Posted Position Title Thermal System Design Lead Engineer (m/f)

Job Number 1897985 Business GE Aviation Business Segment Aviation About Us GE Aviation, a division of GE's Technology Infrastructure business, is a world-leading producer of commercial jet engines and components as well as integrated digital, electric power, and mechanical systems for aircraft with an extensive global service network to support these products. Technological excellence, supported by continuing substantial investments in research and development, has been the foundation of GE Aviation's growth and helps to ensure quality products for customers. GE Aviation is increasing our presence in Europe, and now is the time to join the technology team at our Munich, Germany location. For more than 125 years, GE has been respected for its performance and innovative spirit. GE people worldwide are dedicated to turning imaginative ideas into leading products and services that help solve some of the world's toughest problems. We are expanding our technology development team to meet the growing demand for new and innovative products. As a member of the technology team, you will cooperate with GE Aviation worldwide and members of GE Global Research and apply your expertise to the design and development of the next generation of aircraft engines and components. Career Level Experienced Function Engineering/Technology Function Segment Product Design and Development Location(s) Where Opening Is Available Germany City Garching b. Munchen Postal Code 85748 Relocation Expenses Yes Role Summary/Purpose The Thermal System Design Lead Engineer is a technical expert in thermal analysis capabilities of aircraft engine components and systems. This includes the development and validation of secondary flow and heat transfer for the purpose of supporting the design of commercial aircraft engines. Essential Responsibilities Your specific responsibilities will include: Develop new technologies or enhance current technologies for the purpose of pushing the technology in aircraft engines forward for lower specific fuel consumption, higher thermodynamic efficiencies and increased hardware life Specific components or regions of investigation are: Rotor/Stator Heat Transfer; Rotor Thrust; Secondary Air System; Turbine Flow Path Heat Transfer Plan and execute component and engine test programs and utilize the results to validate engine designs, systems and analytical models Work with a variety of engineering organizations and contribute to the development of the engine systems and designs Provide technical leadership to personnel supporting the assigned project and participate as a presenter or reviewer in technical and program reviews Qualifications/Requirements Master’s degree in Mechanical Engineering, Aerospace Engineering, or related discipline with a minimum of 10 years of relevant experience in the area of aero engine or industrial gas turbine heat transfer or secondary flow Experience with analytical software such as CFX, FLUENT, STAR-CD, ANSYS, Matlab, etc. Experience with 1-D flow network codes Experience in integrating thermal system design in the context of the overall propulsion system, with sound understanding of how component design impact the larger engine design Proven ability to create and execute strategic vision for product advancement Excellent communication and influencing skills with the ability to communicate at a variety of levels, from detailed design reviews to high-level leadership reviews Strong connections to relevant professional societies, and recognition through publications and patents Fluency in English Desired Characteristics Masters or PhD in Mechanical Engineering, Aerospace Engineering, or related discipline Passion for technical excellence and technology advancement Able to self-manage workload across a number of designs Strong focus on identifying and improving processes and tools Self–directed and motivated For further questions please contact the Recruiter Anna Bartlewski 0049-89-5528 3121