Staff Engineer – Large Military Engines Thermal Systems Design
| Company | GE Aerospace |
|---|---|
| Location | Sharonville, OH, USA |
| Salary | $Not Provided – $Not Provided |
| Type | Full-Time |
| Degrees | Bachelor’s, Master’s, PhD |
| Experience Level | Senior |
Requirements
- Bachelor of Science in Mechanical or Aerospace Engineering from an accredited college or university.
- A minimum of 5 years of experience in an Aerospace or Mechanical Engineering position related to heat transfer.
- A minimum of 2 years of experience exclusively with Secondary Air Systems at a systems level and/or cooling analysis of turbomachinery components.
- Legal authorization to work in the U.S. is required. We will not sponsor individuals for employment visas, now or in the future, for this job opening.
Responsibilities
- Execute, Coordinate and Lead turbo machinery at systems level – Module/Component heat transfer, cooling design, modeling and analysis for all Large Combat engines including fielded products and New Product Introductions.
- Execute, with minimal guidance, the design, analysis, and evaluation of assigned projects using sound engineering principles and adhering to business standards, practices, procedures, and product & program requirements.
- Formulate and implement achievable and sustainable plans to establish technical and program requirements, schedules, and contract commitments.
- Monitor and communicate project status, business issues and significant developments to cross functional team leads and leadership.
- Develop action plans to anticipate and respond to thermal system design challenges to meet internal design practice requirements as well as external customer requirements.
- Prepare and present accurate technical data to internal and external customers.
- Provide mentoring, technical guidance and coaching to personnel supporting assigned projects.
- Assure proper documentation of technical data generated for the assigned projects and/or tasks consistent with engineering policies and procedures.
- Concurrently lead multiple projects, ensuring adherence to program cost, quality, and schedule requirements.
Preferred Qualifications
- MS/PhD in Mechanical or Aerospace Engineering related to heat transfer and fluid mechanics from an accredited college or university.
- Experience exclusively in component cooling analysis of turbine blades, nozzles and shrouds with film cooling.
- Deep understanding of Gas Turbine Thermal Systems module/component level design, tools, analysis, and processes.
- Effective in contributing in a structured, cross functional team-oriented environment.
- Strong oral and written communication skills.
- Strong interpersonal and leadership skills.
- Proven analytical and organizational ability.
- Highly motivated with good engineering judgment.