USPTO Examiner XAVIER VALENTINA - Art Unit 3642

Recent Applications

Detailed information about the 100 most recent patent applications.

Application NumberTitleFiling DateDisposal DateDispositionTime (months)Office ActionsRestrictionsInterviewAppeal
19141304TRANSMISSION SYSTEMJune 2025February 2026Allow800NoNo
19226668AIRCRAFT STRUCTUREJune 2025November 2025Allow600NoNo
19217117Stabilizers for Aerial ProjectilesMay 2025December 2025Allow700NoNo
19121782FLAPPING DEVICEApril 2025January 2026Allow900NoNo
19110231PROPULSION SYSTEM FOR MULTICOPTERS AND RELATED AIRCRAFTSMarch 2025March 2026Allow1200YesNo
18552079PASSENGER TRANSPORT SYSTEM PROPELLED BY A SPACE LAUNCHER, HAVING A SEAT WITH VARIABLE INCLINATION BASED ON THE LOAD FACTORJanuary 2025October 2025Allow2500NoNo
19037788SATELLITE DISPENSING SYSTEMJanuary 2025September 2025Allow800NoNo
19033472Collapsible Fuel Cells for AircraftJanuary 2025July 2025Allow600NoNo
19006885SYSTEM AND METHOD OF EJECTING A PAYLOAD FROM AN EXTRATERRESTRIAL SURFACEDecember 2024June 2025Allow600NoNo
18978723RELIABLE SEPARATION OF A CLAMPED HDRM INTERFACEDecember 2024June 2025Allow601NoNo
18976639DEVICE FOR ABSORBING ENERGY BY COMPRESSION, AIRCRAFT COMPRISING AT LEAST ONE SUCH DEVICEDecember 2024June 2025Allow600NoNo
18867836AERODYNAMIC POD FOR AIRCRAFTSNovember 2024June 2025Allow700NoNo
18930844ATMOSPHERIC RE-ENTRY VEHICLE WITH SKEWED BASE HEAT SHIELDOctober 2024May 2025Allow700NoNo
18923918ARTIFICIAL SATELLITE AND ARTIFICIAL SATELLITE SYSTEMOctober 2024May 2025Allow700NoNo
18855836DETERMINATION OF SPACECRAFT INERTIAL PROPERTIESOctober 2024October 2025Allow1200NoNo
18907917AIRCRAFT RUDDER PEDAL WITH MECHANICAL KINEMATIC CHAINOctober 2024June 2025Allow800NoNo
18905523AIRCRAFT COMPRISING AT LEAST ONE ENGINE ATTACHMENT SYSTEM THAT HAS REDUCED VERTICAL BULKOctober 2024May 2025Allow700NoNo
18829462ELECTRICAL UMBILICAL SYSTEM FOR SPACE LAUNCH VEHICLE, USING ELECTROMAGNETSeptember 2024May 2025Allow800NoNo
18809177PROPULSOR ASSEMBLY POWERED BY A DUAL MOTOR SYSTEMAugust 2024November 2025Abandon1510NoNo
18807132Panels for use in a galley of an aircraftAugust 2024January 2026Allow1710YesNo
18776800AIRCRAFT TAKE-OFF AND LANDING DEVICEJuly 2024April 2025Allow900NoNo
18728281ORBITAL DEPLOYMENT MODULE WITH A THREE-POINT SPACE PROPULSION SYSTEMJuly 2024March 2025Allow900NoNo
18755692VTOL Aircraft Using Fixed Forward Canted Rotors With Forward-Facing RotorsJune 2024January 2026Allow1900NoNo
18753030HELICOPTER ROTOR SYSTEMJune 2024June 2025Allow1110NoNo
18747187VERTICAL TAKE-OFF AND LANDING AIRCRAFTJune 2024February 2026Allow2000NoNo
18744822AIR DIRECTING ARRANGEMENT FOR CONTROLLING AIRFLOW AT AN OUTLETJune 2024January 2026Allow1910NoNo
18744203MOVEABLE WING TIP ACTUATION SYSTEMJune 2024November 2025Allow1710YesNo
18717204Airship with Self-Ballasting AirframeJune 2024January 2026Allow1920NoNo
18732012ROTOR ASSEMBLY AND UNMANNED AERIAL VEHICLE HAVING THE SAMEJune 2024March 2025Allow900NoNo
18664116SYSTEM AND METHOD FOR DIMPLED SPHERICAL STORAGE UNITSMay 2024April 2025Allow1110NoNo
18663365SYSTEM AND METHOD FOR A STRATOSPHERIC AIRCRAFTMay 2024March 2025Allow1000NoNo
18663355SYSTEM AND METHOD FOR A SPACECRAFT DOCKING STATIONMay 2024May 2025Allow1210NoNo
18661207COVER FOR A TRANSITION FROM A LINING TO A MONUMENTMay 2024October 2025Allow1710NoNo
18657688TRAM SYSTEM AND METHODS FOR AUTONOMOUS TAKEOFF AND LANDING OF AIRCRAFTMay 2024December 2024Allow700NoNo
18654560MOVABLE WALL SECTION FOR REDUCED MOBILITY PASSENGER ACCESSMay 2024March 2025Allow1000NoNo
18648328Rotor Deployment Mechanism For Vertical Take-Off And Landing AircraftApril 2024December 2024Allow700NoNo
18705023ANTI-MISUSE SYSTEM, CONTROL SYSTEM, CHILD SAFETY SEAT, ANTI-MISUSE CONTROL METHOD AND METHOD FOR CONTROLLING CHILD SAFETY SEATApril 2024February 2026Allow2200NoNo
18645615COVER SYSTEM FOR WRAPPING A BACKREST FRAMEApril 2024January 2026Allow2100NoNo
18702297AIRCRAFT LANDING GEAR HAVING INTERLOCKED MALE AND FEMALE PARTS FOR TRANSMITTING MECHANICAL TORQUEApril 2024January 2025Allow900NoNo
18629943SENSOR-EQUIPPED SEATApril 2024October 2025Allow1800NoNo
18628323PAYLOAD CONTAINER FOR PARACHUTE DELIVERY SYSTEMSApril 2024August 2025Allow1710NoNo
18616112Electric Vertical Take-Off And Landing AircraftMarch 2024August 2025Allow1700NoNo
18695211CONVEYANCE SEATMarch 2024October 2025Allow1900NoNo
18612132FLIGHT CONTROL OF LIFT PLUS CRUISE QUADCOPTER AIRCRAFTMarch 2024June 2025Allow1500NoNo
18610401CONTROL OF LIFT PLUS CRUISE QUADCOPTER AIRCRAFTMarch 2024February 2026Abandon2320NoNo
18593719Oblique Flying Wing Aircraft With Internal Ducting And Internal PropulsionMarch 2024December 2024Allow1000NoNo
18592141LIFT NACELLEFebruary 2024October 2024Allow700NoNo
18584242SPACE STRUCTURE CONTROL SYSTEM AND SPACE STRUCTURE CONTROL METHODFebruary 2024January 2025Allow1000NoNo
18444624Electric Vertical Take-Off And Landing AircraftFebruary 2024September 2025Allow1950NoNo
18416966SUPPORT ASSEMBLY FOR AN AIRCRAFT DOORJanuary 2024January 2026Allow2410NoNo
18413453Solar Sail for Orbital ManeuversJanuary 2024November 2025Allow2220NoNo
18576155SATELLITE WITH SPOT LIGHT MODE FOR EXTENDED DURATION TARGET IMAGINGJanuary 2024May 2025Allow1620NoNo
18575661METHOD FOR CONTROLLING THE ENERGY SET-UP OF A HYBRID PROPULSION SYSTEMDecember 2023September 2025Allow2110NoNo
18400150ICE PROTECTION SYSTEM HAVING MEMORY-BASED ICE REMOVAL ELEMENTSDecember 2023February 2026Abandon2620YesNo
18401316VTOL AIRCRAFT WITH DUAL PROPELLERS AND DIRECTIONAL CLUTCHDecember 2023August 2025Allow2020NoNo
18391266SYSTEMS AND METHODS FOR IMPROVED GEARBOXES FOR EVTOL AIRCRAFTDecember 2023June 2024Allow600NoNo
18544463MAIN FRAME STRUCTURE HAVING BOX-SECTION BEARING BEAMS OF LAUNCH VEHICLE ENGINEDecember 2023February 2024Allow200NoNo
18541910AEROSPACE VEHICLE SYSTEM AND METHOD OF OPERATIONDecember 2023November 2025Abandon2310NoNo
18536837AERIAL VEHICLE WITH INDEPENDENT NAVIGATION IN SIX DEGREES OF FREEDOMDecember 2023August 2025Allow2110NoNo
18521655NACELLE DEVICE AND VTOL AIRCRAFTNovember 2023November 2025Abandon2310NoNo
18511258TORQUE TRANSMISSION DEVICENovember 2023March 2025Allow1610NoNo
18511275CONTROL UNIT RESISTIVE AND LOCKING SYSTEMNovember 2023December 2024Allow1400YesNo
18561051AIR INLET FOR AN AIRCRAFT PROPULSION UNIT COMPRISING MOBILE MEMBERS FOR PROMOTING A THRUST REVERSAL PHASE, AND METHOD FOR USING SUCH AN AIR INLETNovember 2023October 2024Allow1100NoNo
18509696ROTORCRAFT WITH A NON-RETRACTABLE WHEEL-TYPE LANDING GEARNovember 2023March 2025Allow1610NoNo
18560854LEADING-EDGE HIGH-LIFT DEVICE, WING, AND AIRCRAFTNovember 2023March 2025Allow1610NoNo
18388255FULLY AUTOMATED TOWING, ALIGNMENT AND HANGAR SYSTEM AND METHOD FOR OFFSHORE OPERATION HELICOPTERNovember 2023January 2024Allow200NoNo
18496850Compound vertical takeoff and landing aircraftOctober 2023June 2025Allow1910NoNo
18383018Spacecraft with Retractable Solar SailsOctober 2023December 2024Allow1400NoNo
18379531ROW OF PASSENGER SEATS CONVERTIBLE TO A BEDOctober 2023March 2025Allow1710NoNo
18554650ANNULAR AEROSPIKE NOZZLE WITH WIDELY-SPACED THRUST CHAMBERS, ENGINE INCLUDING THE ANNULAR AEROSPIKE NOZZLE, AND VEHICLE INCLUDING THE ENGINEOctober 2023July 2024Allow900YesNo
18554587A NON-AXISYMMETRIC HEAT SHIELD, A NOZZLE DEFINED AT LEAST PARTIALLY BY THE HEAT SHIELD, AN ENGINE INCLUDING THE NOZZLE, AND A VEHICLE INCLUDING THE ENGINEOctober 2023July 2024Allow900NoNo
18373276AIRCRAFT PORTION WITH A REDUCED DRAGSeptember 2023October 2024Allow1200NoNo
18282846AN ADAPTABLE LATTICE STRUCTURE FOR MULTI-MISSION DRONESSeptember 2023January 2025Allow1610NoNo
18243229LONG RANGE FREIGHTER AIRCRAFTSeptember 2023June 2024Allow1020YesNo
18240914PROPULSOR ASSEMBLY POWERED BY A DUAL MOTOR SYSTEMAugust 2023April 2024Allow700NoNo
18458594DUAL SPEED PLANETARY GEAR SYSTEM FOR CONVERTIBLE ENGINESAugust 2023September 2024Allow1200NoNo
18238487INTEGRATED WORKSTATION FOR AN IMMERSIVE EXPERIENCE AND VIDEO COMMUNICATIONSAugust 2023November 2025Abandon2710NoNo
18276051FLYING OBJECT COPING SYSTEM, DEFENSE INFORMATION INTEGRATION CENTER, COMMUNICATION ROUTE SEARCH DEVICE, AND FLIGHT PATH PREDICTION DEVICEAugust 2023September 2024Allow1300NoNo
18275404FLYING 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 CONSTELLATIONAugust 2023September 2024Allow1400NoNo
18358406AIRCRAFT WALL ASSEMBLYJuly 2023March 2025Allow2010NoNo
18205842TRAM SYSTEM AND METHODS FOR AUTONOMOUS TAKEOFF AND LANDING OF AIRCRAFTJune 2023February 2024Allow800NoNo
18201944BLENDED WING BODY AIRCRAFTMay 2023February 2024Allow920YesNo
18321097LUGGAGE COMPARTMENT, CABIN COMPONENT ASSEMBLY AND AIRCRAFTMay 2023June 2024Allow1300NoNo
18037887Cable Tilt Actuator for an AircraftMay 2023November 2024Allow1810YesNo
18320346LANDING GEAR ASSEMBLYMay 2023June 2024Allow1300NoNo
18320406INDEPENDENT NON-SOLAR POWERED EXPLORATORY CRAFT FOR ORBITAL RENDEZVOUS AND POSITIONING FRAMEWORKMay 2023August 2025Allow2700NoNo
18314757FUEL CELLS CONFIGURED TO DELIVER BI-POLAR HIGH VOLTAGE DC POWERMay 2023April 2024Allow1100YesNo
18313112MONUMENT FIXTURESMay 2023September 2024Allow1720YesNo
18141936Dual-state rotatable propulsion systemMay 2023July 2024Allow1400NoNo
18298973Aircraft-based Modular Door Panel AssemblyApril 2023August 2024Allow1600NoNo
18030797SYSTEM FOR PROVIDING PROTECTION FROM ICING USING A FUEL CELLApril 2023August 2024Allow1700NoNo
18131771Collapsible Fuel Cells for AircraftApril 2023December 2024Allow2010NoNo
18295329HELICOPTER ROTOR SYSTEMApril 2023April 2024Allow1200NoNo
18194738ENGINE ATTACHMENT SYSTEM FOR AIRCRAFT AND METHOD FOR ATTACHING AN ENGINEApril 2023June 2025Allow2620YesNo
18189537SYSTEMS AND METHODS FOR ROUTING ELECTRICAL WIRING THROUGH AN AIRCRAFT STRUCTUREMarch 2023August 2024Allow1710YesNo
18122974SYSTEM INCLUDING STOWABLE TABLET HOLDER APPARATUSMarch 2023June 2024Allow1500NoNo
18183530DYNAMIC AXIAL PRELOADING WITH FLEXURE PLATEMarch 2023March 2024Allow1200NoNo
18118129AIRCRAFT RUDDER PEDAL WITH MECHANICAL KINEMATIC CHAINMarch 2023August 2024Allow1700NoNo
18044177AIRCRAFT RADOME INCORPORATING A LIGHTNING PROTECTION SYSTEM, AND AIRCRAFT COMPRISING SUCH A RADOMEMarch 2023December 2024Allow2210NoNo
18176219Thermal Control Systems and Methods for SpacecraftFebruary 2023August 2024Allow1810NoNo

Appeals Overview

This analysis examines appeal outcomes and the strategic value of filing appeals for examiner XAVIER, VALENTINA.

Patent Trial and Appeal Board (PTAB) Decisions

Total PTAB Decisions
1
Examiner Affirmed
1
(100.0%)
Examiner Reversed
0
(0.0%)
Reversal Percentile
16.3%
Lower than average

What This Means

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.

Strategic Value of Filing an Appeal

Total Appeal Filings
9
Allowed After Appeal Filing
3
(33.3%)
Not Allowed After Appeal Filing
6
(66.7%)
Filing Benefit Percentile
54.2%
Higher 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, 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.

Strategic Recommendations

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 - Prosecution Strategy Guide

Executive Summary

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.

Allowance Patterns

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.

Office Action Patterns

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.

Prosecution Timeline

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.

Interview Effectiveness

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.

Request for Continued Examination (RCE) Effectiveness

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.

After-Final Amendment Practice

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.

Pre-Appeal Conference Effectiveness

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.

Appeal Withdrawal and 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.

Petition Practice

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 Cooperation and Flexibility

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.

Prosecution Strategy Recommendations

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

  • 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.