Detailed information about the 100 most recent patent applications.
| Application Number | Title | Filing Date | Disposal Date | Disposition | Time (months) | Office Actions | Restrictions | Interview | Appeal |
|---|---|---|---|---|---|---|---|---|---|
| 18631772 | LIQUID AIR POWER AND STORAGE | April 2024 | April 2025 | Allow | 12 | 0 | 0 | Yes | No |
| 18461709 | SPLITTER AND GUIDE VANE ARRANGEMENT FOR GAS TURBINE ENGINES | September 2023 | April 2025 | Allow | 19 | 0 | 0 | Yes | No |
| 18225089 | TURBINE ENGINE WITH CENTRIFUGAL COMPRESSOR HAVING IMPELLER BACKPLATE OFFTAKE | July 2023 | June 2025 | Allow | 22 | 1 | 0 | Yes | No |
| 18252119 | AIRCRAFT TURBINE ENGINE DRIVE LINE SHAFT COMPRISING A CONNECTING RING FOR DISASSEMBLING THE DRIVE LINE | May 2023 | May 2025 | Allow | 24 | 1 | 0 | Yes | No |
| 18162964 | ENGINE SYSTEM AND METHOD OF OPERATING THE SAME | February 2023 | March 2025 | Allow | 25 | 2 | 0 | Yes | No |
| 18096178 | COMBINATION OF A GAS TURBINE ENGINE AND A POWER ELECTRONICS | January 2023 | June 2025 | Allow | 29 | 6 | 0 | Yes | No |
| 18085728 | ELECTRIC MACHINE ASSEMBLY | December 2022 | March 2025 | Allow | 27 | 2 | 1 | Yes | No |
| 17896442 | CONTROLLING SOOT | August 2022 | October 2024 | Allow | 26 | 2 | 1 | Yes | No |
| 17889542 | METHOD AND APPARATUS FOR ENDWALL TREATMENTS | August 2022 | January 2025 | Abandon | 29 | 3 | 0 | No | No |
| 17869060 | COOLING AIR DELIVERY SYSTEM AND METHODS THEREOF | July 2022 | February 2025 | Allow | 31 | 3 | 0 | Yes | No |
| 17865908 | VARIABLE PITCH FAN THRUST REVERSER | July 2022 | January 2025 | Abandon | 30 | 3 | 0 | Yes | No |
| 17864851 | AIRCRAFT POWER PLANT WITH HYDROGEN TURBO-EXPANDER | July 2022 | September 2024 | Abandon | 27 | 2 | 1 | No | No |
| 17841175 | RESTARTING A PLURALITY OF ENGINES OF AN AIRCRAFT IN FLIGHT | June 2022 | April 2024 | Allow | 22 | 2 | 0 | Yes | No |
| 17838167 | Pressure Drag Jet Engine | June 2022 | August 2024 | Allow | 27 | 2 | 0 | Yes | No |
| 17836681 | MONITORING SYSTEMS FOR HYDROGEN FUELED AIRCRAFT | June 2022 | June 2025 | Abandon | 36 | 4 | 0 | No | No |
| 17805986 | MULTI-TEMPERATURE FUEL INJECTORS FOR A GAS TURBINE ENGINE | June 2022 | October 2024 | Allow | 28 | 4 | 1 | Yes | No |
| 17747960 | TURBINE ENGINE WITH CENTRIFUGAL COMPRESSOR HAVING IMPELLER BACKPLATE OFFTAKE | May 2022 | April 2023 | Allow | 11 | 1 | 0 | Yes | No |
| 17663698 | THROUGH-FLOW GAS TURBINE ENGINE WITH ELECTRIC MOTOR AND ELECTRIC GENERATOR | May 2022 | February 2023 | Allow | 9 | 0 | 1 | Yes | No |
| 17663079 | FLOW CONTROL WALL FOR HEAT ENGINE | May 2022 | June 2025 | Abandon | 37 | 4 | 1 | Yes | No |
| 17658903 | COMBINED CYCLE PROPULSION SYSTEM FOR HYPERSONIC FLIGHT | April 2022 | November 2024 | Allow | 31 | 4 | 1 | Yes | No |
| 17687769 | FUEL NOZZLE STRUCTURE FOR AIR ASSIST INJECTION | March 2022 | April 2024 | Allow | 25 | 3 | 0 | Yes | No |
| 17556743 | SYSTEM AND METHOD FOR LOAD CONTROL WITH DIFFUSION COMBUSTION IN A STOICHIOMETRIC EXHAUST GAS RECIRCULATION GAS TURBINE SYSTEM | December 2021 | January 2025 | Abandon | 37 | 4 | 0 | Yes | No |
| 17554844 | EXHAUST SYSTEM FOR A GAS TURBINE ENGINE AND METHOD FOR USING SAME | December 2021 | December 2024 | Abandon | 36 | 4 | 0 | Yes | No |
| 17550703 | SPALL PLATE FOR CONSUMABLE COMBUSTOR SUPPORT STRUCTURES | December 2021 | September 2022 | Allow | 10 | 0 | 0 | Yes | No |
| 17542900 | TRAPPED VORTEX COMBUSTOR FOR A GAS TURBINE ENGINE WITH A DRIVER AIRFLOW CHANNEL | December 2021 | June 2023 | Allow | 18 | 2 | 0 | Yes | No |
| 17497152 | FUEL NOZZLE FOR GAS TURBINE ENGINE COMBUSTOR | October 2021 | September 2024 | Abandon | 36 | 4 | 0 | Yes | No |
| 17494738 | HEAT EXCHANGER | October 2021 | December 2024 | Allow | 38 | 6 | 1 | Yes | No |
| 17479502 | ENGINE BLEED GENERATORS AND AIRCRAFT GENERATOR SYSTEMS | September 2021 | June 2023 | Allow | 21 | 1 | 1 | Yes | No |
| 17469844 | REDUNDANT ELECTRICALLY DRIVEN FUEL AND OIL PUMPING SYSTEM FOR GAS TURBINES | September 2021 | September 2024 | Abandon | 37 | 4 | 0 | Yes | No |
| 17469843 | ELECTRICALLY DRIVEN REDUNDANT FUEL AND OIL PUMPING SYSTEM FOR GAS TURBINE ENGINES | September 2021 | August 2024 | Abandon | 36 | 4 | 0 | Yes | No |
| 17406690 | AIR MANIFOLDS FOR FUEL INJECTORS WITH FUEL AIR HEAT EXCHANGERS | August 2021 | September 2023 | Abandon | 24 | 2 | 0 | Yes | No |
| 17401647 | MODULAR CABIN BLOWER SYSTEM FOR AIRCRAFT | August 2021 | December 2024 | Allow | 40 | 4 | 1 | Yes | No |
| 17389144 | GAS TURBINE ENGINE STARTER SYSTEMS AND ASSOCIATED METHODS | July 2021 | September 2023 | Abandon | 26 | 2 | 0 | No | No |
| 17358169 | AIR TURBINE STARTER WITH PRIMARY AND SECONDARY AIR FLOW PATHS | June 2021 | December 2022 | Allow | 18 | 1 | 0 | Yes | No |
| 17344185 | TURBOFAN ENGINE AND METHOD OF OPERATING SAME | June 2021 | October 2022 | Allow | 16 | 0 | 1 | Yes | No |
| 17342738 | HYBRID ELECTRIC IDLE TRANSITION FOR AIRCRAFT | June 2021 | November 2023 | Abandon | 29 | 3 | 0 | No | No |
| 17342100 | Geared Architecture for High Speed and Small Volume Fan Drive Turbine | June 2021 | December 2022 | Allow | 18 | 1 | 0 | Yes | No |
| 17330616 | GAS TURBINE ENGINE WITH IMPROVED DYNAMIC CHARACTERISTICS | May 2021 | May 2022 | Abandon | 11 | 0 | 0 | No | No |
| 17297079 | TURBOFAN ENGINE COMPRISING AN OUTLET CONE COOLED BY ITS SECONDARY FLOW | May 2021 | November 2023 | Allow | 29 | 1 | 0 | Yes | No |
| 17329501 | METHODS AND SYSTEMS FOR STARTING HYDROGEN POWERED GAS GENERATORS | May 2021 | January 2023 | Allow | 20 | 1 | 1 | Yes | No |
| 17287487 | AIRCRAFT TURBINE ENGINE EQUIPPED WITH AN ELECTRICAL MACHINE | May 2021 | March 2024 | Allow | 35 | 3 | 0 | Yes | No |
| 17321212 | RECUPERATIVE HEAT EXCHANGER SYSTEM | May 2021 | November 2024 | Allow | 42 | 3 | 1 | Yes | No |
| 17321052 | TURBINE ENGINES HAVING HYDROGEN FUEL SYSTEMS | May 2021 | September 2024 | Abandon | 41 | 4 | 0 | Yes | No |
| 17319439 | VARIABLE GEOMETRY INLET SYSTEM | May 2021 | January 2023 | Allow | 20 | 2 | 0 | Yes | No |
| 17317199 | GAS TURBINE ENGINE STALL MARGIN MANAGEMENT | May 2021 | August 2024 | Abandon | 39 | 4 | 0 | Yes | No |
| 17246382 | SWEEP FLOW STRUCTURES FOR FUEL SYSTEMS | April 2021 | May 2024 | Allow | 37 | 3 | 1 | Yes | No |
| 17237439 | ELECTRONICS ENCLOSURE FOR GAS TURBINE ENGINE | April 2021 | May 2024 | Abandon | 37 | 4 | 1 | Yes | No |
| 17231421 | NACELLE FOR GAS TURBINE ENGINE | April 2021 | June 2022 | Allow | 14 | 1 | 0 | Yes | No |
| 17206433 | AIR TURBINE STARTER CONTAINMENT SYSTEM | March 2021 | May 2023 | Abandon | 26 | 2 | 1 | Yes | No |
| 17205242 | EXHAUST BAFFLE COMPONENT FOR AN AIR TURBINE STARTER ASSEMBLY | March 2021 | August 2024 | Allow | 41 | 5 | 1 | Yes | No |
| 17181566 | INTERNAL STRUCTURE OF A PRIMARY EXHAUST DUCT HAVING A SEPARATOR OF WHICH THE GEOMETRY VARIES DEPENDING ON THE TEMPERATURE | February 2021 | August 2022 | Allow | 18 | 1 | 0 | Yes | No |
| 17181773 | Compact Low-Pressure Compressor | February 2021 | September 2022 | Allow | 18 | 1 | 0 | Yes | No |
| 17170135 | COMPARTMENT UNIT FOR TURBINE ENGINE | February 2021 | October 2022 | Allow | 20 | 5 | 0 | Yes | No |
| 17152139 | GAS TURBINE ENGINE COOLING SYSTEM | January 2021 | December 2022 | Allow | 23 | 2 | 0 | Yes | No |
| 17142345 | STARTER ASSEMBLY AND METHODS FOR STARTING A COMBUSTION ENGINE | January 2021 | July 2022 | Allow | 18 | 1 | 0 | Yes | No |
| 17129612 | GAS TURBINE ENGINE EXHAUST CHEVRONS | December 2020 | December 2024 | Allow | 48 | 4 | 1 | Yes | No |
| 17128080 | TURBINE ENGINE SYSTEM UTILIZING AN AUGMENTED COMBUSTION MODULE | December 2020 | March 2022 | Allow | 14 | 1 | 0 | Yes | No |
| 17101623 | STARTER TURBINE BEARING COMPARTMENT BUFFER AIR | November 2020 | March 2023 | Abandon | 28 | 2 | 0 | No | No |
| 17080361 | GAS TURBINE PROPULSION SYSTEM | October 2020 | October 2022 | Allow | 24 | 3 | 1 | Yes | Yes |
| 17071018 | UNDUCTED SINGLE ROTOR ENGINE AND METHOD FOR OPERATION | October 2020 | February 2025 | Allow | 52 | 6 | 0 | Yes | No |
| 17032477 | GAS TURBINE ENGINE | September 2020 | March 2024 | Abandon | 42 | 4 | 1 | Yes | No |
| 17018795 | TAIL CONE EJECTOR FOR POWER CABLE COOLING SYSTEM IN A GAS TURBINE ENGINE | September 2020 | October 2022 | Allow | 26 | 1 | 1 | Yes | No |
| 17014051 | SPLIT COMPRESSOR GAS TURBINE ENGINE | September 2020 | April 2024 | Abandon | 43 | 4 | 1 | No | No |
| 16976218 | METHOD AND CONTROL UNIT FOR CONTROLLING THE PLAY OF A HIGH-PRESSURE TURBINE | August 2020 | December 2022 | Allow | 28 | 2 | 0 | Yes | No |
| 16971566 | TWO-SHAFT GAS TURBINE POWER GENERATION FACILITY, CONTROL DEVICE THEREFOR, AND CONTROL METHOD THEREFOR | August 2020 | December 2021 | Allow | 16 | 0 | 0 | Yes | No |
| 16970815 | TURBINE ENGINE COMPRISING A HEAT EXCHANGER IN THE SECONDARY PATH | August 2020 | February 2023 | Allow | 30 | 2 | 0 | Yes | No |
| 16990688 | MULTISTAGE INFRARED SUPPRESSION EXHAUST SYSTEM | August 2020 | December 2022 | Allow | 28 | 3 | 1 | Yes | No |
| 16940538 | GEARED GAS TURBINE ENGINE WITH GEAR DRIVING LOW PRESSURE COMPRESSOR AND FAN AT A COMMON SPEED AND A SHEAR SECTION TO PROVIDE OVERSPEED PROTECTION | July 2020 | March 2022 | Allow | 19 | 1 | 0 | Yes | No |
| 16902433 | FUEL STAGING SYSTEM | June 2020 | April 2022 | Allow | 22 | 2 | 0 | Yes | No |
| 16772480 | VARIABLE AREA FAN NOZZLE FOR TURBOFAN AIRCRAFT ENGINE | June 2020 | March 2022 | Allow | 21 | 2 | 0 | Yes | No |
| 16899337 | CLOSED-LOOP CONTROLLED AIR TURBINE START SYSTEM | June 2020 | August 2022 | Abandon | 26 | 2 | 0 | No | No |
| 16771813 | PORTION OF A FLUID DRAINAGE CONDUIT FOR A TURBOMACHINE | June 2020 | April 2022 | Allow | 22 | 1 | 1 | Yes | No |
| 16897776 | THROUGH-FLOW GAS TURBINE ENGINE WITH ELECTRIC MOTOR AND ELECTRIC GENERATOR | June 2020 | March 2022 | Allow | 21 | 1 | 1 | Yes | No |
| 16891492 | SPLITTER AND GUIDE VANE ARRANGEMENT FOR GAS TURBINE ENGINES | June 2020 | June 2023 | Allow | 36 | 2 | 0 | Yes | No |
| 16857055 | PLUMBING WITH INTERNAL FLOW GUIDES | April 2020 | March 2022 | Allow | 22 | 1 | 1 | Yes | No |
| 16852856 | SYSTEM AND METHOD FOR CONTROLLING ENGINE SPEED WITH BOWED ROTOR MITIGATION | April 2020 | February 2022 | Allow | 22 | 1 | 0 | Yes | No |
| 16849508 | INERTIAL PARTICLE SEPARATOR FOR TURBINE ENGINE | April 2020 | August 2021 | Allow | 16 | 0 | 0 | Yes | No |
| 16843349 | DYNAMIC THERMAL LOAD MONITORING AND MITIGATION FOR AIRCRAFT SYSTEMS | April 2020 | April 2022 | Allow | 24 | 1 | 1 | Yes | No |
| 16754076 | METHOD FOR THE CONTROL OF THE ANTI-ICING SYSTEM OF THE AIRCRAFT GAS TURBINE ENGINE | April 2020 | July 2022 | Abandon | 28 | 2 | 0 | No | No |
| 16824171 | TURBINE ENGINE WITH CENTRIFUGAL COMPRESSOR HAVING IMPELLER BACKPLATE OFFTAKE | March 2020 | February 2022 | Allow | 23 | 0 | 0 | Yes | No |
| 16818995 | SYSTEM AND METHOD FOR ENGINE PRE-SHUTDOWN MOTORING | March 2020 | October 2023 | Abandon | 43 | 3 | 0 | Yes | No |
| 16781424 | STAGGERED HEAT EXCHANGER ARRAY WITH SIDE CURTAINS | February 2020 | April 2022 | Allow | 26 | 2 | 0 | Yes | No |
| 16774221 | GAS TURBINE ENGINE WITH CLUTCH SYSTEM BETWEEN LOW-PRESSURE COMPRESSOR AND LOW-PRESSURE TURBINE | January 2020 | January 2023 | Allow | 36 | 2 | 1 | Yes | No |
| 16745312 | ANTI-ICING SYSTEM HAVING A NOZZLE WITH A DEFLECTOR PLATE AND METHOD | January 2020 | March 2022 | Allow | 26 | 1 | 1 | Yes | No |
| 16629418 | Hydraulic System | January 2020 | August 2021 | Allow | 19 | 0 | 1 | Yes | No |
| 16725177 | AIR TURBINE STARTER AIR VALVE | December 2019 | October 2021 | Allow | 22 | 1 | 0 | Yes | No |
| 16693430 | SPARK PLUG ASSEMBLIES FOR TURBOMACHINES | November 2019 | May 2024 | Allow | 54 | 3 | 1 | Yes | No |
| 16678682 | LIQUID AIR POWER AND STORAGE | November 2019 | May 2024 | Abandon | 55 | 4 | 0 | No | No |
| 16609557 | INTAKE DUCT FOR A GAS-FUELLED OR DIESEL-FUELLED TURBINE EQUIPPED WITH A WATER SATURATION STRUCTURE | October 2019 | October 2022 | Allow | 36 | 2 | 1 | Yes | No |
| 16661677 | AIR TURBINE START SYSTEM | October 2019 | November 2021 | Abandon | 25 | 1 | 0 | No | No |
| 16656262 | SCAVENGE METHODOLOGIES FOR TURBINE ENGINE PARTICLE SEPARATION CONCEPTS | October 2019 | April 2022 | Allow | 30 | 1 | 1 | Yes | No |
| 16654436 | Turbine Powered Electricity Generation | October 2019 | March 2024 | Allow | 53 | 6 | 1 | Yes | Yes |
| 16654706 | GAS TURBINE ENGINE WITH REVERSIBLE HEAT EXCHANGER | October 2019 | January 2022 | Allow | 27 | 1 | 1 | Yes | No |
| 16600942 | FLEXIBLE SEAL FOR GAS TURBINE ENGINE | October 2019 | October 2021 | Allow | 24 | 0 | 1 | Yes | No |
| 16593746 | ELECTRIC PUMP ASSISTED FUEL SYSTEM | October 2019 | August 2024 | Abandon | 58 | 4 | 1 | Yes | No |
| 16590430 | METHOD OF REPLACING A FAN MODULE, ENGINE CORE MODULE, OR FAN CASE MODULE IN A GAS TURBINE ENGINE | October 2019 | February 2021 | Allow | 17 | 2 | 1 | Yes | No |
| 16586016 | FUEL NOZZLE STRUCTURE FOR AIR ASSIST INJECTION | September 2019 | December 2021 | Allow | 26 | 1 | 1 | Yes | No |
| 16577649 | SPALL PLATE FOR CONSUMABLE COMBUSTOR SUPPORT STRUCTURES | September 2019 | September 2021 | Allow | 24 | 0 | 1 | Yes | No |
| 16574946 | TURBOMACHINE FITTED WITH A THERMO-ACOUSTIC SYSTEM | September 2019 | December 2021 | Allow | 27 | 1 | 1 | Yes | No |
| 16573013 | INERTIAL PARTICLE SEPARATOR FOR AIRCRAFT ENGINE | September 2019 | January 2022 | Allow | 28 | 0 | 1 | Yes | No |
This analysis examines appeal outcomes and the strategic value of filing appeals for examiner SEBASCO CHENG, STEPHANIE.
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.
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.
⚠ 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 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.
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.
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.
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.
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.
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.
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.
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.
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.
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'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).
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.