Detailed information about the 100 most recent patent applications.
| Application Number | Title | Filing Date | Disposal Date | Disposition | Time (months) | Office Actions | Restrictions | Interview | Appeal |
|---|---|---|---|---|---|---|---|---|---|
| 18937193 | ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE | November 2024 | June 2025 | Allow | 7 | 1 | 0 | No | No |
| 18802196 | GAS TURBINE CONTROL DEVICE AND GAS TURBINE CONTROL METHOD | August 2024 | January 2025 | Allow | 5 | 0 | 0 | No | No |
| 18753121 | GAS TURBINE FUEL TEMPERATURE | June 2024 | April 2025 | Allow | 10 | 2 | 0 | Yes | No |
| 18753446 | FUELDRAULIC HEAT MANAGEMENT SYSTEM | June 2024 | April 2025 | Allow | 10 | 3 | 0 | Yes | No |
| 18750497 | ANNULAR DOME ASSEMBLY FOR A COMBUSTOR | June 2024 | May 2025 | Allow | 11 | 1 | 0 | No | No |
| 18675809 | GAS TURBINE ENGINE COMPRESSION SYSTEM WITH CORE COMPRESSOR PRESSURE RATIO | May 2024 | March 2025 | Allow | 10 | 1 | 0 | No | No |
| 18656372 | FUEL SUPPLY CIRCUIT OF AN AIRCRAFT ENGINE | May 2024 | April 2025 | Allow | 11 | 1 | 0 | Yes | No |
| 18646753 | ATTENUATED COMBUSTION FOR CLEAN POWER AND HYDROGEN CAPTURE | April 2024 | February 2025 | Allow | 10 | 2 | 0 | Yes | No |
| 18634812 | SYSTEM AND METHOD HAVING FLAME STABILIZERS FOR ISOTHERMAL EXPANSION IN TURBINE STAGE OF GAS TURBINE ENGINE | April 2024 | March 2025 | Allow | 11 | 1 | 0 | Yes | No |
| 18634814 | SYSTEM AND METHOD HAVING FLAME STABILIZERS FOR ISOTHERMAL EXPANSION IN TURBINE STAGE OF GAS TURBINE ENGINE | April 2024 | November 2024 | Allow | 7 | 1 | 0 | Yes | No |
| 18620155 | COMPACT SINGLE VARIABLE DISPLACEMENT PUMP FUEL SYSTEM WITH AUGMENTOR CONTROLLED HIGH PRESSURE FUEL OIL COOLER AND GAS GENERATOR FAULT ACCOMMODATION | March 2024 | February 2025 | Allow | 11 | 0 | 0 | No | No |
| 18608132 | PROPULSION ASSEMBLY COMPRISING A FUEL CONDITIONING SYSTEM POSITIONED BEHIND A DEBRIS EJECTION ZONE, AIRCRAFT COMPRISING AT LEAST ONE SUCH PROPULSION ASSEMBLY | March 2024 | June 2025 | Allow | 15 | 1 | 0 | No | No |
| 18592194 | METHODS AND APPARATUS TO PRODUCE HYDROGEN GAS TURBINE PROPULSION | February 2024 | February 2025 | Allow | 11 | 1 | 0 | No | No |
| 18591414 | THERMAL MANAGEMENT SYSTEMS HAVING AN OIL TANK COMPRISING SOLID-SOLID PHASE CHANGE MATERIAL FOR GAS TURBINE ENGINES | February 2024 | January 2025 | Allow | 10 | 1 | 0 | No | No |
| 18442719 | INDUCER ASSEMBLY FOR A TURBINE ENGINE | February 2024 | March 2025 | Allow | 13 | 1 | 0 | No | No |
| 18293825 | IMPROVED METHOD FOR ESTIMATING AND SETTING EXHAUST PURGE TIME IN A COMBUSTION SYSTEM AND COMBUSTION SYSTEM THEREOF | January 2024 | May 2025 | Allow | 16 | 1 | 0 | Yes | No |
| 18423788 | INJECTOR WITH TANGENTIAL FEED CONDUITS FOR HYDROGEN-DRIVEN GAS TURBINE ENGINE | January 2024 | May 2025 | Allow | 16 | 2 | 0 | No | No |
| 18292047 | ELECTRICITY GENERATION SYSTEM AND AIRCRAFT | January 2024 | February 2025 | Allow | 12 | 1 | 0 | No | No |
| 18291558 | TRANSFER OF POWER BETWEEN THE HIGH-PRESSURE SHAFT AND THE LOW-PRESSURE SHAFT OF A TURBOMACHINE | January 2024 | June 2025 | Allow | 17 | 1 | 0 | No | No |
| 18410493 | AIRCRAFT PERFORMANCE OPTIMIZATION BASED ON ENGINE PERFORMANCE MONITORING | January 2024 | January 2025 | Allow | 12 | 1 | 0 | No | No |
| 18539824 | MULTI-COMPONENT SWIRL VALVES | December 2023 | June 2025 | Allow | 18 | 1 | 1 | No | No |
| 18536711 | PLANETARY GEAR SYSTEM ARRANGEMENT WITH AUXILIARY OIL SYSTEM | December 2023 | May 2025 | Allow | 17 | 1 | 0 | No | No |
| 18537161 | STEAM INJECTED TURBINE ENGINE STEAM GENERATION CONTROL | December 2023 | March 2025 | Allow | 15 | 1 | 0 | No | No |
| 18533447 | THERMODYNAMIC APPARATUS | December 2023 | August 2024 | Allow | 9 | 1 | 0 | Yes | No |
| 18567408 | FUEL CONDITIONING SYSTEM AND METHOD CONFIGURED TO SUPPLY AN AIRCRAFT TURBINE ENGINE WITH FUEL FROM A CRYOGENIC TANK | December 2023 | August 2024 | Allow | 8 | 0 | 0 | No | No |
| 18524753 | CMC STEPPED COMBUSTOR LINER | November 2023 | March 2025 | Allow | 16 | 2 | 0 | No | No |
| 18509536 | COMBINED CYCLE POWER PLANTS WITH EXHAUST GAS RECIRCULATION INTERCOOLING | November 2023 | May 2025 | Allow | 18 | 2 | 0 | Yes | No |
| 18503279 | STRUT MICROTUBE COUNTERFLOW EVAPORATOR | November 2023 | March 2025 | Allow | 17 | 1 | 0 | No | No |
| 18559497 | FUEL INJECTOR AND FUEL NOZZLE FOR A GAS TURBINE, AND GAS TURBINE ENGINE INCLUDING THE NOZZLE | November 2023 | March 2025 | Allow | 16 | 1 | 0 | Yes | No |
| 18287745 | FUEL SUPPLY SYSTEM WITH AIR EXPULSION DRAIN FOR AN AIRCRAFT ENGINE | October 2023 | January 2025 | Allow | 15 | 2 | 0 | Yes | No |
| 18555890 | DIFFUSION CONE FOR THE REAR PART OF A JET ENGINE INCORPORATING A FLAME-HOLDER RING AT THE TRAILING EDGE | October 2023 | August 2024 | Allow | 10 | 1 | 0 | No | No |
| 18372493 | AIR INTAKE FOR AN AIRCRAFT PROPULSION SYSTEM ENGINE ASSEMBLY | September 2023 | December 2024 | Allow | 15 | 2 | 0 | Yes | No |
| 18244425 | VARIABLE DISPLACEMENT PUMP (VDP) SYSTEMS WITH DRY-OUT CENTRIFUGAL MAIN PUMP | September 2023 | April 2025 | Allow | 19 | 1 | 0 | Yes | No |
| 18244390 | VARIABLE DISPLACEMENT PUMP (VDP) SYSTEMS WITH DUAL DRY OUT PUMPS | September 2023 | April 2025 | Allow | 19 | 1 | 0 | Yes | No |
| 18453017 | Fuel Unit Health Monitoring System | August 2023 | November 2024 | Allow | 14 | 1 | 0 | No | No |
| 18230805 | FUEL SYSTEM FOR DUAL USE GAS TURBINE ENGINE MAIN FUEL PUMP | August 2023 | November 2024 | Allow | 15 | 1 | 1 | Yes | No |
| 18264328 | THRUST REVERSER COMPRISING MOVABLE GRIDS AND COWLS ASSEMBLED BY RECESSING | August 2023 | July 2024 | Allow | 11 | 1 | 0 | No | No |
| 18275081 | PREMIXER INJECTOR IN GAS TURBINE ENGINE | July 2023 | September 2024 | Allow | 13 | 2 | 0 | No | No |
| 18275097 | THRUST ENHANCING DEVICE | July 2023 | June 2024 | Allow | 11 | 1 | 0 | No | No |
| 18226163 | HYDRAULIC MOTORING OF ENGINE | July 2023 | October 2024 | Allow | 15 | 0 | 1 | Yes | No |
| 18224753 | VARIABLE RESTRICTION OF A FUEL CIRCUIT OF A FUEL NOZZLE | July 2023 | December 2024 | Allow | 17 | 2 | 0 | Yes | No |
| 18270634 | GAS TURBINE EQUIPMENT WITH COMPRESSOR AIRFLOW CONTROL RESPONSIVE TO NOx CONCENTRATION AND CONTROL METHOD THEREOF | June 2023 | April 2024 | Allow | 10 | 0 | 0 | No | No |
| 18216141 | AIRCRAFT PROPULSION SYSTEM WITH TURBINE ENGINE AND EXHAUST HEAT EXCHANGER | June 2023 | October 2024 | Allow | 16 | 1 | 0 | No | No |
| 18215394 | ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE | June 2023 | September 2024 | Allow | 14 | 1 | 0 | No | No |
| 18214250 | FUEL SYSTEM HAVING VARIABLE DISPLACEMENT PUMP FAILURE MODES | June 2023 | March 2024 | Allow | 9 | 1 | 0 | No | No |
| 18340508 | REDUNDANT ELECTRO-HYDRAULIC SERVO VALVE (EHSV) CONTROL IN A FUEL METERING SYSTEM | June 2023 | December 2023 | Allow | 6 | 0 | 0 | No | No |
| 18213053 | FUEL SYSTEMS HAVING THERMAL RECIRCULATION | June 2023 | December 2023 | Allow | 5 | 0 | 0 | Yes | No |
| 18337559 | FUEL MANAGEMENT SYSTEM | June 2023 | March 2024 | Allow | 8 | 1 | 0 | No | No |
| 18208451 | DIRECT CONTROLLED VARIABLE DISPLACEMENT PUMP FUEL SYSTEMS WITH LOW PRESSURE THERMAL RECIRCULATION PUMPING | June 2023 | April 2025 | Allow | 22 | 1 | 0 | No | No |
| 18327629 | TURBINE ENGINE HAVING A THRUST REVERSER SYSTEM | June 2023 | March 2025 | Abandon | 21 | 2 | 0 | No | No |
| 18202606 | COOLING FLUID USED AS SECONDARY FUEL SOURCE | May 2023 | September 2024 | Allow | 16 | 0 | 0 | No | No |
| 18199742 | AXIALLY OFFSET VANE ARRAYS IN TURBINE ENGINE BYPASS | May 2023 | August 2024 | Allow | 15 | 2 | 0 | No | No |
| 18197499 | PUMP SYSTEM FOR A GAS TURBINE ENGINE | May 2023 | May 2024 | Allow | 12 | 2 | 0 | No | No |
| 18196704 | SYSTEM AND METHOD FOR IDENTIFYING BLOCKAGE OF AN AIR INTAKE FOR AN AIRCRAFT PROPULSION SYSTEM | May 2023 | March 2024 | Allow | 10 | 1 | 0 | No | No |
| 18311660 | FUEL SYSTEMS FOR AIRCRAFT ENGINES | May 2023 | June 2024 | Allow | 13 | 1 | 0 | No | No |
| 18310365 | DOUBLE-SKIN LINER FOR A GAS TURBINE | May 2023 | May 2024 | Abandon | 12 | 1 | 0 | No | No |
| 18307450 | COMPRESSOR WITH ANTI-ICE INLET | April 2023 | September 2024 | Allow | 17 | 2 | 0 | No | No |
| 18137887 | DUCTED FIREWALL WITH UPPER BIFI BLEED FOR MODULATED CORE VENTILATION | April 2023 | August 2024 | Allow | 16 | 2 | 0 | Yes | No |
| 18303111 | SYSTEMS AND METHODS WITH DISTRIBUTED BLEED FOR GAS TURBINE ENGINE COMPRESSOR STABILIZATION | April 2023 | September 2024 | Allow | 17 | 2 | 0 | Yes | No |
| 18302081 | BYPASS HEAT EXCHANGER CONFIGURATION TO REROUTE CORE FLOW | April 2023 | April 2024 | Allow | 12 | 1 | 0 | Yes | No |
| 18132257 | COMPACT SAFETY IGNITION DEVICE FOR DUAL PULSE MOTOR | April 2023 | January 2024 | Allow | 9 | 1 | 0 | Yes | No |
| 18122067 | MICRO-TURBINE GAS GENERATOR AND PROPULSIVE SYSTEM | March 2023 | February 2025 | Abandon | 23 | 3 | 0 | No | No |
| 18119017 | SYSTEM AND METHOD FOR OPERATING A MULTI-ENGINE AIRCRAFT | March 2023 | August 2023 | Allow | 6 | 1 | 0 | No | No |
| 18176777 | METHODS AND SYSTEMS FOR CONTROLLING AN ENGINE SYSTEM OF A VEHICLE | March 2023 | January 2025 | Allow | 23 | 1 | 0 | No | No |
| 18176246 | Heat Driven Thermal Management Systems and Methods for Operating the Same | February 2023 | September 2024 | Allow | 19 | 2 | 0 | Yes | No |
| 18114747 | AIRCRAFT ENGINE FOR NITROGEN OXIDE REDUCTION | February 2023 | November 2024 | Allow | 21 | 2 | 0 | Yes | No |
| 18113729 | BAFFLED THERMOCLINES IN THERMODYNAMIC CYCLE SYSTEMS | February 2023 | June 2024 | Allow | 16 | 2 | 0 | Yes | No |
| 18173175 | Afterburner structure with self-excited sweeping oscillating fuel injection nozzles | February 2023 | November 2023 | Allow | 9 | 1 | 0 | No | No |
| 18109441 | ADJUSTABLE PRIMARY AND SUPPLEMENTAL POWER UNITS | February 2023 | January 2024 | Allow | 11 | 1 | 0 | Yes | No |
| 18104408 | GAS TURBINE ENGINE COMBUSTOR WITH A SET OF DILUTION PASSAGES | February 2023 | July 2024 | Allow | 18 | 3 | 0 | Yes | No |
| 18098463 | GAS TURBINE ENGINE COMPRESSION SYSTEM WITH CORE COMPRESSOR PRESSURE RATIO | January 2023 | March 2024 | Allow | 14 | 1 | 0 | Yes | No |
| 18154134 | ACCESSORY GEARBOX COVER WITH PLANAR LINKING MEMBER | January 2023 | June 2024 | Allow | 17 | 1 | 0 | No | No |
| 18096140 | SYSTEMS AND METHODS FOR STARTING A GAS TURBINE ENGINE | January 2023 | June 2023 | Allow | 5 | 0 | 0 | No | No |
| 18093091 | REHEAT ASSEMBLY | January 2023 | August 2023 | Allow | 7 | 1 | 0 | No | No |
| 18093166 | TANGENTIAL TURBOFAN PROPULSION SYSTEM | January 2023 | July 2024 | Abandon | 19 | 2 | 0 | No | No |
| 18092120 | SYSTEM AND METHOD HAVING FLAME STABILIZERS FOR ISOTHERMAL EXPANSION IN TURBINE STAGE OF GAS TURBINE ENGINE | December 2022 | December 2023 | Allow | 12 | 1 | 0 | Yes | No |
| 18069669 | ALTERNATIVE FUEL FAST START SYSTEMS FOR GAS TURBINE ENGINES | December 2022 | May 2024 | Allow | 17 | 2 | 0 | No | No |
| 18084768 | PUMPS WITH BACKUP CAPABILITY | December 2022 | December 2023 | Allow | 12 | 1 | 0 | No | No |
| 18082008 | METHOD AND SYSTEM FOR GOVERNING AN ENGINE AT LOW POWER | December 2022 | December 2023 | Allow | 12 | 1 | 0 | No | No |
| 17993082 | INDUCER ASSEMBLY FOR A TURBINE ENGINE | November 2022 | October 2023 | Allow | 11 | 1 | 0 | No | No |
| 17964134 | JET ENGINE HAVING ELECTRICALLY POWERED SUPERHEATING SECTION | October 2022 | November 2023 | Allow | 13 | 2 | 0 | Yes | No |
| 17963029 | TURBINE ENGINE INDUCER ASSEMBLY | October 2022 | August 2023 | Allow | 10 | 1 | 0 | No | No |
| 17937605 | FLAME DETECTOR LENS MAINTENANCE SYSTEM | October 2022 | April 2025 | Allow | 30 | 2 | 0 | No | No |
| 17907420 | THERMODYNAMIC APPARATUS | September 2022 | October 2023 | Allow | 13 | 2 | 0 | Yes | No |
| 17946708 | HYDROGEN FUEL SYSTEM FOR A GAS TURBINE ENGINE | September 2022 | October 2023 | Allow | 13 | 1 | 0 | No | No |
| 17946499 | GAS TURBINE ENGINES WITH A FUEL CELL ASSEMBLY | September 2022 | February 2025 | Allow | 29 | 4 | 0 | Yes | No |
| 17929359 | AERODYNAMIC COMBUSTOR LINER DESIGN FOR EMISSIONS REDUCTIONS | September 2022 | April 2023 | Allow | 7 | 1 | 0 | No | No |
| 17929360 | ACOUSTIC DAMPER FOR COMBUSTOR | September 2022 | May 2023 | Allow | 9 | 1 | 0 | No | No |
| 17901383 | HYDROGEN FUEL SYSTEM | September 2022 | May 2024 | Allow | 20 | 2 | 0 | No | No |
| 17823732 | FUEL DELIVERY SYSTEM WITH PURGE GAS STEP AND FUEL GAS FLUSHING STEP AND METHOD THEREOF | August 2022 | May 2023 | Allow | 8 | 1 | 0 | No | No |
| 17896762 | VARIABLE RESTRICTION OF A FUEL CIRCUIT OF A FUEL NOZZLE | August 2022 | October 2023 | Allow | 14 | 1 | 0 | No | No |
| 17895969 | FUEL INJECTOR MANIFOLD HAVING TRIM DEVICE THEREIN | August 2022 | May 2023 | Allow | 8 | 1 | 0 | Yes | No |
| 17759208 | FUEL SUPPLY CIRCUIT OF AN AIRCRAFT ENGINE | July 2022 | February 2024 | Allow | 18 | 2 | 0 | Yes | No |
| 17870078 | FUEL SYSTEM WITH BACKUP PUMP SOURCE SELECTION | July 2022 | September 2023 | Allow | 14 | 1 | 0 | Yes | No |
| 17869428 | MODULATING FUEL FOR A TURBINE ENGINE | July 2022 | December 2023 | Allow | 17 | 2 | 0 | Yes | No |
| 17868222 | TWO STAGE FUEL DELIVERY SYSTEM FOR AN AIRCRAFT | July 2022 | April 2024 | Allow | 21 | 1 | 1 | Yes | No |
| 17863011 | COMBINED CYCLE POWER PLANTS WITH EXHAUST GAS RECIRCULATION INTERCOOLING | July 2022 | August 2023 | Allow | 13 | 2 | 0 | Yes | No |
| 17811762 | ANNULAR DOME ASSEMBLY FOR A COMBUSTOR | July 2022 | March 2024 | Allow | 20 | 3 | 0 | No | No |
| 17857996 | SYSTEMS AND METHODS FOR BLEED VALVE CONTROL IN FUEL SYSTEMS | July 2022 | March 2023 | Allow | 8 | 1 | 0 | Yes | No |
| 17854643 | SYSTEM AND METHOD FOR CONTROLLING DUAL STARTER AIR VALVE | June 2022 | July 2023 | Allow | 13 | 2 | 1 | No | No |
This analysis examines appeal outcomes and the strategic value of filing appeals for examiner CHAU, ALAIN.
With a 36.4% reversal rate, the PTAB reverses the examiner's rejections in a meaningful percentage of cases. This reversal rate is above the USPTO average, indicating that appeals have better success 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, 33.3% 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 show good success rates. If you have a strong case on the merits, consider fully prosecuting the appeal to a Board decision.
✓ Filing a Notice of Appeal is strategically valuable. The act of filing often prompts favorable reconsideration during the mandatory appeal conference.
Examiner CHAU, ALAIN works in Art Unit 3741 and has examined 559 patent applications in our dataset. With an allowance rate of 79.2%, this examiner has a below-average tendency to allow applications. Applications typically reach final disposition in approximately 33 months.
Examiner CHAU, ALAIN's allowance rate of 79.2% places them in the 41% percentile among all USPTO examiners. This examiner has a below-average tendency to allow applications.
On average, applications examined by CHAU, ALAIN 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 CHAU, ALAIN is 33 months. This places the examiner in the 29% percentile for prosecution speed. Prosecution timelines are slightly slower than average with this examiner.
Conducting an examiner interview provides a +30.0% benefit to allowance rate for applications examined by CHAU, ALAIN. This interview benefit is in the 81% 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, 28.0% of applications are subsequently allowed. This success rate is in the 40% 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 40.6% of cases where such amendments are filed. This entry rate is in the 55% percentile among all examiners. Strategic Recommendation: This examiner shows above-average receptiveness to after-final amendments. If your amendments clearly overcome the rejections and do not raise new issues, consider filing after-final amendments before resorting to an RCE.
When applicants request a pre-appeal conference (PAC) with this examiner, 33.3% result in withdrawal of the rejection or reopening of prosecution. This success rate is in the 32% 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 54.2% of appeals filed. This is in the 20% percentile among all examiners. Of these withdrawals, 15.4% 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, 50.0% are granted (fully or in part). This grant rate is in the 62% percentile among all examiners. Strategic Note: Petitions show above-average success regarding this examiner's actions. Petitionable matters include restriction requirements (MPEP § 1002.02(c)(2)) and various procedural issues.
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 1.8% of allowed cases (in the 63% 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.