Gas Turbine Thermal System Engineer - Thermal SAS Whole Engine

POWERTECH; Abu Dhabi; On-site; AED 120,000 - 180,000; Full time

Job summary

PowerTech in Abu Dhabi is seeking a Thermal System Design Engineer to drive gas turbine component thermal analysis, secondary air and oil system design within turbojet and turbofan development programs. You should have a strong background in heat transfer, thermodynamics and fluid mechanics, plus fluency in English.

The role involves developing and applying numerical and experimental methods for verification, mentoring junior engineers, and reviewing designs and testing guidelines to mitigate

Qualifications

• Aerospace/Mechanical Engineering degree or related field.
• Strong background in gas turbine propulsion, heat transfer, thermodynamics and fluid mechanics.
• Fluent in English.
• Experience: 5-15 years or more.

Responsibilities

• Carry out component thermal analysis simulations for engine thermal mapping.
• Assess steady and transient thermal and secondary flows in turbine components.
• Size and design oil/lubrication system, seals, sump, bearings and pumps.
• Develop numerical and experimental methods for verification/validation.
• Support team, mentor junior engineers and provide feedback.
• Review designs, simulations and testing guidelines.
• Identify project risks and plan mitigations.

Skills

Gas turbine propulsion

Heat transfer

Thermodynamics

Fluid mechanics

Communication skills

Problem solving

Education

Bachelor's degree in Aerospace or Mechanical Engineering

Tools

Ansys Workbench

FEA

CFD

Flomaster

Amesim

MATLAB/Simulink

C

Job description

Job Description:

External Job Description

About Us

PowerTech is a leading innovator in propulsion technologies, specializing in cutting-edge microjets, turbofan engines, and internal combustion engines. We are dedicated to advancing propulsion systems through rigorous testing, precision engineering, and robust manufacturing processes.

Job Overview:

Thermal System Design Engineer will be responsible for carrying out the gas turbine component thermal analysis, secondary air system and oil system design & analysis activities within the turbojet & turbofan development programs. This role requires expert knowledge in heat transfer, fluid mechanics, gas turbine propulsion, planning for projects and ability to develop individuals.

Key Responsibilities

• Carry out component thermal analysis simulations for thermal mapping of the engine
• Carry out steady and transient thermal & secondary flows assessment in gas turbine engine components
• Carry out sizing and design studies for the oil / lubrication system, seals, sump, bearings & pumps.
• Develop numerical and experimental methods for method verification and validation
• Support other team members, develop junior engineers and provide constructive feedback
• Review the designs, simulations and generate testing guidelines
• Identify project risks and plan for mitigation

Qualifications & Experience

• Aerospace, Mechanical Engineering degree or a related field.
• Strong background in gas turbine propulsion, heat transfer, thermodynamics and fluid mechanics.
• Fluent in English
• Experience: 5-15 years or more.

Skills

• Technical skills in one or a combination of stated topics.
• Using commercial tools such as Ansys Workbench or similar.
• Experience in FEA, CFD or lower order simulation methods.
• Experience in 1D flow network software such as Flomaster and Amesim
• Experience in programming using C, Matlab/Simulink or similar.
• Awareness on the state-of-the-art technologies in materials, aerodynamics and structural mechanics to link with thermal system design for gas turbine propulsion
• Good communication and presentation skills to interact with team members, clients, and vendors.
• Ability to solve problems, prioritize tasks and delegate when necessary