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19 часов назад

Senior Principal Engineer - Turbine Blade Mechanical Design

128 470 - 192 710$
Формат работы
onsite
Тип работы
fulltime
Грейд
senior
Английский
b2
Страна
US
Релокация
US
Вакансия из списка Hirify.GlobalВакансия из Hirify Global, списка международных tech-компаний
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TL;DR
Senior Principal Engineer - Turbine Blade Mechanical Design (Gas Turbine Mechanical Design): Developing internally cooled turbine blade components for new gas turbine engine products with an accent on structural and modal analysis, producible investment-cast designs, and materials and coatings for harsh operating conditions. Focus on blade life prediction, design reviews, supplier manufacturing support, and validating hardware performance during development and early production testing.

Location: San Diego, California; onsite five days a week. Relocation is available. Visa sponsorship is not available.

Salary: $128,470–$192,710 per year

Company

Develops turbine engine products and hardware for demanding industrial applications.

What you will do

  • Develop turbine blade design iterations for new engine products in collaboration with turbine aerodynamics, heat transfer, and product definition teams.
  • Establish and correct design direction through preliminary structural and modal analysis.
  • Collect producibility and cost feedback from investment casting suppliers from concept through validation.
  • Work with materials and processes engineering to develop materials, coatings, and technologies for harsh operating conditions.
  • Chair peer and formal design reviews and support tooling and hardware definition release.
  • Provide supplier manufacturing support, disposition hardware, and validate blade condition and design intent during development and early production testing.

Requirements

  • 10+ years of directly applicable mechanical design experience.
  • Bachelor’s degree in mechanical, aerospace, or a closely related engineering discipline.
  • Direct experience designing and analyzing internally cooled airfoil components for gas turbine engines.
  • Experience with investment-cast components, single-crystal nickel-based superalloys, thermal barrier coatings, and harsh-environment treatments.
  • Knowledge of blade life prediction methods, component durability limitations, and failure mechanisms.
  • Expert-level GD&T and CAD modeling experience.

Nice to have

  • 15+ years of relevant mechanical design experience.
  • Master’s degree in mechanical engineering.
  • Expert CAD modeling with Creo or NX, including parametric design and advanced surfacing.
  • General knowledge of heat transfer and aerodynamics fundamentals.

Culture & Benefits

  • Medical, dental, and vision benefits, subject to plan eligibility.
  • Paid vacation, holidays, volunteer time, and other paid time off.
  • 401(k), HSA, FSA, disability, life insurance, and parental leave benefits.
  • Career development, tuition reimbursement, incentive bonus, employee assistance, and voluntary benefit programs.

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