Mechanical Design Engineer II (2688) - Gas Turbine Hot Gas Path / Rotor Components | ANSYS & NX (Remote)

RISINGSUN TECHNOLOGIES is seeking experienced Mechanical Design Engineers to support the design and analysis of gas turbine hot gas path and rotor components for heavy-duty gas turbine and aeroderivative engine applications. The role involves collaborating with cross-functional teams to ensure hardware meets product requirements and quality expectations while performing mechanical design and analysis tasks.

Responsibilities:

• Perform mechanical design and analysis of heavy-duty and aeroderivative gas turbine components
• Evaluate hot gas path and rotor components, including turbine blades, nozzles, shrouds, and rotors
• Execute assigned hardware design and evaluation tasks using sound engineering principles
• Ensure designs comply with business standards, procedures, product requirements, and program expectations
• Participate in formal and informal technical reviews for design tasks and outputs
• Collaborate with engineering title holders, heat transfer teams, manufacturing, sourcing, and supply chain teams
• Support component and subsystem optimization with a focus on:
• Design for Cost
• Design for Variation
• Design for Manufacturability
• Product and lifecycle cost improvements

Requirements:

• Must be a US Citizen / Green Card Holder
• Must be willing to work on our W2
• Bachelor's Degree in Mechanical Engineering or a related Engineering/Science discipline from an accredited college or university
• 4–8 years of engineering analysis experience
• Experience with mechanical design and analysis of gas turbine components
• Prior experience designing and analyzing turbine blades, nozzles, shrouds, and/or rotors
• Hands-on experience using ANSYS for engineering analysis
• Proficiency with CAD software, preferably NX
• Strong understanding of mechanical engineering principles
• Ability to apply engineering fundamentals to component design and analysis
• Effective written and verbal communication skills
• Demonstrated ability to work in cross-functional engineering teams
• Direct experience with gas turbine hot gas path components, rotor components, ANSYS analysis, and NX CAD design
• Experience supporting heavy-duty gas turbine or aeroderivative engine programs is highly preferred