREVENTION | February 2024 | January 2026 | Abandon | 24 | 1 | 0 | No | No |
| 18427292 | Method and System for Controlling an Aircraft Propulsion System in an Aircraft Susceptible to Ground Resonance | January 2024 | March 2025 | Allow | 13 | 0 | 0 | No | No |
| 18425093 | FLAP SYSTEM FOR AN AIRCRAFT AND METHOD OF OPERATING A FLAP FAIRING AT AN AIRCRAFT WING | January 2024 | March 2025 | Allow | 13 | 0 | 0 | No | No |
| 18422546 | FURNITURE ITEM WITH CIRCUIT BOARD ASSEMBLY | January 2024 | March 2026 | Allow | 26 | 1 | 0 | No | No |
| 18422657 | Motor Vehicle Seat Mounting System | January 2024 | October 2025 | Allow | 21 | 1 | 0 | No | No |
| 18417424 | AIRCRAFT COMPONENT WITH STRUCTURAL FOAM | January 2024 | August 2024 | Allow | 7 | 1 | 1 | No | No |
| 18406989 | WING FOR AN AIRCRAFT | January 2024 | March 2025 | Allow | 14 | 1 | 0 | No | No |
| 18396967 | AIRCRAFT FLAP SYSTEM | December 2023 | March 2025 | Allow | 15 | 1 | 0 | No | No |
| 18543103 | FAIRING ARRANGEMENT FOR A HIGH-LIFT MECHANISM OF AN AIRCRAFT | December 2023 | February 2025 | Allow | 14 | 0 | 0 | No | No |
| 18570500 | AIRCRAFT LANDING GEAR PROVIDED WITH A SHAPE SENSOR | December 2023 | June 2025 | Allow | 18 | 1 | 0 | No | No |
| 18538235 | TRIMMABLE HORIZONTAL STABILISATION ACTUATOR | December 2023 | August 2025 | Allow | 20 | 2 | 0 | No | No |
| 18535981 | AEROSPACE VEHICLES | December 2023 | December 2025 | Allow | 24 | 1 | 0 | No | No |
| 18535363 | METHOD FOR MANAGING THE CONFIGURATION OF AN AIRCRAFT ALTERNATELY COMPRISING TAIL CONES INCORPORATING OR NOT AT LEAST ONE AUXILIARY POWER UNIT OR NOT, AIRCRAFT AND DEVICE MAKING IT POSSIBLE TO IMPLEMENT SAID METHOD | December 2023 | May 2025 | Allow | 17 | 1 | 0 | Yes | No |
| 18568384 | SERIES OF CONVERTIBLE AIRCRAFT CAPABLE OF HOVERING AND METHOD FOR CONFIGURING A CONVERTIBLE AIRCRAFT CAPABLE OF HOVERING | December 2023 | May 2025 | Allow | 17 | 1 | 0 | No | No |
| 18520239 | FLOOR SYSTEM FOR A CABIN OF A VEHICLE | November 2023 | December 2024 | Allow | 12 | 0 | 0 | No | No |
| 18560880 | LOW GRAVITY POWER DISTRIBUTION SYSTEM AND DEVICE | November 2023 | May 2025 | Allow | 18 | 0 | 0 | No | No |
| 18389081 | SYSTEM AND METHOD FOR FLIGHT CONTROL OF AN ELECTRIC VERTICAL TAKEOFF AND LANDING AIRCRAFT | November 2023 | February 2025 | Allow | 15 | 1 | 0 | No | No |
| 18493939 | METHOD FOR AUTONOMOUS SERVICING OF AN AIRCRAFT, AND A SERVICE PANEL, AIRCRAFT AND SYSTEM PROVIDING FOR AUTONOMOUS SERVICING OF AN AIRCRAFT | October 2023 | March 2025 | Allow | 16 | 1 | 0 | No | No |
| 18493186 | PROPULSION SYSTEM ARCHITECTURE | October 2023 | August 2025 | Allow | 22 | 1 | 0 | Yes | No |
| 18380237 | LANDING GEAR WITH RETRACTABLE ROCKER ARM PROVIDED WITH AN ELECTRIC MOTOR AND AIRCRAFT PROVIDED WITH AT LEAST ONE SUCH LANDING GEAR | October 2023 | October 2024 | Allow | 12 | 0 | 0 | No | No |
| 18486669 | TONER CARTRIDGE | October 2023 | May 2025 | Allow | 19 | 1 | 0 | No | No |
| 18484394 | SYSTEMS AND METHODS FOR AERODYNAMIC DEPLOYMENT OF WING STRUCTURES | October 2023 | March 2025 | Allow | 17 | 1 | 0 | Yes | No |
| 18482451 | Serrated Fitting | October 2023 | January 2025 | Allow | 16 | 1 | 1 | Yes | No |
| 18376802 | EXPLORATION VEHICLE STOWAGE AND DEPLOYMENT SYSTEMS | October 2023 | March 2025 | Allow | 18 | 1 | 0 | No | No |
| 18479879 | Multi-Payload Drone Delivery System and Method | October 2023 | March 2025 | Allow | 17 | 1 | 0 | No | No |
| 18475084 | FLIGHT CONTROL SURFACE | September 2023 | February 2025 | Allow | 17 | 1 | 0 | Yes | No |
| 18371185 | AUTOMATED DETERMINATION OF COST OWNERSHIP OF SPACE DEBRIS | September 2023 | February 2025 | Allow | 16 | 1 | 0 | Yes | No |
| 18470763 | RECOVERING FUEL VAPOUR FROM AIRCRAFT FUEL TANK | September 2023 | February 2025 | Allow | 17 | 1 | 0 | Yes | No |
| 18460173 | TEMPERATURE COMPENSATED LANDING GEAR SHOCK STRUT | September 2023 | January 2025 | Allow | 16 | 1 | 0 | No | No |
| 18238603 | RIB MOUNTING FLANGES FOR AN UNMANNED AERIAL VEHICLE | August 2023 | August 2024 | Allow | 12 | 1 | 0 | No | No |
| 18239039 | Aircraft with Wingtip Positioned Propellers | August 2023 | January 2025 | Allow | 17 | 1 | 0 | No | No |
| 18234480 | VEHICLE, SYSTEM, AND METHOD FOR VERTICAL TAKE-OFF AND LANDING | August 2023 | September 2024 | Allow | 13 | 1 | 0 | No | No |
| 18228371 | CONTAINMENT ZONE FOR AN ELECTRIC MACHINE IN A HYBRID POWERPLANT FOR AN AIRCRAFT | July 2023 | January 2025 | Allow | 17 | 1 | 0 | No | No |
| 18274809 | Electrical Power Transmission for Propeller Deicing | July 2023 | September 2024 | Allow | 14 | 0 | 0 | No | No |
| 18227756 | AIRCRAFT WITH MODULAR COMPONENTS | July 2023 | January 2025 | Allow | 17 | 1 | 0 | No | No |
| 18227685 | THERMOPLASTIC COMPOSITE STRUCTURE AND METHODS FOR FORMING | July 2023 | March 2025 | Allow | 19 | 2 | 0 | No | No |
| 18226364 | BREAKOVER VEHICLE OPERATOR SEAT CONVERTIBLE TO NON-BREAKOVER CONFIGURATION | July 2023 | December 2024 | Allow | 16 | 1 | 0 | No | No |
| 18226526 | RAM FILTER PURGE SYSTEM | July 2023 | September 2024 | Allow | 13 | 0 | 0 | No | No |
| 18226325 | AIRCRAFT SEAT WITH DOUBLE SHEAR TRACK FITTING ASSEMBLY | July 2023 | December 2024 | Allow | 16 | 1 | 0 | No | No |
| 18224985 | BASE STATION FOR DRONE BATTERY SWAP | July 2023 | December 2024 | Allow | 17 | 1 | 0 | No | No |
| 18262269 | AIRCRAFT HAVING RETRACTABLE VORTEX GENERATORS | July 2023 | January 2025 | Allow | 18 | 1 | 0 | No | No |
| 18355779 | PROPELLER PROPULSION UNIT FOR AN AIRCRAFT | July 2023 | October 2024 | Allow | 14 | 0 | 0 | No | No |
This analysis examines appeal outcomes and the strategic value of filing appeals for examiner BONNETTE, RODNEY ANDREW.
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, 0.0% of applications that filed an appeal were subsequently allowed. This appeal filing benefit rate is in the bottom 25% across the USPTO, indicating that filing appeals is less effective here than in most other areas.
⚠ Filing a Notice of Appeal shows limited benefit. Consider other strategies like interviews or amendments before appealing.
Examiner BONNETTE, RODNEY ANDREW works in Art Unit 3647 and has examined 434 patent applications in our dataset. With an allowance rate of 94.0%, this examiner allows applications at a higher rate than most examiners at the USPTO. Applications typically reach final disposition in approximately 26 months.
Examiner BONNETTE, RODNEY ANDREW's allowance rate of 94.0% places them in the 82% percentile among all USPTO examiners. This examiner is more likely to allow applications than most examiners at the USPTO.
On average, applications examined by BONNETTE, RODNEY ANDREW receive 1.01 office actions before reaching final disposition. This places the examiner in the 10% 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 BONNETTE, RODNEY ANDREW is 26 months. This places the examiner in the 77% percentile for prosecution speed. Applications move through prosecution relatively quickly with this examiner.
Conducting an examiner interview provides a +4.0% benefit to allowance rate for applications examined by BONNETTE, RODNEY ANDREW. This interview benefit is in the 27% percentile among all examiners. Recommendation: Interviews provide a below-average benefit with this examiner.
When applicants file an RCE with this examiner, 42.5% of applications are subsequently allowed. This success rate is in the 94% 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 64.9% of cases where such amendments are filed. This entry rate is in the 89% percentile among all examiners. Strategic Recommendation: This examiner is highly receptive to after-final amendments compared to other examiners. Per MPEP § 714.12, after-final amendments may be entered "under justifiable circumstances." Consider filing after-final amendments with a clear showing of allowability rather than immediately filing an RCE, as this examiner frequently enters such amendments.
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 18% 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 100.0% of appeals filed. This is in the 97% 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, 37.5% are granted (fully or in part). This grant rate is in the 26% 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 0.9% of allowed cases (in the 66% 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 7.4% of allowed cases (in the 85% percentile). Per MPEP § 714.14, a Quayle action indicates that all claims are allowable but formal matters remain. This examiner frequently uses Quayle actions compared to other examiners, which is a positive indicator that once substantive issues are resolved, allowance follows quickly.
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.