Detailed information about the 100 most recent patent applications.
| Application Number | Title | Filing Date | Disposal Date | Disposition | Time (months) | Office Actions | Restrictions | Interview | Appeal |
|---|---|---|---|---|---|---|---|---|---|
| 18990685 | GEARBOX ASSEMBLY WITH LUBRICANT EXTRACTION VOLUME RATIO | December 2024 | June 2025 | Allow | 5 | 1 | 0 | Yes | No |
| 18990706 | GEARBOX ASSEMBLY WITH LUBRICANT EXTRACTION VOLUME RATIO | December 2024 | February 2025 | Allow | 2 | 0 | 0 | No | No |
| 18852382 | SUSPENSION OF A TRIPLE-FLOW AIRCRAFT TURBINE ENGINE | September 2024 | June 2025 | Allow | 8 | 0 | 0 | No | No |
| 18850333 | COMBUSTOR AND GAS TURBINE | September 2024 | May 2025 | Allow | 8 | 0 | 0 | No | No |
| 18753092 | OPERATING A GAS TURBINE ENGINE | June 2024 | October 2024 | Allow | 4 | 1 | 0 | No | No |
| 18753081 | FUEL CHARACTERISTIC | June 2024 | April 2025 | Allow | 9 | 3 | 0 | No | No |
| 18616576 | PROPULSION ASSEMBLY COMPRISING AT LEAST ONE REGULATED VENTILATION DEVICE, AIRCRAFT COMPRISING SUCH A PROPULSION ASSEMBLY | March 2024 | June 2025 | Allow | 14 | 2 | 0 | No | No |
| 18601267 | THRUST REVERSER BLOCKER DOOR WITH FAIRING | March 2024 | February 2025 | Allow | 11 | 1 | 0 | No | No |
| 18601959 | HEAT TRANSFER DEVICE WITH NESTED LAYERS OF HELICAL FLUID CHANNELS | March 2024 | January 2025 | Allow | 11 | 1 | 0 | No | No |
| 18594975 | ENGINE NACELLE ANTI-ICE SWIRL SYSTEM WITH UNSTEADY FLUID FLOW | March 2024 | December 2024 | Allow | 9 | 1 | 0 | Yes | No |
| 18434128 | GAS TURBINE ENGINE HAVING A HEAT EXCHANGER LOCATED IN AN ANNULAR DUCT | February 2024 | March 2025 | Allow | 14 | 1 | 0 | Yes | No |
| 18434047 | GAS TURBINE ENGINE HAVING A HEAT EXCHANGER LOCATED IN AN ANNULAR DUCT | February 2024 | February 2025 | Allow | 13 | 1 | 0 | Yes | No |
| 18432285 | GAS TURBINE ENGINE HAVING A HEAT EXCHANGER LOCATED IN AN ANNULAR DUCT | February 2024 | September 2024 | Allow | 8 | 1 | 0 | No | No |
| 18432315 | GAS TURBINE ENGINE HAVING A HEAT EXCHANGER LOCATED IN AN ANNULAR DUCT | February 2024 | June 2025 | Allow | 17 | 1 | 0 | No | No |
| 18430907 | GAS TURBINE ENGINE HAVING A HEAT EXCHANGER LOCATED IN AN ANNULAR DUCT | February 2024 | February 2025 | Allow | 13 | 1 | 0 | Yes | No |
| 18425207 | LINE REPLACEABLE FUEL INJECTOR PANELS WITH SINGLE HATCH INSTALLATION | January 2024 | March 2025 | Allow | 14 | 2 | 0 | No | No |
| 18407648 | WATER PRESSURE AND QUANTITY MONITORING FOR HYDROGEN STEAM INJECTED AND INTER-COOLED TURBINE ENGINE | January 2024 | January 2025 | Allow | 13 | 1 | 0 | No | No |
| 18404364 | GAS TURBINE ENGINE AND FUEL CELL ASSEMBLY | January 2024 | December 2024 | Allow | 11 | 1 | 0 | No | No |
| 18404083 | GAS TURBINE ENGINE AND FUEL CELL ASSEMBLY | January 2024 | November 2024 | Allow | 11 | 1 | 0 | No | No |
| 18575948 | GAS TURBINE FACILITY AND METHOD FOR SUPPRESSING DISCHARGE OF AMMONIA FROM GAS TURBINE FACILITY | January 2024 | October 2024 | Allow | 9 | 0 | 0 | No | No |
| 18394655 | VARIABLE AREA NOZZLE ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEM | December 2023 | June 2024 | Allow | 5 | 0 | 0 | No | No |
| 18540064 | MULTI-VOLUME ACOUSTIC RESONATOR FOR ROCKET ENGINE | December 2023 | July 2024 | Allow | 7 | 0 | 0 | No | No |
| 18525046 | BLEED VALVE ASSEMBLY FOR AIRCRAFT ENGINES | November 2023 | October 2024 | Allow | 10 | 1 | 0 | No | No |
| 18522393 | HYBRID AIRCRAFT POWER PLANT | November 2023 | November 2024 | Allow | 11 | 1 | 0 | No | No |
| 18523042 | AUXILIARY POWER SYSTEM | November 2023 | January 2025 | Allow | 14 | 1 | 0 | No | No |
| 18518811 | GAS TURBINE COMBUSTOR | November 2023 | August 2024 | Allow | 9 | 1 | 0 | No | No |
| 18515074 | TORCH ACTIVE CONTROL SYSTEM | November 2023 | October 2024 | Allow | 11 | 1 | 0 | No | No |
| 18560510 | THRUST REVERSER WITH CASCADES OF MOBILE VANES, COMPRISING A REAR STRUCTURE SUPPORTING THE CASCADES OF VANES AND INCORPORATING AN ACOUSTIC FUNCTION | November 2023 | August 2024 | Allow | 9 | 2 | 0 | No | No |
| 18503751 | COMBUSTOR FOR A GAS TURBINE ENGINE | November 2023 | April 2024 | Allow | 5 | 0 | 0 | No | No |
| 18494181 | EXHAUST NOZZLE ASSEMBLY, PROPULSION SYSTEM EMPLOYING THE EXHAUST NOZZLE ASSEMBLY, AND AIRCRAFT EMPLOYING THE PROPULSION SYSTEM | October 2023 | November 2024 | Allow | 13 | 1 | 0 | No | No |
| 18377406 | MAIN MIXER IN AN AXIAL STAGED COMBUSTOR FOR A GAS TURBINE ENGINE | October 2023 | April 2025 | Allow | 18 | 2 | 0 | No | No |
| 18469251 | METHOD OF CONTROLLING A DEVICE FOR SUPPLYING A PROPULSION SYSTEM OF AN AIRCRAFT AND SUPPLY DEVICE ENABLING EXECUTION OF THAT METHOD | September 2023 | May 2025 | Abandon | 20 | 2 | 0 | No | No |
| 18367302 | FUEL CONTAINMENT STRUCTURE FOR ENGINE FUEL DELIVERY SYSTEM | September 2023 | May 2024 | Allow | 8 | 0 | 0 | No | No |
| 18244780 | GAS TURBINE ENGINE | September 2023 | July 2024 | Allow | 10 | 1 | 0 | No | No |
| 18463793 | TURBINE ENGINE HAVING A BLEED SYSTEM | September 2023 | September 2024 | Allow | 12 | 1 | 0 | No | No |
| 18239459 | SYSTEMS AND METHOD FOR DETECTING AND RESPONDING TO ICING CONDITIONS IN GAS TURBINE ENGINES | August 2023 | July 2024 | Allow | 11 | 1 | 0 | No | No |
| 18454160 | HEAT EXCHANGER DIFFERENTIAL OIL TEMPERATURE DETERMINATION | August 2023 | December 2024 | Allow | 15 | 1 | 0 | No | No |
| 18452203 | TURBINE ENGINE WITH FAN BYPASS WATER INJECTION TO AUGMENT THRUST | August 2023 | August 2024 | Allow | 12 | 1 | 0 | No | No |
| 18233502 | THERMAL MANAGEMENT SYSTEM FOR AN AIRCRAFT | August 2023 | March 2025 | Allow | 19 | 1 | 0 | No | No |
| 18233607 | THERMAL MANAGEMENT SYSTEM FOR AN AIRCRAFT | August 2023 | March 2025 | Allow | 19 | 1 | 0 | Yes | No |
| 18446532 | TRAILING EDGE COOLING CIRCUIT | August 2023 | February 2025 | Allow | 18 | 2 | 0 | No | No |
| 18228424 | TRANSMISSION ASSEMBLY FOR AN AIRCRAFT ENGINE ASSEMBLY AND ARCHITECTURE FOR CONTROLLING SAME | July 2023 | July 2024 | Allow | 12 | 1 | 0 | Yes | No |
| 18360935 | TURBINE ENGINE INCLUDING AN ENGINE STARTER ASSEMBLY | July 2023 | March 2025 | Allow | 20 | 2 | 0 | Yes | No |
| 18360933 | ELECTRIC STARTER VERIFICATION DURING GAS-TURBINE ENGINE BARRING | July 2023 | August 2024 | Allow | 13 | 1 | 0 | No | No |
| 18224430 | AIRCRAFT PROPULSION SYSTEM WITH INLET AIR MONITORING SYSTEM AND METHOD | July 2023 | November 2024 | Allow | 16 | 1 | 0 | No | No |
| 18337749 | GAS TURBINE OPERATION | June 2023 | November 2023 | Allow | 5 | 1 | 0 | Yes | No |
| 18211092 | GAS TURBINE ENGINE WITH WATER RECOVERY SYSTEM | June 2023 | June 2025 | Allow | 24 | 4 | 0 | Yes | No |
| 18211083 | GAS TURBINE ENGINE WITH HYDROGEN FUEL SYSTEM | June 2023 | October 2024 | Allow | 16 | 2 | 0 | No | No |
| 18334009 | GAS TURBINE ENGINE WITH AIR/OIL COOLER HAVING AN AIRFLOW CONTROL BAFFLE | June 2023 | January 2024 | Allow | 8 | 0 | 0 | No | No |
| 18039800 | METHOD FOR PRODUCING ELECTRICAL AND/OR MECHANICAL ENERGY FOR A CONSUMER SYSTEM AND ASSOCIATED PRODUCTION SYSTEM | June 2023 | January 2025 | Allow | 20 | 2 | 0 | Yes | No |
| 18202727 | SELECTIVE POWER DISTRIBUTION FOR AN AIRCRAFT PROPULSION SYSTEM | May 2023 | May 2024 | Allow | 12 | 1 | 0 | No | No |
| 18318460 | JET PUMP SYSTEM | May 2023 | October 2024 | Allow | 17 | 1 | 0 | Yes | No |
| 18316505 | HYDROGEN FUELED TURBINE ENGINE PINCH POINT WATER SEPARATOR | May 2023 | July 2024 | Allow | 14 | 1 | 0 | No | No |
| 18140708 | RETAINER AND METHOD FOR DISASSEMBLING AN AIRCRAFT ENGINE | April 2023 | November 2024 | Allow | 18 | 1 | 1 | No | No |
| 18250964 | TURBOMACHINE TURBINE ASSEMBLY | April 2023 | September 2024 | Allow | 16 | 2 | 0 | Yes | No |
| 18307938 | REVERSE FLOW GAS TURBINE ENGINE HAVING ELECTRIC MACHINE | April 2023 | September 2023 | Allow | 5 | 0 | 0 | No | No |
| 18138508 | PLANETARY GEARBOX FOR GAS TURBINE ENGINE | April 2023 | July 2024 | Allow | 15 | 2 | 0 | No | No |
| 18186159 | Plasma Ignition and Combustion Assist System for Gas Turbine Engines | March 2023 | November 2024 | Allow | 20 | 1 | 0 | Yes | No |
| 18186161 | Plasma Ignition and Combustion Assist System for Gas Turbine Engines | March 2023 | April 2024 | Allow | 13 | 1 | 0 | No | No |
| 18184755 | AIRCRAFT ENGINE FLUID SYSTEM WITH SHUT-OFF VALVE | March 2023 | April 2024 | Allow | 13 | 1 | 0 | No | No |
| 18183758 | INTEGRAL ENGINE INLET FRAME AIR-COOLED OIL COOLING APPARATUS | March 2023 | October 2024 | Allow | 19 | 2 | 0 | Yes | No |
| 18176784 | COMBINED CYCLES | March 2023 | July 2024 | Allow | 16 | 1 | 0 | No | No |
| 18109593 | LINE REPLACEABLE FUEL INJECTOR PANELS WITH SINGLE HATCH INSTALLATION | February 2023 | October 2024 | Allow | 20 | 1 | 0 | No | No |
| 18168173 | HEAT EXCHANGER WITH BYPASS VALVE AND THERMAL FUSE | February 2023 | January 2024 | Allow | 11 | 0 | 1 | Yes | No |
| 18167643 | JET ENGINE THERMAL TRANSPORT BUS PUMPS | February 2023 | July 2023 | Allow | 5 | 0 | 0 | No | No |
| 18104990 | COMBUSTOR WITH CENTRAL FUEL INJECTION AND DOWNSTREAM AIR MIXING | February 2023 | June 2024 | Allow | 16 | 2 | 0 | Yes | Yes |
| 18104935 | COMBUSTOR WITH FUEL PLENUM WITH MIXING PASSAGES HAVING BAFFLES | February 2023 | September 2023 | Allow | 7 | 1 | 0 | Yes | No |
| 18160375 | GAS TURBINE ENGINE HAVING A HEAT EXCHANGER LOCATED IN AN ANNULAR DUCT | January 2023 | June 2023 | Allow | 5 | 0 | 0 | No | No |
| 18154683 | CENTRIFUGALLY PUMPED FUEL SYSTEM | January 2023 | January 2024 | Allow | 12 | 1 | 0 | No | No |
| 18082888 | CRYOGENIC COOLING SYSTEM FOR AN AIRCRAFT | December 2022 | March 2025 | Allow | 27 | 1 | 0 | No | No |
| 18082848 | CRYOGENIC COOLING SYSTEM FOR AN AIRCRAFT | December 2022 | March 2025 | Allow | 27 | 1 | 0 | No | No |
| 18074847 | PASSIVE SECONDARY AIR ASSIST NOZZLES | December 2022 | August 2023 | Allow | 9 | 1 | 0 | No | No |
| 17999343 | STRUCTURE FOR ASSEMBLING A PIECE COMPRISING A FIRST METAL PART AND A SECOND PART MADE OF AN ORGANIC MATRIX COMPOSITE MATERIAL | November 2022 | October 2023 | Allow | 11 | 0 | 0 | No | No |
| 17999180 | NACELLE FOR A PROPULSION ASSEMBLY WITH A VERY HIGH BYPASS RATIO, COMPRISING A REMOVABLE AND STRUCTURAL FRONT INTERNAL STRUCTURE | November 2022 | November 2023 | Allow | 12 | 1 | 0 | No | No |
| 17999106 | THRUST REVERSER FOR AN AIRCRAFT BYPASS TURBOJET ENGINE NACELLE | November 2022 | May 2024 | Allow | 17 | 3 | 0 | Yes | No |
| 17972604 | COMBINED CYCLE POWER PLANT HAVING REDUCED PARASITIC PUMPING LOSSES | October 2022 | July 2024 | Allow | 21 | 1 | 1 | Yes | No |
| 17972033 | AIRCRAFT PROPULSION ASSEMBLY COMPRISING A PLATE HEAT EXCHANGER, OF HEXAGONAL LONGITUDINAL SECTION, POSITIONED IN A BIFURCATION | October 2022 | July 2024 | Allow | 21 | 2 | 0 | No | No |
| 17918901 | MICRO-CATHODE ARC PROPULSION SYSTEM | October 2022 | December 2024 | Abandon | 26 | 2 | 0 | No | No |
| 17965662 | Turbine Engine with Preheat of Cryogenic Fuel via Intermediate Fluid | October 2022 | December 2023 | Allow | 14 | 1 | 0 | No | No |
| 17963237 | PROPULSION ASSEMBLY FOR AN AIRCRAFT | October 2022 | September 2023 | Allow | 11 | 1 | 0 | No | No |
| 17961667 | WASTE HEAT RECOVERY SYSTEM | October 2022 | February 2024 | Allow | 16 | 1 | 0 | No | No |
| 17995638 | ACOUSTICALLY OPTIMIZED DISCHARGE LINE GRID WITH CHANNELS | October 2022 | March 2023 | Allow | 5 | 0 | 0 | No | No |
| 17959534 | HEAT EXCHANGER FOR A GAS TURBINE ENGINE | October 2022 | February 2024 | Allow | 16 | 1 | 0 | No | No |
| 17905055 | AIR OUTLET FOR A NACELLE FOR AN AIRCRAFT BYPASS TURBOJET ENGINE COMPRISING A GUIDING DEVICE TO FAVOR A REVERSE THRUST PHASE | August 2022 | August 2024 | Allow | 23 | 2 | 0 | Yes | No |
| 17882643 | COMBINED POWER SYSTEM | August 2022 | February 2024 | Allow | 18 | 1 | 0 | No | No |
| 17796491 | COMBUSTOR AND GAS TURBINE | July 2022 | April 2024 | Allow | 20 | 1 | 0 | No | No |
| 17796377 | TURBINE | July 2022 | October 2023 | Allow | 14 | 1 | 0 | No | No |
| 17870123 | WATER PRESSURE AND QUANTITY MONITORING FOR HYDROGEN STEAM INJECTED AND INTER-COOLED TURBINE ENGINE | July 2022 | October 2023 | Allow | 15 | 0 | 1 | Yes | No |
| 17860746 | TURBO EXPANDERS FOR TURBINE ENGINES HAVING HYDROGEN FUEL SYSTEMS | July 2022 | February 2024 | Allow | 19 | 1 | 0 | Yes | No |
| 17859092 | HEAT EXCHANGER FOR A HYDROGEN FUEL DELIVERY SYSTEM | July 2022 | January 2024 | Allow | 18 | 1 | 0 | No | No |
| 17790661 | THRUST REVERSER COMPRISING DOORS FORMING AN UPWARD AIR DEFLECTION OPENING IN THE OPEN POSITION | July 2022 | February 2024 | Allow | 20 | 2 | 0 | No | No |
| 17790230 | ION BOOSTER FOR THRUST GENERATION | June 2022 | October 2024 | Abandon | 27 | 2 | 0 | No | No |
| 17852580 | SYSTEM AND METHOD FOR INSTALLATION OR REMOVAL OF ONE OR MORE COMBUSTION CANS | June 2022 | March 2025 | Allow | 32 | 1 | 1 | No | No |
| 17848798 | COMBUSTOR WITH IMPROVED AERODYNAMICS | June 2022 | January 2023 | Allow | 7 | 1 | 0 | No | No |
| 17843484 | MULTI-VOLUME ACOUSTIC RESONATOR FOR ROCKET ENGINE | June 2022 | August 2023 | Allow | 14 | 1 | 0 | Yes | No |
| 17842245 | TURBINE EXHAUST GAS RECIRCULATION MIXER BOX | June 2022 | August 2023 | Allow | 14 | 1 | 0 | No | No |
| 17745396 | Turbine Engine Gas-Inlet Cooling System and Turbine Engine Apparatus | May 2022 | July 2023 | Allow | 14 | 1 | 0 | No | No |
| 17742786 | TURBOFAN ENGINE WITH PRECOOLER | May 2022 | November 2023 | Allow | 18 | 1 | 0 | No | No |
| 17734723 | PASSIVELY ACTUATED VARIABLE AREA NOZZLE FOR AN AIRCRAFT PROPULSION SYSTEM | May 2022 | October 2022 | Allow | 6 | 0 | 0 | Yes | No |
| 17734282 | RETAINING EJECTED GAS TURBINE BLADES | May 2022 | August 2023 | Allow | 15 | 1 | 0 | Yes | No |
This analysis examines appeal outcomes and the strategic value of filing appeals for examiner KIM, CRAIG SANG.
With a 55.0% reversal rate, the PTAB has reversed the examiner's rejections more often than affirming them. This reversal rate is in the top 25% across the USPTO, indicating that appeals are more successful here than in most other areas.
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, 54.2% of applications that filed an appeal were subsequently allowed. This appeal filing benefit rate is in the top 25% across the USPTO, indicating that filing appeals is particularly effective here. The act of filing often prompts favorable reconsideration during the mandatory appeal conference.
✓ 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 KIM, CRAIG SANG works in Art Unit 3741 and has examined 852 patent applications in our dataset. With an allowance rate of 87.6%, this examiner has an above-average tendency to allow applications. Applications typically reach final disposition in approximately 34 months.
Examiner KIM, CRAIG SANG's allowance rate of 87.6% places them in the 63% percentile among all USPTO examiners. This examiner has an above-average tendency to allow applications.
On average, applications examined by KIM, CRAIG SANG receive 1.64 office actions before reaching final disposition. This places the examiner in the 45% percentile for office actions issued. This examiner issues fewer office actions than average, which may indicate efficient prosecution or a more lenient examination style.
The median time to disposition (half-life) for applications examined by KIM, CRAIG SANG is 34 months. This places the examiner in the 25% percentile for prosecution speed. Applications take longer to reach final disposition with this examiner compared to most others.
Conducting an examiner interview provides a +11.3% benefit to allowance rate for applications examined by KIM, CRAIG SANG. This interview benefit is in the 49% percentile among all examiners. Recommendation: Interviews provide a below-average benefit with this examiner.
When applicants file an RCE with this examiner, 34.7% of applications are subsequently allowed. This success rate is in the 72% 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 34.3% of cases where such amendments are filed. This entry rate is in the 43% 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, 66.7% result in withdrawal of the rejection or reopening of prosecution. This success rate is in the 55% 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 71.4% of appeals filed. This is in the 55% percentile among all examiners. Of these withdrawals, 34.0% occur early in the appeal process (after Notice of Appeal but before Appeal Brief). Strategic Insight: This examiner shows above-average willingness to reconsider rejections during appeals. The mandatory appeal conference (MPEP § 1207.01) provides an opportunity for reconsideration.
When applicants file petitions regarding this examiner's actions, 40.8% are granted (fully or in part). This grant rate is in the 41% percentile among all examiners. Strategic Note: Petitions show below-average success regarding this examiner's actions. Ensure you have a strong procedural basis before filing.
Examiner's Amendments: This examiner makes examiner's amendments in 5.8% of allowed cases (in the 90% percentile). Per MPEP § 1302.04, examiner's amendments are used to place applications in condition for allowance when only minor changes are needed. This examiner frequently uses this tool compared to other examiners, indicating a cooperative approach to getting applications allowed. Strategic Insight: If you are close to allowance but minor claim amendments are needed, this examiner may be willing to make an examiner's amendment rather than requiring another round of prosecution.
Quayle Actions: This examiner issues Ex Parte Quayle actions in 0.3% of allowed cases (in the 46% 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.