USPTO Examiner RODRIGUEZ WILLIAM H - Art Unit 3741

Recent Applications

Detailed information about the 100 most recent patent applications.

Application NumberTitleFiling DateDisposal DateDispositionTime (months)Office ActionsRestrictionsInterviewAppeal
19292361MEDICAL DEVICES AND RELATED SYSTEMS AND METHODSAugust 2025December 2025Allow500NoNo
19247856GAS TURBINE ENGINE AND METHOD THEREOF FOR REDUCING NON-VOLATILE PARTICULATE MATTER EMISSIONSJune 2025February 2026Allow710NoNo
19232069TURBINE AIRFOIL AND GAS TURBINE INCLUDING THE SAMEJune 2025February 2026Allow810NoNo
19228827GAS TURBINE ENGINE AND METHOD THEREOF FOR REDUCING NONVOLATILE PARTICULATE MATTER EMISSIONSJune 2025October 2025Allow510YesNo
19215969MATRIX FOR CERAMIC-CONTAINING MATERIALSMay 2025November 2025Allow601NoNo
19192976SEAL PLATE METHOD FOR COMMUNICATING RETRACT OIL TO RETRACT SIDE OF PISTON IN HYDRAULIC CYLINDERApril 2025January 2026Allow910NoNo
19096780GAS TURBINE ENGINE HYDRAULIC SYSTEMApril 2025February 2026Allow1010NoNo
19092052NOZZLE BODY FOR FUEL INJECTORMarch 2025October 2025Allow700NoNo
19082771METHOD FOR STARTING GAS TURBINEMarch 2025October 2025Allow700NoNo
190803583D DIFFUSER FED SCOOP FUEL INJECTORMarch 2025November 2025Allow800NoNo
19063927SENSING OF ISOLATOR SHOCK SYSTEMSFebruary 2025September 2025Allow600NoNo
19059571ACTIVE DE-AERATOR FOR AIRCRAFT POWER PLANTFebruary 2025July 2025Allow500NoNo
19041081AEROSPACE THERMAL MANAGEMENT SYSTEMJanuary 2025February 2026Allow1210NoNo
19035668SYSTEM AND METHOD FOR GENERATING ELECTRICITY AND HEAT FROM THE COMBUSTION OF TAIL GAS CONTAINING BIOGENIC METHANE USING A GAS TURBINEJanuary 2025April 2025Allow200YesNo
19029020OPERATION METHOD FOR GAS TURBINE AND CONTROL DEVICE FOR GAS TURBINEJanuary 2025September 2025Allow810NoNo
19023061CMC COMPONENT WITH COVER PLATEJanuary 2025July 2025Allow600NoNo
19016733ELECTRONIC CONTROLLER COOLING FOR AIRCRAFT PROPULSION SYSTEMJanuary 2025September 2025Allow810NoNo
19016574ELECTRIC POWER ARRANGEMENT FOR PROPULSIONJanuary 2025September 2025Allow810YesNo
19005225COMBINED CYCLE POWER GENERATION FACILITYDecember 2024June 2025Allow600NoNo
18877913THRUST REVERSER COMPRISING AT LEAST ONE DEPLOYABLE DEFLECTING MEMBRANEDecember 2024February 2026Allow1400NoNo
18985499ENGINE PROTECTION COVER DEVICE FOR AIRTIGHT SEALING AN ENGINE OF AN AIRCRAFT OR SPACECRAFTDecember 2024September 2025Allow910NoNo
18981043HEAT SOURCE FOR HYDROGEN FUEL SUPPLY SYSTEMDecember 2024September 2025Allow910NoNo
18979990HEAT MANAGEMENT SYSTEM AND METHOD FOR HYDROGEN-FUELED ENGINEDecember 2024July 2025Allow710NoNo
18977983COMBUSTION DEVICE CONTROL SYSTEM AND COMBUSTION DEVICE CONTROL METHODDecember 2024September 2025Allow910NoNo
18979020GAS TURBINE ENGINE DUCTING SYSTEM HAVING A PLURALITY OF SPHERICAL JOINTSDecember 2024September 2025Allow910NoNo
18977606AIRCRAFT POWERPLANT GEARBOX WITH SELECTABLE POWER COUPLERDecember 2024May 2025Allow500NoNo
18973847APPARATUS FOR CONTROL OF MULTIPLE FLUID POWERED ACTUATORSDecember 2024January 2026Allow1410YesNo
18868810COMBUSTOR HAVING SECONDARY FUEL INJECTORNovember 2024February 2026Allow1410NoNo
18950877Additively Manufactured Turbine Engine Case with Fuel ManifoldNovember 2024September 2025Allow1010NoNo
18947604COMBUSTOR NOZZLE, COMBUSTOR, AND GAS TURBINE INCLUDING SAMENovember 2024April 2025Allow500NoNo
18910173THRUST REVERSER IN CONDENSER EXIT DUCTOctober 2024April 2025Allow600NoNo
18894458MULTI-STAGE MICRO-DECOMPOSITION SWIRL BURNER WITH AN AMMONIA-DOPED FUEL AND LOW NOX CONTROL METHODSeptember 2024November 2024Allow200NoNo
18892765GAS TURBINE ENGINE AND METHOD FOR REDUCING NONVOLATILE PARTICULATE MATTER EMISSIONS IN THE EXHAUSTSeptember 2024February 2025Allow410NoNo
18886005GAS TURBINE COMBUSTOR HAVING A FIRST COMBUSTION ZONE RECEIVING MULTIPLE FUELS AND A SECOND COMBUSTION ZONE RECEIVING A FUEL NOT CONTAINING NITROGEN ATOMSSeptember 2024December 2025Allow1510NoNo
18807428HIGH TEMPERATURE ANTI-ICE SYSTEMS FOR AIRCRAFT ENGINESAugust 2024June 2025Allow1011NoNo
18805691GAS TURBINE ENGINE FUEL NOZZLE HAVING A SECONDARY FUEL PASSAGE THROUGH A SWIRLERAugust 2024July 2025Allow1110YesNo
18793126CRYOGENIC FUEL SEMI-CLOSED INJECTION COOLED BOTTOMING CYCLEAugust 2024March 2025Allow800NoNo
18789883COMBINED CYCLE POWER PLANT WITH STEAM TURBINE BYPASS FOR SIMPLE CYCLE OPERATION WITH HEAT RECOVERY STEAM GENERATOR AND METHOD OF USEJuly 2024July 2025Allow1110NoNo
18834516A FUEL NOZZLE FOR A GAS TURBINE, COMBUSTOR INCLUDING THE FUEL NOZZLE, AND GAS TURBINEJuly 2024June 2025Allow1110YesNo
18767604THERMAL IMPACT OF GAS STORAGEJuly 2024March 2025Allow800NoNo
18765725GAS TURBINE AND FUEL NOZZLE ASSEMBLY FOR MIXING HYDROGEN FUEL AND STEAM TO CONTROL FLAME SPEEDJuly 2024May 2025Allow1020NoNo
18765533GAS TURBINE ENGINE HAVING A HEAT EXCHANGER ARRANGEMENT FOR HEATING OR COOLING A FUELJuly 2024September 2025Allow1410NoNo
18727215CONTROL METHOD FOR GAS TURBINE COMBUSTOR AND CONTROL DEVICE FOR GAS TURBINE COMBUSTORJuly 2024June 2025Allow1210NoNo
18763619Mixing Elements For Rotating Detonation Combustion SystemsJuly 2024June 2025Allow1110YesNo
18760805COMBINED HEAT AND POWER SYSTEM USING AND PRODUCING CO2 AND METHOD OF OPERATIONJuly 2024June 2025Allow1210NoNo
18741964GAS TURBINE ENGINE FUEL SYSTEM COMPRISING MULTIPLE FUEL HEATERSJune 2024July 2025Allow1310NoNo
18735712DUAL CYCLE INTERCOOLED HYDROGEN ENGINE ARCHITECTUREJune 2024June 2025Allow1210NoNo
18716550FUEL DISTRIBUTION ASSEMBLY FOR A TURBOMACHINEJune 2024February 2025Allow900NoNo
18734201SYSTEM AND METHOD FOR BLENDING MULTIPLE FUELSJune 2024March 2025Allow910NoNo
18731709LIQUID ROCKET ENGINE INJECTOR WITH VARIABLE FLOW AREAJune 2024March 2025Allow910NoNo
18665376GAS TURBINE PLANT WITH AMMONIA DECOMPOSITION SYSTEMMay 2024November 2024Allow600NoNo
18710368HEAT ENGINE SYSTEM COMPRISING A RESERVOIR FOR RECEIVING AND SUPPLYING A WORKING FLUID FROM AND TO A COMPRESSOR VIA A BLEED VALVE AND AN INTAKE VALVEMay 2024January 2025Allow810YesNo
18662660DUAL FUEL GAS TURBINE COMBUSTION CHAMBER MODULE HAVING AN ANNULAR COMBUSTION CHAMBERMay 2024June 2025Allow1310NoNo
18659364AXIAL FUEL STAGE INJECTOR WITH FUEL INJECTION IN SAME DIRECTION AS HIGH-PRESSURE AIR FLOWMay 2024June 2025Allow1410YesNo
18657325HIGH BANDWIDTH CONTROL OF TURBOFAN/TURBOPROP THRUST RESPONSE USING EMBEDDED ELECTRIC MACHINESMay 2024March 2025Allow1010NoNo
18652159AN IMPROVED COMBUSTOR APPARATUSMay 2024March 2025Allow1110NoNo
18652134COMBUSTOR APPARATUSMay 2024September 2024Allow400NoNo
18651069EXHAUST NOZZLE ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEMApril 2024June 2025Allow1310NoNo
18638783INLET CONDITIONING SYSTEMS AND METHODS FOR A TURBOMACHINEApril 2024October 2024Allow600NoNo
18633110FUEL INJECTOR MANIFOLD HAVING A VARIABLE FUEL FLOW SYSTEM FOR A TURBINE ENGINEApril 2024February 2025Allow1110NoNo
18626821FUEL NOZZLE FOR HYDROGEN-BASED FUEL OPERATIONApril 2024January 2025Allow900NoNo
18626818FUEL NOZZLE FOR HYDROGEN-BASED FUEL OPERATIONApril 2024September 2024Allow500NoNo
18626811FUEL NOZZLE FOR HYDROGEN-BASED FUEL OPERATIONApril 2024March 2025Allow1110NoNo
18621810FUEL LEAK COMBUSTION ASSEMBLY FOR IGNITING A GASEOUS FUEL LEAKING FROM A POTENTIAL LEAK LOCATIONMarch 2024November 2025Allow1920NoNo
18622263AIRCRAFT GAS TURBINE ENGINE INCLUDING A STEAM SYSTEMMarch 2024March 2025Allow1110NoNo
18613824TURBINE ENGINE WITH FUEL NOZZLEMarch 2024June 2025Allow1500NoNo
18610437COOLING STRUCTURE FOR RADIAL TURBINEMarch 2024February 2025Allow1110YesNo
18609726DUAL-MODE RAMJET ENGINE WITH VARIABLE FUEL INJECTIONMarch 2024September 2024Allow600NoNo
18608525COMBUSTION SYSTEM WITH DUAL FUEL CAPABILITYMarch 2024December 2024Allow910NoNo
18601912CLUSTER OF SWIRLED MINI-MIXERS FOR FUEL-STAGED, AXIALLY STAGED COMBUSTIONMarch 2024December 2024Allow910NoNo
18438977PILOT FUEL NOZZLE ASSEMBLY WITH MULTI-ANGLED VENTURIFebruary 2024August 2025Allow1810NoNo
18433160REUSABLE UPPER STAGE ROCKET WITH AEROSPIKE ENGINEFebruary 2024March 2025Allow1310NoNo
18433223SYSTEM AND METHOD HAVING MULTI-FLUID INJECTORS FOR ISOTHERMAL EXPANSION IN TURBINE STAGE OF GAS TURBINE ENGINEFebruary 2024September 2024Allow810NoNo
18429920Turbine Engine Including a Condenser SystemFebruary 2024June 2025Allow1610YesNo
18423649INJECTOR WITH DISC FOR HYDROGEN-DRIVEN GAS TURBINE ENGINEJanuary 2024October 2024Allow800NoNo
18421471GAS TURBINE ENGINE COMPRISING FUEL-OIL HEAT EXCHANGERS FLUIDLY CONNECTED TO FUEL SPRAY NOZZLESJanuary 2024March 2025Allow1410NoNo
18579841A DEVICE TO PRODUCE HIGHER PRESSURE AND TEMPERATURE IN A GASJanuary 2024September 2024Allow800NoNo
18409690GAS TURBINE FUEL NOZZLE HAVING AN INNER AIR PASSAGE AND PLURAL OUTER FUEL PASSAGESJanuary 2024September 2024Allow910NoNo
18577686THERMALLY INTEGRATED AMMONIA FUELLED ENGINEJanuary 2024February 2025Abandon1410NoNo
18401572METHOD OF OPERATING GAS TURBINE COMBUSTOR WITH MULTIPLE FUEL STAGESDecember 2023March 2025Allow1520YesNo
18394407TURBINE ENGINE HAVING A COMBUSTION SECTION WITH A FUEL NOZZLE ASSEMBLYDecember 2023October 2024Allow1000NoNo
18571617INDUSTRIAL PREMIXED GAS COMBUSTOR USING INTERNAL EXHAUST GAS RECIRCULATION AND OPERATING METHOD THEREOFDecember 2023June 2025Allow1810NoNo
18541041CENTRAL STAGED COMBUSTION CHAMBER WITH SELF-EXCITED SWEEPING OSCILLATING FUEL INJECTION NOZZLESDecember 2023September 2024Allow910NoNo
18529360METHOD OF OPERATING A GAS TURBINE COMBUSTOR COMPRISING INJECTING A DILUENT INTO THE PRIMARY AND SECONDARY COMBUSTION ZONESDecember 2023September 2024Allow1010NoNo
18507877SEQUENTIAL COMBUSTION GAS TURBINE ENGINE INCLUDING A STEAM SYSTEM FOR INJECTING STEAM TO EACH COMBUSTORNovember 2023April 2025Allow1720YesNo
18488217METHOD OF STARTING A GAS TURBINE ENGINEOctober 2023September 2024Allow1101NoNo
18484827DRIVE SYSTEM FOR AN AIRCRAFT, AIRCRAFT HAVING A DRIVE SYSTEM AND METHOD FOR OPERATING AN AIRCRAFTOctober 2023February 2025Allow1720YesNo
18482949FUEL-AIR MIXING ASSEMBLY IN A TURBINE ENGINEOctober 2023June 2024Allow900NoNo
18377776FUEL NOZZLE HAVING INNER AND OUTER MIXING CHAMBERS FED WITH FUEL VIA FIRST AND SECOND HOLE PATTERNSOctober 2023December 2024Allow1410NoNo
18479992GAS TURBINE COMBUSTION SYSTEM HAVING AN AMMONIA AUTOTHERMAL CRACKING DEVICEOctober 2023November 2024Allow1410NoNo
18372796INJECTION MANIFOLD WITH TESLA VALVES FOR ROTATING DETONATION ENGINESSeptember 2023August 2024Allow1110NoNo
18473246GAS TURBINE COMBUSTOR INJECTOR ASSEMBLY COMPRISING AN AIR SUPPLY UNIT HAVING AN INCLINED SURFACE RELATIVE TO AN INCLINED INJECTION PIPESeptember 2023September 2024Allow1210NoNo
18472568METHOD FOR DETECTING AND ANNUNCIATING GAS TURBINE ENGINE COMPRESSOR STALLSeptember 2023July 2024Allow900NoNo
18464565GAS TURBINE COMBUSTOR STRUCTURESeptember 2023June 2024Allow900NoNo
18463016COMBUSTION DEVICE COMPRISING PLURAL SWIRLING BLADES AND GAS TURBINE SYSTEM HAVING THE SAMESeptember 2023September 2024Allow1310NoNo
18460078COMBUSTOR SWIRLER WITH VANES INCORPORATING OPEN AREASeptember 2023October 2024Allow1420NoNo
18240655GAS TURBINE ENGINE EXHAUST DIFFUSER HAVING MULTIPLE INCLINED SURFACES AT DIFFERENT ANGLESAugust 2023August 2024Allow1220NoNo
18238792CONTROLLABLE FUEL NOZZLE VALVES WITH REDUNDANCYAugust 2023July 2024Allow1110NoNo
18452958GAS TURBINE COMBUSTOR FUEL NOZZLE ASSEMBLY AND COMBUSTOR LINER HAVING DILUTION HOLES IN ARRANGEMENTSAugust 2023September 2024Allow1310NoNo
18234340ROTATING DETONATION AUGMENTORS WITH ADJUSTABLE THROATS FOR GAS TURBINE ENGINESAugust 2023April 2024Allow800NoNo

Appeals Overview

This analysis examines appeal outcomes and the strategic value of filing appeals for examiner RODRIGUEZ, WILLIAM H.

Patent Trial and Appeal Board (PTAB) Decisions

Total PTAB Decisions
7
Examiner Affirmed
3
(42.9%)
Examiner Reversed
4
(57.1%)
Reversal Percentile
82.3%
Higher than average

What This Means

With a 57.1% reversal rate, the PTAB has reversed the examiner's rejections more often than affirming them. This reversal rate is in the top 25% across the USPTO, indicating that appeals are more successful here than in most other areas.

Strategic Value of Filing an Appeal

Total Appeal Filings
15
Allowed After Appeal Filing
8
(53.3%)
Not Allowed After Appeal Filing
7
(46.7%)
Filing Benefit Percentile
85.5%
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, 53.3% 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.

Strategic Recommendations

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 RODRIGUEZ, WILLIAM H - Prosecution Strategy Guide

Executive Summary

Examiner RODRIGUEZ, WILLIAM H works in Art Unit 3741 and has examined 775 patent applications in our dataset. With an allowance rate of 89.4%, this examiner has an above-average tendency to allow applications. Applications typically reach final disposition in approximately 37 months.

Allowance Patterns

Examiner RODRIGUEZ, WILLIAM H's allowance rate of 89.4% places them in the 71% percentile among all USPTO examiners. This examiner has an above-average tendency to allow applications.

Office Action Patterns

On average, applications examined by RODRIGUEZ, WILLIAM H receive 1.39 office actions before reaching final disposition. This places the examiner in the 22% 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 RODRIGUEZ, WILLIAM H is 37 months. This places the examiner in the 34% percentile for prosecution speed. Prosecution timelines are slightly slower than average with this examiner.

Interview Effectiveness

Conducting an examiner interview provides a +7.1% benefit to allowance rate for applications examined by RODRIGUEZ, WILLIAM H. This interview benefit is in the 35% 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, 37.6% of applications are subsequently allowed. This success rate is in the 86% 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 62.5% of cases where such amendments are filed. This entry rate is in the 87% 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, 50.0% result in withdrawal of the rejection or reopening of prosecution. This success rate is in the 46% percentile among all examiners. Note: Pre-appeal conferences show below-average success with this examiner. Consider whether your arguments are strong enough to warrant a PAC request.

Appeal Withdrawal and Reconsideration

This examiner withdraws rejections or reopens prosecution in 65.0% of appeals filed. This is in the 45% percentile among all examiners. Of these withdrawals, 38.5% occur early in the appeal process (after Notice of Appeal but before Appeal Brief). Strategic Insight: This examiner shows below-average willingness to reconsider rejections during appeals. Be prepared to fully prosecute appeals if filed.

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 4.4% of allowed cases (in the 84% percentile). Per MPEP § 1302.04, examiner's amendments are used to place applications in condition for allowance when only minor changes are needed. This examiner frequently uses this tool compared to other examiners, indicating a cooperative approach to getting applications allowed. Strategic Insight: If you are close to allowance but minor claim amendments are needed, this examiner may be willing to make an examiner's amendment rather than requiring another round of prosecution.

Quayle Actions: This examiner issues Ex Parte Quayle actions in 8.1% of allowed cases (in the 86% 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.
  • Examiner cooperation: This examiner frequently makes examiner's amendments to place applications in condition for allowance. If you are close to allowance, the examiner may help finalize the claims.

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.