Gas Turbine - Heat Transfer Engineer Job in Gurugram at Siemens

Siemens is hiring for the role of Gas Turbine - Heat Transfer Engineer!

Responsibilities of the Candidate:

• Heat transfer and cooling design and analysis of gas turbine parts (rotating or stationary or system).
• Heat transfer and flow analysis using in-house & commercial 1D,2D,3D & CFD codes e.g., CFX, Star CCM+. Able to understand physics, apply relevant assumptions, interpret results & perform basic hand calculations in fluid mechanics & heat transfer discipline.
• Thermal modeling using flow network approach with pressure loss and heat transfer correlations. Able to apply boundary conditions to an FE solver (NX- Sim center/ NASTRAN, ANSYS, ABAQUS) for the calculations of material temperature.
• Able to understand the product function, design requirements and design principles.
• Be a point of contact, and speaking partner and provide expertise regarding hot gas path heat transfer related topics in a project.
• Work with the project lead to understand the project requirements, find solutions to design challenges, and deliver results within the agreed timeline & quality.

Requirements:

• Mechanical engineer with an MTech in Mechanical engineering (major- Fluid & Thermal Science) with a focus on fluid mechanics, heat transfer & thermodynamics.
• Minimum 6 years of relevant experience in thermal analysis and design of cooled gas turbine components.
• Experience in utilizing heat transfer and cooling design engineering skills to analyze technical requirements and applying appropriate skill set to design hot gas path, Casing & Rotor turbine components.
• Ability to analyze/create thermal boundary conditions and perform Flow & Heat Transfer engineering calculations both for analytical, flow network, correlation-based and CFD & Conjugate Heat Transfer (CHT) based tasks.
• Finite element analysis & ability to review the results. Good Familiarity with FE codes like ANSYS or general-purpose FEA tools.
• Heat Transfer-design fundamentals & problem-solving skills (Gas Turbine Component, System level)
• Basic understanding of Mechanical integrity (Strength, Fatigue, Creep, Fracture) Turbomachinery Aerodynamics, and manufacturing aspects for gas turbine blading.
• Experience using Pro / E, NX (Uni-graphics) or other similar solid modeling CAD software for visualization of cooling channel/scheme layout of components or engine assembly is a merit.