Engineer

The primary job responsibility is to work on Aero Engine components and to take complete ownership of his or her work on various tasks involved in Design Engineering. Candidate shall support independently thermal analysis/design of aero engine components with strong understanding of Thermal and fluid sciences. The execution will be in accordance with established design practices and work instructions.

Candidate should able to drive and lead product improvements activities, method development and continuous improvement activities through various internal forums of GKN. He should coach/mentor Junior engineers.

Key accountabilities

Individual contributor working in Design engineering delivering thermal analysis tasks mainly

Supporting the structural design process to ensure required quality is achieved within direct area of responsibility

Supporting continuous improvement initiatives to increase team efficiency

Develop, implement, and check technical solutions and compliance documentation to ensure they are compliant with all relevant customer, regulatory, and airworthiness requirements, within agreed program, schedule, and manufacturing constraints.

Identify technical problems and apply/integrate solutions.

Execute and implement methods plans, toolsets and approaches that are appropriate and compliant to achieve the design and programme objectives.

Identify and assess technical risk for own work and propose mitigations within assigned programmes/projects.

Generate assigned project deliverables, documents, and reports according to the project signature authorizations.

Support technical and customer reviews, including formal gate reviews, including the creation and preparation of technical data and presentations of product design.

Perform all activities at a level of minimal supervision and support other engineers with peer-to-peer reviews. He or She will make sure OTD & FTR always above the set target for his/her team.

Person specification

Essential:

Master’s degree in Engineering, Mechanical/Thermal/Aerodynamics /Aerospace or equivalent

Must have  hands-on experience in thermal analysis/design of aero engine components with strong understanding of Thermal and fluid sciences

Excellent fundamentals in Thermodynamics

Experience in fluid dynamic and heat transfer using Fluent/Ansys

Knowledge of Thermal Boundary creations

• Knowledge of tools, HYPERMESH/Simcentre and ANSYS mechanical & APDL

Knowledge of scripting languages (MATLAB/Python/Shell/awk..etc.)

Knowledge on Workbench

Knowledge on Flow master

Experience in mathematical modeling and statistical analysis

Ability to interpret results applying physics and propose design solutions

Good technical report writing skills

Good product knowledge related to aero engines. Especially IMC/TEC or any other casings

Contributed to the technical development of processes/methods, products or people

Contribute to Dept./Org. KPI & also TIP