Schedule: Monday–Friday, 8:00 AM–5:00 PM
Opportunity: 12-Month W2 Contract (No C2C or 1099)
Role Overview
The Mechanical Design Engineer will be responsible for the design and analysis of Turbine Hot Gas Path and Rotor components for Heavy Duty Gas Turbine (HDGT) and Aeroderivative engines. This role involves close collaboration with cross‑functional engineering teams and Global Supply Chain partners to ensure hardware meets all Product and Design Practice Critical‑to‑Quality (CTQ) requirements.
The engineer will work closely with Controlled Title Holders, Heat Transfer, Manufacturing, and Sourcing teams to optimize components and subsystems, with a strong focus on:
- Design for Cost (product and total lifecycle)
- Design for Variation
- Design for Manufacturability
Key Responsibilities
- Perform mechanical design and analysis of Heavy Duty and Aeroderivative gas turbine components, with emphasis on hot gas path and rotor hardware.
- Execute the design and evaluation of assigned components using sound engineering principles and in compliance with business standards, procedures, and program requirements.
- Participate in and present design work during formal and informal technical reviews in collaboration with Controlled Title Holders.
- Adhere to documented New Product Introduction (NPI) and Root Cause Analysis (RCA) processes for all design activities and deliverables.
Minimum Qualifications
- Bachelor’s degree in Mechanical Engineering or a related engineering or science discipline from an accredited institution
- 4–8 years of engineering analysis experience
Qualifications & Skills
- Experience designing and analyzing turbine blades, nozzles, shrouds, and/or rotors using ANSYS
- Proficiency in CAD software, preferably Siemens NX
- Solid understanding of core engineering principles and the ability to apply them effectively
- Strong written and verbal communication skills
- Proven ability to collaborate effectively within cross-functional teams