1. Stats
  2. USPTO
  3. TC 3600
  4. Group 3640
  5. Art Unit 3642
  6. Examiner Dangol

Examiner Dangol Ashesh

3642-DANGOL-ASHESH

Employment Information

Art Unit:3642 — Aeronautics and astronautics
Group:3640 — Aeronautics, Agriculture, Fishing, Trapping, Vermin Destroying, Plant and Animal Husbandry, Weaponry, Nuclear Systems, and License and Review
Classes: 244 — Aeronautics and astronautics
297 — Chairs and seats
701 — Data processing: vehicles, navigation, and relative location
415 — Rotary kinetic fluid motors or pumps
702 — Data processing: measuring, calibrating, or testing
Phone:(303) 297-4455
Email:ashesh.dangol@uspto.gov
Location:CO 80294
Title:Pat Examnr Mechl Engrg
Service:6 years
Grade:GS-13

Grant Rate and Difficulty Ranking

66
3-Year Grant rate: 66% over 130 cases
Difficulty: Harder
Difficulty Percentile: 66th

With Examiner Dangol, you have a 66% chance of getting an issued patent by 3 years after the first office action. Examiner Dangol is a harder examiner and in the 66th percentile across all examiners (with 100th percentile most difficult).

Grant Rate

Grant Rate Timeline

Below is the grant rate timeline for Examiner Dangol, where the timeline is relative to the date of the first office action. The three-year grant rate is the percentage of applications granted at three years after the first office action.

Comparison with Art Unit 3642

Examiner Dangol's grant rate is lower than that of Art Unit 3642 and lower than that of the USPTO.

Average Office Actions Per Grant
Examiner Dangol 2.0
Art Unit 3642 1.3

Interview Benefit

Grant Rate without Interview

Examiner Dangol has granted 46 of 70 cases without any applicant-requested interviews for a grant rate of 66%.

Grant Rate with Interview

Examiner Dangol has granted 40 of 60 cases with at least one applicant-requested interview for a grant rate of 67%.

Interview Benefit

With Examiner Dangol, conducting an interview increases your chance of getting a patent granted by 2%.

Recent Dispositions

Recent Dispositions

Number Title OA Rejections Status IFW
19074596 Debris Barrier For Aircraft Window Assembly And Method Rejection information available with a Premium Stats subscription. See our pricing. Patented View
17867851 Methods And Systems For Venting A Fuel Tank On A Blended Wing Body Aircraft Patented View
17934706 Autothrottle System For Aircraft Patented View
17292658 Aircraft Propulsion System And Method For Operating Such A System Patented View
19084591 Moving Object Patented View
18484507 Aircraft Propulsion System Patented View
18564445 Leading-Edge High-Lift Device, Wing, Aircraft, And Buffering Member Patented View
18695734 Flight Vehicle Abandoned View
18563497 Restructurable Hybrid-Wing Vertical Take-Off And Landing Aircraft Abandoned View
18101626 Variable Compression Air Intakes For Aircraft Propulsion Systems And Methods For Varying Compression Of An Air Intake Patented View
18161567 Load-Alleviation Systems For Aircraft Having Centrally Stored Fuel Abandoned View
18594630 Passenger Seating Apparatus With Movable Display Abandoned View
17964986 Aircraft Hold Comprising At Least One Longitudinally Disposed And Transversely Movable Cabinet, And Method For The Arrangement Of Said Hold Abandoned View
18556715 Aircraft Seat Arrangement Patented View
18512046 Wing-And-Rotary-Wing Mixed Folding And Unfolding System Of Flying Vehicle, And Flying Vehicle Patented View
18103397 Canopy Deployment And Retraction Device With Line Tension Control Abandoned View
17596966 Fuselage For Transporting Medical Cargo In An Unmanned Aerial Vehicle Abandoned View
17977457 Reducing Induced Drag By Creating Additional Airflow At The Wing Tip Patented View
17887041 Balloon Altitude Control Abandoned View
18250638 Nacelle For An Aircraft Propulsion Unit, Comprising A Safety Rod Forming A Structural Reinforcement Patented View
18605226 Aircraft Cooling System And Aircraft Patented View
18182015 Solar Parasol Abandoned View
18530825 Aircraft Refuelling System Abandoned View
17284272 Portable Aircraft Shelter Abandoned View
18945644 Aerodynamic Fairing Patented View
19071237 Wing For An Aircraft And High Lift Assembly Connection Method Patented View
18533603 Leading-Edge Droop Actuation System Patented View
18535900 Aerodynamic Rotor Blade Strake Patented View
18637605 Vertical Air Vehicle Takeoff And Landing Stabilization Apparatuses, Systems, And Methods Patented View
18176312 Personal Aircraft Including A Rotor Patented View
18521996 Aircraft Landing Gear With Tension Drag Brace Patented View
18636631 Vertical Air Vehicle Takeoff And Landing Stabilization Apparatuses, Systems, And Methods Patented View
18512248 Ceramic Kelvin Foam With Geometry Optimized For Hydrostatic Loading Patented View
17731728 Aircraft With Fuel Tanks Stored Aft Of A Cabin In A Main Body And A Method For Manufacturing Patented View
16499617 Seating Assembly With Staggered Arrangement Patented View
18004439 Aircraft And Power Device Patented View
17360356 Cfrp Fuselage Frame With Securement To Vertical Tail Fin Patented View
18670164 Assembly For An Aircraft Comprising A Wing And An Engine Pylon For Coupling A Propulsion System To Said Wing Patented View
17334285 Flight Efficiency Improving System For Compound Helicopter Patented View
18514928 Nacelle Apparatus With Air-Conducting Device And Vertical Take-Off And Landing Aircraft Abandoned View
18029079 Propeller Guard, Flying Body, And Resilient Member Abandoned View
17554371 Uav With Augmented Lift Rotors Abandoned View
18222416 Methods, Systems, And Devices For A Seat For A Vehicle Patented View
17961747 Systems And Methods For Deicing Aircraft Patented View
17958779 Aircraft With Outboard-Stowed Landing Gear Patented View
17433545 Hybrid-Electric Propulsion Architecture And Method For Dissipating Electrical Energy In Such An Architecture Patented View
18398013 Aircraft Wing Unit With Pressure Fence Patented View
18370187 Battery Load Support Structure Of Fuselage Patented View
18119005 Arrangements Of Lie Flat Seats With Oblique Front Row Patented View
17419106 Manned Aircraft Patented View

Appeals Statistics

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Disclaimer: We do not provide any guarantees as to the accuracy of the statistics presented above and under
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