Be part of a team responsible for mechanical design, simulation, analysis and test of Fans and Compressors in gas turbine engine applications within Honeywell Aerospace Technologies. You will support currently fielded products and assist in developing new products for a variety of turbofan, turboshaft and auxiliary power unit applications. You will apply mechanical design theory and physics to both execute analysis and contribute to continuous improvement of simulation methods.

Key Responsibilities with Compressor Blades, Vanes, Disks and Impellers:

• Execute mechanical design and analysis – including vibration, deflection, fatigue crack growth, burst, HCF, LCF, thermal and stack analysis – and generate accompanying documentation capturing findings and results
• Support mechanical testing of components and engine modules in various lifecycle stages (rig, development, production) and perform data reduction/analysis on test data
• Develop and present engineering artifacts during structured design reviews
• Interpret engineering drawings via geometric dimensioning and tolerancing (GD&T)
• Contribute to technical mentoring, process/tool improvement and knowledge capture

U.S. PERSON REQUIREMENTS
Due to compliance with U.S. export control laws and regulations, candidate must be a U.S. Person, which is defined as, a U.S. citizen, a U.S. permanent resident, or have protected status in the U.S. under asylum or refugee status.