USPTO Examiner THOMAS KYLE ROBERT - Art Unit 3741

Recent Applications

Detailed information about the 100 most recent patent applications.

Application NumberTitleFiling DateDisposal DateDispositionTime (months)Office ActionsRestrictionsInterviewAppeal
19277730GAS TURBINE ENGINE HAVING A THRUST REVERSER SYSTEM WITH DRAG LINK CONNECTORS AT INTER-COMPRESSOR FRAME STRUCTUREJuly 2025October 2025Allow300NoNo
19213938AIRCRAFT ENGINE ENTRAINED PARTICLE REMOVAL SYSTEM AND METHODMay 2025October 2025Allow500NoNo
19209005DIFFUSERS, GAS TURBINE ENGINES COMPRISING THE SAME, AND METHODS FOR OPERATION THEREOFMay 2025August 2025Allow300NoNo
19203919FAN BLADE ASSEMBLY WITH LEADING EDGE FILLETMay 2025September 2025Allow400NoNo
19201178SUPERCHARGED COMBUSTOR COOLING USING TURBOMACHINERYMay 2025October 2025Allow500NoNo
19175700TURBOMACHINE POWER AUGMENTATION FEATURES AND METHODSApril 2025November 2025Allow700YesNo
19169657TURBOMACHINE FOR A FLIGHT PROPULSION DRIVEApril 2025March 2026Abandon1110NoNo
19093578Air-Breathing Plasma ThrusterMarch 2025August 2025Allow400NoNo
19089168HYDROGEN FUELLED AIRCRAFT PROPULSION SYSTEMMarch 2025June 2025Allow200NoNo
19080369UNITARY CASE INTEGRATED FLOW SCOOPSMarch 2025August 2025Allow500YesNo
19041620Electron Propulsion Engine and Method of Operation ThereofJanuary 2025June 2025Allow400NoNo
19038327ROCKET ENGINE WITH DUAL CONTOUR NOZZLEJanuary 2025October 2025Allow910NoNo
19031064TRANSPIRATION-COOLED SYSTEMS HAVING PERMEABLE AND NON-PERMEABLE PORTIONSJanuary 2025January 2026Allow1210YesNo
18949069NUCLEAR THERMAL PROPULSION SYSTEM WITH REACTOR DIRECT DRIVE OF CRYOCOOLER TURBINENovember 2024March 2025Allow400NoNo
18856612HYDROGEN STORAGE POWER PLANT, AND METHOD FOR OPERATING SAMEOctober 2024November 2025Allow1310NoNo
18913593TRANSPIRATION-COOLED SYSTEMS HAVING PERMEABLE AND NON-PERMEABLE PORTIONSOctober 2024January 2026Allow1610YesNo
18904352GAS TURBINE ENGINEOctober 2024August 2025Allow1010NoNo
18904832INLET BLEED DIVERSION THROUGH ROTATING DETONATION ROCKET ENGINEOctober 2024November 2025Allow1310NoNo
18886348TURBINE ENGINE HAVING A COMBUSTION SECTIONSeptember 2024July 2025Allow1010NoNo
18846327LUBRICATION AND COOLING OF EQUIPMENT OF AN AIRCRAFT TURBOMACHINESeptember 2024May 2025Allow800YesNo
18845814NOZZLE ASSEMBLY WITH A CENTRAL FUEL PIPE THAT IS SEALED AGAINST AN IN-FLOW OF AIRSeptember 2024November 2025Allow1410YesNo
18845796NOZZLE ASSEMBLY HAVING SWIRL-FREE AIR AND HYDROGEN INFLOWSeptember 2024October 2025Allow1310NoNo
18805867AIR RECUPERATED ENGINE WITH AIR REINJECTIONAugust 2024April 2025Allow810YesNo
18806257REUSABLE UPPER STAGE ROCKETAugust 2024December 2025Allow1610NoNo
18838100TURBOMACHINE FOR AN AIRCRAFTAugust 2024March 2025Allow700NoNo
18786333MULTI-MODE ROCKET-BASED COMBINED CYCLEJuly 2024March 2025Allow810YesNo
18774773INTEGRATED VEHICLE FLUIDS WITH HOT GAS LINE AND COLD GAS LINE MERGING TO INCREASE ENTHALPYJuly 2024January 2025Allow600NoNo
18768015ACTUATION MECHANISMJuly 2024February 2025Allow800NoNo
18749428OMNIVOROUS SOLAR THERMAL THRUSTER, COOLING SYSTEMS, AND THERMAL ENERGY TRANSFER IN ROCKETSJune 2024July 2025Allow1310NoNo
18736958COMBUSTOR FOR A TURBINE ENGINE INCLUDING AN INSULATING MEMBERJune 2024March 2026Allow2121YesNo
18734472SYSTEM AND METHOD FOR BLENDING MULTIPLE FUELSJune 2024April 2025Allow1010YesNo
18714334ASSEMBLY FOR AN EJECTION CONE OF AN AIRCRAFT TURBOMACHINEMay 2024August 2025Allow1410NoNo
18677659GAS TURBINE PLANT WITH AMMONIA DECOMPOSITION SYSTEMMay 2024November 2025Allow1711YesNo
18639030METHOD AND APPARATUS FOR REDUCING CONSEQUENCES OF A BULKHEAD FAILURE FOR A LIQUID METHANE AND LIQUID OXYGEN ROCKETApril 2024June 2024Allow200NoNo
18638449ROCKET ENGINE WITH DUAL CONTOUR NOZZLEApril 2024September 2024Allow500YesNo
18635986PASSIVE BYPASS FOR MITIGATION OF INLET BUZZ IN SUPERSONIC OR HYPERSONIC AIR-BREATHING ENGINESApril 2024October 2024Allow600YesNo
18634822RAMJET PROPULSION METHODApril 2024March 2025Allow1110YesNo
18632124NUCLEAR THERMAL PROPULSION SYSTEM WITH REACTOR DIRECT DRIVE OF CRYOCOOLER TURBINEApril 2024August 2024Allow400NoNo
18625769TURBINE OVERSPEED PROTECTIONApril 2024April 2025Allow1310NoNo
18621655IGNITION DEVICE, METHOD FOR PRODUCING THE SAME, IGNITION METHOD AND ROCKET COMBUSTION SYSTEMMarch 2024January 2026Allow2220YesNo
18619703GAS TURBINE ENGINE WITH HEAT EXCHANGER ASSEMBLYMarch 2024October 2025Allow1910NoNo
18608517VEHICLE FIRE-EXTINGUISHING AND PASSENGER-COOLING DEVICEMarch 2024December 2025Allow2100NoNo
18599516Vehicle Comprising Battery Device and Fire Extinguishing Agent TankMarch 2024January 2026Allow2310NoNo
18598211UPRIGHT SPRINKLER AND A SPRINKLER SYSTEMMarch 2024October 2025Allow1900NoNo
18588257DE-ICE SYSTEM AND APPARATUS FOR TURBINE ENGINESFebruary 2024November 2024Allow810NoNo
18581297ADDITIVELY MANUFACTURED ROCKET FUEL GRAINS AND COMPETITIVE SIMULATION OF THE SAMEFebruary 2024July 2024Allow500NoNo
18444483DETONATION PRE-COMBUSTORSFebruary 2024August 2025Abandon1830NoNo
18436698Air Turbine Starter With DecouplerFebruary 2024December 2024Allow1000NoNo
18436180GAS TURBINE ENGINE HAVING A COMBUSTION SECTION WITH STEAM PROVIDED TO SECOND COMBSUTOR PLENUMFebruary 2024January 2025Allow1100NoNo
18681099SINGLE STAGE TO ORBIT ROCKET ENGINEFebruary 2024August 2024Allow700NoNo
18421427WARM GAS THRUSTER SYSTEM WITH CONTROL VALVE THAT HAS A SOFT SEALJanuary 2024June 2025Allow1710YesNo
18291406OXY-COMBUSTION COMBINED CYCLE POWER PLANTSJanuary 2024October 2025Allow2130YesNo
18419876POWER SWITCHING SYSTEM OF AN ANTI-ICE SYSTEM FOR USE WITH A MAIN POWER SUPPLY AND AN AUXILIARY POWER SUPPLYJanuary 2024February 2025Allow1300NoNo
18411832VARIABLE AREA NOZZLE FOR AN AIRCRAFT ENGINEJanuary 2024July 2024Allow600YesNo
18396488ANNULAR VORTEX TANK VALVE FOR ROCKET MOTOR AND CONFIGURATION IN A ROCKETDecember 2023May 2024Allow400YesNo
18390927TRANSPIRATION-COOLED SYSTEMS HAVING PERMEABLE AND NON-PERMEABLE PORTIONSDecember 2023September 2024Allow900YesNo
18543739CENTRIFUGAL FORCE PROPULSION DEVICEDecember 2023November 2024Allow1101YesNo
18527491INJECTOR WITH INJECTOR ELEMENTS IN CIRCUMFERENTIAL ROWS THAT ALTERNATE BETWEEN COUNTER-CLOCKWISE AND CLOCKWISE SWIRLDecember 2023February 2026Allow2620NoNo
18565461THRUST REVERSER ASSEMBLY FOR A TURBOJET ENGINENovember 2023June 2024Allow700YesNo
18518558Electrically Powered Supersonic and Hypersonic PropulsorNovember 2023January 2025Allow1310YesNo
18510495ROCKET INJECTOR SUBSCALE STABILITY ASSESSMENT WITH TELESCOPING PISTONNovember 2023June 2025Allow1920YesNo
18510359ROCKET INJECTOR SUBSCALE STABILITY ASSESSMENT WITH TELESCOPING THROAT OR MOVEABLE INJECTOR PLATENovember 2023July 2025Allow2020YesNo
18558800PROPULSION SYSTEM FOR A VEHICLE USING HEAT ENERGY ABSORBED IN AN ACTIVE COOLING SYSTEMNovember 2023February 2025Allow1610YesNo
18501983SYSTEM AND METHOD FOR ASYNCHRONOUS AUTOGENOUSLY PRESSURIZED IN-SPACE PROPULSIONNovember 2023April 2024Allow500NoNo
18497442MULTIMODE PROPULSION SYSTEMOctober 2023August 2024Allow1010NoNo
18384659MODULAR INJECTOR BOLT FOR AN ENGINEOctober 2023November 2025Allow2530YesNo
18493479OIL NOZZLE FOR BEARING CHAMBEROctober 2023November 2025Allow2410NoNo
18380892SYSTEM AND METHOD OF GRAIN IGNITION AND INHIBITOR RELEASE USING PHASE ALLOY FILMSOctober 2023October 2024Allow1210YesNo
18483106AIRCRAFT ENGINE FUEL SYSTEMOctober 2023November 2024Allow1410NoNo
18377151SERIAL ROTATING DETONATION COMBUSTOR SYSTEMSOctober 2023February 2025Allow1711YesNo
18480471Bobbin-Form Solid Controlled and Filament Fed Hybrid Propulsion Methods for Space Vehicle Innovative ArchitecturesOctober 2023March 2025Abandon1810NoNo
18374941Air-Breathing Plasma ThrusterSeptember 2023February 2025Allow1710NoNo
18284639A PUMPING APPARATUSSeptember 2023April 2025Allow1810NoNo
18477507QUICK-FILL LAVAGE SYSTEMSeptember 2023March 2026Allow2900NoNo
18471881HEAVY INERT GAS INSULATED BLAST TUBESeptember 2023April 2024Allow710NoNo
18457301AFTERBURNING TURBINE EXHAUST CYCLE (ABTEC)August 2023February 2024Allow610YesNo
18457283DUAL MODE ROCKET ENGINE WITH BIPROPELLANT INJECTION IN THE NOZZLEAugust 2023March 2024Allow600YesNo
18278463ROCKET PROPULSION SYSTEMAugust 2023September 2024Abandon1310NoNo
18264992ROCKET MOTORAugust 2023October 2025Allow2610YesNo
18365767DETONATION OF UN-DECOMPOSED LIQUID OXIDIZER IN A ROCKET ENGINEAugust 2023August 2024Allow1230NoNo
18228649INTEGRATED AUXILIARY COMPRESSORS FOR COOLING IN GAS TURBINE ENGINESJuly 2023February 2025Abandon1920NoNo
18274999TRANSITION WITH UNEVEN SURFACEJuly 2023November 2024Abandon1510NoNo
18262685LIQUID PROPELLANT GASIFIER AND PRESSURIZERJuly 2023April 2025Allow2000NoNo
18356394Recoverable Rocket and an Associated Recovery MethodJuly 2023October 2024Allow1510NoNo
18223433SAFETY IGNITION DEVICE FOR HIGH ALTITUDE DUAL PULSE MOTOR INCLUDING THE SAMEJuly 2023January 2024Allow610YesNo
18353342GAS TURBINE OVERSPEED PROTECTION METHOD AND APPARATUS, ELECTRONIC DEVICE AND STORAGE MEDIUMJuly 2023November 2024Allow1610YesNo
18353487NOZZLE DEVICE FOR FEEDING FUEL INTO A COMBUSTION CHAMBER OF A GAS TURBINE ASSEMBLY, AND GAS TURBINE ASSEMBLYJuly 2023May 2024Allow1010NoNo
18271834AEROSPIKE ENGINES, LAUNCH VEHICLES INCORPORATING SUCH ENGINES AND METHODSJuly 2023January 2025Abandon1820NoNo
18349285ROTOR BOW MITIGATIONJuly 2023October 2024Allow1510NoNo
18217228PRE-HEATING AIRCRAFT ENGINE IN STANDBY MODEJune 2023June 2024Allow1100YesNo
18270301SEALING MEMBER AND GAS TURBINEJune 2023April 2024Allow1000YesNo
18211277STAGED COMBUSTION LIQUID ROCKET ENGINE CYCLE WITH THE TURBOPUMP UNIT AND PREBURNER INTEGRATED INTO THE STRUCTURE OF THE COMBUSTION CHAMBERJune 2023December 2023Allow600YesNo
18335340SYSTEM AND METHOD FOR EFFICIENTLY DETERMINING A PHASE SHIFT IN A PROPULSION SYSTEMJune 2023April 2025Allow2220NoNo
18195179VAPOR RETENTION DEVICEMay 2023May 2024Allow1210NoNo
18033428DESIGN AND MANUFACTURING OF A SINGLE PIECE ROCKET ENGINEApril 2023April 2025Allow2430YesNo
18304575FLAMMABLE FLUID RESERVOIRApril 2023October 2024Allow1810NoNo
18133124INTEGRATED VEHICLE FLUIDS FOR UPPER STAGE LAUNCH VEHICLE WITH INTERNAL COMBUSTION ENGINEApril 2023September 2023Allow500YesNo
18133134INTEGRATED VEHICLE FLUIDSApril 2023December 2023Allow900YesNo
18133111INTEGRATED VEHICLE FLUIDSApril 2023March 2024Allow1110NoNo
18130683COMBUSTOR WITH FUEL AND AIR MIXING PLENUMApril 2023December 2024Allow2030YesNo

Appeals Overview

This analysis examines appeal outcomes and the strategic value of filing appeals for examiner THOMAS, KYLE ROBERT.

Patent Trial and Appeal Board (PTAB) Decisions

Total PTAB Decisions
17
Examiner Affirmed
12
(70.6%)
Examiner Reversed
5
(29.4%)
Reversal Percentile
46.1%
Lower than average

What This Means

With a 29.4% reversal rate, the PTAB affirms the examiner's rejections in the vast majority of cases. This reversal rate is below the USPTO average, indicating that appeals face more challenges here than typical.

Strategic Value of Filing an Appeal

Total Appeal Filings
26
Allowed After Appeal Filing
6
(23.1%)
Not Allowed After Appeal Filing
20
(76.9%)
Filing Benefit Percentile
31.4%
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, 23.1% of applications that filed an appeal were subsequently allowed. This appeal filing benefit rate is below the USPTO average, suggesting that filing an appeal has limited effectiveness in prompting favorable 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 shows limited benefit. Consider other strategies like interviews or amendments before appealing.

Examiner THOMAS, KYLE ROBERT - Prosecution Strategy Guide

Executive Summary

Examiner THOMAS, KYLE ROBERT works in Art Unit 3741 and has examined 282 patent applications in our dataset. With an allowance rate of 68.8%, this examiner has a below-average tendency to allow applications. Applications typically reach final disposition in approximately 34 months.

Allowance Patterns

Examiner THOMAS, KYLE ROBERT's allowance rate of 68.8% places them in the 31% percentile among all USPTO examiners. This examiner has a below-average tendency to allow applications.

Office Action Patterns

On average, applications examined by THOMAS, KYLE ROBERT receive 2.33 office actions before reaching final disposition. This places the examiner in the 66% 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 THOMAS, KYLE ROBERT is 34 months. This places the examiner in the 45% percentile for prosecution speed. Prosecution timelines are slightly slower than average with this examiner.

Interview Effectiveness

Conducting an examiner interview provides a +40.6% benefit to allowance rate for applications examined by THOMAS, KYLE ROBERT. This interview benefit is in the 88% 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, 23.5% of applications are subsequently allowed. This success rate is in the 32% 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 19.3% of cases where such amendments are filed. This entry rate is in the 23% 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, 88.9% result in withdrawal of the rejection or reopening of prosecution. This success rate is in the 67% 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 46.9% of appeals filed. This is in the 12% percentile among all examiners. Of these withdrawals, 26.7% 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, 38.9% are granted (fully or in part). This grant rate is in the 28% 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 0.0% of allowed cases (in the 43% 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 0.0% of allowed cases (in the 47% 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:

  • 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.