Job Family: Research & Development

Req ID: 412439

Looking for challenging role? If you really want to make a difference - make it with us

Energy, Siemens Limited India is seeking a responsible, professional, and self-motivated individual to join the Gas Turbine R&D, Gurgaon as “Gas Turbine- Engine Integration (SAS & Heat Transfer) Engineer”. This position provides an exciting opportunity to work in a fast-paced, dynamic, global product development & service environment. This position is for an experienced professional, who will be responsible for assessment of flows (Secondary air system model) thermals and displacements (Whole engine model) to support R&D projects of Gas turbines.

The selected candidate will join an aspiring team of engine integration engineers working on existing GT product and/or the next generation of Siemens Gas turbines.

Your new role – challenging and future- oriented:

• Synthesis and Analysis of Secondary air system (SAS) & Whole engine (WE) models to estimate mass flows, thermals & displacements of gas turbine development programs.

• Complete ownership of the Secondary air system & Whole engine models for different gas turbine variants.

• Fully accountable for model results and successful completion of design or gate reviews for NPI’s and service upgrades.

• Perform quick design trade studies via. Secondary air system and Whole engine model assessment.

• Incorporate best practices from Siemens gas turbines regarding engine operations and controls.

• Develop instrumentation and testing plans to support engine development program and calibrate/validate SAS & WE models based on the measured instrumentations.

• Post-processing of Secondary air system results to be applied in Whole Engine thermo-mechanical model for metal temperature predictions and clearance’s optimization.

• Collaborate with different design groups to drive design changes in order to optimize engine performance.

We don’t need superheroes, just super minds:

• Bachelor / Master’s degree in Mechanical/aerospace engineering discipline from recognized university.

• 2 to 6 years of experience in the design and development of Gas turbine components in context to Secondary air system, whole engine modeling, clearances & sealing design.

• Basic understanding of gas turbine components and operations, including key design criteria in context to Secondary air system & Whole engine models.

• Experience with Fluid Mechanics & Heat Transfer techniques in Gas turbines.

• Knowledge of fluid and structure interactions to simulate SS and transient conjugate thermal analysis.

• Proficiency in one or multiple computational modeling tools for thermo-mechanical or computational fluid dynamics analysis (e.g., SC03, CFX, Ansys, Abaqus, NASTRAN, ProE, NX etc.).

• Problem-solving ability.

• Data analysis skills.

• Verbal and written communication skills.

• Positive Interpersonal skills ((i.e., team player, quick learner, ability to adapt quickly & effectively etc.).