Job Description

:Energy, Siemens Limited India is seeking a responsible, professional, and self-motivated individual to join the Gas Turbine R&D, Gurgaon as \xe2\x80\x9cGas Turbine- Engine Integration (SAS & Heat Transfer) Engineer\xe2\x80\x9d. 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\xe2\x80\x99s 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\xe2\x80\x99s optimization.
• Collaborate with different design groups to drive design changes in order to optimize engine performance.

We don\xe2\x80\x99t need superheroes, just super minds:

• Bachelor / Master\xe2\x80\x99s 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.).

Siemens