USPTO Examiner NGUYEN ANDREW H - Art Unit 3741

Recent Applications

Detailed information about the 100 most recent patent applications.

Application NumberTitleFiling DateDisposal DateDispositionTime (months)Office ActionsRestrictionsInterviewAppeal
18909133GUIDE VANE ASSEMBLYOctober 2024May 2025Allow700YesNo
18794116DUCTING ARRANGEMENT FOR A GAS TURBINE ENGINEAugust 2024May 2025Allow1011NoNo
18742458AIRCRAFT NACELLE EQUIPPED WITH AT LEAST ONE THRUST REVERSAL DEVICE COMPRISING AT LEAST ONE LONGITUDINAL DEFLECTOR CONFIGURED TO HOUSE A LONGITUDINAL ACTUATORJune 2024May 2025Allow1110YesNo
18666193LIMITED FLOW THRUST REVERSER ACTUATINGMay 2024March 2025Allow1010YesNo
18597532THRUST REVERSER WITH BLOCKER DOOR FOLDING LINKAGEMarch 2024March 2025Allow1201YesNo
18597547THRUST REVERSER WITH LOST MOTION DEVICEMarch 2024April 2025Allow1310YesNo
18390025MODULATING INTERNAL BALLISTICS IN A 3D-PRINTED ROCKET MOTOR AND AN ADDITIVE MANUFACTURING PROCESSDecember 2023January 2025Allow1210YesNo
18541303TURBINE ENGINE HAVING A FIRE BOXDecember 2023March 2025Allow1510YesNo
18559218METHOD FOR CONTROLLING A TURBOMACHINE COMPRISING AT LEAST ONE ELECTRIC MACHINE, AND ASSOCIATED CONTROL SYSTEMNovember 2023February 2025Allow1510YesNo
18287958CONTROL DEVICE FOR GAS TURBINE, GAS TURBINE FACILITY, METHOD FOR CONTROLLING GAS TURBINE, AND CONTROL PROGRAM FOR GAS TURBINEOctober 2023September 2024Allow1010NoNo
18556702AIRCRAFT PROPULSION ASSEMBLY COMPRISING AN ACTUATOR CONNECTED TO A STRUCTURAL ARM SUCH AS AN OUTLET GUIDE VANEOctober 2023June 2025Allow2020YesNo
18378861Control Device And Plasma Energy Protective Apparatus For An Ion ThrusterOctober 2023February 2025Allow1610NoNo
18377983Duplex Turbine Guide Vane AssemblyOctober 2023January 2025Abandon1510NoNo
18470590GUIDE ASSEMBLY FOR AN AIRCRAFT PROPULSION UNITSeptember 2023April 2025Allow1921YesNo
18453069Uncommanded or Uncontrollable High Thrust Detection and MitigationAugust 2023March 2025Allow1811YesNo
18233671Plug Nozzle and Thrust Reverser for High Mach Gas Turbine EnginesAugust 2023October 2024Allow1410YesNo
18361205ARTICULATING SLIDER FOR NACELLEJuly 2023August 2024Allow1310NoNo
18222700Aircraft Heat ExchangerJuly 2023May 2025Allow2220YesNo
18350378METHOD AND APPARATUS TO MEASURE GAS TURBINE COMPRESSOR EXIT TEMPERATUREJuly 2023February 2025Allow1911YesNo
18347722ANTI-ICE SYSTEM FOR GAS TURBINE ENGINE AND INLET GUIDE VANEJuly 2023November 2024Allow1611YesNo
18211105AIRCRAFT PROPULSION SYSTEM WITH TURBINE ENGINE AND EXHAUST CONDENSERJune 2023April 2024Allow1000YesNo
18211125AIRCRAFT PROPULSION SYSTEM WITH TURBINE ENGINE AND EXHAUST CONDENSERJune 2023April 2024Allow1000YesNo
18335366SYSTEM AND METHOD FOR SYNCHROPHASING A PROPULSION SYSTEM USING ELECTRIC MACHINESJune 2023November 2024Allow1711YesNo
18207136POWER CONVERSION SYSTEM INCLUDING ENGINE AND HEAT EXCHANGERJune 2023February 2025Abandon2111NoNo
18205775LONG THROW LATCH FOR AIRCRAFT SYSTEMJune 2023January 2025Allow1910YesNo
18199245GAS TURBINE ENGINEMay 2023October 2023Allow500YesNo
18318137ENVIRONMENTAL CONTROL SYSTEMMay 2023April 2025Allow2320YesNo
18314322SELF-DAMPING ACTUATORMay 2023August 2024Allow1611NoNo
18314401TURBINE ENGINE HAVING A COMPOSITE ASSEMBLYMay 2023February 2025Allow2120YesNo
18312342COWLING LATCH INTERLOCK MECHANISMMay 2023August 2024Allow1500YesNo
18141825MISALIGNMENT LATCH FOR AN AIRCRAFT SYSTEMMay 2023May 2025Allow2520YesNo
18302952COMBUSTION SYSTEMApril 2023May 2024Allow1210NoNo
18303076DEFLECTOR PROVIDED WITH A SPOILER FOR A THRUST REVERSER OF AN AIRCRAFT ENGINE NACELLEApril 2023November 2024Allow1920YesNo
18299526MIXED FLOW EXHAUST THRUST REVERSER WITH AREA CONTROL NOZZLE SYSTEMS AND METHODSApril 2023July 2024Allow1511YesNo
18297835SYSTEM FOR CONTROLLING BLADE CLEARANCES WITHIN A GAS TURBINE ENGINEApril 2023January 2024Allow900YesNo
18124382THRUST REVERSER CASCADE AND METHOD OF MANUFACTUREMarch 2023June 2025Abandon2720NoNo
18245199METHOD FOR MANUFACTURING A COMPOSITE MATERIAL PART HAVING A CELLULAR STRUCTURE AND CORRESPONDING PARTMarch 2023March 2025Allow2430YesNo
18175102TWO SERVOVALVE THRUST REVERSER ACTUATOR SYSTEMFebruary 2023June 2024Allow1511YesNo
18109428GAS TURBINE ENGINE NOZZLE LOFT FOR THRUST REVERSERFebruary 2023February 2024Allow1210YesNo
18100765ICING CONDITION IDENTIFICATION FOR GAS TURBINE ENGINEJanuary 2023September 2024Allow2020YesNo
18005871THRUST REVERSER COMPRISING PIVOTING HALF-ASSEMBLIES AND A CONNECTING BEAM FOR THE HALF-ASSEMBLIES AT THE SIX O'CLOCK POSITIONJanuary 2023January 2025Allow2430YesNo
18063814REVERSE THRUST SYSTEM AND METHODDecember 2022November 2023Allow1101YesNo
18074152BALK DEVICE FOR DOOR LOCKDecember 2022September 2024Allow2210NoNo
17965921WEAPON ENERGY HARVESTING BY GAS TURBINE ELECTRIC GENERATOROctober 2022October 2023Allow1210NoNo
17962147THRUST REVERSER SYSTEM WITH ANGLED DOOR PIVOT AXESOctober 2022October 2024Allow2521YesNo
17939000ASSEMBLY FOR AN AIRCRAFT NACELLE AND COMPRISING A SUPPORT PANEL, A THERMAL PROTECTION ELEMENT AND A FASTENING SYSTEMSeptember 2022July 2024Allow2200NoNo
17902559LATCH ASSEMBLYSeptember 2022February 2024Allow1710YesNo
17900946TEXTILE CASCADE ASSEMBLYSeptember 2022August 2023Allow1100YesNo
17797528DEVICE FOR ATTACHING A CONNECTING ROD SMALL END FOR A THRUST REVERSAL CASCADE FLAPAugust 2022September 2024Allow2510NoNo
17817166TERTIARY LOCKAugust 2022November 2023Allow1610NoNo
17878360ASSEMBLY 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 COWLAugust 2022January 2024Allow1810YesNo
17874825DRIVE SYSTEM FOR TRANSLATING STRUCTUREJuly 2022December 2023Allow1711YesNo
17869488THRUST REVERSER SYSTEM LATCH ASSEMBLY AND METHOD OF OPERATING SAMEJuly 2022November 2023Allow1601YesNo
17867507SURGE RECOVERY SYSTEM AND METHODSJuly 2022February 2024Allow1911YesNo
17853691Multi-Mode Combined Cycle Propulsion EngineJune 2022August 2023Allow1410YesNo
17842586DRIVE SYSTEM FOR TRANSLATING STRUCTUREJune 2022April 2024Allow2221YesNo
17837992SEAL FOR GIMBALING AND/OR FIXED ROCKET ENGINE NOZZLES, AND ASSOCIATED SYSTEMS AND METHODSJune 2022March 2025Allow3430YesNo
17828868Oblique Detonation Rocket EngineMay 2022July 2023Allow1310YesNo
17664971COMBUSTOR WITH SECONDARY FUEL NOZZLE IN DILUTION FENCEMay 2022September 2024Allow2831YesNo
17742620GAS TURBINE ENGINEMay 2022December 2023Allow1911YesNo
17662684ACTUATOR SYSTEMS FOR THRUST REVERSERMay 2022May 2023Allow1210YesNo
17734941THRUST REVERSER SINGLE DEGREE OF FREEDOM ACTUATOR MECHANISM SYSTEMS AND METHODSMay 2022October 2023Allow1810YesNo
17720519THRUST REVERSER ACTUATION ARRANGEMENT AND DEPLOYABLE FAIRING SYSTEMS AND METHODSApril 2022September 2023Allow1710YesNo
17716897AIRCRAFT SAFETY KEEPER FOR LATCH UTILIZATIONApril 2022January 2024Allow2110NoNo
17708220AIRCRAFT ENGINE PYLON HAVING A MOVABLE ASSEMBLY OF COWLSMarch 2022December 2023Allow2010NoNo
17707647GUIDE SYSTEMS FOR INSTALLING AIRCRAFT STRUCTURESMarch 2022September 2024Allow2921YesNo
17695560SHEARED EXHAUST NOZZLEMarch 2022May 2025Abandon3840YesNo
17690540THRUST REVERSER CASCADE AND METHOD OF MANUFACTUREMarch 2022January 2023Allow1100NoNo
17689418DEPLOYABLE FAIRING FOR DOOR REVERSERS SYSTEMS AND METHODSMarch 2022October 2023Allow1920YesNo
17688419VARIABLE AREA NOZZLE FOR AIRCRAFT PROPULSION SYSTEMMarch 2022March 2024Allow2430NoNo
17685649THRUST REVERSER PROVIDED WITH CABLE KINEMATICS FOR SCOOP FLAPSMarch 2022January 2024Allow2211YesNo
17678583ULTRA QUIET SPLIT FLOW THRUST REVERSERFebruary 2022January 2024Allow2311YesNo
17650318INLET ARRANGEMENT, A PROPULSION SYSTEM, AND AN AIRCRAFTFebruary 2022October 2024Abandon3320NoNo
17632832THRUST REVERSER FOR TURBOFAN PROPULSION SYSTEM OF AN AIRCRAFT AND THRUST REVERSAL METHODFebruary 2022May 2024Abandon2720NoNo
17631281ACOUSTIC ATTENUATION STRUCTURE MADE OF COMPOSITE MATERIAL AND METHOD FOR MANUFACTURING SAMEJanuary 2022January 2024Allow2440YesNo
17648764THERMOPLASTIC ACOUSTIC BLOCKER DOORJanuary 2022September 2024Abandon3240NoNo
17579938OPERABILITY GEARED TURBOFAN ENGINE INCLUDING COMPRESSOR SECTION VARIABLE GUIDE VANESJanuary 2022July 2023Allow1720NoNo
17575686AIRCRAFT TURBOJET ENGINE COMPRISING TWO THRUST REVERSER MODULESJanuary 2022February 2023Allow1301YesNo
17570728GEARED TURBOFAN WITH OVERSPEED PROTECTIONJanuary 2022April 2025Allow3920NoYes
17558019RESTRAINING PLUGDecember 2021April 2025Allow4021YesYes
17554695AIRCRAFT PROPULSION SYSTEM EXHAUST NOZZLE WITH EJECTOR PASSAGE(S)December 2021April 2023Allow1610YesNo
17554874VARIABLE AREA NOZZLE ASSEMBLY AND METHOD FOR OPERATING SAMEDecember 2021June 2023Allow1811YesNo
17554067ARTICULATING SLIDER FOR NACELLEDecember 2021May 2023Allow1711YesNo
17544236HYBRID ROCKET ENGINE FUEL GRAINS WITH RADIAL ENERGY COMPOSITIONAL VARIATIONSDecember 2021December 2024Abandon3650YesNo
17596136Thrust unit for a propulsion device and associated propulsion deviceDecember 2021August 2024Allow3240YesNo
17532673MIXED FLOW EXHAUST THRUST REVERSER WITH AREA CONTROL NOZZLE SYSTEMS AND METHODSNovember 2021January 2023Allow1401NoNo
17525684AIRCRAFT SAFETY LATCHNovember 2021March 2025Allow4040YesNo
17608265THRUST REVERSER CASCADE INCLUDING ACCOUSTIC TREATMENTNovember 2021June 2023Allow1910YesNo
17608311THRUST REVERSER CASCADE INCLUDING ACCOUSTIC TREATMENTNovember 2021November 2023Allow2520YesNo
17594884THRUST REVERSER CASCADE INCLUDING ACOUSTIC TREATMENTNovember 2021February 2025Allow3940YesNo
17594896THRUST REVERSER CASCADE INCLUDING ACOUSTIC TREATMENTNovember 2021October 2023Allow2320YesNo
17507836THRUST REVERSER INTERSPATIAL BLOCKER SYSTEMOctober 2021February 2023Allow1610YesNo
17451137PROPULSION SYSTEM FOR AN AIRCRAFTOctober 2021February 2023Allow1610YesNo
17501862MULTI-LOBED BULLNOSE RAMPOctober 2021July 2023Allow2120YesNo
17494265THRUST REVERSER SYSTEM WITH HIDDEN TURNING DOOROctober 2021March 2023Allow1710YesNo
17479900MULTIPLE PIECE PISTONSeptember 2021November 2022Allow1410YesNo
17438992NACELLE FOR A BYPASS TURBOMACHINE COMPRISING A THRUST REVERSER, BYPASS TURBOMACHINE COMPRISING SUCH A NACELLE, AND AIRCRAFT COMPRISING AT LEAST ONE SUCH TURBOMACHINESeptember 2021April 2023Allow1900YesNo
17409156TRANSLATING COWL THRUST REVERSER SYSTEM WITH EFFLUX MANAGEMENTAugust 2021July 2022Allow1100YesNo
17405510FEATURED BULLNOSE RAMP FOR A THRUST REVERSER SYSTEMAugust 2021June 2023Allow2211YesNo
17402041DOOR-CLOSING SYSTEM FOR A THRUST REVERSER OF AN AIRCRAFT NACELLEAugust 2021May 2023Allow2101YesNo

Appeals Overview

This analysis examines appeal outcomes and the strategic value of filing appeals for examiner NGUYEN, ANDREW H.

Patent Trial and Appeal Board (PTAB) Decisions

Total PTAB Decisions
38
Examiner Affirmed
30
(78.9%)
Examiner Reversed
8
(21.1%)
Reversal Percentile
33.3%
Lower than average

What This Means

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.

Strategic Value of Filing an Appeal

Total Appeal Filings
59
Allowed After Appeal Filing
12
(20.3%)
Not Allowed After Appeal Filing
47
(79.7%)
Filing Benefit Percentile
23.7%
Lower than average

Understanding Appeal Filing Strategy

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.

Strategic Recommendations

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 - Prosecution Strategy Guide

Executive Summary

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.

Allowance Patterns

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.

Office Action Patterns

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.

Prosecution Timeline

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.

Interview Effectiveness

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.

Request for Continued Examination (RCE) Effectiveness

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.

After-Final Amendment Practice

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.

Pre-Appeal Conference Effectiveness

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.

Appeal Withdrawal and Reconsideration

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.

Petition Practice

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 Cooperation and Flexibility

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).

Prosecution Strategy Recommendations

Based on the statistical analysis of this examiner's prosecution patterns, here are tailored strategic recommendations:

  • Prioritize examiner interviews: Interviews are highly effective with this examiner. Request an interview after the first office action to clarify issues and potentially expedite allowance.
  • Plan for extended prosecution: Applications take longer than average with this examiner. Factor this into your continuation strategy and client communications.
  • Examiner cooperation: This examiner frequently makes examiner's amendments to place applications in condition for allowance. If you are close to allowance, the examiner may help finalize the claims.

Relevant MPEP Sections for Prosecution Strategy

  • MPEP § 713.10: Examiner interviews - available before Notice of Allowance or transfer to PTAB
  • MPEP § 714.12: After-final amendments - may be entered "under justifiable circumstances"
  • MPEP § 1002.02(c): Petitionable matters to Technology Center Director
  • MPEP § 1004: Actions requiring primary examiner signature (allowances, final rejections, examiner's answers)
  • MPEP § 1207.01: Appeal conferences - mandatory for all appeals
  • MPEP § 1214.07: Reopening prosecution after appeal

Important Disclaimer

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.