Detailed information about the 100 most recent patent applications.
| Application Number | Title | Filing Date | Disposal Date | Disposition | Time (months) | Office Actions | Restrictions | Interview | Appeal |
|---|---|---|---|---|---|---|---|---|---|
| 18909133 | GUIDE VANE ASSEMBLY | October 2024 | May 2025 | Allow | 7 | 0 | 0 | Yes | No |
| 18794116 | DUCTING ARRANGEMENT FOR A GAS TURBINE ENGINE | August 2024 | May 2025 | Allow | 10 | 1 | 1 | No | No |
| 18742458 | AIRCRAFT NACELLE EQUIPPED WITH AT LEAST ONE THRUST REVERSAL DEVICE COMPRISING AT LEAST ONE LONGITUDINAL DEFLECTOR CONFIGURED TO HOUSE A LONGITUDINAL ACTUATOR | June 2024 | May 2025 | Allow | 11 | 1 | 0 | Yes | No |
| 18666193 | LIMITED FLOW THRUST REVERSER ACTUATING | May 2024 | March 2025 | Allow | 10 | 1 | 0 | Yes | No |
| 18597532 | THRUST REVERSER WITH BLOCKER DOOR FOLDING LINKAGE | March 2024 | March 2025 | Allow | 12 | 0 | 1 | Yes | No |
| 18597547 | THRUST REVERSER WITH LOST MOTION DEVICE | March 2024 | April 2025 | Allow | 13 | 1 | 0 | Yes | No |
| 18390025 | MODULATING INTERNAL BALLISTICS IN A 3D-PRINTED ROCKET MOTOR AND AN ADDITIVE MANUFACTURING PROCESS | December 2023 | January 2025 | Allow | 12 | 1 | 0 | Yes | No |
| 18541303 | TURBINE ENGINE HAVING A FIRE BOX | December 2023 | March 2025 | Allow | 15 | 1 | 0 | Yes | No |
| 18559218 | METHOD FOR CONTROLLING A TURBOMACHINE COMPRISING AT LEAST ONE ELECTRIC MACHINE, AND ASSOCIATED CONTROL SYSTEM | November 2023 | February 2025 | Allow | 15 | 1 | 0 | Yes | No |
| 18287958 | CONTROL DEVICE FOR GAS TURBINE, GAS TURBINE FACILITY, METHOD FOR CONTROLLING GAS TURBINE, AND CONTROL PROGRAM FOR GAS TURBINE | October 2023 | September 2024 | Allow | 10 | 1 | 0 | No | No |
| 18556702 | AIRCRAFT PROPULSION ASSEMBLY COMPRISING AN ACTUATOR CONNECTED TO A STRUCTURAL ARM SUCH AS AN OUTLET GUIDE VANE | October 2023 | June 2025 | Allow | 20 | 2 | 0 | Yes | No |
| 18378861 | Control Device And Plasma Energy Protective Apparatus For An Ion Thruster | October 2023 | February 2025 | Allow | 16 | 1 | 0 | No | No |
| 18377983 | Duplex Turbine Guide Vane Assembly | October 2023 | January 2025 | Abandon | 15 | 1 | 0 | No | No |
| 18470590 | GUIDE ASSEMBLY FOR AN AIRCRAFT PROPULSION UNIT | September 2023 | April 2025 | Allow | 19 | 2 | 1 | Yes | No |
| 18453069 | Uncommanded or Uncontrollable High Thrust Detection and Mitigation | August 2023 | March 2025 | Allow | 18 | 1 | 1 | Yes | No |
| 18233671 | Plug Nozzle and Thrust Reverser for High Mach Gas Turbine Engines | August 2023 | October 2024 | Allow | 14 | 1 | 0 | Yes | No |
| 18361205 | ARTICULATING SLIDER FOR NACELLE | July 2023 | August 2024 | Allow | 13 | 1 | 0 | No | No |
| 18222700 | Aircraft Heat Exchanger | July 2023 | May 2025 | Allow | 22 | 2 | 0 | Yes | No |
| 18350378 | METHOD AND APPARATUS TO MEASURE GAS TURBINE COMPRESSOR EXIT TEMPERATURE | July 2023 | February 2025 | Allow | 19 | 1 | 1 | Yes | No |
| 18347722 | ANTI-ICE SYSTEM FOR GAS TURBINE ENGINE AND INLET GUIDE VANE | July 2023 | November 2024 | Allow | 16 | 1 | 1 | Yes | No |
| 18211105 | AIRCRAFT PROPULSION SYSTEM WITH TURBINE ENGINE AND EXHAUST CONDENSER | June 2023 | April 2024 | Allow | 10 | 0 | 0 | Yes | No |
| 18211125 | AIRCRAFT PROPULSION SYSTEM WITH TURBINE ENGINE AND EXHAUST CONDENSER | June 2023 | April 2024 | Allow | 10 | 0 | 0 | Yes | No |
| 18335366 | SYSTEM AND METHOD FOR SYNCHROPHASING A PROPULSION SYSTEM USING ELECTRIC MACHINES | June 2023 | November 2024 | Allow | 17 | 1 | 1 | Yes | No |
| 18207136 | POWER CONVERSION SYSTEM INCLUDING ENGINE AND HEAT EXCHANGER | June 2023 | February 2025 | Abandon | 21 | 1 | 1 | No | No |
| 18205775 | LONG THROW LATCH FOR AIRCRAFT SYSTEM | June 2023 | January 2025 | Allow | 19 | 1 | 0 | Yes | No |
| 18199245 | GAS TURBINE ENGINE | May 2023 | October 2023 | Allow | 5 | 0 | 0 | Yes | No |
| 18318137 | ENVIRONMENTAL CONTROL SYSTEM | May 2023 | April 2025 | Allow | 23 | 2 | 0 | Yes | No |
| 18314322 | SELF-DAMPING ACTUATOR | May 2023 | August 2024 | Allow | 16 | 1 | 1 | No | No |
| 18314401 | TURBINE ENGINE HAVING A COMPOSITE ASSEMBLY | May 2023 | February 2025 | Allow | 21 | 2 | 0 | Yes | No |
| 18312342 | COWLING LATCH INTERLOCK MECHANISM | May 2023 | August 2024 | Allow | 15 | 0 | 0 | Yes | No |
| 18141825 | MISALIGNMENT LATCH FOR AN AIRCRAFT SYSTEM | May 2023 | May 2025 | Allow | 25 | 2 | 0 | Yes | No |
| 18302952 | COMBUSTION SYSTEM | April 2023 | May 2024 | Allow | 12 | 1 | 0 | No | No |
| 18303076 | DEFLECTOR PROVIDED WITH A SPOILER FOR A THRUST REVERSER OF AN AIRCRAFT ENGINE NACELLE | April 2023 | November 2024 | Allow | 19 | 2 | 0 | Yes | No |
| 18299526 | MIXED FLOW EXHAUST THRUST REVERSER WITH AREA CONTROL NOZZLE SYSTEMS AND METHODS | April 2023 | July 2024 | Allow | 15 | 1 | 1 | Yes | No |
| 18297835 | SYSTEM FOR CONTROLLING BLADE CLEARANCES WITHIN A GAS TURBINE ENGINE | April 2023 | January 2024 | Allow | 9 | 0 | 0 | Yes | No |
| 18124382 | THRUST REVERSER CASCADE AND METHOD OF MANUFACTURE | March 2023 | June 2025 | Abandon | 27 | 2 | 0 | No | No |
| 18245199 | METHOD FOR MANUFACTURING A COMPOSITE MATERIAL PART HAVING A CELLULAR STRUCTURE AND CORRESPONDING PART | March 2023 | March 2025 | Allow | 24 | 3 | 0 | Yes | No |
| 18175102 | TWO SERVOVALVE THRUST REVERSER ACTUATOR SYSTEM | February 2023 | June 2024 | Allow | 15 | 1 | 1 | Yes | No |
| 18109428 | GAS TURBINE ENGINE NOZZLE LOFT FOR THRUST REVERSER | February 2023 | February 2024 | Allow | 12 | 1 | 0 | Yes | No |
| 18100765 | ICING CONDITION IDENTIFICATION FOR GAS TURBINE ENGINE | January 2023 | September 2024 | Allow | 20 | 2 | 0 | Yes | No |
| 18005871 | THRUST REVERSER COMPRISING PIVOTING HALF-ASSEMBLIES AND A CONNECTING BEAM FOR THE HALF-ASSEMBLIES AT THE SIX O'CLOCK POSITION | January 2023 | January 2025 | Allow | 24 | 3 | 0 | Yes | No |
| 18063814 | REVERSE THRUST SYSTEM AND METHOD | December 2022 | November 2023 | Allow | 11 | 0 | 1 | Yes | No |
| 18074152 | BALK DEVICE FOR DOOR LOCK | December 2022 | September 2024 | Allow | 22 | 1 | 0 | No | No |
| 17965921 | WEAPON ENERGY HARVESTING BY GAS TURBINE ELECTRIC GENERATOR | October 2022 | October 2023 | Allow | 12 | 1 | 0 | No | No |
| 17962147 | THRUST REVERSER SYSTEM WITH ANGLED DOOR PIVOT AXES | October 2022 | October 2024 | Allow | 25 | 2 | 1 | Yes | No |
| 17939000 | ASSEMBLY FOR AN AIRCRAFT NACELLE AND COMPRISING A SUPPORT PANEL, A THERMAL PROTECTION ELEMENT AND A FASTENING SYSTEM | September 2022 | July 2024 | Allow | 22 | 0 | 0 | No | No |
| 17902559 | LATCH ASSEMBLY | September 2022 | February 2024 | Allow | 17 | 1 | 0 | Yes | No |
| 17900946 | TEXTILE CASCADE ASSEMBLY | September 2022 | August 2023 | Allow | 11 | 0 | 0 | Yes | No |
| 17797528 | DEVICE FOR ATTACHING A CONNECTING ROD SMALL END FOR A THRUST REVERSAL CASCADE FLAP | August 2022 | September 2024 | Allow | 25 | 1 | 0 | No | No |
| 17817166 | TERTIARY LOCK | August 2022 | November 2023 | Allow | 16 | 1 | 0 | No | No |
| 17878360 | ASSEMBLY FOR A NACELLE OF AN AIRCRAFT ENGINE, SAID ASSEMBLY COMPRISING A FIXED COWL AND A COWL MOUNTED SO AS TO BE ABLE TO MOVE ON THE FIXED COWL | August 2022 | January 2024 | Allow | 18 | 1 | 0 | Yes | No |
| 17874825 | DRIVE SYSTEM FOR TRANSLATING STRUCTURE | July 2022 | December 2023 | Allow | 17 | 1 | 1 | Yes | No |
| 17869488 | THRUST REVERSER SYSTEM LATCH ASSEMBLY AND METHOD OF OPERATING SAME | July 2022 | November 2023 | Allow | 16 | 0 | 1 | Yes | No |
| 17867507 | SURGE RECOVERY SYSTEM AND METHODS | July 2022 | February 2024 | Allow | 19 | 1 | 1 | Yes | No |
| 17853691 | Multi-Mode Combined Cycle Propulsion Engine | June 2022 | August 2023 | Allow | 14 | 1 | 0 | Yes | No |
| 17842586 | DRIVE SYSTEM FOR TRANSLATING STRUCTURE | June 2022 | April 2024 | Allow | 22 | 2 | 1 | Yes | No |
| 17837992 | SEAL FOR GIMBALING AND/OR FIXED ROCKET ENGINE NOZZLES, AND ASSOCIATED SYSTEMS AND METHODS | June 2022 | March 2025 | Allow | 34 | 3 | 0 | Yes | No |
| 17828868 | Oblique Detonation Rocket Engine | May 2022 | July 2023 | Allow | 13 | 1 | 0 | Yes | No |
| 17664971 | COMBUSTOR WITH SECONDARY FUEL NOZZLE IN DILUTION FENCE | May 2022 | September 2024 | Allow | 28 | 3 | 1 | Yes | No |
| 17742620 | GAS TURBINE ENGINE | May 2022 | December 2023 | Allow | 19 | 1 | 1 | Yes | No |
| 17662684 | ACTUATOR SYSTEMS FOR THRUST REVERSER | May 2022 | May 2023 | Allow | 12 | 1 | 0 | Yes | No |
| 17734941 | THRUST REVERSER SINGLE DEGREE OF FREEDOM ACTUATOR MECHANISM SYSTEMS AND METHODS | May 2022 | October 2023 | Allow | 18 | 1 | 0 | Yes | No |
| 17720519 | THRUST REVERSER ACTUATION ARRANGEMENT AND DEPLOYABLE FAIRING SYSTEMS AND METHODS | April 2022 | September 2023 | Allow | 17 | 1 | 0 | Yes | No |
| 17716897 | AIRCRAFT SAFETY KEEPER FOR LATCH UTILIZATION | April 2022 | January 2024 | Allow | 21 | 1 | 0 | No | No |
| 17708220 | AIRCRAFT ENGINE PYLON HAVING A MOVABLE ASSEMBLY OF COWLS | March 2022 | December 2023 | Allow | 20 | 1 | 0 | No | No |
| 17707647 | GUIDE SYSTEMS FOR INSTALLING AIRCRAFT STRUCTURES | March 2022 | September 2024 | Allow | 29 | 2 | 1 | Yes | No |
| 17695560 | SHEARED EXHAUST NOZZLE | March 2022 | May 2025 | Abandon | 38 | 4 | 0 | Yes | No |
| 17690540 | THRUST REVERSER CASCADE AND METHOD OF MANUFACTURE | March 2022 | January 2023 | Allow | 11 | 0 | 0 | No | No |
| 17689418 | DEPLOYABLE FAIRING FOR DOOR REVERSERS SYSTEMS AND METHODS | March 2022 | October 2023 | Allow | 19 | 2 | 0 | Yes | No |
| 17688419 | VARIABLE AREA NOZZLE FOR AIRCRAFT PROPULSION SYSTEM | March 2022 | March 2024 | Allow | 24 | 3 | 0 | No | No |
| 17685649 | THRUST REVERSER PROVIDED WITH CABLE KINEMATICS FOR SCOOP FLAPS | March 2022 | January 2024 | Allow | 22 | 1 | 1 | Yes | No |
| 17678583 | ULTRA QUIET SPLIT FLOW THRUST REVERSER | February 2022 | January 2024 | Allow | 23 | 1 | 1 | Yes | No |
| 17650318 | INLET ARRANGEMENT, A PROPULSION SYSTEM, AND AN AIRCRAFT | February 2022 | October 2024 | Abandon | 33 | 2 | 0 | No | No |
| 17632832 | THRUST REVERSER FOR TURBOFAN PROPULSION SYSTEM OF AN AIRCRAFT AND THRUST REVERSAL METHOD | February 2022 | May 2024 | Abandon | 27 | 2 | 0 | No | No |
| 17631281 | ACOUSTIC ATTENUATION STRUCTURE MADE OF COMPOSITE MATERIAL AND METHOD FOR MANUFACTURING SAME | January 2022 | January 2024 | Allow | 24 | 4 | 0 | Yes | No |
| 17648764 | THERMOPLASTIC ACOUSTIC BLOCKER DOOR | January 2022 | September 2024 | Abandon | 32 | 4 | 0 | No | No |
| 17579938 | OPERABILITY GEARED TURBOFAN ENGINE INCLUDING COMPRESSOR SECTION VARIABLE GUIDE VANES | January 2022 | July 2023 | Allow | 17 | 2 | 0 | No | No |
| 17575686 | AIRCRAFT TURBOJET ENGINE COMPRISING TWO THRUST REVERSER MODULES | January 2022 | February 2023 | Allow | 13 | 0 | 1 | Yes | No |
| 17570728 | GEARED TURBOFAN WITH OVERSPEED PROTECTION | January 2022 | April 2025 | Allow | 39 | 2 | 0 | No | Yes |
| 17558019 | RESTRAINING PLUG | December 2021 | April 2025 | Allow | 40 | 2 | 1 | Yes | Yes |
| 17554695 | AIRCRAFT PROPULSION SYSTEM EXHAUST NOZZLE WITH EJECTOR PASSAGE(S) | December 2021 | April 2023 | Allow | 16 | 1 | 0 | Yes | No |
| 17554874 | VARIABLE AREA NOZZLE ASSEMBLY AND METHOD FOR OPERATING SAME | December 2021 | June 2023 | Allow | 18 | 1 | 1 | Yes | No |
| 17554067 | ARTICULATING SLIDER FOR NACELLE | December 2021 | May 2023 | Allow | 17 | 1 | 1 | Yes | No |
| 17544236 | HYBRID ROCKET ENGINE FUEL GRAINS WITH RADIAL ENERGY COMPOSITIONAL VARIATIONS | December 2021 | December 2024 | Abandon | 36 | 5 | 0 | Yes | No |
| 17596136 | Thrust unit for a propulsion device and associated propulsion device | December 2021 | August 2024 | Allow | 32 | 4 | 0 | Yes | No |
| 17532673 | MIXED FLOW EXHAUST THRUST REVERSER WITH AREA CONTROL NOZZLE SYSTEMS AND METHODS | November 2021 | January 2023 | Allow | 14 | 0 | 1 | No | No |
| 17525684 | AIRCRAFT SAFETY LATCH | November 2021 | March 2025 | Allow | 40 | 4 | 0 | Yes | No |
| 17608265 | THRUST REVERSER CASCADE INCLUDING ACCOUSTIC TREATMENT | November 2021 | June 2023 | Allow | 19 | 1 | 0 | Yes | No |
| 17608311 | THRUST REVERSER CASCADE INCLUDING ACCOUSTIC TREATMENT | November 2021 | November 2023 | Allow | 25 | 2 | 0 | Yes | No |
| 17594884 | THRUST REVERSER CASCADE INCLUDING ACOUSTIC TREATMENT | November 2021 | February 2025 | Allow | 39 | 4 | 0 | Yes | No |
| 17594896 | THRUST REVERSER CASCADE INCLUDING ACOUSTIC TREATMENT | November 2021 | October 2023 | Allow | 23 | 2 | 0 | Yes | No |
| 17507836 | THRUST REVERSER INTERSPATIAL BLOCKER SYSTEM | October 2021 | February 2023 | Allow | 16 | 1 | 0 | Yes | No |
| 17451137 | PROPULSION SYSTEM FOR AN AIRCRAFT | October 2021 | February 2023 | Allow | 16 | 1 | 0 | Yes | No |
| 17501862 | MULTI-LOBED BULLNOSE RAMP | October 2021 | July 2023 | Allow | 21 | 2 | 0 | Yes | No |
| 17494265 | THRUST REVERSER SYSTEM WITH HIDDEN TURNING DOOR | October 2021 | March 2023 | Allow | 17 | 1 | 0 | Yes | No |
| 17479900 | MULTIPLE PIECE PISTON | September 2021 | November 2022 | Allow | 14 | 1 | 0 | Yes | No |
| 17438992 | NACELLE FOR A BYPASS TURBOMACHINE COMPRISING A THRUST REVERSER, BYPASS TURBOMACHINE COMPRISING SUCH A NACELLE, AND AIRCRAFT COMPRISING AT LEAST ONE SUCH TURBOMACHINE | September 2021 | April 2023 | Allow | 19 | 0 | 0 | Yes | No |
| 17409156 | TRANSLATING COWL THRUST REVERSER SYSTEM WITH EFFLUX MANAGEMENT | August 2021 | July 2022 | Allow | 11 | 0 | 0 | Yes | No |
| 17405510 | FEATURED BULLNOSE RAMP FOR A THRUST REVERSER SYSTEM | August 2021 | June 2023 | Allow | 22 | 1 | 1 | Yes | No |
| 17402041 | DOOR-CLOSING SYSTEM FOR A THRUST REVERSER OF AN AIRCRAFT NACELLE | August 2021 | May 2023 | Allow | 21 | 0 | 1 | Yes | No |
This analysis examines appeal outcomes and the strategic value of filing appeals for examiner NGUYEN, ANDREW H.
With a 21.1% 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, 20.3% 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 NGUYEN, ANDREW H works in Art Unit 3741 and has examined 935 patent applications in our dataset. With an allowance rate of 77.9%, this examiner has a below-average tendency to allow applications. Applications typically reach final disposition in approximately 38 months.
Examiner NGUYEN, ANDREW H's allowance rate of 77.9% places them in the 38% percentile among all USPTO examiners. This examiner has a below-average tendency to allow applications.
On average, applications examined by NGUYEN, ANDREW H receive 1.70 office actions before reaching final disposition. This places the examiner in the 49% 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 NGUYEN, ANDREW H is 38 months. This places the examiner in the 13% percentile for prosecution speed. Applications take longer to reach final disposition with this examiner compared to most others.
Conducting an examiner interview provides a +48.8% benefit to allowance rate for applications examined by NGUYEN, ANDREW H. This interview benefit is in the 94% 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, 29.2% of applications are subsequently allowed. This success rate is in the 45% 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 27.1% of cases where such amendments are filed. This entry rate is in the 29% 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, 26.7% result in withdrawal of the rejection or reopening of prosecution. This success rate is in the 28% 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 40.6% of appeals filed. This is in the 5% percentile among all examiners. Of these withdrawals, 23.1% 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, 46.7% are granted (fully or in part). This grant rate is in the 53% 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 6.1% of allowed cases (in the 91% 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 1.4% of allowed cases (in the 60% 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.