RELOCATION ASSISTANCE and SIGN ON BONUS
Be part of a team responsible for mechanical design, simulation, analysis and test of Fans and Compressors in gas turbine engine applications within Honeywell Aerospace Technologies. You will support currently fielded products and assist in developing new products for a variety of turbofan, turboshaft and auxiliary power unit applications. You will apply mechanical design theory and physics to both execute analysis and contribute to continuous improvement of simulation methods.
Key Responsibilities with Compressor Blades, Vanes, Disks and Impellers:
U.S. PERSON REQUIREMENTS
Due to compliance with U.S. export control laws and regulations, candidate must be a U.S. Person, which is defined as, a U.S. citizen, a U.S. permanent resident, or have protected status in the U.S. under asylum or refugee status.
#LI
#Fans
#Compressors
#Engines
#Turbomachinery
#Impellers
#stack analysis
#DARWIN
# NASGRO
# ANSYS
YOU MUST HAVE
WE VALUE
B.S., M.S. or PhD in aerospace or mechanical engineeringKnowledge of test methodologies for mechanical robustness assessmentMechanical knowledge related to manufacturing, product support and field supportAbility to conduct risk assessment and abatement planProblem solving with root cause analysis (RCCA)Strong writing, speaking and presenting skillsCAD based modeling experience (NX, UG, Solidworks, CATIA)Additional InformationJOB ID: req479763Category: EngineeringLocation: 111 S 34th St.,Phoenix,Arizona,85034,United StatesExemptDue to US export control laws, must be a US citizen, permanent resident or have protected status.Engineering (GLOBAL)Honeywell is an equal opportunity employer. Qualified applicants will be considered without regard to age, race, creed, color, national origin, ancestry, marital status, affectional or sexual orientation, gender identity or expression, disability, nationality, sex, religion, or veteran status.