USPTO Examiner CHAU ALAIN - Art Unit 3741

Recent Applications

Detailed information about the 100 most recent patent applications.

Application NumberTitleFiling DateDisposal DateDispositionTime (months)Office ActionsRestrictionsInterviewAppeal
18937193ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINENovember 2024June 2025Allow710NoNo
18802196GAS TURBINE CONTROL DEVICE AND GAS TURBINE CONTROL METHODAugust 2024January 2025Allow500NoNo
18753121GAS TURBINE FUEL TEMPERATUREJune 2024April 2025Allow1020YesNo
18753446FUELDRAULIC HEAT MANAGEMENT SYSTEMJune 2024April 2025Allow1030YesNo
18750497ANNULAR DOME ASSEMBLY FOR A COMBUSTORJune 2024May 2025Allow1110NoNo
18675809GAS TURBINE ENGINE COMPRESSION SYSTEM WITH CORE COMPRESSOR PRESSURE RATIOMay 2024March 2025Allow1010NoNo
18656372FUEL SUPPLY CIRCUIT OF AN AIRCRAFT ENGINEMay 2024April 2025Allow1110YesNo
18646753ATTENUATED COMBUSTION FOR CLEAN POWER AND HYDROGEN CAPTUREApril 2024February 2025Allow1020YesNo
18634812SYSTEM AND METHOD HAVING FLAME STABILIZERS FOR ISOTHERMAL EXPANSION IN TURBINE STAGE OF GAS TURBINE ENGINEApril 2024March 2025Allow1110YesNo
18634814SYSTEM AND METHOD HAVING FLAME STABILIZERS FOR ISOTHERMAL EXPANSION IN TURBINE STAGE OF GAS TURBINE ENGINEApril 2024November 2024Allow710YesNo
18620155COMPACT SINGLE VARIABLE DISPLACEMENT PUMP FUEL SYSTEM WITH AUGMENTOR CONTROLLED HIGH PRESSURE FUEL OIL COOLER AND GAS GENERATOR FAULT ACCOMMODATIONMarch 2024February 2025Allow1100NoNo
18608132PROPULSION ASSEMBLY COMPRISING A FUEL CONDITIONING SYSTEM POSITIONED BEHIND A DEBRIS EJECTION ZONE, AIRCRAFT COMPRISING AT LEAST ONE SUCH PROPULSION ASSEMBLYMarch 2024June 2025Allow1510NoNo
18592194METHODS AND APPARATUS TO PRODUCE HYDROGEN GAS TURBINE PROPULSIONFebruary 2024February 2025Allow1110NoNo
18591414THERMAL MANAGEMENT SYSTEMS HAVING AN OIL TANK COMPRISING SOLID-SOLID PHASE CHANGE MATERIAL FOR GAS TURBINE ENGINESFebruary 2024January 2025Allow1010NoNo
18442719INDUCER ASSEMBLY FOR A TURBINE ENGINEFebruary 2024March 2025Allow1310NoNo
18293825IMPROVED METHOD FOR ESTIMATING AND SETTING EXHAUST PURGE TIME IN A COMBUSTION SYSTEM AND COMBUSTION SYSTEM THEREOFJanuary 2024May 2025Allow1610YesNo
18423788INJECTOR WITH TANGENTIAL FEED CONDUITS FOR HYDROGEN-DRIVEN GAS TURBINE ENGINEJanuary 2024May 2025Allow1620NoNo
18292047ELECTRICITY GENERATION SYSTEM AND AIRCRAFTJanuary 2024February 2025Allow1210NoNo
18291558TRANSFER OF POWER BETWEEN THE HIGH-PRESSURE SHAFT AND THE LOW-PRESSURE SHAFT OF A TURBOMACHINEJanuary 2024June 2025Allow1710NoNo
18410493AIRCRAFT PERFORMANCE OPTIMIZATION BASED ON ENGINE PERFORMANCE MONITORINGJanuary 2024January 2025Allow1210NoNo
18539824MULTI-COMPONENT SWIRL VALVESDecember 2023June 2025Allow1811NoNo
18536711PLANETARY GEAR SYSTEM ARRANGEMENT WITH AUXILIARY OIL SYSTEMDecember 2023May 2025Allow1710NoNo
18537161STEAM INJECTED TURBINE ENGINE STEAM GENERATION CONTROLDecember 2023March 2025Allow1510NoNo
18533447THERMODYNAMIC APPARATUSDecember 2023August 2024Allow910YesNo
18567408FUEL CONDITIONING SYSTEM AND METHOD CONFIGURED TO SUPPLY AN AIRCRAFT TURBINE ENGINE WITH FUEL FROM A CRYOGENIC TANKDecember 2023August 2024Allow800NoNo
18524753CMC STEPPED COMBUSTOR LINERNovember 2023March 2025Allow1620NoNo
18509536COMBINED CYCLE POWER PLANTS WITH EXHAUST GAS RECIRCULATION INTERCOOLINGNovember 2023May 2025Allow1820YesNo
18503279STRUT MICROTUBE COUNTERFLOW EVAPORATORNovember 2023March 2025Allow1710NoNo
18559497FUEL INJECTOR AND FUEL NOZZLE FOR A GAS TURBINE, AND GAS TURBINE ENGINE INCLUDING THE NOZZLENovember 2023March 2025Allow1610YesNo
18287745FUEL SUPPLY SYSTEM WITH AIR EXPULSION DRAIN FOR AN AIRCRAFT ENGINEOctober 2023January 2025Allow1520YesNo
18555890DIFFUSION CONE FOR THE REAR PART OF A JET ENGINE INCORPORATING A FLAME-HOLDER RING AT THE TRAILING EDGEOctober 2023August 2024Allow1010NoNo
18372493AIR INTAKE FOR AN AIRCRAFT PROPULSION SYSTEM ENGINE ASSEMBLYSeptember 2023December 2024Allow1520YesNo
18244425VARIABLE DISPLACEMENT PUMP (VDP) SYSTEMS WITH DRY-OUT CENTRIFUGAL MAIN PUMPSeptember 2023April 2025Allow1910YesNo
18244390VARIABLE DISPLACEMENT PUMP (VDP) SYSTEMS WITH DUAL DRY OUT PUMPSSeptember 2023April 2025Allow1910YesNo
18453017Fuel Unit Health Monitoring SystemAugust 2023November 2024Allow1410NoNo
18230805FUEL SYSTEM FOR DUAL USE GAS TURBINE ENGINE MAIN FUEL PUMPAugust 2023November 2024Allow1511YesNo
18264328THRUST REVERSER COMPRISING MOVABLE GRIDS AND COWLS ASSEMBLED BY RECESSINGAugust 2023July 2024Allow1110NoNo
18275081PREMIXER INJECTOR IN GAS TURBINE ENGINEJuly 2023September 2024Allow1320NoNo
18275097THRUST ENHANCING DEVICEJuly 2023June 2024Allow1110NoNo
18226163HYDRAULIC MOTORING OF ENGINEJuly 2023October 2024Allow1501YesNo
18224753VARIABLE RESTRICTION OF A FUEL CIRCUIT OF A FUEL NOZZLEJuly 2023December 2024Allow1720YesNo
18270634GAS TURBINE EQUIPMENT WITH COMPRESSOR AIRFLOW CONTROL RESPONSIVE TO NOx CONCENTRATION AND CONTROL METHOD THEREOFJune 2023April 2024Allow1000NoNo
18216141AIRCRAFT PROPULSION SYSTEM WITH TURBINE ENGINE AND EXHAUST HEAT EXCHANGERJune 2023October 2024Allow1610NoNo
18215394ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINEJune 2023September 2024Allow1410NoNo
18214250FUEL SYSTEM HAVING VARIABLE DISPLACEMENT PUMP FAILURE MODESJune 2023March 2024Allow910NoNo
18340508REDUNDANT ELECTRO-HYDRAULIC SERVO VALVE (EHSV) CONTROL IN A FUEL METERING SYSTEMJune 2023December 2023Allow600NoNo
18213053FUEL SYSTEMS HAVING THERMAL RECIRCULATIONJune 2023December 2023Allow500YesNo
18337559FUEL MANAGEMENT SYSTEMJune 2023March 2024Allow810NoNo
18208451DIRECT CONTROLLED VARIABLE DISPLACEMENT PUMP FUEL SYSTEMS WITH LOW PRESSURE THERMAL RECIRCULATION PUMPINGJune 2023April 2025Allow2210NoNo
18327629TURBINE ENGINE HAVING A THRUST REVERSER SYSTEMJune 2023March 2025Abandon2120NoNo
18202606COOLING FLUID USED AS SECONDARY FUEL SOURCEMay 2023September 2024Allow1600NoNo
18199742AXIALLY OFFSET VANE ARRAYS IN TURBINE ENGINE BYPASSMay 2023August 2024Allow1520NoNo
18197499PUMP SYSTEM FOR A GAS TURBINE ENGINEMay 2023May 2024Allow1220NoNo
18196704SYSTEM AND METHOD FOR IDENTIFYING BLOCKAGE OF AN AIR INTAKE FOR AN AIRCRAFT PROPULSION SYSTEMMay 2023March 2024Allow1010NoNo
18311660FUEL SYSTEMS FOR AIRCRAFT ENGINESMay 2023June 2024Allow1310NoNo
18310365DOUBLE-SKIN LINER FOR A GAS TURBINEMay 2023May 2024Abandon1210NoNo
18307450COMPRESSOR WITH ANTI-ICE INLETApril 2023September 2024Allow1720NoNo
18137887DUCTED FIREWALL WITH UPPER BIFI BLEED FOR MODULATED CORE VENTILATIONApril 2023August 2024Allow1620YesNo
18303111SYSTEMS AND METHODS WITH DISTRIBUTED BLEED FOR GAS TURBINE ENGINE COMPRESSOR STABILIZATIONApril 2023September 2024Allow1720YesNo
18302081BYPASS HEAT EXCHANGER CONFIGURATION TO REROUTE CORE FLOWApril 2023April 2024Allow1210YesNo
18132257COMPACT SAFETY IGNITION DEVICE FOR DUAL PULSE MOTORApril 2023January 2024Allow910YesNo
18122067MICRO-TURBINE GAS GENERATOR AND PROPULSIVE SYSTEMMarch 2023February 2025Abandon2330NoNo
18119017SYSTEM AND METHOD FOR OPERATING A MULTI-ENGINE AIRCRAFTMarch 2023August 2023Allow610NoNo
18176777METHODS AND SYSTEMS FOR CONTROLLING AN ENGINE SYSTEM OF A VEHICLEMarch 2023January 2025Allow2310NoNo
18176246Heat Driven Thermal Management Systems and Methods for Operating the SameFebruary 2023September 2024Allow1920YesNo
18114747AIRCRAFT ENGINE FOR NITROGEN OXIDE REDUCTIONFebruary 2023November 2024Allow2120YesNo
18113729BAFFLED THERMOCLINES IN THERMODYNAMIC CYCLE SYSTEMSFebruary 2023June 2024Allow1620YesNo
18173175Afterburner structure with self-excited sweeping oscillating fuel injection nozzlesFebruary 2023November 2023Allow910NoNo
18109441ADJUSTABLE PRIMARY AND SUPPLEMENTAL POWER UNITSFebruary 2023January 2024Allow1110YesNo
18104408GAS TURBINE ENGINE COMBUSTOR WITH A SET OF DILUTION PASSAGESFebruary 2023July 2024Allow1830YesNo
18098463GAS TURBINE ENGINE COMPRESSION SYSTEM WITH CORE COMPRESSOR PRESSURE RATIOJanuary 2023March 2024Allow1410YesNo
18154134ACCESSORY GEARBOX COVER WITH PLANAR LINKING MEMBERJanuary 2023June 2024Allow1710NoNo
18096140SYSTEMS AND METHODS FOR STARTING A GAS TURBINE ENGINEJanuary 2023June 2023Allow500NoNo
18093091REHEAT ASSEMBLYJanuary 2023August 2023Allow710NoNo
18093166TANGENTIAL TURBOFAN PROPULSION SYSTEMJanuary 2023July 2024Abandon1920NoNo
18092120SYSTEM AND METHOD HAVING FLAME STABILIZERS FOR ISOTHERMAL EXPANSION IN TURBINE STAGE OF GAS TURBINE ENGINEDecember 2022December 2023Allow1210YesNo
18069669ALTERNATIVE FUEL FAST START SYSTEMS FOR GAS TURBINE ENGINESDecember 2022May 2024Allow1720NoNo
18084768PUMPS WITH BACKUP CAPABILITYDecember 2022December 2023Allow1210NoNo
18082008METHOD AND SYSTEM FOR GOVERNING AN ENGINE AT LOW POWERDecember 2022December 2023Allow1210NoNo
17993082INDUCER ASSEMBLY FOR A TURBINE ENGINENovember 2022October 2023Allow1110NoNo
17964134JET ENGINE HAVING ELECTRICALLY POWERED SUPERHEATING SECTIONOctober 2022November 2023Allow1320YesNo
17963029TURBINE ENGINE INDUCER ASSEMBLYOctober 2022August 2023Allow1010NoNo
17937605FLAME DETECTOR LENS MAINTENANCE SYSTEMOctober 2022April 2025Allow3020NoNo
17907420THERMODYNAMIC APPARATUSSeptember 2022October 2023Allow1320YesNo
17946708HYDROGEN FUEL SYSTEM FOR A GAS TURBINE ENGINESeptember 2022October 2023Allow1310NoNo
17946499GAS TURBINE ENGINES WITH A FUEL CELL ASSEMBLYSeptember 2022February 2025Allow2940YesNo
17929359AERODYNAMIC COMBUSTOR LINER DESIGN FOR EMISSIONS REDUCTIONSSeptember 2022April 2023Allow710NoNo
17929360ACOUSTIC DAMPER FOR COMBUSTORSeptember 2022May 2023Allow910NoNo
17901383HYDROGEN FUEL SYSTEMSeptember 2022May 2024Allow2020NoNo
17823732FUEL DELIVERY SYSTEM WITH PURGE GAS STEP AND FUEL GAS FLUSHING STEP AND METHOD THEREOFAugust 2022May 2023Allow810NoNo
17896762VARIABLE RESTRICTION OF A FUEL CIRCUIT OF A FUEL NOZZLEAugust 2022October 2023Allow1410NoNo
17895969FUEL INJECTOR MANIFOLD HAVING TRIM DEVICE THEREINAugust 2022May 2023Allow810YesNo
17759208FUEL SUPPLY CIRCUIT OF AN AIRCRAFT ENGINEJuly 2022February 2024Allow1820YesNo
17870078FUEL SYSTEM WITH BACKUP PUMP SOURCE SELECTIONJuly 2022September 2023Allow1410YesNo
17869428MODULATING FUEL FOR A TURBINE ENGINEJuly 2022December 2023Allow1720YesNo
17868222TWO STAGE FUEL DELIVERY SYSTEM FOR AN AIRCRAFTJuly 2022April 2024Allow2111YesNo
17863011COMBINED CYCLE POWER PLANTS WITH EXHAUST GAS RECIRCULATION INTERCOOLINGJuly 2022August 2023Allow1320YesNo
17811762ANNULAR DOME ASSEMBLY FOR A COMBUSTORJuly 2022March 2024Allow2030NoNo
17857996SYSTEMS AND METHODS FOR BLEED VALVE CONTROL IN FUEL SYSTEMSJuly 2022March 2023Allow810YesNo
17854643SYSTEM AND METHOD FOR CONTROLLING DUAL STARTER AIR VALVEJune 2022July 2023Allow1321NoNo

Appeals Overview

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

Patent Trial and Appeal Board (PTAB) Decisions

Total PTAB Decisions
11
Examiner Affirmed
7
(63.6%)
Examiner Reversed
4
(36.4%)
Reversal Percentile
56.9%
Higher than average

What This Means

With a 36.4% reversal rate, the PTAB reverses the examiner's rejections in a meaningful percentage of cases. This reversal rate is above the USPTO average, indicating that appeals have better success here than typical.

Strategic Value of Filing an Appeal

Total Appeal Filings
18
Allowed After Appeal Filing
6
(33.3%)
Not Allowed After Appeal Filing
12
(66.7%)
Filing Benefit Percentile
52.3%
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 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 CHAU, ALAIN - Prosecution Strategy Guide

Executive Summary

Examiner CHAU, ALAIN works in Art Unit 3741 and has examined 559 patent applications in our dataset. With an allowance rate of 79.2%, this examiner has a below-average tendency to allow applications. Applications typically reach final disposition in approximately 33 months.

Allowance Patterns

Examiner CHAU, ALAIN's allowance rate of 79.2% places them in the 41% percentile among all USPTO examiners. This examiner has a below-average tendency to allow applications.

Office Action Patterns

On average, applications examined by CHAU, ALAIN receive 1.86 office actions before reaching final disposition. This places the examiner in the 58% percentile for office actions issued. This examiner issues a slightly above-average number of office actions.

Prosecution Timeline

The median time to disposition (half-life) for applications examined by CHAU, ALAIN is 33 months. This places the examiner in the 29% percentile for prosecution speed. Prosecution timelines are slightly slower than average with this examiner.

Interview Effectiveness

Conducting an examiner interview provides a +30.0% benefit to allowance rate for applications examined by CHAU, ALAIN. This interview benefit is in the 81% percentile among all examiners. Recommendation: Interviews are highly effective with this examiner and should be strongly considered as a prosecution strategy. Per MPEP § 713.10, interviews are available at any time before the Notice of Allowance is mailed or jurisdiction transfers to the PTAB.

Request for Continued Examination (RCE) Effectiveness

When applicants file an RCE with this examiner, 28.0% of applications are subsequently allowed. This success rate is in the 40% percentile among all examiners. Strategic Insight: RCEs show below-average effectiveness with this examiner. Carefully evaluate whether an RCE or continuation is the better strategy.

After-Final Amendment Practice

This examiner enters after-final amendments leading to allowance in 40.6% of cases where such amendments are filed. This entry rate is in the 55% 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, 33.3% result in withdrawal of the rejection or reopening of prosecution. This success rate is in the 32% 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 54.2% of appeals filed. This is in the 20% percentile among all examiners. Of these withdrawals, 15.4% occur early in the appeal process (after Notice of Appeal but before Appeal Brief). Strategic Insight: This examiner rarely withdraws rejections during the appeal process compared to other examiners. If you file an appeal, be prepared to fully prosecute it to a PTAB decision. Per MPEP § 1207, the examiner will prepare an Examiner's Answer maintaining the rejections.

Petition Practice

When applicants file petitions regarding this examiner's actions, 50.0% are granted (fully or in part). This grant rate is in the 62% percentile among all examiners. Strategic Note: Petitions show above-average success regarding this examiner's actions. Petitionable matters include restriction requirements (MPEP § 1002.02(c)(2)) and various procedural issues.

Examiner Cooperation and Flexibility

Examiner's Amendments: This examiner makes examiner's amendments in 0.0% of allowed cases (in the 39% percentile). This examiner makes examiner's amendments less often than average. You may need to make most claim amendments yourself.

Quayle Actions: This examiner issues Ex Parte Quayle actions in 1.8% of allowed cases (in the 63% percentile). This examiner issues Quayle actions more often than average when claims are allowable but formal matters remain (MPEP § 714.14).

Prosecution Strategy Recommendations

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

  • Prioritize examiner interviews: Interviews are highly effective with this examiner. Request an interview after the first office action to clarify issues and potentially expedite allowance.

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.