Job Description SummaryAs the Large Military Systems Technology Integration Aerothermal Staff Engineer, you will be responsible for the thermal characterization of hardware and management of secondary flows in large combat aircraft engines. You will be responsible for addressing and completing individual work projects, work with team on defining tasks, technical related deliverables, associated milestones and cost with an on time deliverable mindset leading and mentoring the work of others, and coordinating work within the engineering design teams.Job Description
Essential Responsibilities :
- Execute, Coordinate and Lead turbine 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 DP 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 while ensuring program cost, quality and schedule requirements are met
Required Qualifications :
- Bachelor of Science in Mechanical or Aeronautical Engineering related to heat transfer and fluid mechanics from an accredited college or university
- A minimum of 5 years of experience in an Aerospace or Mechanical Engineering position
Desired Characteristics :
- Master of Science in Mechanical or Aeronautical Engineering related to heat transfer and fluid mechanics from an accredited college or university
- Ph.D. Degree in Mechanical or Aeronautical Engineering related to heat transfer and fluid mechanics from an accredited college or university
- Strong understanding of Heat Transfer and fluid mechanics/dynamics fundamentals, design, analysis and processes related to turbomachinery thermal design
- 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
- Skilled in Heat Transfer fundamentals and systems level module/component turbomachinery thermal design
- Deep understanding of Gas Turbine thermal systems level module/component design, tools, analysis and processes
LI-MF1
This role requires access to U.S. export-controlled information. If applicable, final offers will be contingent on ability to obtain authorization for access to U.S. export-controlled information from the U.S. Government.
Additional Information
GE offers a great work environment, professional development, challenging careers, and competitive compensation. GE is an Equal Opportunity Employer. Employment decisions are made without regard to race, color, religion, national or ethnic origin, sex, sexual orientation, gender identity or expression, age, disability, protected veteran status or other characteristics protected by law.
GE will only employ those who are legally authorized to work in the United States for this opening. Any offer of employment is conditioned upon the successful completion of a drug screen (as applicable).
Relocation Assistance Provided: Yes
