Detailed information about the 100 most recent patent applications.
| Application Number | Title | Filing Date | Disposal Date | Disposition | Time (months) | Office Actions | Restrictions | Interview | Appeal |
|---|---|---|---|---|---|---|---|---|---|
| 18715796 | HIGH-POWER HYBRID-ELECTRIC PROPULSION SYSTEMS AND METHODS | June 2024 | June 2025 | Abandon | 13 | 1 | 0 | No | No |
| 18678576 | CIRCUMFERENTIAL FLOW CONDENSER ARRANGEMENT FOR AN AIRCRAFT PROPULSION SYSTEM | May 2024 | February 2025 | Allow | 9 | 1 | 0 | No | No |
| 18594689 | ADJUSTABLE GASEOUS FUEL INJECTOR | March 2024 | January 2025 | Allow | 10 | 0 | 0 | Yes | No |
| 18396562 | METHOD FOR TESTING A HYBRID DRIVE SYSTEM ON AN AIRCRAFT, ASSOCIATED COMPUTER PROGRAM AND AIRCRAFT | December 2023 | January 2025 | Allow | 13 | 0 | 0 | No | No |
| 18563040 | ASSEMBLY FOR SUPPORTING AN ACCESSORY GEARBOX OF AN AIRCRAFT TURBINE ENGINE | November 2023 | January 2025 | Allow | 14 | 1 | 0 | Yes | No |
| 18386816 | POWERPLANT WITH MULTIPLE INTEGRATED GAS TURBINE ENGINES | November 2023 | April 2025 | Allow | 18 | 2 | 0 | No | No |
| 18243480 | AIRCRAFT ENGINE ASSEMBLY FOR CONTROLLING ENGINE OIL FLOW DURING FIRE CONDITIONS AND METHOD FOR USING SAME | September 2023 | September 2024 | Allow | 13 | 0 | 0 | No | No |
| 18456586 | POWERPLANT FOR AN AIRCRAFT | August 2023 | December 2024 | Allow | 16 | 0 | 1 | No | No |
| 18230442 | ANTI-ICE MIXING UNIT UTILIZING BLEED AIR FOR A GAS TURBINE ENGINE | August 2023 | June 2024 | Allow | 10 | 1 | 0 | Yes | No |
| 18358213 | VERTICAL TYPE ONCE-THROUGH HEAT RECOVERY STEAM GENERATOR AND COMBINED POWER GENERATION SYSTEM INCLUDING | July 2023 | November 2024 | Allow | 16 | 2 | 1 | No | No |
| 18213543 | ADJUSTABLE GASEOUS FUEL INJECTOR | June 2023 | October 2023 | Allow | 4 | 0 | 0 | Yes | No |
| 18327965 | INLET SYSTEM FOR AUXILIARY POWER UNIT | June 2023 | December 2024 | Allow | 18 | 1 | 0 | Yes | No |
| 18036058 | GAS TURBINE STATIONARY BLADE AND GAS TURBINE | May 2023 | April 2025 | Allow | 23 | 1 | 1 | Yes | No |
| 18035803 | GUIDING ARRAY | May 2023 | October 2024 | Allow | 17 | 1 | 0 | No | No |
| 18142379 | AIRCRAFT POWERPLANT WITH STEAM SYSTEM AND BYPASS | May 2023 | February 2025 | Allow | 21 | 3 | 0 | Yes | No |
| 18250920 | COMPRESSED AIR SUPPLY SYSTEM | April 2023 | March 2025 | Allow | 22 | 2 | 0 | Yes | No |
| 18308603 | HYPERSONIC VEHICLE AND SCRAMJET ENGINE WITH VARIABLE FUEL INJECTION FOR OPERATION OVER A LARGE MACH NUMBER RANGE | April 2023 | January 2025 | Abandon | 21 | 1 | 0 | No | No |
| 18030143 | ADJUSTABLE FUEL INJECTOR FOR FLAME DYNAMICS CONTROL | April 2023 | March 2024 | Allow | 12 | 1 | 0 | No | No |
| 18123787 | COMBUSTOR NOZZLE, COMBUSTOR, AND GAS TURBINE INCLUDING THE SAME | March 2023 | July 2024 | Allow | 16 | 2 | 1 | No | No |
| 18186518 | COMBUSTOR WITH A DILUTION PASSAGE | March 2023 | March 2025 | Abandon | 24 | 1 | 1 | Yes | No |
| 18026601 | CRYOGENIC ENGINE FOR SPACE APPARATUS | March 2023 | March 2024 | Allow | 12 | 1 | 0 | Yes | No |
| 18121503 | STEAM COOLING TURBINE ENGINE COMBUSTOR WALL | March 2023 | May 2024 | Allow | 14 | 2 | 0 | No | No |
| 18117919 | HEAT EXCHANGER(S) FOR RECOVERING WATER AND/OR HEAT ENERGY FROM TURBINE ENGINE COMBUSTION PRODUCTS | March 2023 | September 2024 | Allow | 18 | 1 | 0 | No | No |
| 18113457 | FUEL INJECTOR ASSEMBLY FOR GAS TURBINE ENGINE | February 2023 | August 2024 | Allow | 18 | 2 | 1 | No | No |
| 18109771 | COMBINED POWER GENERATION SYSTEM AND DRIVING METHOD THEREOF | February 2023 | September 2023 | Allow | 7 | 1 | 0 | No | No |
| 18163361 | MICRO-MIXER WITH MULTI-STAGE FUEL SUPPLY AND GAS TURBINE INCLUDING SAME | February 2023 | May 2024 | Allow | 16 | 2 | 1 | Yes | No |
| 18085714 | ACCESSORY GEARBOX FOR A TURBINE ENGINE | December 2022 | August 2024 | Allow | 19 | 3 | 0 | Yes | No |
| 18001441 | RECOVERED-CYCLE AIRCRAFT TURBOMACHINE | December 2022 | February 2025 | Allow | 26 | 2 | 0 | Yes | No |
| 18074270 | SUPPORT STRUCTURE FOR ATTACHING A GAS TURBINE ENGINE TO AN AIRCRAFT PYLON | December 2022 | February 2024 | Allow | 14 | 0 | 0 | No | No |
| 18060659 | AIRCRAFT ENGINE WITH EXHAUST HAVING REMOVABLE DEFLECTOR | December 2022 | March 2025 | Allow | 27 | 2 | 1 | No | No |
| 18057468 | COMBUSTOR NOZZLE, COMBUSTOR, AND GAS TURBINE INCLUDING SAME | November 2022 | August 2023 | Allow | 9 | 1 | 0 | No | No |
| 17988862 | ENGINE PYLON FOR COUPLING A JET ENGINE TO A WING OF AN AIRCRAFT | November 2022 | July 2024 | Allow | 19 | 1 | 1 | No | No |
| 17988504 | RESTARTING A GAS TURBINE ENGINE | November 2022 | December 2023 | Allow | 13 | 1 | 0 | No | No |
| 17962994 | DISSIMILARLY SHAPED AIRCRAFT NOZZLES WITH TANDEM MIXING DEVICES, AND ASSOCIATED SYSTEMS AND METHODS | October 2022 | August 2024 | Allow | 22 | 1 | 1 | Yes | No |
| 17947273 | AIRCRAFT PROPULSION ASSEMBLY COMPRISING A THRUST FORCE UPTAKE DEVICE | September 2022 | September 2023 | Allow | 12 | 0 | 0 | No | No |
| 17902316 | ENGINE EXHAUST NOZZLE WITH ACOUSTIC ATTENUATION | September 2022 | August 2024 | Allow | 23 | 4 | 0 | No | No |
| 17899673 | FRONT ENGINE ATTACHMENT SYSTEM FOR AN AIRCRAFT ENGINE, WHICH HAS A COMPACT STRUCTURE | August 2022 | January 2024 | Allow | 17 | 1 | 0 | Yes | No |
| 17896467 | CONTROLLING SOOT | August 2022 | May 2023 | Allow | 8 | 1 | 0 | No | No |
| 17856550 | IN-FLIGHT ENGINE RE-START | July 2022 | November 2024 | Allow | 28 | 3 | 0 | Yes | No |
| 17849882 | AIRCRAFT PROPULSION ASSEMBLY COMPRISING A FRONT ENGINE MOUNT WHICH COMPRISES A TRANSVERSE BEAM WHICH IS PARTIALLY POSITIONED OPPOSITE A FRONT TRANSVERSE REINFORCEMENT OF A PRIMARY STRUCTURE OF A STRUT | June 2022 | January 2024 | Allow | 19 | 2 | 0 | No | No |
| 17837100 | TURBO ENGINE WITH COOLER FOR COOLING INLET AIR AND TURBINE FOR EXPANDING CRYOGENIC FUEL | June 2022 | February 2023 | Allow | 8 | 0 | 0 | Yes | No |
| 17804631 | TWIN-ENGINE SYSTEM WITH ELECTRIC DRIVE | May 2022 | March 2023 | Allow | 9 | 1 | 0 | Yes | No |
| 17752450 | ADJUSTABLE SUPPORT LINKS FOR AIRCRAFT | May 2022 | August 2023 | Allow | 15 | 1 | 0 | Yes | No |
| 17733065 | ASSEMBLY OF A PRIMARY STRUCTURE OF AN AIRCRAFT PYLON AND A REAR ENGINE ATTACHMENT COMPRISING AT LEAST ONE LATERAL FASTENING ELEMENT AND AIRCRAFT COMPRISING AT LEAST ONE SUCH ASSEMBLY | April 2022 | June 2024 | Abandon | 26 | 2 | 0 | No | No |
| 17725641 | DEVICE FOR CONNECTING AN AIRCRAFT ENGINE AND A PRIMARY STRUCTURE OF AN AIRCRAFT PYLON COMPRISING A RUDDER AND A SYSTEM FOR LIMITING THE DISPLACEMENT OF THE RUDDER INCORPORATING A DOUBLE STOP, AIRCRAFT COMPRISING SUCH A DEVICE | April 2022 | February 2023 | Allow | 10 | 0 | 0 | No | No |
| 17715450 | LOBED MIXER NOZZLES FOR SUPERSONIC AND SUBSONIC AIRCRAFT, AND ASSOCIATED SYSTEMS AND METHODS | April 2022 | April 2024 | Abandon | 24 | 2 | 0 | Yes | No |
| 17711445 | AIRCRAFT BLEED AIR SYSTEMS AND METHODS | April 2022 | April 2024 | Abandon | 24 | 3 | 0 | No | No |
| 17709700 | PROPULSION SYSTEM WITH GROOVED INERT RODS FOR REACTIVE WIRE | March 2022 | April 2023 | Allow | 13 | 0 | 0 | Yes | No |
| 17688503 | Hydrogen-Fueled Combustor for Gas Turbines | March 2022 | March 2023 | Abandon | 12 | 1 | 0 | No | No |
| 17686871 | PASSIVE VALVE ASSEMBLY FOR A NOZZLE OF A GAS TURBINE ENGINE | March 2022 | February 2023 | Allow | 11 | 0 | 0 | No | No |
| 17753220 | CONVERGENT-DIVERGENT FLAP PAIR FOR A VARIABLE-GEOMETRY TURBOJET ENGINE NOZZLE COMPRISING COOLING AIR CIRCULATION DUCTS CONNECTED THROUGH CONTACT SURFACES | February 2022 | March 2023 | Allow | 12 | 0 | 0 | Yes | No |
| 17597047 | AIRCRAFT TURBOMACHINE COMPRISING MEANS FOR PRIMING THE LUBRICATING PUMP | December 2021 | September 2024 | Allow | 33 | 2 | 0 | No | No |
| 17539401 | PROPULSION SYSTEM FOR A GAS TURBINE ENGINE | December 2021 | July 2024 | Abandon | 31 | 4 | 0 | No | No |
| 17539719 | SYSTEMS AND METHODS FOR EXPANDING AN OPERATING SPEED RANGE OF A HIGH SPEED FLIGHT VEHICLE | December 2021 | December 2024 | Abandon | 36 | 2 | 1 | Yes | No |
| 17535995 | FUSELAGE FOR AN AIRCRAFT WITH FUSELAGE-INTEGRATED TAILPLANE | November 2021 | August 2023 | Allow | 20 | 2 | 0 | Yes | No |
| 17533009 | Automated Initiation of Starter Motor Operation for Starting an Aircraft Engine | November 2021 | June 2023 | Abandon | 18 | 2 | 0 | No | No |
| 17455099 | METHOD AND DEVICE TO IMPROVE THE PERFORMANCE OF A POWER PLANT INTEGRATED WITH A THERMAL ENERGY STORAGE SYSTEM | November 2021 | November 2022 | Allow | 12 | 1 | 0 | No | No |
| 17509113 | BRACED-PYLON ARCHITECTURE FOR MOUNTING AN ENGINE TO AN AIRCRAFT | October 2021 | August 2023 | Allow | 22 | 2 | 0 | Yes | No |
| 17502054 | FUEL NOZZLE AND COMBUSTOR AND GAS TURBINE INCLUDING THE SAME | October 2021 | April 2023 | Allow | 18 | 2 | 0 | Yes | No |
| 17492114 | ELECTRIC ENHANCED TRANSMISSION FOR MULTI-SPOOL LOAD-SHARING TURBOFAN ENGINE | October 2021 | April 2024 | Allow | 31 | 1 | 1 | Yes | No |
| 17472146 | TURBINE POSITIONING IN A GAS TURBINE ENGINE | September 2021 | November 2022 | Abandon | 14 | 0 | 0 | No | No |
| 17411529 | ELECTRO-PNEUMATIC ENVIRONMENTAL CONTROL SYSTEM AIR CIRCUIT | August 2021 | September 2022 | Allow | 12 | 0 | 0 | Yes | No |
| 17389450 | ORIFICE PACK FOR COMPRESSOR BLEED VALVE | July 2021 | August 2023 | Allow | 24 | 1 | 0 | Yes | No |
| 17383559 | PROPULSIVE ASSEMBLY FOR AIRCRAFT | July 2021 | January 2024 | Allow | 30 | 3 | 1 | Yes | No |
| 17362514 | GAS TURBINE ENGINE AND AIRCRAFT WITH A GAS TURBINE ENGINE | June 2021 | August 2022 | Abandon | 13 | 1 | 0 | No | No |
| 17339208 | AIR BREATHING SOLID FUEL ROTATING DETONATION ENGINE | June 2021 | September 2022 | Allow | 15 | 1 | 1 | Yes | No |
| 17313267 | Aircraft Air Intake Systems Employing Gills | May 2021 | March 2023 | Allow | 22 | 1 | 0 | Yes | No |
| 17235239 | VARIABLE ENGINE-INLET BYPASS CONTROL SYSTEMS AND METHOD | April 2021 | November 2023 | Abandon | 31 | 4 | 0 | No | No |
| 17235225 | VARIABLE ENGINE-INLET BYPASS CONTROL METHOD AND SYSTEM | April 2021 | October 2023 | Abandon | 30 | 4 | 0 | No | No |
| 17200915 | EXHAUST DIFFUSER HUB STRUCTURE FOR REDUCING FLOW SEPARATION | March 2021 | September 2022 | Allow | 18 | 2 | 0 | No | No |
| 17188780 | COMPRESSOR APPARATUS WITH BLEED SLOT AND SUPPLEMENTAL FLANGE | March 2021 | August 2022 | Allow | 18 | 1 | 0 | Yes | No |
| 17178708 | INSTRUMENTED TURBINE EXHAUST DUCT | February 2021 | June 2022 | Allow | 16 | 1 | 0 | Yes | No |
| 17148859 | TURBINE ENGINE AND METHOD OF COOLING THEREOF | January 2021 | November 2023 | Abandon | 34 | 4 | 0 | No | No |
| 17128704 | REGENERATIVE FUEL HEATING SYSTEM | December 2020 | June 2024 | Allow | 41 | 3 | 1 | Yes | No |
| 17044412 | AIRCRAFT ENGINE ASSEMBLY WITH A SUPPLY PATH TO AN INTER-FLOW COMPARTMENT TANK OF TURBINE ENGINE | October 2020 | November 2022 | Allow | 25 | 1 | 0 | Yes | No |
| 17037027 | ACCESSORY GEARBOX FOR A TURBINE ENGINE | September 2020 | September 2022 | Allow | 24 | 1 | 0 | Yes | No |
| 17014513 | THRUST MOUNTS WITH LOAD-BALANCING THRUST LINK-LEVER | September 2020 | June 2023 | Allow | 33 | 1 | 1 | Yes | No |
| 17014884 | AIRFRAME INTEGRATED SCRAMJET WITH FIXED GEOMETRY AND SHAPE TRANSITION FOR HYPERSONIC OPERATION OVER A LARGE MACH NUMBER RANGE | September 2020 | January 2023 | Allow | 29 | 1 | 0 | No | No |
| 17014527 | ACTIVE DEVICE FOR ATTENUATING ACOUSTIC EMISSIONS FOR A TURBOJET ENGINE INCLUDING CONTROLLED TURBINES | September 2020 | March 2022 | Allow | 19 | 3 | 0 | Yes | No |
| 16991143 | ELECTRIC POWER ASSIST FOR IN-FLIGHT ENGINE RE-START | August 2020 | June 2023 | Allow | 34 | 3 | 0 | Yes | No |
| 16938356 | All-Purpose Foreign Object Debris Detection and Retrieval Device | July 2020 | June 2025 | Allow | 58 | 4 | 0 | Yes | No |
| 16936602 | HYBRID GAS TURBINE ENGINE STARTING CONTROL | July 2020 | September 2022 | Allow | 25 | 3 | 0 | Yes | No |
| 16908566 | MULTI-SPOOL GEARED TURBOFAN ARRANGEMENT WITH INTEGRATED STARTER/GENERATOR | June 2020 | October 2021 | Allow | 16 | 1 | 0 | No | No |
| 16954053 | PROPELLING NOZZLE FOR A TURBOFAN ENGINE ON A SUPERSONIC AIRCRAFT | June 2020 | June 2022 | Allow | 24 | 1 | 0 | Yes | No |
| 16875470 | TWIN-ENGINE SYSTEM WITH ELECTRIC DRIVE | May 2020 | April 2022 | Allow | 23 | 1 | 0 | Yes | No |
| 16866908 | TURBO ENGINE WITH COOLER FOR COOLING INLET AIR AND TURBINE FOR EXPANDING CRYOGENIC FUEL | May 2020 | April 2022 | Allow | 24 | 1 | 0 | Yes | No |
| 16857570 | High Speed Aircraft Flight Technologies | April 2020 | November 2023 | Abandon | 43 | 2 | 1 | No | No |
| 16753345 | DEVICE FOR CLEANING TURBINE BLADES OF A JET ENGINE | April 2020 | December 2022 | Abandon | 33 | 1 | 0 | No | No |
| 16839341 | PRESSURE REGULATOR AND BLEED AIR SYSTEM FOR AIRCRAFT ENGINE | April 2020 | September 2022 | Allow | 29 | 2 | 1 | Yes | No |
| 16836080 | RECONFIGURABLE EXHAUST NOZZLE FOR A GAS TURBINE ENGINE | March 2020 | April 2022 | Allow | 24 | 1 | 1 | Yes | No |
| 16834180 | EXHAUST DUCT AND EXHAUST DUCT ASSEMBLY AND AIRCRAFT USING THE EXHAUST DUCT | March 2020 | December 2021 | Allow | 21 | 2 | 0 | No | No |
| 16811673 | SOLID-PROPELLANT GAS GENERATOR ASSEMBLIES AND METHODS | March 2020 | July 2022 | Allow | 28 | 1 | 0 | Yes | No |
| 16811368 | PROPULSION SYSTEM ARCHITECTURE | March 2020 | March 2024 | Allow | 48 | 5 | 0 | Yes | No |
| 16797100 | CONTROL SYSTEM AND METHODS OF CONTROLLING AN ENGINE-MOUNTING LINK SYSTEM | February 2020 | January 2024 | Allow | 47 | 2 | 1 | Yes | No |
| 16796051 | TURBINE POSITIONING IN A GAS TURBINE ENGINE | February 2020 | June 2021 | Allow | 16 | 2 | 0 | Yes | No |
| 16796256 | TURBOFAN ENGINE WITH CORE EXHAUST AND BYPASS FLOW MIXING | February 2020 | January 2023 | Abandon | 35 | 3 | 1 | Yes | No |
| 16780261 | TURBO CLUSTER GAS TURBINE SYSTEM AND ACTIVATION METHOD THEREOF | February 2020 | January 2022 | Allow | 23 | 2 | 1 | Yes | No |
| 16775559 | GAS TURBINE EXHAUST HEAT RECOVERY PLANT | January 2020 | March 2023 | Allow | 38 | 3 | 0 | Yes | No |
| 16735778 | GAS TURBINE ENGINE | January 2020 | April 2022 | Abandon | 27 | 1 | 1 | No | No |
| 16734693 | MOUNTING APPARATUS FOR A GAS TURBINE ENGINE | January 2020 | April 2022 | Allow | 27 | 1 | 0 | No | No |
This analysis examines appeal outcomes and the strategic value of filing appeals for examiner AMAR, MARC J.
With a 16.7% 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.
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, 35.3% 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.
⚠ Appeals to PTAB face challenges. Ensure your case has strong merit before committing to full Board review.
✓ Filing a Notice of Appeal is strategically valuable. The act of filing often prompts favorable reconsideration during the mandatory appeal conference.
Examiner AMAR, MARC J works in Art Unit 3741 and has examined 417 patent applications in our dataset. With an allowance rate of 79.9%, this examiner has a below-average tendency to allow applications. Applications typically reach final disposition in approximately 35 months.
Examiner AMAR, MARC J's allowance rate of 79.9% places them in the 42% percentile among all USPTO examiners. This examiner has a below-average tendency to allow applications.
On average, applications examined by AMAR, MARC J 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.
The median time to disposition (half-life) for applications examined by AMAR, MARC J is 35 months. This places the examiner in the 21% percentile for prosecution speed. Applications take longer to reach final disposition with this examiner compared to most others.
Conducting an examiner interview provides a +38.2% benefit to allowance rate for applications examined by AMAR, MARC J. 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.
When applicants file an RCE with this examiner, 32.7% of applications are subsequently allowed. This success rate is in the 62% percentile among all examiners. Strategic Insight: RCEs show above-average effectiveness with this examiner. Consider whether your amendments or new arguments are strong enough to warrant an RCE versus filing a continuation.
This examiner enters after-final amendments leading to allowance in 26.2% of cases where such amendments are filed. This entry rate is in the 28% percentile among all examiners. Strategic Recommendation: This examiner shows below-average receptiveness to after-final amendments. You may need to file an RCE or appeal rather than relying on after-final amendment entry.
When applicants request a pre-appeal conference (PAC) with this examiner, 40.0% result in withdrawal of the rejection or reopening of prosecution. This success rate is in the 36% 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.
This examiner withdraws rejections or reopens prosecution in 66.7% of appeals filed. This is in the 46% percentile among all examiners. Of these withdrawals, 25.0% occur early in the appeal process (after Notice of Appeal but before Appeal Brief). Strategic Insight: This examiner shows below-average willingness to reconsider rejections during appeals. Be prepared to fully prosecute appeals if filed.
When applicants file petitions regarding this examiner's actions, 31.2% are granted (fully or in part). This grant rate is in the 24% 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 0.5% of allowed cases (in the 59% percentile). This examiner makes examiner's amendments more often than average to place applications in condition for allowance (MPEP § 1302.04).
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.