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Component Design Engineer: Turbomachinery - Cold End Design; Fans, Compressors, and Rotatives

Job in Indianapolis, Hamilton County, Indiana, 46262, USA
Listing for: Rolls-Royce
Part Time position
Listed on 2026-09-25
Job specializations:
  • Engineering
    Mechanical Engineer, Aerospace / Aviation / Avionics, Manufacturing Engineer
Salary/Wage Range or Industry Benchmark: 94000 - 153000 USD Yearly USD 94000.00 153000.00 YEAR
Job Description & How to Apply Below
Position: Component Design Engineer: Turbo machinery - Cold End Design (Fans, Compressors, and Rotatives)
Location: Indianapolis

Job Description

Job Title:

Component Design Engineer:
Turbo machinery
- Cold End Design (Fans, Compressors, and Rotatives) Working Pattern:
Hybrid/Onsite In office 3 days/week Working location:
Indianapolis, IN

Relocation is available for this position if appropriate

Job Description

Job Title:

Component Design Engineer:
Turbo machinery
- Cold End Design (Fans, Compressors, and Rotatives) Working Pattern:
Hybrid/Onsite In office 3 days/week Working location:
Indianapolis, IN

Relocation is available for this position if appropriate

Why Rolls-Royce?

At Rolls-Royce we are proud to be a business that has truly helped to shape the modern world and are committed to always being a force for progress; powering, protecting and connecting people everywhere.

By joining Rolls-Royce, you’ll have the opportunity to create world-class power and propulsion solutions, pushing your problem-solving and ingenuity, to deliver real impact that puts safety first.

You’ll be given responsibility and the opportunity to grow in our high-performance culture. This is Infinite Potential
. And it’s your chance to really shine and contribute to one of the world’s most recognized brands and a beacon for engineering excellence.

Position Summary

As a Component Design Engineer for gas turbine Turbo machinery components you will be part of the global Engineering, Technology & Safety (ET&S) Turbo machinery organization. You will develop complex engineering solutions that satisfy cutting-edge aerospace functional and physical requirements and exhibit robustness for manufacturing capability. Within your assigned propulsion system program, you’ll be responsible for developing, assessing, and delivering high-performance gas turbine turbo machinery components that push the envelope with performance, life, and efficiency.

What

You Will Be Doing
  • Create component design definition in accordance with module, system, and customer interface requirements.
  • Create dimensional tolerance stacks, establish Geometric Dimensioning & Tolerancing (GD&T) requirements, and support manufacturing to produce conforming hardware.
  • Support the supply chain in procuring hardware including review of supplier documentation, assessment of non-conforming hardware, and review of supplier change proposals.
  • Review and approve component requirements for their responsible sub-system’s hardware. Develop, approve, and execute validation plans to demonstrate compliance to the requirements.
  • Present and defend design solutions and technical work to program leadership and other stakeholders.
  • Support manufacturing, assembly, service, and aftermarket issues promptly as they arise to keep production on target and the fleet in operation.
  • Perform a leadership role in investigations of in-service and/or development hardware issues including Engine Investigations, failure analysis, root cause / corrective action (RCCA), Technical Variance consultation, reporting, and documentation. Share findings with the global turbo machinery team in accordance with export control regulations.
Basic Requirements
  • A Bachelor’s degree in Engineering with 2+ years of experience in Design engineering, Mechanical and/or Aerospace Engineering OR;
  • A Master’s degree in Mechanical and/or Aerospace Engineering OR;
  • JD/PHD in Mechanical and/or Aerospace Engineering.
  • To be considered for this opportunity, you must be a US Citizen or permanent resident.
Preferred
  • 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,…
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