Gas Turbine - Engine Integration (SAS & Heat Transfer) Engineer

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.

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.

More than 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.).

Full time