Sr Stress Engineer 1st Shift (On site)

at  Collins Aerospace

QUALIFICATIONS YOU MUST HAVE:

• Experience in classical hand analysis methods used in aerospace applications, along with Finite Element Analysis Tools such as NASTRAN & PATRAN or similar software applications.
• Understanding of load paths and various aspects of airframe design using metals and composites.
• Strong technical writing and PC skills with proficiency in MS Office (Word, Excel, PowerPoint).
• Provide solutions to a variety of technical problems of basic scope and complexity.
• Expresses problems, issues, and opportunities to peers and supervision.
• Uses and validates SW and CI tools to solve problems. Awareness of assigned tasks and activities on product metrics.
• Excellent communication and presentation skills with the ability to work closely as a team with other international locations.
• Must be able to communicate effectively in English, both verbally and in writing
• Must have a current travel visa to enter the USA for training and event attendance purposes

QUALIFICATIONS WE PREFER

• Previous experience in EBU & Nacelle components is very desirable.
• Experience in aircraft structural components static, durability and damage tolerance analysis.
• Experience of material (Composite & Metallic) or structural testing.
• Engine Build up (EBU) systems experience.
  Collins Aerospace, a Raytheon Technologies company, is a leader in technologically advanced and intelligent solutions for the global aerospace and defense industry. Collins Aerospace has the capabilities, comprehensive portfolio and expertise to solve customers’ toughest challenges and to meet the demands of a rapidly evolving global market.

Unspecified

What You Will Do:

• Conduct stress, fracture and fatigue structural analysis of aerospace components.
• Perform structural analysis nature using conventional hand analysis and/ computer analysis.
• Develop and document structural test efforts to assess structural integrity of metallic and non-metallic aerospace products.
• Works to design parameters to access the structural integrity of metallic and non-metallic aerospace component parts.
• Provide solutions to a variety of technical problems of basic scope and complexity.
• Use and validate CI tools to solve problems. Previous experience in EBU components is very desirable.