Lead Engineer - Gas Turbine Heat Transfer

Job Description

We are looking for a heat transfer engineer to be responsible for turbine blades and vanes heat transfer calculation and cooling design for heavy duty gas turbine development.

What are my responsibilities?

  • You will be responsible for gas turbine hot path parts design including heat transfer and friction correlations, Impingement cooling, film cooling, & compressible flow design to fulfill the turbine performance requirements defined in product requirement specifications
  • Closely work within turbine blades and vanes design integrated project team with different disciplines including aerodynamics, second air system engineering, mechanical design, mechanical integrity, material and manufacturing.

What do I need to qualify for this job?

  • Master’s degree or above in mechanical engineering, thermal engineering, aeronautical engineering or turbomachinery
  • 5 years or above working experience in various gas turbine vane and blades heat transfer design
  • Familiar with heat transfer and friction correlations, impingement cooling, film cooling and compressible flow. Hands-on experience on 1D flow network analysis.
  • Familiar with design modeling tools such as NX, 3D CFD Pre-Processing tools, commercial or in-house aerodynamics and heat transfer calculation tools such as CFX.
  • Good understanding on turbine blades and vanes manufacturing and mechanical integrity.
  • Proficient in idea generation and be able to transfer know-how or search for outside available sources to various contexts and solve difficult technical problems independently
  • Strong interpersonal skills to work with multi-cultural colleagues, customers, industry experts, and university associates.
  • Good teamwork, ownership and results oriented
  • Good communication and presentation skills.
  • Professional proficiency in English language

Job ID: 120812

Organization: Gas and Power

Company: Siemens Ltd., China

Experience Level: Experienced Professional

Job Type: Full-time

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