Anthony Stanco, Eit Email & Phone Number

Indianapolis, In, Us

• Provide IPT support to Collins Aerospace

Glen Cove, New York, United States

• Actively seeking an exciting new opportunity. While searching, I have taken courses in Stress analysis, C++, SOLIDWORKS, and Computer Science.

Rocky Hill,Ct

• Conducted Finite Element Analysis (FEA) stress and temperature analysis in ANSYS to develop repairs that restored V2500 and PW4000 engine components to serviceable condition. Obtained the LCF life for various locations on HPC, HPT, and LPT rotors. • Increased company-wide efficiency by automating multiple tasks for myself and team members using Python.• Made sub-models in Siemens NX and imported into ANSYS. Leveraged GD&T and engineering drawings to create part models.• Prepared Structural Analysis Memos (SAMs) to report the viability of the repairs.

East Hartford, Ct

• Managed budget, project lifecycle, EVM, and customer reporting for 3 Military Lifing projects (F100, F119 and F135) as a cross-functional project lead. • Initiated development of standard work and trained 7 other engineers to help with project tasks. Liaison between QuEST Global and Pratt & Whitney teams. • Increased company-wide efficiency with claimed cost savings greater than 25% of project budget by automating multiple tasks for myself and team members using Python, Perl, MATLAB, Minitab, Shell/Batch scripts. • Developed, verified and validated 50 CGR/LCF Advanced Lifing Algorithm (ALA) regressions in Matlab for Pratt & Whitney F100, F119, and F135 (ALIS) engine programs. • Expedited 1000’s of F119/F135 flight mission performance data run through Advanced Lifing Algorithm (ALA) regressions by creating custom data parsing Python script. Reduced turnaround time from 4 weeks to 1 week.• Observed and communicated the status of vibrations to Engine Dynamics & Loads (ED&L) Team throughout the A320 Neo Bombardier C Series and MRJ engines during 3-shift engine certification testing. • Spearheaded development of advanced MATLAB visualization tool in one day to show 3-dimensional engine case deflection using Nastran data.

• Designed and implemented a procedure to collect pilot’s control data at NASA Langley facility. Total of 20 subjects tested.• Utilized linear control design and analysis to simulate frequency sweep and step responses for the control inceptor located in the Generic Flight Deck (GFD) Flight Simulator. • Control design and frequency domain analysis conducted in MATLAB and Simulink.• Employed PSD analysis, coherence analysis and other signal processing tools to determine how a high fidelity control loader affects the pilot. • Presented above research at AIAA Guidance and Control Conference in Portland, Oregon.

New York, Ny

• Produced drawings for plumbing, sprinkler and HVAC systems using AutoCAD.• Partnered with mechanical and electrical engineers and plumbing experts to review and design mechanical systems.• Calculated heat loads to determine the proper size for heat convectors while accounting for the total wall area, the change in temperature and the factor of heat loss for each room in the buildings.• Sized duct work for the ventilation in the buildings based on the CFM required for each room.• Drafted riser diagrams for mechanical, electrical and plumbing systems in AutoCAD.• Verified the amount of BTUs coming into the apartment rooms using Carrier HAPS program.

Master Of Science, Mechanical Engineering, 3.5/4.0

Activities and Societies: American Society of Mechanical Engineers (ASME) American Institute of Aeronautics and Astronautics (AIAA).

Bachelor Of Science, Mechanical Engineering, 3.0/4.0