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
18949069NUCLEAR THERMAL PROPULSION SYSTEM WITH REACTOR DIRECT DRIVE OF CRYOCOOLER TURBINENovember 2024March 2025Allow400NoNo
18846327LUBRICATION AND COOLING OF EQUIPMENT OF AN AIRCRAFT TURBOMACHINESeptember 2024May 2025Allow800YesNo
18805867AIR RECUPERATED ENGINE WITH AIR REINJECTIONAugust 2024April 2025Allow810YesNo
18838100TURBOMACHINE FOR AN AIRCRAFTAugust 2024March 2025Allow700NoNo
18774773INTEGRATED VEHICLE FLUIDS WITH HOT GAS LINE AND COLD GAS LINE MERGING TO INCREASE ENTHALPYJuly 2024January 2025Allow600NoNo
18768015ACTUATION MECHANISMJuly 2024February 2025Allow800NoNo
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
18588257DE-ICE SYSTEM AND APPARATUS FOR TURBINE ENGINESFebruary 2024November 2024Allow810NoNo
18581297ADDITIVELY MANUFACTURED ROCKET FUEL GRAINS AND COMPETITIVE SIMULATION OF THE SAMEFebruary 2024July 2024Allow500NoNo
18436698Air Turbine Starter With DecouplerFebruary 2024December 2024Allow1000NoNo
18681099SINGLE STAGE TO ORBIT ROCKET ENGINEFebruary 2024August 2024Allow700NoNo
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
18565461THRUST REVERSER ASSEMBLY FOR A TURBOJET ENGINENovember 2023June 2024Allow700YesNo
18518558Electrically Powered Supersonic and Hypersonic PropulsorNovember 2023January 2025Allow1310YesNo
18510359ROCKET INJECTOR SUBSCALE STABILITY ASSESSMENT WITH TELESCOPING THROAT OR MOVEABLE INJECTOR PLATENovember 2023July 2025Allow2020YesNo
18510495ROCKET INJECTOR SUBSCALE STABILITY ASSESSMENT WITH TELESCOPING PISTONNovember 2023June 2025Allow1920YesNo
18501983SYSTEM AND METHOD FOR ASYNCHRONOUS AUTOGENOUSLY PRESSURIZED IN-SPACE PROPULSIONNovember 2023April 2024Allow500NoNo
18558800PROPULSION SYSTEM FOR A VEHICLE USING HEAT ENERGY ABSORBED IN AN ACTIVE COOLING SYSTEMNovember 2023February 2025Allow1610YesNo
18497442MULTIMODE PROPULSION SYSTEMOctober 2023August 2024Allow1010NoNo
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
18471881HEAVY INERT GAS INSULATED BLAST TUBESeptember 2023April 2024Allow710NoNo
18457283DUAL MODE ROCKET ENGINE WITH BIPROPELLANT INJECTION IN THE NOZZLEAugust 2023March 2024Allow600YesNo
18457301AFTERBURNING TURBINE EXHAUST CYCLE (ABTEC)August 2023February 2024Allow610YesNo
18278463ROCKET PROPULSION SYSTEMAugust 2023September 2024Abandon1310NoNo
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
18133134INTEGRATED VEHICLE FLUIDSApril 2023December 2023Allow900YesNo
18133111INTEGRATED VEHICLE FLUIDSApril 2023March 2024Allow1110NoNo
18133124INTEGRATED VEHICLE FLUIDS FOR UPPER STAGE LAUNCH VEHICLE WITH INTERNAL COMBUSTION ENGINEApril 2023September 2023Allow500YesNo
18130683COMBUSTOR WITH FUEL AND AIR MIXING PLENUMApril 2023December 2024Allow2030YesNo
18129245ROCKET PROPULSION SYSTEMS AND ASSOCIATED METHODSMarch 2023October 2023Allow700YesNo
18193005TRANSPIRATION-COOLED SYSTEMS HAVING PERMEABLE AND NON-PERMEABLE PORTIONSMarch 2023July 2024Allow1620YesNo
18192875FEED SYSTEM FOR ROCKET ENGINEMarch 2023March 2024Abandon1210NoNo
18191181SPARK IGNITER WITH MAGNETIC FIELD FOR PUSHING SPARKMarch 2023August 2024Allow1710NoNo
18186347METHOD AND SYSTEM FOR DE-PRIMING AN AIRCRAFT ENGINE COMPONENT CONTAINING A FLAMMABLE FLUID FOR FIRE SAFETYMarch 2023August 2024Allow1701YesNo
18118606AIRBREATHING PROPULSION ENGINES INCLUDING ROTATING DETONATION AND BLUFF BODY SYSTEMSMarch 2023April 2024Allow1310NoNo
18117403INTEGRATED PROPULSION SYSTEM FOR HYBRID ROCKETSMarch 2023August 2023Allow500NoNo
18040444AIRCRAFTFebruary 2023January 2024Allow1210NoNo
18103460VORTEX HYBRID ROCKET MOTORJanuary 2023April 2024Allow1520YesNo
18100130Aircraft Heat ExchangersJanuary 2023January 2024Allow1210YesNo
181526783D-PRINTED CATALYST BEDJanuary 2023November 2023Allow1020NoNo
18004577METHOD FOR STARTING AN AIRCRAFT ENGINEJanuary 2023May 2025Allow2840YesNo
18094300REACTION CONTROL VORTEX THRUSTER SYSTEMJanuary 2023October 2023Allow910NoNo
18085925CATALYTIC DECOMPOSITION REACTORSDecember 2022May 2025Allow2921YesNo
17972680COMBUSTOR FOR ROCKET ENGINE AND METHOD FOR MANUFACTURING ITOctober 2022July 2024Allow2120YesNo
17967941ELECTRIC PROPULSION BASED SPACECRAFT PROPULSION SYSTEMS AND METHODS UTILIZING MULTIPLE PROPELLANTSOctober 2022January 2024Allow1510YesNo
18046790ROCKET ENGINE WITH DUAL CONTOUR NOZZLEOctober 2022February 2024Allow1620YesNo
17951972AIR RECUPERATED ENGINE WITH AIR REINJECTIONSeptember 2022April 2024Allow1920YesNo
17948870EXHAUST NOZZLE ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEMSeptember 2022May 2024Allow2020YesNo
17944790CANTILEVERED AIRFOILS AND METHODS OF FORMING THE SAMESeptember 2022May 2024Allow2020YesNo
17930741METHOD FOR REDUCING JET TAB EXPOSURE DURING THRUST VECTORINGSeptember 2022November 2023Allow1410YesNo
17802468TWO-STAGE LOW-POWER AND HIGH-THRUST TO POWER ELECTRIC PROPULSION SYSTEMAugust 2022March 2024Allow1810YesNo
17820512REACTOR ROCKET ENGINEAugust 2022August 2023Allow1110YesNo
17889066Air Turbine Starter With DecouplerAugust 2022November 2023Allow1510NoNo
17878531THRUST REVERSER CASCADE WITH ONE OR MORE FLOW DISRUPTERSAugust 2022December 2024Allow2840YesNo
17878497THRUST REVERSER CASCADE WITH ONE OR MORE FLOW STABILIZERSAugust 2022August 2023Allow1310YesNo
17813312OMNIVOROUS SOLAR THERMAL THRUSTER, COOLING SYSTEMS, AND THERMAL ENERGY TRANSFER IN ROCKETSJuly 2022February 2024Allow1910YesNo
17808256NUCLEAR THERMAL PROPULSION SYSTEM WITH REACTOR DIRECT DRIVE OF CRYOCOOLER TURBINEJune 2022December 2023Allow1810YesNo
17840715DESCENT OPERATION FOR AN AIRCRAFT PARALLEL HYBRID GAS TURBINE ENGINE PROPULSION SYSTEMJune 2022November 2023Allow1710YesNo
17836835ROCKET ENGINE WITH POROUS STRUCTUREJune 2022December 2024Abandon3141YesNo
17740958LIQUID ROCKET ENGINE TAP-OFF POWER SOURCEMay 2022March 2023Allow1010NoNo
17740111ACTIVE ON ORBIT FLUID PROPELLANT MANAGEMENT AND REFUELING SYSTEMS AND METHODSMay 2022October 2023Allow1810YesNo
17770156VALVE TIMING SYSTEM FOR LIQUID FUEL ROCKETSApril 2022March 2024Allow2300NoNo
17769753HYBRID PROPULSION UNIT FOR SPACE VEHICLEApril 2022February 2025Allow3430NoNo
17754787Augmented Aerospike Nozzle, Engine Including the Augmented Aerospike Nozzle, and Vehicle Including the EngineApril 2022April 2024Allow2410YesNo
17715416PROPULSION ASSEMBLY FOR A ROCKETApril 2022April 2024Abandon2420NoNo
17683014INTEGRATED VEHICLE FLUIDSFebruary 2022July 2023Allow1610YesNo
17651936Motor And Fuel-Powered Hybrid System for a Rocket ThrusterFebruary 2022January 2023Allow1100YesNo
17666612EXPENDABLE MULTISTAGE PRESSURE-FED ABLATIVE-COOLING NONTOXIC NON-HEAVY LAUNCH VEHICLEFebruary 2022January 2024Abandon2420NoNo
17618231TANK FOR CONTAINING A COMPONENT FLUID, SUCH AS A PROPELLANTDecember 2021December 2024Allow3701YesNo
17544220LIQUID-COOLED AIR-BREATHING ROCKET ENGINEDecember 2021February 2023Allow1410YesNo
17539479MULTI-STAGE PROPELLANT SYSTEMS, ASSEMBLIES, AND METHODSDecember 2021October 2023Allow2220YesNo

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
13
Examiner Affirmed
9
(69.2%)
Examiner Reversed
4
(30.8%)
Reversal Percentile
46.8%
Lower than average

What This Means

With a 30.8% reversal rate, the PTAB reverses the examiner's rejections in a meaningful percentage 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
21
Allowed After Appeal Filing
5
(23.8%)
Not Allowed After Appeal Filing
16
(76.2%)
Filing Benefit Percentile
29.1%
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, 23.8% 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 357 patent applications in our dataset. With an allowance rate of 73.1%, this examiner has a below-average tendency to allow applications. Applications typically reach final disposition in approximately 30 months.

Allowance Patterns

Examiner THOMAS, KYLE ROBERT's allowance rate of 73.1% places them in the 29% 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 2.03 office actions before reaching final disposition. This places the examiner in the 67% 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 30 months. This places the examiner in the 44% percentile for prosecution speed. Prosecution timelines are slightly slower than average with this examiner.

Interview Effectiveness

Conducting an examiner interview provides a +36.8% benefit to allowance rate for applications examined by THOMAS, KYLE ROBERT. This interview benefit is in the 87% 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, 25.9% 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 19.6% of cases where such amendments are filed. This entry rate is in the 16% 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 65% 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 48.0% of appeals filed. This is in the 10% 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, 30.4% are granted (fully or in part). This grant rate is in the 22% 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 0.0% of allowed cases (in the 40% 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.