Honeywell Lead Mechanical Design Engineer 

United States 

809999790

KEY RESPONSIBLITIES

The engineer will be a module leader who will provide technical direction for all analyses performed on static structural components and systems for an exciting new gas turbine engine development program. Responsibilities include guiding the analysis, design, development, and test planning for static structural components to meet requirements for life, cost, weight, maintainability, and durability. The module leader will direct trade studies to inform engine architecture decisions.

Openings exist for the following engine modules:

Compressor: includes structural design of engine cases, flow path components, and a variable vane actuation system

Combustor & Turbine: includes engine cases, nozzles, seals, heat shields, and transition of advanced technology component concepts to production readiness

Bypass Ducts, Exhaust, & Externals: includes inner and outer bypass ducts, plumbing, and brackets.

The module leader must be adept at overseeing strength, vibration, fatigue, containment, heat transfer, deflection, and clearance analyses. In addition, the module leader will be responsible for ensuring that analysis results are presented clearly and effectively in design reviews and documented in reports to meet program deliverables and requirements. The lead engineer must have experience performing complex Finite Element Analyses (i.e., contact, preloaded fasteners, modal and forced vibration) to provide the necessary problem-solving guidance to the team. They may also at times be called upon to perform some analyses of key components themselves.

Driving process transformation to reduce design cost and cycle time is an important aspect of the position.

YOU MUST HAVE:

Requires a Bachelor's degree in engineering and 8+ years of experience in the field or in a related area.

WE VALUE

Knowledge of the gas turbine engine industry, specifically in one or more of the modules described above.

FEA (ANSYS or equivalent) and 3D modeling (CAD) of gas turbine engine static structures and systems

Capability 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

Experience with analyzing composite materials

System-level understanding of a gas turbine engine.

Knowledge of Six Sigma tools and application

• JOB ID: req445104
• Category: Engineering
• Location: 111 S 34th St.,Phoenix,Arizona,85034,United States
• Exempt
• Due to US export control laws, must be a US citizen, permanent resident or have protected status.