Detailed information about the 100 most recent patent applications.
| Application Number | Title | Filing Date | Disposal Date | Disposition | Time (months) | Office Actions | Restrictions | Interview | Appeal |
|---|---|---|---|---|---|---|---|---|---|
| 18949069 | NUCLEAR THERMAL PROPULSION SYSTEM WITH REACTOR DIRECT DRIVE OF CRYOCOOLER TURBINE | November 2024 | March 2025 | Allow | 4 | 0 | 0 | No | No |
| 18846327 | LUBRICATION AND COOLING OF EQUIPMENT OF AN AIRCRAFT TURBOMACHINE | September 2024 | May 2025 | Allow | 8 | 0 | 0 | Yes | No |
| 18805867 | AIR RECUPERATED ENGINE WITH AIR REINJECTION | August 2024 | April 2025 | Allow | 8 | 1 | 0 | Yes | No |
| 18838100 | TURBOMACHINE FOR AN AIRCRAFT | August 2024 | March 2025 | Allow | 7 | 0 | 0 | No | No |
| 18774773 | INTEGRATED VEHICLE FLUIDS WITH HOT GAS LINE AND COLD GAS LINE MERGING TO INCREASE ENTHALPY | July 2024 | January 2025 | Allow | 6 | 0 | 0 | No | No |
| 18768015 | ACTUATION MECHANISM | July 2024 | February 2025 | Allow | 8 | 0 | 0 | No | No |
| 18639030 | METHOD AND APPARATUS FOR REDUCING CONSEQUENCES OF A BULKHEAD FAILURE FOR A LIQUID METHANE AND LIQUID OXYGEN ROCKET | April 2024 | June 2024 | Allow | 2 | 0 | 0 | No | No |
| 18638449 | ROCKET ENGINE WITH DUAL CONTOUR NOZZLE | April 2024 | September 2024 | Allow | 5 | 0 | 0 | Yes | No |
| 18635986 | PASSIVE BYPASS FOR MITIGATION OF INLET BUZZ IN SUPERSONIC OR HYPERSONIC AIR-BREATHING ENGINES | April 2024 | October 2024 | Allow | 6 | 0 | 0 | Yes | No |
| 18634822 | RAMJET PROPULSION METHOD | April 2024 | March 2025 | Allow | 11 | 1 | 0 | Yes | No |
| 18632124 | NUCLEAR THERMAL PROPULSION SYSTEM WITH REACTOR DIRECT DRIVE OF CRYOCOOLER TURBINE | April 2024 | August 2024 | Allow | 4 | 0 | 0 | No | No |
| 18625769 | TURBINE OVERSPEED PROTECTION | April 2024 | April 2025 | Allow | 13 | 1 | 0 | No | No |
| 18588257 | DE-ICE SYSTEM AND APPARATUS FOR TURBINE ENGINES | February 2024 | November 2024 | Allow | 8 | 1 | 0 | No | No |
| 18581297 | ADDITIVELY MANUFACTURED ROCKET FUEL GRAINS AND COMPETITIVE SIMULATION OF THE SAME | February 2024 | July 2024 | Allow | 5 | 0 | 0 | No | No |
| 18436698 | Air Turbine Starter With Decoupler | February 2024 | December 2024 | Allow | 10 | 0 | 0 | No | No |
| 18681099 | SINGLE STAGE TO ORBIT ROCKET ENGINE | February 2024 | August 2024 | Allow | 7 | 0 | 0 | No | No |
| 18411832 | VARIABLE AREA NOZZLE FOR AN AIRCRAFT ENGINE | January 2024 | July 2024 | Allow | 6 | 0 | 0 | Yes | No |
| 18396488 | ANNULAR VORTEX TANK VALVE FOR ROCKET MOTOR AND CONFIGURATION IN A ROCKET | December 2023 | May 2024 | Allow | 4 | 0 | 0 | Yes | No |
| 18390927 | TRANSPIRATION-COOLED SYSTEMS HAVING PERMEABLE AND NON-PERMEABLE PORTIONS | December 2023 | September 2024 | Allow | 9 | 0 | 0 | Yes | No |
| 18543739 | CENTRIFUGAL FORCE PROPULSION DEVICE | December 2023 | November 2024 | Allow | 11 | 0 | 1 | Yes | No |
| 18565461 | THRUST REVERSER ASSEMBLY FOR A TURBOJET ENGINE | November 2023 | June 2024 | Allow | 7 | 0 | 0 | Yes | No |
| 18518558 | Electrically Powered Supersonic and Hypersonic Propulsor | November 2023 | January 2025 | Allow | 13 | 1 | 0 | Yes | No |
| 18510359 | ROCKET INJECTOR SUBSCALE STABILITY ASSESSMENT WITH TELESCOPING THROAT OR MOVEABLE INJECTOR PLATE | November 2023 | July 2025 | Allow | 20 | 2 | 0 | Yes | No |
| 18510495 | ROCKET INJECTOR SUBSCALE STABILITY ASSESSMENT WITH TELESCOPING PISTON | November 2023 | June 2025 | Allow | 19 | 2 | 0 | Yes | No |
| 18501983 | SYSTEM AND METHOD FOR ASYNCHRONOUS AUTOGENOUSLY PRESSURIZED IN-SPACE PROPULSION | November 2023 | April 2024 | Allow | 5 | 0 | 0 | No | No |
| 18558800 | PROPULSION SYSTEM FOR A VEHICLE USING HEAT ENERGY ABSORBED IN AN ACTIVE COOLING SYSTEM | November 2023 | February 2025 | Allow | 16 | 1 | 0 | Yes | No |
| 18497442 | MULTIMODE PROPULSION SYSTEM | October 2023 | August 2024 | Allow | 10 | 1 | 0 | No | No |
| 18380892 | SYSTEM AND METHOD OF GRAIN IGNITION AND INHIBITOR RELEASE USING PHASE ALLOY FILMS | October 2023 | October 2024 | Allow | 12 | 1 | 0 | Yes | No |
| 18483106 | AIRCRAFT ENGINE FUEL SYSTEM | October 2023 | November 2024 | Allow | 14 | 1 | 0 | No | No |
| 18377151 | SERIAL ROTATING DETONATION COMBUSTOR SYSTEMS | October 2023 | February 2025 | Allow | 17 | 1 | 1 | Yes | No |
| 18480471 | Bobbin-Form Solid Controlled and Filament Fed Hybrid Propulsion Methods for Space Vehicle Innovative Architectures | October 2023 | March 2025 | Abandon | 18 | 1 | 0 | No | No |
| 18374941 | Air-Breathing Plasma Thruster | September 2023 | February 2025 | Allow | 17 | 1 | 0 | No | No |
| 18284639 | A PUMPING APPARATUS | September 2023 | April 2025 | Allow | 18 | 1 | 0 | No | No |
| 18471881 | HEAVY INERT GAS INSULATED BLAST TUBE | September 2023 | April 2024 | Allow | 7 | 1 | 0 | No | No |
| 18457283 | DUAL MODE ROCKET ENGINE WITH BIPROPELLANT INJECTION IN THE NOZZLE | August 2023 | March 2024 | Allow | 6 | 0 | 0 | Yes | No |
| 18457301 | AFTERBURNING TURBINE EXHAUST CYCLE (ABTEC) | August 2023 | February 2024 | Allow | 6 | 1 | 0 | Yes | No |
| 18278463 | ROCKET PROPULSION SYSTEM | August 2023 | September 2024 | Abandon | 13 | 1 | 0 | No | No |
| 18365767 | DETONATION OF UN-DECOMPOSED LIQUID OXIDIZER IN A ROCKET ENGINE | August 2023 | August 2024 | Allow | 12 | 3 | 0 | No | No |
| 18228649 | INTEGRATED AUXILIARY COMPRESSORS FOR COOLING IN GAS TURBINE ENGINES | July 2023 | February 2025 | Abandon | 19 | 2 | 0 | No | No |
| 18274999 | TRANSITION WITH UNEVEN SURFACE | July 2023 | November 2024 | Abandon | 15 | 1 | 0 | No | No |
| 18262685 | LIQUID PROPELLANT GASIFIER AND PRESSURIZER | July 2023 | April 2025 | Allow | 20 | 0 | 0 | No | No |
| 18356394 | Recoverable Rocket and an Associated Recovery Method | July 2023 | October 2024 | Allow | 15 | 1 | 0 | No | No |
| 18223433 | SAFETY IGNITION DEVICE FOR HIGH ALTITUDE DUAL PULSE MOTOR INCLUDING THE SAME | July 2023 | January 2024 | Allow | 6 | 1 | 0 | Yes | No |
| 18353342 | GAS TURBINE OVERSPEED PROTECTION METHOD AND APPARATUS, ELECTRONIC DEVICE AND STORAGE MEDIUM | July 2023 | November 2024 | Allow | 16 | 1 | 0 | Yes | No |
| 18353487 | NOZZLE DEVICE FOR FEEDING FUEL INTO A COMBUSTION CHAMBER OF A GAS TURBINE ASSEMBLY, AND GAS TURBINE ASSEMBLY | July 2023 | May 2024 | Allow | 10 | 1 | 0 | No | No |
| 18271834 | AEROSPIKE ENGINES, LAUNCH VEHICLES INCORPORATING SUCH ENGINES AND METHODS | July 2023 | January 2025 | Abandon | 18 | 2 | 0 | No | No |
| 18349285 | ROTOR BOW MITIGATION | July 2023 | October 2024 | Allow | 15 | 1 | 0 | No | No |
| 18217228 | PRE-HEATING AIRCRAFT ENGINE IN STANDBY MODE | June 2023 | June 2024 | Allow | 11 | 0 | 0 | Yes | No |
| 18270301 | SEALING MEMBER AND GAS TURBINE | June 2023 | April 2024 | Allow | 10 | 0 | 0 | Yes | No |
| 18211277 | STAGED COMBUSTION LIQUID ROCKET ENGINE CYCLE WITH THE TURBOPUMP UNIT AND PREBURNER INTEGRATED INTO THE STRUCTURE OF THE COMBUSTION CHAMBER | June 2023 | December 2023 | Allow | 6 | 0 | 0 | Yes | No |
| 18335340 | SYSTEM AND METHOD FOR EFFICIENTLY DETERMINING A PHASE SHIFT IN A PROPULSION SYSTEM | June 2023 | April 2025 | Allow | 22 | 2 | 0 | No | No |
| 18195179 | VAPOR RETENTION DEVICE | May 2023 | May 2024 | Allow | 12 | 1 | 0 | No | No |
| 18033428 | DESIGN AND MANUFACTURING OF A SINGLE PIECE ROCKET ENGINE | April 2023 | April 2025 | Allow | 24 | 3 | 0 | Yes | No |
| 18304575 | FLAMMABLE FLUID RESERVOIR | April 2023 | October 2024 | Allow | 18 | 1 | 0 | No | No |
| 18133134 | INTEGRATED VEHICLE FLUIDS | April 2023 | December 2023 | Allow | 9 | 0 | 0 | Yes | No |
| 18133111 | INTEGRATED VEHICLE FLUIDS | April 2023 | March 2024 | Allow | 11 | 1 | 0 | No | No |
| 18133124 | INTEGRATED VEHICLE FLUIDS FOR UPPER STAGE LAUNCH VEHICLE WITH INTERNAL COMBUSTION ENGINE | April 2023 | September 2023 | Allow | 5 | 0 | 0 | Yes | No |
| 18130683 | COMBUSTOR WITH FUEL AND AIR MIXING PLENUM | April 2023 | December 2024 | Allow | 20 | 3 | 0 | Yes | No |
| 18129245 | ROCKET PROPULSION SYSTEMS AND ASSOCIATED METHODS | March 2023 | October 2023 | Allow | 7 | 0 | 0 | Yes | No |
| 18193005 | TRANSPIRATION-COOLED SYSTEMS HAVING PERMEABLE AND NON-PERMEABLE PORTIONS | March 2023 | July 2024 | Allow | 16 | 2 | 0 | Yes | No |
| 18192875 | FEED SYSTEM FOR ROCKET ENGINE | March 2023 | March 2024 | Abandon | 12 | 1 | 0 | No | No |
| 18191181 | SPARK IGNITER WITH MAGNETIC FIELD FOR PUSHING SPARK | March 2023 | August 2024 | Allow | 17 | 1 | 0 | No | No |
| 18186347 | METHOD AND SYSTEM FOR DE-PRIMING AN AIRCRAFT ENGINE COMPONENT CONTAINING A FLAMMABLE FLUID FOR FIRE SAFETY | March 2023 | August 2024 | Allow | 17 | 0 | 1 | Yes | No |
| 18118606 | AIRBREATHING PROPULSION ENGINES INCLUDING ROTATING DETONATION AND BLUFF BODY SYSTEMS | March 2023 | April 2024 | Allow | 13 | 1 | 0 | No | No |
| 18117403 | INTEGRATED PROPULSION SYSTEM FOR HYBRID ROCKETS | March 2023 | August 2023 | Allow | 5 | 0 | 0 | No | No |
| 18040444 | AIRCRAFT | February 2023 | January 2024 | Allow | 12 | 1 | 0 | No | No |
| 18103460 | VORTEX HYBRID ROCKET MOTOR | January 2023 | April 2024 | Allow | 15 | 2 | 0 | Yes | No |
| 18100130 | Aircraft Heat Exchangers | January 2023 | January 2024 | Allow | 12 | 1 | 0 | Yes | No |
| 18152678 | 3D-PRINTED CATALYST BED | January 2023 | November 2023 | Allow | 10 | 2 | 0 | No | No |
| 18004577 | METHOD FOR STARTING AN AIRCRAFT ENGINE | January 2023 | May 2025 | Allow | 28 | 4 | 0 | Yes | No |
| 18094300 | REACTION CONTROL VORTEX THRUSTER SYSTEM | January 2023 | October 2023 | Allow | 9 | 1 | 0 | No | No |
| 18085925 | CATALYTIC DECOMPOSITION REACTORS | December 2022 | May 2025 | Allow | 29 | 2 | 1 | Yes | No |
| 17972680 | COMBUSTOR FOR ROCKET ENGINE AND METHOD FOR MANUFACTURING IT | October 2022 | July 2024 | Allow | 21 | 2 | 0 | Yes | No |
| 17967941 | ELECTRIC PROPULSION BASED SPACECRAFT PROPULSION SYSTEMS AND METHODS UTILIZING MULTIPLE PROPELLANTS | October 2022 | January 2024 | Allow | 15 | 1 | 0 | Yes | No |
| 18046790 | ROCKET ENGINE WITH DUAL CONTOUR NOZZLE | October 2022 | February 2024 | Allow | 16 | 2 | 0 | Yes | No |
| 17951972 | AIR RECUPERATED ENGINE WITH AIR REINJECTION | September 2022 | April 2024 | Allow | 19 | 2 | 0 | Yes | No |
| 17948870 | EXHAUST NOZZLE ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEM | September 2022 | May 2024 | Allow | 20 | 2 | 0 | Yes | No |
| 17944790 | CANTILEVERED AIRFOILS AND METHODS OF FORMING THE SAME | September 2022 | May 2024 | Allow | 20 | 2 | 0 | Yes | No |
| 17930741 | METHOD FOR REDUCING JET TAB EXPOSURE DURING THRUST VECTORING | September 2022 | November 2023 | Allow | 14 | 1 | 0 | Yes | No |
| 17802468 | TWO-STAGE LOW-POWER AND HIGH-THRUST TO POWER ELECTRIC PROPULSION SYSTEM | August 2022 | March 2024 | Allow | 18 | 1 | 0 | Yes | No |
| 17820512 | REACTOR ROCKET ENGINE | August 2022 | August 2023 | Allow | 11 | 1 | 0 | Yes | No |
| 17889066 | Air Turbine Starter With Decoupler | August 2022 | November 2023 | Allow | 15 | 1 | 0 | No | No |
| 17878531 | THRUST REVERSER CASCADE WITH ONE OR MORE FLOW DISRUPTERS | August 2022 | December 2024 | Allow | 28 | 4 | 0 | Yes | No |
| 17878497 | THRUST REVERSER CASCADE WITH ONE OR MORE FLOW STABILIZERS | August 2022 | August 2023 | Allow | 13 | 1 | 0 | Yes | No |
| 17813312 | OMNIVOROUS SOLAR THERMAL THRUSTER, COOLING SYSTEMS, AND THERMAL ENERGY TRANSFER IN ROCKETS | July 2022 | February 2024 | Allow | 19 | 1 | 0 | Yes | No |
| 17808256 | NUCLEAR THERMAL PROPULSION SYSTEM WITH REACTOR DIRECT DRIVE OF CRYOCOOLER TURBINE | June 2022 | December 2023 | Allow | 18 | 1 | 0 | Yes | No |
| 17840715 | DESCENT OPERATION FOR AN AIRCRAFT PARALLEL HYBRID GAS TURBINE ENGINE PROPULSION SYSTEM | June 2022 | November 2023 | Allow | 17 | 1 | 0 | Yes | No |
| 17836835 | ROCKET ENGINE WITH POROUS STRUCTURE | June 2022 | December 2024 | Abandon | 31 | 4 | 1 | Yes | No |
| 17740958 | LIQUID ROCKET ENGINE TAP-OFF POWER SOURCE | May 2022 | March 2023 | Allow | 10 | 1 | 0 | No | No |
| 17740111 | ACTIVE ON ORBIT FLUID PROPELLANT MANAGEMENT AND REFUELING SYSTEMS AND METHODS | May 2022 | October 2023 | Allow | 18 | 1 | 0 | Yes | No |
| 17770156 | VALVE TIMING SYSTEM FOR LIQUID FUEL ROCKETS | April 2022 | March 2024 | Allow | 23 | 0 | 0 | No | No |
| 17769753 | HYBRID PROPULSION UNIT FOR SPACE VEHICLE | April 2022 | February 2025 | Allow | 34 | 3 | 0 | No | No |
| 17754787 | Augmented Aerospike Nozzle, Engine Including the Augmented Aerospike Nozzle, and Vehicle Including the Engine | April 2022 | April 2024 | Allow | 24 | 1 | 0 | Yes | No |
| 17715416 | PROPULSION ASSEMBLY FOR A ROCKET | April 2022 | April 2024 | Abandon | 24 | 2 | 0 | No | No |
| 17683014 | INTEGRATED VEHICLE FLUIDS | February 2022 | July 2023 | Allow | 16 | 1 | 0 | Yes | No |
| 17651936 | Motor And Fuel-Powered Hybrid System for a Rocket Thruster | February 2022 | January 2023 | Allow | 11 | 0 | 0 | Yes | No |
| 17666612 | EXPENDABLE MULTISTAGE PRESSURE-FED ABLATIVE-COOLING NONTOXIC NON-HEAVY LAUNCH VEHICLE | February 2022 | January 2024 | Abandon | 24 | 2 | 0 | No | No |
| 17618231 | TANK FOR CONTAINING A COMPONENT FLUID, SUCH AS A PROPELLANT | December 2021 | December 2024 | Allow | 37 | 0 | 1 | Yes | No |
| 17544220 | LIQUID-COOLED AIR-BREATHING ROCKET ENGINE | December 2021 | February 2023 | Allow | 14 | 1 | 0 | Yes | No |
| 17539479 | MULTI-STAGE PROPELLANT SYSTEMS, ASSEMBLIES, AND METHODS | December 2021 | October 2023 | Allow | 22 | 2 | 0 | Yes | No |
This analysis examines appeal outcomes and the strategic value of filing appeals for examiner THOMAS, KYLE ROBERT.
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.
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.
⚠ 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 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.
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.
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.
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.
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.
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.
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.
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.
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.
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'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.
Based on the statistical analysis of this examiner's prosecution patterns, here are tailored strategic recommendations:
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.