USPTO Examiner ZAMORA ALVAREZ ERIC J - Art Unit 3745

Recent Applications

Detailed information about the 100 most recent patent applications.

Application NumberTitleFiling DateDisposal DateDispositionTime (months)Office ActionsRestrictionsInterviewAppeal
19255078AIRFOIL-MOUNTED ACOUSTIC RESONATOR ARRAY FOR GAS TURBINE ENGINE COMPONENTJune 2025March 2026Allow811YesNo
19239186TEST BLADE FOR GAS TURBINE ENGINE AND METHOD OF MAKINGJune 2025February 2026Allow810NoNo
19215171Mixing UtensilMay 2025December 2025Allow711YesNo
19201295SEALING ARRANGEMENT FOR A TURBOMACHINE, SEAL CARRIER ELEMENT FOR THE SEALING ARRANGEMENT, GUIDE BLADE ELEMENT, AND TURBOMACHINEMay 2025December 2025Allow711NoNo
19084572AIR MOVING DEVICES, AERODYNAMIC ROTOR, AND METHODSMarch 2025December 2025Allow911YesNo
19082910FLUID FLOW DISTRIBUTOR FOR VAPOR PHASE COATING OF TURBINE COMPONENTSMarch 2025October 2025Allow700YesNo
19044230GAS TURBINE ENGINE ROTOR BLADE GEOMETRY AND METHOD FOR SELECTING SAMEFebruary 2025November 2025Allow910NoNo
19021666UNDUCTED AIRFOIL ASSEMBLYJanuary 2025October 2025Allow911YesNo
18878775AIR GUIDE RING AND AXIAL FLOW FAN COMPRISING SAMEDecember 2024March 2026Allow1410YesNo
18872664METHOD FOR CONTROLLING OF A PUMP UNIT AND A PUMP UNIT FOR PUMPING LIQUID OR SUSPENSIONDecember 2024February 2026Allow1410YesNo
18926574AIRCRAFT ENGINE HAVING A SCROLL CASE AND A TURBINE SUPPORT CASE SECURED TOGETHEROctober 2024November 2025Allow1210NoNo
18859818PROPELLER BLADE OR AIRFOIL WITH HOLLOW COMPOSITE ROOTOctober 2024August 2025Allow1011YesNo
18857316WIND TURBINE BLADE AND METHOD FOR MANUFACTURING A WIND TURBINE BLADEOctober 2024December 2025Allow1410YesNo
18891746AIR MOVING DEVICES, AERODYNAMIC ROTOR, AND METHODSSeptember 2024December 2025Allow1511YesNo
18813053TURBINE COMPONENT FOR GAS TURBINE ENGINEAugust 2024August 2025Allow1201NoNo
18810890CENTRIFUGAL FANAugust 2024December 2025Allow1611YesNo
18806936INTEGRATED AIR CYCLE MACHINE FOR AN ENVIRONMENTAL CONTROL SYSTEM OF AN AIRCRAFTAugust 2024October 2025Allow1411NoNo
18805478Masking SystemAugust 2024January 2026Allow1811NoNo
18765490FAN LOAD TENSION STRUCTURAL GUIDE VANE WITH BYPASS COOLING CAVITIESJuly 2024August 2025Allow1321YesNo
18753294MILL SPINDLE FANJune 2024August 2025Allow1421YesNo
18752669OIL-LUBRICATED VACUUM PUMP WITH IMPROVED OIL SEALINGJune 2024December 2025Allow1810NoNo
18750076DUAL-WALLED COMPONENTS FOR A GAS TURBINE ENGINEJune 2024October 2025Allow1621YesNo
18749190SLIP BASED RADIAL BEARING SUPPORTJune 2024October 2025Allow1511NoNo
18721922MODULAR WIND TURBINE BLADEJune 2024November 2025Allow1710NoNo
18715603AUXILIARY ARM FOR A TURBOMACHINE EXHAUST CASINGJune 2024October 2025Allow1710YesNo
18731044Compact Blade Pitch Mechanism And Aircraft Using SameMay 2024September 2025Allow1611YesNo
18731058PASSIVE NOISE DISSIPATOR FOR LAPTOP COOLING FANSMay 2024October 2025Allow1721YesNo
18678000GAS TURBINE ENGINEMay 2024August 2025Allow1511YesNo
18678281TURBINE ENGINE INCLUDING A VANE SUPPORT AND A VANEMay 2024August 2025Allow1421YesNo
18678876TURBINE SHROUD ASSEMBLIES WITH STRIP SEALSMay 2024June 2025Allow1211NoNo
18675388COMPRESSOR ROTOR BLADE AIRFOILSMay 2024September 2024Allow400NoNo
18673618TURBOCHARGER BEARING HOUSINGMay 2024September 2025Allow1621YesNo
18661272SRV OPEN ROTOR WITH CORE INLET FORWARD OF ROTORMay 2024July 2025Allow1421YesNo
18657373AXIAL EXPANDABLE EXHAUST DUCTMay 2024January 2025Allow810NoNo
18655692Lowering Ceiling Fan DeviceMay 2024September 2025Allow1621YesNo
18655958FLANGE WITH STRESS ATTENTUATION FEATUREMay 2024August 2025Allow1521NoNo
18654134ENGINE COMPONENTMay 2024May 2025Allow1221YesNo
18653052COMPOSITE AIRFOIL ASSEMBLY HAVING A COMPOSITE AIRFOIL AND SPARMay 2024June 2025Allow1421YesNo
18652338TURBOMACHINE WITH TURBINE SECTION HAVING INTEGRATED FLUID SEPARATORMay 2024March 2025Allow1111NoNo
18651631RADIAL TURBINE ROTOR WITH ADDITIVE LAYER MANUFACTURED COMPONENTSApril 2024December 2025Abandon2021YesNo
18646941AFT MOUNTED PUSHER FAN FOR GAS TURBINE ENGINEApril 2024September 2025Allow1621YesNo
18643284ANGULARLY POSITIONED MARINE PROPELLER COMBINATION AND A METHOD OF OPERATING A MARINE PROPELLER COMBINATIONApril 2024August 2025Allow1621YesNo
18638440MULTI-STAGE PARTIAL ADMISSION AXIAL TURBINEApril 2024August 2025Allow1610NoNo
18638410CONNECTION COMPONENT AND FANApril 2024March 2025Allow1121NoNo
18636837ANNULUS FILLER FOR A GAS TURBINE ENGINEApril 2024August 2025Allow1610YesNo
18636729ENERGY CONVERSION DEVICE, ASSOCIATED SYSTEMS AND METHODSApril 2024November 2025Allow1911NoNo
18635858AERODYNAMICALLY MISTUNED AIRFOILS FOR UNSTEADY LOSS REDUCTIONApril 2024April 2025Allow1211YesNo
18632841LEADING EDGE PLATING ON LOW PRESSURE COMPRESSOR VANE FOR WEIGHT AND STRENGTH OPTIMIZATIONApril 2024November 2025Allow2031YesNo
18619014FLUID FLOW DISTRIBUTOR FOR VAPOR PHASE COATING OF TURBINE COMPONENTSMarch 2024December 2024Allow911YesNo
18692557TURBINE ENGINE ELEMENT COMPRISING AT LEAST ONE BLADE OBTAINED BY ADDITIVE MANUFACTURINGMarch 2024March 2026Allow2421YesNo
18600604SEGMENTED VARIABLE FAN OUTLET GUIDE VANE WITH PASS THROUGH ACTUATION MECHANISMSMarch 2024July 2025Allow1721YesNo
18594658SYSTEMS AND METHODS FOR SENSORS ON CIRCUMFERENTIAL INTERIOR SURFACE OF TURBOMACHINE CASINGMarch 2024November 2024Allow810NoNo
18687378DAMPING DEVICE FOR A ROTOR WHEEL OF AN AIRCRAFT TURBINE ENGINE, ROTOR WHEEL FOR AN AIRCRAFT TURBINE ENGINE, TURBINE ENGINE FOR AN AIRCRAFT, AND METHOD FOR MANUFACTURING A DAMPING DEVICEFebruary 2024October 2025Allow1911YesNo
18588230DUST-COLLECTING DEVICE FOR FAN BLADESFebruary 2024October 2024Allow710YesNo
18686496Splash RingFebruary 2024September 2025Abandon1811NoNo
18586012COVER PLATE CONNECTIONS FOR A HOLLOW FAN BLADEFebruary 2024October 2025Allow1931YesNo
18583544AIRCRAFT ENGINE IMPELLER WITH EXDUCER SHROUD FORWARD SWEEPFebruary 2024December 2025Allow2231YesNo
18581641AXIALLY ADJUSTABLE INSERTED RING WITHIN PACKING RING AND METHOD OF USING SAMEFebruary 2024April 2025Allow1421YesNo
18581225PARTITION DAMPER SEAL CONFIGURATIONS FOR SEGMENTED INTERNAL COOLING HARDWAREFebruary 2024October 2024Allow810YesNo
18684371STATOR PART OF A TURBOMACHINE COMPRISING A BLADE AND A FIN DEFINING BETWEEN THEM A DECREASING SURFACE FROM UPSTREAM TO DOWNSTREAM IN THE GAS FLOW DIRECTIONFebruary 2024January 2025Allow1120YesNo
18683579METHODS OF SEMI-PERMANENTLY ATTACHING COMPONENTS ON A WIND TURBINE ROTOR BLADEFebruary 2024August 2025Allow1811YesNo
18434049VANE WITH SEALFebruary 2024May 2025Allow1511NoNo
18681111LIQUID-FEED-TYPE GAS COMPRESSORFebruary 2024May 2025Allow1611NoNo
18430130AIRFOIL-MOUNTED ACOUSTIC RESONATOR ARRAY FOR GAS TURBINE ENGINE COMPONENTFebruary 2024March 2025Allow1421YesNo
18424383GAS TURBINE ENGINE ROTOR BLADE GEOMETRY AND METHOD FOR SELECTING SAMEJanuary 2024September 2024Allow801YesNo
18408739FLOW BODY FOR A GAS TURBINE, GAS TURBINE, METHOD FOR MANUFACTURING A FLOW BODY FOR A GAS TURBINE, AND METHOD FOR REPAIRING A FLOW BODY OF A GAS TURBINEJanuary 2024April 2025Allow1511YesNo
18408722BLISKJanuary 2024October 2024Allow911YesNo
18572095FAN FOR HANDHELD BLOWERDecember 2023March 2025Allow1520NoNo
18541234AERONAUTICAL PROPULSION SYSTEMDecember 2023May 2025Allow1711YesNo
18541060AERONAUTICAL PROPULSION SYSTEMDecember 2023July 2024Allow711YesNo
18571100SHEAR WEB FOR A WIND TURBINE BLADE AND METHOD OF MAKING SAMEDecember 2023April 2025Allow1611YesNo
18570342SYSTEM FOR CHANGING THE PITCH OF THE BLADES OF A TURBOMACHINE PROPELLERDecember 2023December 2024Allow1220NoNo
18536428COMPONENT FOR A TURBINE ENGINE WITH A COOLING HOLEDecember 2023January 2025Allow1421YesNo
18530937Rotor Blade with Frangible Spar for a Gas Turbine EngineDecember 2023March 2026Allow2711NoNo
18565112COOLING A WIND TURBINENovember 2023March 2026Allow2731YesNo
18511237ADDITIVE MANUFACTURED SEAL ROTOR; AND METHODNovember 2023November 2024Allow1220NoNo
18560043WING STRUCTURE AND WING STRUCTURE MANUFACTURING METHODNovember 2023September 2025Allow2221YesNo
18497452COMPRESSOR ROTOR BLADE AIRFOILSOctober 2023November 2024Allow1200YesNo
18496251FAN BLADE FOR A GAS TURBINE ENGINEOctober 2023September 2024Allow1111NoNo
18383506Morphing AirfoilOctober 2023September 2024Allow1120YesNo
18381062AIRCRAFT POWER SYSTEM MODULE WITH INTEGRAL LUBRICANT RESERVOIROctober 2023February 2025Allow1620YesNo
18381066LUBRICATION SYSTEM FOR AIRCRAFT POWERPLANT AND CLUTCH SYSTEMOctober 2023May 2025Allow1931NoNo
18377397BEARING ASSEMBLY FOR A GAS TURBINE ENGINEOctober 2023December 2024Allow1510NoNo
18552853Device for sealing and reinjecting a bypass flow for a turbine nozzleSeptember 2023April 2025Allow1820NoNo
18550414IMPELLER ASSEMBLY AND MIXING APPARATUSSeptember 2023February 2025Allow1710NoNo
18462425PROPELLER CONTROL MECHANISMSeptember 2023November 2023Allow211NoNo
18463013THRUST GENERATING DEVICESeptember 2023April 2025Allow1911NoNo
18238491Rotor Structure for Fluid Kinetic Power Generation TurbineAugust 2023September 2025Abandon2421NoNo
18452246FAN BLADE OR VANE WITH IMPROVED BIRD IMPACT CAPABILITYAugust 2023March 2025Allow1920YesNo
18231561ROTOR ASSEMBLY FOR GAS TURBINE ENGINES WITH REPLACEABLE BALANCE WEIGHT BANDSAugust 2023September 2024Allow1311NoNo
18446078FAN BLADE OR VANE WITH IMPROVED BIRD IMPACT CAPABILITYAugust 2023April 2025Allow2020YesNo
18354714INTEGRALLY BLADED ROTOR WITH INCREASED RIM BENDING STIFFNESSJuly 2023October 2024Allow1510YesNo
18348452COMPOSITE AIRFOIL ASSEMBLY FOR A TURBINE ENGINEJuly 2023January 2025Allow1811YesNo
18345018UNDUCTED AIRFOIL ASSEMBLYJune 2023October 2024Allow1521NoNo
18215308ADVANCED THERMALLY CONDUCTIVE LIGHTWEIGHT ELASTOMERIC SEALJune 2023August 2024Allow1311NoNo
18337533TURBINE BLADE SQUEALER TIP WALL WITH CHAMFERED SURFACEJune 2023September 2024Allow1530YesNo
18208684NON-CIRCULAR STRESS REDUCING CROSSOVERJune 2023February 2024Allow811YesNo
18207749ROTARY WING AIR VEHICLEJune 2023October 2024Allow1710YesNo
18200220ADDITIVELY MANUFACTURED RADIAL TURBINE ROTOR WITH COOLING MANIFOLDSMay 2023January 2024Allow810YesNo
18316656VARIABLE PITCH FAN OF A GAS TURBINE ENGINEMay 2023June 2024Allow1311YesNo

Appeals Overview

This analysis examines appeal outcomes and the strategic value of filing appeals for examiner ZAMORA ALVAREZ, ERIC J.

Patent Trial and Appeal Board (PTAB) Decisions

Total PTAB Decisions
8
Examiner Affirmed
5
(62.5%)
Examiner Reversed
3
(37.5%)
Reversal Percentile
59.4%
Higher than average

What This Means

With a 37.5% 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.

Strategic Value of Filing an Appeal

Total Appeal Filings
18
Allowed After Appeal Filing
9
(50.0%)
Not Allowed After Appeal Filing
9
(50.0%)
Filing Benefit Percentile
83.6%
Higher 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, 50.0% 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.

Strategic Recommendations

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 ZAMORA ALVAREZ, ERIC J - Prosecution Strategy Guide

Executive Summary

Examiner ZAMORA ALVAREZ, ERIC J works in Art Unit 3745 and has examined 403 patent applications in our dataset. With an allowance rate of 86.6%, this examiner has an above-average tendency to allow applications. Applications typically reach final disposition in approximately 29 months.

Allowance Patterns

Examiner ZAMORA ALVAREZ, ERIC J's allowance rate of 86.6% places them in the 65% percentile among all USPTO examiners. This examiner has an above-average tendency to allow applications.

Office Action Patterns

On average, applications examined by ZAMORA ALVAREZ, ERIC J receive 1.77 office actions before reaching final disposition. This places the examiner in the 39% 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 ZAMORA ALVAREZ, ERIC J is 29 months. This places the examiner in the 67% percentile for prosecution speed. Prosecution timelines are slightly faster than average with this examiner.

Interview Effectiveness

Conducting an examiner interview provides a +28.3% benefit to allowance rate for applications examined by ZAMORA ALVAREZ, ERIC J. This interview benefit is in the 76% 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, 31.4% of applications are subsequently allowed. This success rate is in the 64% 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.

After-Final Amendment Practice

This examiner enters after-final amendments leading to allowance in 49.2% of cases where such amendments are filed. This entry rate is in the 74% 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.

Pre-Appeal Conference Effectiveness

When applicants request a pre-appeal conference (PAC) with this examiner, 0.0% result in withdrawal of the rejection or reopening of prosecution. This success rate is in the 22% percentile among all examiners. Note: Pre-appeal conferences show limited success with this examiner compared to others. While still worth considering, be prepared to proceed with a full appeal brief if the PAC does not result in favorable action.

Appeal Withdrawal and Reconsideration

This examiner withdraws rejections or reopens prosecution in 63.6% of appeals filed. This is in the 43% percentile among all examiners. Strategic Insight: This examiner shows below-average willingness to reconsider rejections during appeals. Be prepared to fully prosecute appeals if filed.

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 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 Cooperation and Flexibility

Examiner's Amendments: This examiner makes examiner's amendments in 0.0% of allowed cases (in the 44% 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 1.7% of allowed cases (in the 66% 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.

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.