Airfoils-Staff Responsible Engineer

The Kemtah Group, Inc.

  • Brisbane, CA
  • 16 days ago
  • $143,000 Per Hour

Highlights

Job Title: Airfoils-Staff Responsible Engineer Location: Brisbane, CA Pay range: $143,000/yr $68.75/hr Shift: 1st Shift Zip Code: 94005 Job Type: Contract-to-Hire or Direct Hire Start Date: ASAP Keywords: #Brisbanejobs; #AirfoilsStaffjobs; #INDREG Job Description: Location: San Francisco/Hybrid Department: Structural & Mechanical Engineering Employment Type: Contractor full-time, convertible to salaried full-time. Expected to perform hand calcs and straightforward FEA / CFD tasks Scope & Ownership Owns the aerodynamic design of axial-compressor and turbine airfoils across the engine: transonic, mid- and final-stage compressor blades & vanes; compressor-turbine (CT) and power-turbine (PT) blades & vanes; and PT / mid-turbine-frame flowpath.

Numbers & Facts

LocationBrisbane, CA

Description

Job Title: Airfoils-Staff Responsible Engineer Location: Brisbane , CA Pay range: $143,000/yr $68.75/hr Shift: 1st Shift Zip Code: 94005 Job Type: Contract-to-Hire or Direct Hire Start Date: ASAP Keywords: #Brisbanejobs; #AirfoilsStaffjobs; #INDREG Job Description: Location: San Francisco/Hybrid Department: Structural & Mechanical Engineering Employment Type: Contractor full-time, convertible to salaried full-time. Responsible Engineer a. Own end-to-end requirements development, design, analysis, test, qualification, and lifecycle management b. Expected to perform hand calcs and straightforward FEA / CFD tasks Scope & Ownership Owns the aerodynamic design of axial-compressor and turbine airfoils across the engine: transonic, mid- and final-stage compressor blades & vanes; compressor-turbine (CT) and power-turbine (PT) blades & vanes; and PT / mid-turbine-frame flowpath. Two scopes - transonic compressor blades and power-turbine blades - are Staff-RE leads. Crossover encouraged: compressorturbine aero, aeroaeromechanics, aerosecondary-air. Minimum Education Bachelor"s degree in Mechanical or Aerospace Engineering Master"s or PhD preferred (a turbomachinery PhD can substitute for some experience) Experience 4-8 years of turbomachinery aerodynamic design or a turbomachinery PhD plus ~2 years 3+ years of blade/vane aerodynamic design from 1D meanline through 3D CFD Rig and/or engine test experience (instrumentation, data reduction, correlation) Aeromechanics / aeroelasticity exposure desirable Skill Requirements Axial compressor and/or turbine aerodynamic design (1D / 2D / 3D) CFD and numerical methods; loss, secondary-flow and tip-clearance modeling Blade/vane parameterization and design optimization Python and/or Matlab; 2D/3D CAD (Solidworks, CATIA, NX/ProE, etc.) Responsibilities Take sole ownership of hardware development from clean-sheet through high rate production across multiple components of the Parallax PE-10 Collaborate with other REs to define interface requirements and manage coupled interactions Collaborate with Analysts to derive loads, environments, and response characteristics of your hardware across its operating envelope Develop and execute test and qualification plans for your hardware Analyze test and qualification data to derive margins and iterate on designs Collaborate with Production to develop and execute prototype, low rate, and full rate production of your hardware while balancing performance, cost, and complexity Flex across multiple disciplines and scopes as necessary If you are interested in this role, please apply via the apply now link provided. Our overriding goal is to provide quality staffing solutions that help people, organizations, and communities succeed. Belcan is a leading provider of qualified personnel to many of the world''s most respected enterprises. We offer excellent opportunities for contract, temporary, temp-to-hire, and direct assignments. We are the employer of choice for thousands worldwide. For more information, please visit our website at Belcan.com Belcan is an equal opportunity employer. Your application and candidacy will not be considered based on race, color, sex, religion, creed, sexual orientation, gender identity, national origin, disability, genetic information, pregnancy, veteran status or any other characteristic protected by federal, state or local laws.

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