Perform detailed structural analyses of dynamic system components, including the rotor system, control system, and blades
Evaluate static strength and fatigue life of critical structures using classical hand calculations and finite element analysis for both flight loads and ground load conditions
Evaluate component life and dynamic response of dynamically loaded metallic and composite components subject to high and low cycle fatigue
Author structural substantiation reports and other required technical documentation to meet program needs
Support full scale component ground testing and flight testing, including test requirements, layout, instrumentation, and data reduction
Develop best practices for structural analysis of critical aerospace structures
Collaborate with the aerodynamics and loads & dynamics teams to design high performance propeller and rotor blades
Collaborate with internal and external customers to ensure on-time delivery of data
Requirements
Required:
Bachelor's degree in aerospace engineering, mechanical engineering, or related field
5+ years of experience in design and analysis of critical aircraft structures
Proficient in ANSYS, NASTRAN, or other FE software
Knowledge of fatigue and damage tolerance of composites
Knowledge of high cycle and low cycle fatigue in metallic components
Ability to read engineering drawings and interpret CAD models
CAD design experience (NX preferred)
Strong technical, written, and verbal communication skills
Experience in a fast-paced design environment
Preferred:
Master's in aerospace engineering, mechanical engineering, or related field
10+ years of experience in design and analysis of rotorcraft dynamic systems, including rotors, controls systems, and propeller or rotor blades
Background in ground and flight testing of critical composite aerospace structures
Familiarity with FAA aircraft and/or rotorcraft loads and dynamics regulations (FAR Part 23, 27, 33, 35) and associated advisory materials
Experience with static and dynamic loads derivation for fixed-wing vehicles and/or VTOL aircraft
Ability to perform aeroelastic analysis on VTOL dynamic systems
Prior involvement in FAA or military rotorcraft certification efforts
Proficiency in Python and/or Matlab scripting
This position will require travel up to 10% to Archer facilities or supplier facilities.
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Archer is unable to provide work visa sponsorship for this position at the present time.
Archer is proud to be an Equal Opportunity employer committed to diversity and inclusivity in the workplace. All aspects of e
Additional Information
Archer is an aerospace company based in San Jose, California building an all-electric vertical takeoff and landing aircraft with a mission to advance the benefits of sustainable air mobility. We are designing, manufacturing, and operating an all-electric aircraft that can carry four passengers while producing minimal noise.
Our sights are set high and our problems are hard, and we believe that diversity in the workplace is what makes us smarter, drives better insights, and will ultimately lift us all to success. We are dedicated to cultivating an equitable and inclusive environment that embraces our differences, and supports and celebrates all of our team members.
Archer Aviation is seeking a highly motivated, experienced engineer to join our team in revolutionizing the aviation industry. The candidate will support analysis and testing of the rotor system on a new unmanned vehicle platform, including the rotor head, blades, and control system. This role requires expertise of structures of metallic and composite structures and a deep understanding of rotorcraft dynamic systems. Candidate should have a good understanding of fatigue life predictions with a strong background in finite element methods as well as analytical first principles. The ideal candidate will act as a mentor to other members of the team with less experience and establish best practices to follow for the program.
Archer56 · San Jose, CA