Component Design Engineer: Turbomachinery - Cold End Design (Fans, Compressors, and Rotatives)
$98,566–$160,169 year
HybridIndianapolis, Indiana, United States
Job Summary
Create component design definitions, establish Geometric Dimensioning & Tolerancing (GD&T) requirements, and support manufacturing to produce conforming hardware for gas turbine turbomachinery. Develop and execute validation plans, review supplier documentation and change proposals, and defend design solutions to program leadership. Perform leadership roles in investigations of in-service hardware issues, conducting failure analysis, root cause/corrective action reporting, and technical variance consultation. Support manufacturing, assembly, and aftermarket issues promptly to maintain production targets and fleet operations. Requires a Bachelor's or Master's degree in Engineering with 2+ years of experience; US citizenship required. Hybrid onsite schedule in Indianapolis, IN.
Required Qualifications
- Bachelor's degree in Engineering
- 2+ years of experience in design engineering
- Mechanical and/or Aerospace Engineering
- Master's degree in Mechanical and/or Aerospace Engineering
- JD/PHD in Mechanical and/or Aerospace Engineering
- US Citizen or permanent resident
Desired Qualifications
- Experience with turbine component design methods and practices to include component integrity, Structural Analysis, Thermals and Lifing spreadsheets
- Experience with coatings and their application within turbine and hot section systems
- Broader experience with rotating and static component design in highly stressed or critical assemblies
- Experience working with Siemens NX, Teamcenter and/or ANSYS Workbench
- Experience with the definition release process and GD&T
- Experience with computer programming and design optimization
- Experience working with manufacturing and/or quality, especially with regards to the assessment of non-conforming hardware
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