USPTO Examiner BONNETTE RODNEY ANDREW - Art Unit 3647

Recent Applications

Detailed information about the 100 most recent patent applications.

Application NumberTitleFiling DateDisposal DateDispositionTime (months)Office ActionsRestrictionsInterviewAppeal
19091000POWER SUPPLY SYSTEM, MOVING OBJECT, AND CONTROL METHOD OF POWER SUPPLY SYSTEMMarch 2025February 2026Allow1000NoNo
19079138ADDITIVE MANUFACTURED INTEGRAL FASTENING SYSTEM FOR MISSION ADAPTABLE UNMANNED AERIAL VEHICLESMarch 2025August 2025Allow510NoNo
19072348JOINT ASSEMBLY IN AN AIRCRAFT STRUCTUREMarch 2025January 2026Allow1110NoNo
19070709AIRCRAFT CONTROL SYSTEM AND METHODMarch 2025November 2025Allow810NoNo
19071178WING FOR AN AIRCRAFTMarch 2025January 2026Allow1010NoNo
19064551ELECTRIC AIRCRAFTFebruary 2025March 2026Allow1210NoNo
19062885AUTOMATED DETERMINATION OF COST OWNERSHIP OF SPACE DEBRISFebruary 2025March 2026Allow1320NoNo
19061304AIRCRAFT AIR INLET COMPRISING AT LEAST A MAIN DE-ICING SYSTEM AND AT LEAST ONE SECONDARY DE-ICING SYSTEM POSITIONED AT A SPLICE PLATEFebruary 2025December 2025Allow1010NoNo
19057341MECHANICAL ARCHITECTURE FOR DISTRIBUTED FLAP ACTUATION SYSTEMFebruary 2025December 2025Allow1010NoNo
19042938Actuation assembly for a trailing edge flap of an aircraft wingJanuary 2025March 2026Allow1410NoNo
19040768ELECTRIC TILTROTOR AIRCRAFTJanuary 2025November 2025Allow1010NoNo
19037907WING ASSEMBLIES AND AIRCRAFT WITH GAP-ADJUSTMENT ASSEMBLIES FOR SLATSJanuary 2025August 2025Allow600NoNo
19032968SHEAR PIN LATCH RECEPTACLE ASSEMBLY FOR AIRCRAFT DOORSJanuary 2025August 2025Allow600NoNo
19016563AIRCRAFT HYBRID MOTIVE POWER SOURCE SYSTEM AND METHOD FOR CONTROLLING SAMEJanuary 2025November 2025Allow1010NoNo
18987937AIRCRAFT WING WITH A WING TIP DEVICEDecember 2024November 2025Allow1010NoNo
18983819REDUCING EDDY CURRENT PROPAGATION IN ELECTRIC DEVICE HOUSINGDecember 2024October 2025Allow1010NoNo
18975286INDEPENDENTLY MODULATED FUEL CELL COMPRESSORSDecember 2024March 2026Abandon1520NoNo
18974246Aircraft Inceptor Trim ApparatusDecember 2024November 2025Allow1110NoNo
18969781AIRCRAFT WITH ELECTRICALLY POWERED ENGINE ACCESSORIESDecember 2024November 2025Allow1110NoNo
18967908DRIVE SYSTEM FOR A LIFT CONTROL DEVICE OF AN AIRCRAFT, AIRCRAFT WING AND AIRCRAFTDecember 2024October 2025Allow1010NoNo
18962386RIB MOUNTING FLANGES FOR AN UNMANNED AERIAL VEHICLENovember 2024September 2025Allow1010NoNo
18962243VTOL Aircraft for Network SystemNovember 2024December 2025Allow1310NoNo
18862468ELECTRIC AIRCRAFTNovember 2024February 2026Abandon1610NoNo
18924577DEVICE AND METHOD FOR GENERATING FLUTTER ON AT LEAST A PART OF AN AIRCRAFTOctober 2024June 2025Allow800NoNo
18918235ELECTRIC PROPULSION SYSTEM FOR A FLIGHT VEHICLEOctober 2024July 2025Allow800NoNo
18913529Hydrofoil Equipped Seaglider TakeoffOctober 2024November 2025Allow1310YesNo
18909392Vertical Take-Off and Landing Aircraft and Methods of Taking-Off, Landing, High Speed Flight, and Aircraft ControlOctober 2024October 2025Allow1210NoNo
18906638FLIGHT VEHICLE AND MAAS PROVISION METHODOctober 2024July 2025Allow910NoNo
18892105DRAG REDUCTION FIN DEPLOYMENT MECHANISMSeptember 2024October 2025Allow1310NoNo
18889012COMPUTER-IMPLEMENTED METHOD FOR REDUCING TIRE WEAR ON AN AIRCRAFTSeptember 2024November 2025Allow1410NoNo
18830730SIDESTICK CONTROL APPARATUSSeptember 2024September 2025Allow1210NoNo
18824571Hybrid Propulsion For Airborne CraftSeptember 2024June 2025Allow900NoNo
18822911Aircraft Control SystemSeptember 2024July 2025Allow1010NoNo
18820617METHOD OF REDUCING AERODYNAMIC LOADS ON AN AIRCRAFT LOCATED ON THE GROUNDAugust 2024January 2026Allow1620NoNo
18816476MONITORING SYSTEM FOR MONITORING A HYBRID POWER PLANT OF A ROTORCRAFT, ASSOCIATED ROTORCRAFT AND METHODAugust 2024October 2025Allow1310NoNo
18814297SYSTEMS AND METHODS FOR OIL MAINTENANCE AND DISTRIBUTION IN ELECTRIC ENGINES FOR EVTOL AIRCRAFTAugust 2024February 2026Allow1800YesNo
18802403SYSTEM AND METHOD FOR AUTOMATED FLIGHT CORRECTION IN AN ELECTRIC AIRCRAFTAugust 2024December 2025Abandon1610NoNo
18764970WING FOR AN AIRCRAFTJuly 2024August 2025Allow1410NoNo
18760211Multi-engine assembly and installation method for electric aircraft propulsionJuly 2024December 2025Allow1710NoNo
18759054CONTROL ASSEMBLY FOR AIRCRAFT PROPULSION SYSTEMSJune 2024July 2025Allow1300NoNo
18745279COUNTERBALANCED RETRACT ACTUATOR FOR LANDING GEARJune 2024August 2025Allow1410YesNo
18712172ELECTRIC FAN AND ELECTRIC AIRCRAFTMay 2024April 2025Allow1100NoNo
18660437AIRCRAFT CONTROL SYSTEMS AND METHODS USING SLIDING MODE CONTROL AND FEEDBACK LINEARIZATIONMay 2024April 2025Allow1100NoNo
18647813TAILORED STRUCTURAL ACTUATION SYSTEMApril 2024April 2025Allow1100NoNo
18646091SEALApril 2024July 2025Allow1510NoNo
18642497REMOTE ACTUATION SYSTEMS AND RELATED SIX-PHASE MOTOR CONTROL METHODSApril 2024July 2025Allow1510NoNo
18701755Hybrid flying deviceApril 2024July 2025Allow1510NoNo
18629363SEAT ASSEMBLY, CLIP, AND METHOD OF MANUFACTUREApril 2024February 2026Allow2310NoNo
18623590ELECTRIC SLIDE RAIL SYSTEMS AND METHODSApril 2024February 2026Allow2310NoNo
18622924EASY-TO-TRANSPORT CHAIRMarch 2024March 2026Allow2420NoNo
18697237ELEMENT FOR COVERING A SEAT SUPPORT ELEMENTMarch 2024February 2026Allow2310NoNo
18612462FLY-BY-WIRE SYSTEM WITH FCC-INTEGRATED SERVO ACTUATORSMarch 2024September 2025Allow1810NoNo
18607424Three-Dimensional Extension Linkage For AircraftMarch 2024March 2025Allow1200NoNo
18602607COMPONENT FOR AIRCRAFT INTERIORSMarch 2024February 2026Allow2310NoNo
18594762PROPULSION SYSTEM WITH CONCENTRIC ROCKET MOTOR AND ELECTRIC MOTORMarch 2024July 2025Allow1600NoNo
18584306VEHICLE SEAT LONGITUDINAL ADJUSTMENT ASSEMBLYFebruary 2024October 2025Allow2000NoNo
18439070HYBRID AIRCRAFT POWER PLANTFebruary 2024May 2025Allow1510NoNo
18429869COMPOSITE BEAM FOR AIRCRAFT SEAT FRAMEFebruary 2024February 2026Allow2410NoNo
18294537SYSTEMS AND METHODS FOR AIRCRAFT TAIL STRIKE PREVENTIONFebruary 2024January 2026Abandon2410NoNo
18427292Method and System for Controlling an Aircraft Propulsion System in an Aircraft Susceptible to Ground ResonanceJanuary 2024March 2025Allow1300NoNo
18425093FLAP SYSTEM FOR AN AIRCRAFT AND METHOD OF OPERATING A FLAP FAIRING AT AN AIRCRAFT WINGJanuary 2024March 2025Allow1300NoNo
18422546FURNITURE ITEM WITH CIRCUIT BOARD ASSEMBLYJanuary 2024March 2026Allow2610NoNo
18422657Motor Vehicle Seat Mounting SystemJanuary 2024October 2025Allow2110NoNo
18417424AIRCRAFT COMPONENT WITH STRUCTURAL FOAMJanuary 2024August 2024Allow711NoNo
18406989WING FOR AN AIRCRAFTJanuary 2024March 2025Allow1410NoNo
18396967AIRCRAFT FLAP SYSTEMDecember 2023March 2025Allow1510NoNo
18543103FAIRING ARRANGEMENT FOR A HIGH-LIFT MECHANISM OF AN AIRCRAFTDecember 2023February 2025Allow1400NoNo
18570500AIRCRAFT LANDING GEAR PROVIDED WITH A SHAPE SENSORDecember 2023June 2025Allow1810NoNo
18538235TRIMMABLE HORIZONTAL STABILISATION ACTUATORDecember 2023August 2025Allow2020NoNo
18535981AEROSPACE VEHICLESDecember 2023December 2025Allow2410NoNo
18535363METHOD 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 METHODDecember 2023May 2025Allow1710YesNo
18568384SERIES OF CONVERTIBLE AIRCRAFT CAPABLE OF HOVERING AND METHOD FOR CONFIGURING A CONVERTIBLE AIRCRAFT CAPABLE OF HOVERINGDecember 2023May 2025Allow1710NoNo
18520239FLOOR SYSTEM FOR A CABIN OF A VEHICLENovember 2023December 2024Allow1200NoNo
18560880LOW GRAVITY POWER DISTRIBUTION SYSTEM AND DEVICENovember 2023May 2025Allow1800NoNo
18389081SYSTEM AND METHOD FOR FLIGHT CONTROL OF AN ELECTRIC VERTICAL TAKEOFF AND LANDING AIRCRAFTNovember 2023February 2025Allow1510NoNo
18493939METHOD FOR AUTONOMOUS SERVICING OF AN AIRCRAFT, AND A SERVICE PANEL, AIRCRAFT AND SYSTEM PROVIDING FOR AUTONOMOUS SERVICING OF AN AIRCRAFTOctober 2023March 2025Allow1610NoNo
18493186PROPULSION SYSTEM ARCHITECTUREOctober 2023August 2025Allow2210YesNo
18380237LANDING GEAR WITH RETRACTABLE ROCKER ARM PROVIDED WITH AN ELECTRIC MOTOR AND AIRCRAFT PROVIDED WITH AT LEAST ONE SUCH LANDING GEAROctober 2023October 2024Allow1200NoNo
18486669TONER CARTRIDGEOctober 2023May 2025Allow1910NoNo
18484394SYSTEMS AND METHODS FOR AERODYNAMIC DEPLOYMENT OF WING STRUCTURESOctober 2023March 2025Allow1710YesNo
18482451Serrated FittingOctober 2023January 2025Allow1611YesNo
18376802EXPLORATION VEHICLE STOWAGE AND DEPLOYMENT SYSTEMSOctober 2023March 2025Allow1810NoNo
18479879Multi-Payload Drone Delivery System and MethodOctober 2023March 2025Allow1710NoNo
18475084FLIGHT CONTROL SURFACESeptember 2023February 2025Allow1710YesNo
18371185AUTOMATED DETERMINATION OF COST OWNERSHIP OF SPACE DEBRISSeptember 2023February 2025Allow1610YesNo
18470763RECOVERING FUEL VAPOUR FROM AIRCRAFT FUEL TANKSeptember 2023February 2025Allow1710YesNo
18460173TEMPERATURE COMPENSATED LANDING GEAR SHOCK STRUTSeptember 2023January 2025Allow1610NoNo
18238603RIB MOUNTING FLANGES FOR AN UNMANNED AERIAL VEHICLEAugust 2023August 2024Allow1210NoNo
18239039Aircraft with Wingtip Positioned PropellersAugust 2023January 2025Allow1710NoNo
18234480VEHICLE, SYSTEM, AND METHOD FOR VERTICAL TAKE-OFF AND LANDINGAugust 2023September 2024Allow1310NoNo
18228371CONTAINMENT ZONE FOR AN ELECTRIC MACHINE IN A HYBRID POWERPLANT FOR AN AIRCRAFTJuly 2023January 2025Allow1710NoNo
18274809Electrical Power Transmission for Propeller DeicingJuly 2023September 2024Allow1400NoNo
18227756AIRCRAFT WITH MODULAR COMPONENTSJuly 2023January 2025Allow1710NoNo
18227685THERMOPLASTIC COMPOSITE STRUCTURE AND METHODS FOR FORMINGJuly 2023March 2025Allow1920NoNo
18226364BREAKOVER VEHICLE OPERATOR SEAT CONVERTIBLE TO NON-BREAKOVER CONFIGURATIONJuly 2023December 2024Allow1610NoNo
18226526RAM FILTER PURGE SYSTEMJuly 2023September 2024Allow1300NoNo
18226325AIRCRAFT SEAT WITH DOUBLE SHEAR TRACK FITTING ASSEMBLYJuly 2023December 2024Allow1610NoNo
18224985BASE STATION FOR DRONE BATTERY SWAPJuly 2023December 2024Allow1710NoNo
18262269AIRCRAFT HAVING RETRACTABLE VORTEX GENERATORSJuly 2023January 2025Allow1810NoNo
18355779PROPELLER PROPULSION UNIT FOR AN AIRCRAFTJuly 2023October 2024Allow1400NoNo

Appeals Overview

This analysis examines appeal outcomes and the strategic value of filing appeals for examiner BONNETTE, RODNEY ANDREW.

Strategic Value of Filing an Appeal

Total Appeal Filings
2
Allowed After Appeal Filing
0
(0.0%)
Not Allowed After Appeal Filing
2
(100.0%)
Filing Benefit Percentile
8.9%
Lower than average

Understanding Appeal Filing Strategy

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.

Strategic Recommendations

Filing a Notice of Appeal shows limited benefit. Consider other strategies like interviews or amendments before appealing.

Examiner BONNETTE, RODNEY ANDREW - Prosecution Strategy Guide

Executive Summary

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.

Allowance Patterns

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.

Office Action Patterns

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.

Prosecution Timeline

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.

Interview Effectiveness

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.

Request for Continued Examination (RCE) Effectiveness

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.

After-Final Amendment Practice

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.

Pre-Appeal Conference Effectiveness

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.

Appeal Withdrawal and Reconsideration

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.

Petition Practice

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 Cooperation and Flexibility

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.

Prosecution Strategy Recommendations

Based on the statistical analysis of this examiner's prosecution patterns, here are tailored strategic recommendations:

  • Consider after-final amendments: This examiner frequently enters after-final amendments. If you can clearly overcome rejections with claim amendments, file an after-final amendment before resorting to an RCE.
  • RCEs are effective: This examiner has a high allowance rate after RCE compared to others. If you receive a final rejection and have substantive amendments or arguments, an RCE is likely to be successful.
  • Appeal filing as negotiation tool: This examiner frequently reconsiders rejections during the appeal process. Filing a Notice of Appeal may prompt favorable reconsideration during the mandatory appeal conference.

Relevant MPEP Sections for Prosecution Strategy

  • MPEP § 713.10: Examiner interviews - available before Notice of Allowance or transfer to PTAB
  • MPEP § 714.12: After-final amendments - may be entered "under justifiable circumstances"
  • MPEP § 1002.02(c): Petitionable matters to Technology Center Director
  • MPEP § 1004: Actions requiring primary examiner signature (allowances, final rejections, examiner's answers)
  • MPEP § 1207.01: Appeal conferences - mandatory for all appeals
  • MPEP § 1214.07: Reopening prosecution after appeal

Important Disclaimer

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.