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- Perform design, analysis and validation testing of static structural components for gas turbine engines. Specific components include turboshaft engine components such as: inlets, frames, mounts, compressor stators, shrouds and cases, gas generator and power turbine shrouds, nozzles, tangential on-board injectors, heat shields and baffles.
- The scope of work includes creation and development of sound design solutions for newly proposed and existing products.
- Analytical results will be presented in design reviews and with appropriate documentation to meet program deliverables and requirements.
- Applicant must work effectively with design teams, global support and chief engineers.
- Responsibilities also include working productivity initiatives to advance the current state of the art and establish standardized processes for criteria, guidelines and practices.
- Bachelor’s Degree in Mechanical or Aerospace Engineering
- Minimum of 6-8 years of experience in a mechanical engineering field
- Minimum of 4 years industry experience performing finite element analysis using ANSYS
- Knowledge of the gas turbine engine industry
- 3D modeling (CAD) and FEA (ANSYS, etc.) of gas turbine engine static structures and systems
- Capable of performing complex analyses and hand calculations of engine components and systems
- Proven understanding and application of solid mechanics, dynamics, fatigue, and finite element analysis
- Tacit knowledge and experience with topological optimization of static structural components for minimum weight
- Ability to lead or act as focal point for the activities being performed by multiple engineers on an engine program or module
- Excellent communication skills (written and oral) are required to interact with engineering teams, other disciplines, and the customer
- Knowledge of Six Sigma tools and applications
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