Job Description Summary
The Thermal System Design Engineer will report to the GE Aerospace Thermal Design & Secondary Flows Sub-Section Manager within the Engineering Sciences organization. In this role you will conduct thermal design, analysis, and test definition tasks in support of new technology introduction engine programs. You will utilize heat transfer and fluid mechanics analysis tools along with established design principles to propose thermal systems that meet program requirements. Potential applications include complex fluid delivery systems and sealing systems throughout engine.
Job Description
Roles and Responsibilities:
- Execute with guidance the analysis, design, test, and integration of fluid systems to meet business standards, established procedures, and program requirements.
- Independently perform thermal assessments using finite element analysis (FEA) and internally developed flow solvers.
- Collaborate with large multifunctional engineering design teams; Align personal priorities with needs of the larger team.
- Resolve design issues using established procedures. Consult with supervisor and senior team members as needed for issues beyond typical experience.
- Clearly communicate design study results and recommendations to technical experts and program leadership.
- Prepare invention disclosures for technology that provides a competitive advantage.
- Assure proper documentation of technical data consistent with engineering policies.
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Qualifications/Requirements:
- Bachelor of Science degree from an accredited university or college in Mechanical Engineering, Aerospace Engineering, or related discipline with an emphasis on heat transfer and design of fluid flow systems with a minimum of 3 years of relevant technical experience.
OR
- Master of Science degree from an accredited university or college in Mechanical Engineering, Aerospace Engineering, or related discipline with an emphasis on heat transfer and design of fluid flow systems with a minimum of 2 years of relevant technical experience.
OR
- PhD from an accredited university or college in Mechanical Engineering, Aerospace Engineering, or related discipline with an emphasis on heat transfer and design of fluid flow systems.
Desired Characteristics:
- Advanced Degree in Mechanical or Aerospace Engineering with emphasis in heat transfer or fluid mechanics.
- Experience in the fundamentals of heat transfer and compressible flows, including applicable engineering tools and systems.
- Experience with gas turbine engine design; Emphasis on cooling circuit design and analysis.
- Ability to plan, execute, and document engineering activities.
- Strong interpersonal and communication skills; Shares critical information, speaks with candor, and contributes constructively.
- Demonstrated effective contribution in a large, cross-functional team environment.
- Strong sense of ownership and an ability to analyze and resolve problems.
- Cognizant of system level interactions and can identify key inputs, outcomes, and contributors.
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