Job description

Responsible for thermo-mechanical design of combustion systems using NX, ANSYS and Honeywell internal lifing methods Responsible for developing innovative combustor cooling schemes to develop full-life combustors Responsible for proposing new material choices in support of full-life combustors Perform stress, lifing, and hot-to-cold deflection analyses Develop innovative combustor designs that is resilient to high thermal loads Contribute to the development of combustion design methodology and multi-dimensional aerodynamic, heat transfer, stress, for both steady state and transient analysis Conduct successful combustion rig tests in support of combustor design validations Able to take ownership of combustor design and establish strong working relationship with combustion-aerodynamicists, design , manufacturing, and project groups Able to communicate effectively with both internal and external customers M.S/Ph.D. in Mechanical/Aerospace/Civil Engineering or related engineering discipline Prior experience in mechanical design of systems subject to high thermal loads Expertise in NX and ANSYS Familiar with standard combustor manufacturing approaches Familiar with combustor cooling schemes and combustor materials U. S. citizenship or permanent residency required Strong oral and written communication skills Strong data-driven decision making skills Additional Qualifications: Experience in the design of combustion systems Expert in combustor stress and lifing analyses Familiar with combustion aerodynamics Experience in CFD analysis Strong hot-section manufacturing background Evidence of strong communication skills, both written and oral, including presentation of technical papers in conferences nick davis 571-267-4182

Requirements

Must-haves

Responsible for thermo-mechanical design of combustion systems using NX, ANSYS and Honeywell internal lifing methods
Responsible for developing innovative combustor cooling schemes to develop full-life combustors
Responsible for proposing new material choices in support of full-life combustors
Perform stress, lifing, and hot-to-cold deflection analyses
Develop innovative combustor designs that is resilient to high thermal loads
Contribute to the development of combustion design methodology and multi-dimensional aerodynamic, heat transfer, stress, for both steady state and transient analysis
Conduct successful combustion rig tests in support of combustor design validations
Able to take ownership of combustor design and establish strong working relationship with combustion-aerodynamicists, design , manufacturing, and project groups
Able to communicate effectively with both internal and external customers
M.S/Ph.D. in Mechanical/Aerospace/Civil Engineering or related engineering discipline
Prior experience in mechanical design of systems subject to high thermal loads
Expertise in NX and ANSYS
Familiar with standard combustor manufacturing approaches
Familiar with combustor cooling schemes and combustor materials
U. S. citizenship or permanent residency required
Strong oral and written communication skills
Strong data-driven decision making skills
Experience in the design of combustion systems
Expert in combustor stress and lifing analyses
Familiar with combustion aerodynamics
Experience in CFD analysis
Strong hot-section manufacturing background
Evidence of strong communication skills, both written and oral, including presentation of technical papers in conferences
571-267-4182

Nice-to-haves

None flagged.

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