USPTO Examiner SEBASCO CHENG STEPHANIE - Art Unit 3741

Recent Applications

Detailed information about the 100 most recent patent applications.

Application NumberTitleFiling DateDisposal DateDispositionTime (months)Office ActionsRestrictionsInterviewAppeal
18631772LIQUID AIR POWER AND STORAGEApril 2024April 2025Allow1200YesNo
18461709SPLITTER AND GUIDE VANE ARRANGEMENT FOR GAS TURBINE ENGINESSeptember 2023April 2025Allow1900YesNo
18225089TURBINE ENGINE WITH CENTRIFUGAL COMPRESSOR HAVING IMPELLER BACKPLATE OFFTAKEJuly 2023June 2025Allow2210YesNo
18252119AIRCRAFT TURBINE ENGINE DRIVE LINE SHAFT COMPRISING A CONNECTING RING FOR DISASSEMBLING THE DRIVE LINEMay 2023May 2025Allow2410YesNo
18162964ENGINE SYSTEM AND METHOD OF OPERATING THE SAMEFebruary 2023March 2025Allow2520YesNo
18096178COMBINATION OF A GAS TURBINE ENGINE AND A POWER ELECTRONICSJanuary 2023June 2025Allow2960YesNo
18085728ELECTRIC MACHINE ASSEMBLYDecember 2022March 2025Allow2721YesNo
17896442CONTROLLING SOOTAugust 2022October 2024Allow2621YesNo
17889542METHOD AND APPARATUS FOR ENDWALL TREATMENTSAugust 2022January 2025Abandon2930NoNo
17869060COOLING AIR DELIVERY SYSTEM AND METHODS THEREOFJuly 2022February 2025Allow3130YesNo
17865908VARIABLE PITCH FAN THRUST REVERSERJuly 2022January 2025Abandon3030YesNo
17864851AIRCRAFT POWER PLANT WITH HYDROGEN TURBO-EXPANDERJuly 2022September 2024Abandon2721NoNo
17841175RESTARTING A PLURALITY OF ENGINES OF AN AIRCRAFT IN FLIGHTJune 2022April 2024Allow2220YesNo
17838167Pressure Drag Jet EngineJune 2022August 2024Allow2720YesNo
17836681MONITORING SYSTEMS FOR HYDROGEN FUELED AIRCRAFTJune 2022June 2025Abandon3640NoNo
17805986MULTI-TEMPERATURE FUEL INJECTORS FOR A GAS TURBINE ENGINEJune 2022October 2024Allow2841YesNo
17747960TURBINE ENGINE WITH CENTRIFUGAL COMPRESSOR HAVING IMPELLER BACKPLATE OFFTAKEMay 2022April 2023Allow1110YesNo
17663698THROUGH-FLOW GAS TURBINE ENGINE WITH ELECTRIC MOTOR AND ELECTRIC GENERATORMay 2022February 2023Allow901YesNo
17663079FLOW CONTROL WALL FOR HEAT ENGINEMay 2022June 2025Abandon3741YesNo
17658903COMBINED CYCLE PROPULSION SYSTEM FOR HYPERSONIC FLIGHTApril 2022November 2024Allow3141YesNo
17687769FUEL NOZZLE STRUCTURE FOR AIR ASSIST INJECTIONMarch 2022April 2024Allow2530YesNo
17556743SYSTEM AND METHOD FOR LOAD CONTROL WITH DIFFUSION COMBUSTION IN A STOICHIOMETRIC EXHAUST GAS RECIRCULATION GAS TURBINE SYSTEMDecember 2021January 2025Abandon3740YesNo
17554844EXHAUST SYSTEM FOR A GAS TURBINE ENGINE AND METHOD FOR USING SAMEDecember 2021December 2024Abandon3640YesNo
17550703SPALL PLATE FOR CONSUMABLE COMBUSTOR SUPPORT STRUCTURESDecember 2021September 2022Allow1000YesNo
17542900TRAPPED VORTEX COMBUSTOR FOR A GAS TURBINE ENGINE WITH A DRIVER AIRFLOW CHANNELDecember 2021June 2023Allow1820YesNo
17497152FUEL NOZZLE FOR GAS TURBINE ENGINE COMBUSTOROctober 2021September 2024Abandon3640YesNo
17494738HEAT EXCHANGEROctober 2021December 2024Allow3861YesNo
17479502ENGINE BLEED GENERATORS AND AIRCRAFT GENERATOR SYSTEMSSeptember 2021June 2023Allow2111YesNo
17469844REDUNDANT ELECTRICALLY DRIVEN FUEL AND OIL PUMPING SYSTEM FOR GAS TURBINESSeptember 2021September 2024Abandon3740YesNo
17469843ELECTRICALLY DRIVEN REDUNDANT FUEL AND OIL PUMPING SYSTEM FOR GAS TURBINE ENGINESSeptember 2021August 2024Abandon3640YesNo
17406690AIR MANIFOLDS FOR FUEL INJECTORS WITH FUEL AIR HEAT EXCHANGERSAugust 2021September 2023Abandon2420YesNo
17401647MODULAR CABIN BLOWER SYSTEM FOR AIRCRAFTAugust 2021December 2024Allow4041YesNo
17389144GAS TURBINE ENGINE STARTER SYSTEMS AND ASSOCIATED METHODSJuly 2021September 2023Abandon2620NoNo
17358169AIR TURBINE STARTER WITH PRIMARY AND SECONDARY AIR FLOW PATHSJune 2021December 2022Allow1810YesNo
17344185TURBOFAN ENGINE AND METHOD OF OPERATING SAMEJune 2021October 2022Allow1601YesNo
17342738HYBRID ELECTRIC IDLE TRANSITION FOR AIRCRAFTJune 2021November 2023Abandon2930NoNo
17342100Geared Architecture for High Speed and Small Volume Fan Drive TurbineJune 2021December 2022Allow1810YesNo
17330616GAS TURBINE ENGINE WITH IMPROVED DYNAMIC CHARACTERISTICSMay 2021May 2022Abandon1100NoNo
17297079TURBOFAN ENGINE COMPRISING AN OUTLET CONE COOLED BY ITS SECONDARY FLOWMay 2021November 2023Allow2910YesNo
17329501METHODS AND SYSTEMS FOR STARTING HYDROGEN POWERED GAS GENERATORSMay 2021January 2023Allow2011YesNo
17287487AIRCRAFT TURBINE ENGINE EQUIPPED WITH AN ELECTRICAL MACHINEMay 2021March 2024Allow3530YesNo
17321212RECUPERATIVE HEAT EXCHANGER SYSTEMMay 2021November 2024Allow4231YesNo
17321052TURBINE ENGINES HAVING HYDROGEN FUEL SYSTEMSMay 2021September 2024Abandon4140YesNo
17319439VARIABLE GEOMETRY INLET SYSTEMMay 2021January 2023Allow2020YesNo
17317199GAS TURBINE ENGINE STALL MARGIN MANAGEMENTMay 2021August 2024Abandon3940YesNo
17246382SWEEP FLOW STRUCTURES FOR FUEL SYSTEMSApril 2021May 2024Allow3731YesNo
17237439ELECTRONICS ENCLOSURE FOR GAS TURBINE ENGINEApril 2021May 2024Abandon3741YesNo
17231421NACELLE FOR GAS TURBINE ENGINEApril 2021June 2022Allow1410YesNo
17206433AIR TURBINE STARTER CONTAINMENT SYSTEMMarch 2021May 2023Abandon2621YesNo
17205242EXHAUST BAFFLE COMPONENT FOR AN AIR TURBINE STARTER ASSEMBLYMarch 2021August 2024Allow4151YesNo
17181566INTERNAL STRUCTURE OF A PRIMARY EXHAUST DUCT HAVING A SEPARATOR OF WHICH THE GEOMETRY VARIES DEPENDING ON THE TEMPERATUREFebruary 2021August 2022Allow1810YesNo
17181773Compact Low-Pressure CompressorFebruary 2021September 2022Allow1810YesNo
17170135COMPARTMENT UNIT FOR TURBINE ENGINEFebruary 2021October 2022Allow2050YesNo
17152139GAS TURBINE ENGINE COOLING SYSTEMJanuary 2021December 2022Allow2320YesNo
17142345STARTER ASSEMBLY AND METHODS FOR STARTING A COMBUSTION ENGINEJanuary 2021July 2022Allow1810YesNo
17129612GAS TURBINE ENGINE EXHAUST CHEVRONSDecember 2020December 2024Allow4841YesNo
17128080TURBINE ENGINE SYSTEM UTILIZING AN AUGMENTED COMBUSTION MODULEDecember 2020March 2022Allow1410YesNo
17101623STARTER TURBINE BEARING COMPARTMENT BUFFER AIRNovember 2020March 2023Abandon2820NoNo
17080361GAS TURBINE PROPULSION SYSTEMOctober 2020October 2022Allow2431YesYes
17071018UNDUCTED SINGLE ROTOR ENGINE AND METHOD FOR OPERATIONOctober 2020February 2025Allow5260YesNo
17032477GAS TURBINE ENGINESeptember 2020March 2024Abandon4241YesNo
17018795TAIL CONE EJECTOR FOR POWER CABLE COOLING SYSTEM IN A GAS TURBINE ENGINESeptember 2020October 2022Allow2611YesNo
17014051SPLIT COMPRESSOR GAS TURBINE ENGINESeptember 2020April 2024Abandon4341NoNo
16976218METHOD AND CONTROL UNIT FOR CONTROLLING THE PLAY OF A HIGH-PRESSURE TURBINEAugust 2020December 2022Allow2820YesNo
16971566TWO-SHAFT GAS TURBINE POWER GENERATION FACILITY, CONTROL DEVICE THEREFOR, AND CONTROL METHOD THEREFORAugust 2020December 2021Allow1600YesNo
16970815TURBINE ENGINE COMPRISING A HEAT EXCHANGER IN THE SECONDARY PATHAugust 2020February 2023Allow3020YesNo
16990688MULTISTAGE INFRARED SUPPRESSION EXHAUST SYSTEMAugust 2020December 2022Allow2831YesNo
16940538GEARED GAS TURBINE ENGINE WITH GEAR DRIVING LOW PRESSURE COMPRESSOR AND FAN AT A COMMON SPEED AND A SHEAR SECTION TO PROVIDE OVERSPEED PROTECTIONJuly 2020March 2022Allow1910YesNo
16902433FUEL STAGING SYSTEMJune 2020April 2022Allow2220YesNo
16772480VARIABLE AREA FAN NOZZLE FOR TURBOFAN AIRCRAFT ENGINEJune 2020March 2022Allow2120YesNo
16899337CLOSED-LOOP CONTROLLED AIR TURBINE START SYSTEMJune 2020August 2022Abandon2620NoNo
16771813PORTION OF A FLUID DRAINAGE CONDUIT FOR A TURBOMACHINEJune 2020April 2022Allow2211YesNo
16897776THROUGH-FLOW GAS TURBINE ENGINE WITH ELECTRIC MOTOR AND ELECTRIC GENERATORJune 2020March 2022Allow2111YesNo
16891492SPLITTER AND GUIDE VANE ARRANGEMENT FOR GAS TURBINE ENGINESJune 2020June 2023Allow3620YesNo
16857055PLUMBING WITH INTERNAL FLOW GUIDESApril 2020March 2022Allow2211YesNo
16852856SYSTEM AND METHOD FOR CONTROLLING ENGINE SPEED WITH BOWED ROTOR MITIGATIONApril 2020February 2022Allow2210YesNo
16849508INERTIAL PARTICLE SEPARATOR FOR TURBINE ENGINEApril 2020August 2021Allow1600YesNo
16843349DYNAMIC THERMAL LOAD MONITORING AND MITIGATION FOR AIRCRAFT SYSTEMSApril 2020April 2022Allow2411YesNo
16754076METHOD FOR THE CONTROL OF THE ANTI-ICING SYSTEM OF THE AIRCRAFT GAS TURBINE ENGINEApril 2020July 2022Abandon2820NoNo
16824171TURBINE ENGINE WITH CENTRIFUGAL COMPRESSOR HAVING IMPELLER BACKPLATE OFFTAKEMarch 2020February 2022Allow2300YesNo
16818995SYSTEM AND METHOD FOR ENGINE PRE-SHUTDOWN MOTORINGMarch 2020October 2023Abandon4330YesNo
16781424STAGGERED HEAT EXCHANGER ARRAY WITH SIDE CURTAINSFebruary 2020April 2022Allow2620YesNo
16774221GAS TURBINE ENGINE WITH CLUTCH SYSTEM BETWEEN LOW-PRESSURE COMPRESSOR AND LOW-PRESSURE TURBINEJanuary 2020January 2023Allow3621YesNo
16745312ANTI-ICING SYSTEM HAVING A NOZZLE WITH A DEFLECTOR PLATE AND METHODJanuary 2020March 2022Allow2611YesNo
16629418Hydraulic SystemJanuary 2020August 2021Allow1901YesNo
16725177AIR TURBINE STARTER AIR VALVEDecember 2019October 2021Allow2210YesNo
16693430SPARK PLUG ASSEMBLIES FOR TURBOMACHINESNovember 2019May 2024Allow5431YesNo
16678682LIQUID AIR POWER AND STORAGENovember 2019May 2024Abandon5540NoNo
16609557INTAKE DUCT FOR A GAS-FUELLED OR DIESEL-FUELLED TURBINE EQUIPPED WITH A WATER SATURATION STRUCTUREOctober 2019October 2022Allow3621YesNo
16661677AIR TURBINE START SYSTEMOctober 2019November 2021Abandon2510NoNo
16656262SCAVENGE METHODOLOGIES FOR TURBINE ENGINE PARTICLE SEPARATION CONCEPTSOctober 2019April 2022Allow3011YesNo
16654436Turbine Powered Electricity GenerationOctober 2019March 2024Allow5361YesYes
16654706GAS TURBINE ENGINE WITH REVERSIBLE HEAT EXCHANGEROctober 2019January 2022Allow2711YesNo
16600942FLEXIBLE SEAL FOR GAS TURBINE ENGINEOctober 2019October 2021Allow2401YesNo
16593746ELECTRIC PUMP ASSISTED FUEL SYSTEMOctober 2019August 2024Abandon5841YesNo
16590430METHOD OF REPLACING A FAN MODULE, ENGINE CORE MODULE, OR FAN CASE MODULE IN A GAS TURBINE ENGINEOctober 2019February 2021Allow1721YesNo
16586016FUEL NOZZLE STRUCTURE FOR AIR ASSIST INJECTIONSeptember 2019December 2021Allow2611YesNo
16577649SPALL PLATE FOR CONSUMABLE COMBUSTOR SUPPORT STRUCTURESSeptember 2019September 2021Allow2401YesNo
16574946TURBOMACHINE FITTED WITH A THERMO-ACOUSTIC SYSTEMSeptember 2019December 2021Allow2711YesNo
16573013INERTIAL PARTICLE SEPARATOR FOR AIRCRAFT ENGINESeptember 2019January 2022Allow2801YesNo

Appeals Overview

This analysis examines appeal outcomes and the strategic value of filing appeals for examiner SEBASCO CHENG, STEPHANIE.

Patent Trial and Appeal Board (PTAB) Decisions

Total PTAB Decisions
12
Examiner Affirmed
11
(91.7%)
Examiner Reversed
1
(8.3%)
Reversal Percentile
21.3%
Lower than average

What This Means

With a 8.3% 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
20
Allowed After Appeal Filing
3
(15.0%)
Not Allowed After Appeal Filing
17
(85.0%)
Filing Benefit Percentile
15.6%
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, 15.0% 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

Appeals to PTAB face challenges. Ensure your case has strong merit before committing to full Board review.

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

Examiner SEBASCO CHENG, STEPHANIE - Prosecution Strategy Guide

Executive Summary

Examiner SEBASCO CHENG, STEPHANIE works in Art Unit 3741 and has examined 316 patent applications in our dataset. With an allowance rate of 62.7%, this examiner allows applications at a lower rate than most examiners at the USPTO. Applications typically reach final disposition in approximately 32 months.

Allowance Patterns

Examiner SEBASCO CHENG, STEPHANIE's allowance rate of 62.7% places them in the 16% percentile among all USPTO examiners. This examiner is less likely to allow applications than most examiners at the USPTO.

Office Action Patterns

On average, applications examined by SEBASCO CHENG, STEPHANIE receive 2.37 office actions before reaching final disposition. This places the examiner in the 81% percentile for office actions issued. This examiner issues more office actions than most examiners, which may indicate thorough examination or difficulty in reaching agreement with applicants.

Prosecution Timeline

The median time to disposition (half-life) for applications examined by SEBASCO CHENG, STEPHANIE is 32 months. This places the examiner in the 33% percentile for prosecution speed. Prosecution timelines are slightly slower than average with this examiner.

Interview Effectiveness

Conducting an examiner interview provides a +74.0% benefit to allowance rate for applications examined by SEBASCO CHENG, STEPHANIE. This interview benefit is in the 99% 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, 22.1% of applications are subsequently allowed. This success rate is in the 19% percentile among all examiners. Strategic Insight: RCEs show lower effectiveness with this examiner compared to others. Consider whether a continuation application might be more strategic, especially if you need to add new matter or significantly broaden claims.

After-Final Amendment Practice

This examiner enters after-final amendments leading to allowance in 14.2% of cases where such amendments are filed. This entry rate is in the 9% percentile among all examiners. Strategic Recommendation: This examiner rarely enters after-final amendments compared to other examiners. You should generally plan to file an RCE or appeal rather than relying on after-final amendment entry. Per MPEP § 714.12, primary examiners have discretion in entering after-final amendments, and this examiner exercises that discretion conservatively.

Pre-Appeal Conference Effectiveness

When applicants request a pre-appeal conference (PAC) with this examiner, 100.0% result in withdrawal of the rejection or reopening of prosecution. This success rate is in the 75% 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 42.9% of appeals filed. This is in the 6% percentile among all examiners. Of these withdrawals, 33.3% 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, 22.7% are granted (fully or in part). This grant rate is in the 13% percentile among all examiners. Strategic Note: Petitions are rarely granted regarding this examiner's actions compared to other examiners. Ensure you have a strong procedural basis before filing a petition, as the Technology Center Director typically upholds this examiner's decisions.

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 2.0% of allowed cases (in the 65% 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:

  • Prepare for rigorous examination: With a below-average allowance rate, ensure your application has strong written description and enablement support. Consider filing a continuation if you need to add new matter.
  • Expect multiple rounds of prosecution: This examiner issues more office actions than average. Address potential issues proactively in your initial response and consider requesting an interview early in prosecution.
  • 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.
  • Plan for RCE after final rejection: This examiner rarely enters after-final amendments. Budget for an RCE in your prosecution strategy if you receive a final rejection.

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.