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Senior Mechanical Design Enginee...

POWERTECH
Dubai, United Arab Emirates
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Senior Mechanical Design Engineer - Compressor

Dubai, United Arab EmiratesPosted 21 days ago
17People have clicked1 open position

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Job Description

Job Overview

The Senior Mechanical Engineer – Compressor Systems will lead the mechanical development of compressor hardware across multiple stages, with a focus on delivering robust, high-performance, and manufacturable solutions for both low- and high-pressure compressor (LPC/HPC) modules in modern turbofan engines.

The role encompasses design responsibility for rotating and static components, integration with cross-functional teams, and lifecycle support from concept through production and in-service maturity.

This position demands strong expertise in turbomachinery mechanics, structural integrity, and engineering excellence across advanced aerospace propulsion systems.
Key Responsibilities
Mechanical Design & Development

Lead design efforts for key compressor components, including

Rotor discs, drums, and spools
Blades and vanes (airfoils, dovetails, roots, platforms)
Cases, spacers, shafts, and retention hardware
Seal segments, shrouds, and tip clearance features
Create detailed 3D CAD models and 2D drawings using CATIA, NX, or equivalent systems.
Ensure design compliance with structural, vibratory, thermal, and aerodynamic requirements for all mission phases.
Structural Analysis & Optimization

Collaborate with structural and lifing teams to assess

Static stress, fatigue (LCF/HCF), creep, and fracture tolerance
Modal and harmonic response of rotating and stationary components
Tip rub, blade flutter, and structural damping behavior
Support design trade studies, margin assessments, and weight-reduction initiatives while maintaining reliability and certification standards.
Manufacturing & Producibility
Apply Design for Manufacturability (DFM) principles to components produced via forging, casting, machining, and additive manufacturing.
Define tolerances, surface treatments, coatings, and interface specifications.
Coordinate with internal manufacturing teams and suppliers to resolve fabrication issues, tooling challenges, and cost targets.
Participate in manufacturing readiness reviews, root cause analysis (RCA), and design iteration loops.
Documentation & Certification

Generate detailed design documentation, including

Component definition drawings, stack-ups, and specifications
Engineering reports for internal reviews and customer/stakeholder presentations
Certification support packages for FAA, EASA, and military authorities
Prepare and participate in design reviews (PDR, CDR) and audits.
Cross-Functional Collaboration

Collaborate closely with

Aerothermal engineers on flowpath integration and stage matching
Structural and dynamics teams on safe design margins
Materials and process engineers for alloy selection, coatings, and durability
Test and validation teams for rig and engine-level test execution
Integrate compressor hardware into broader engine system architecture and ensure compatibility with adjacent modules.
Innovation & Technology Development

Drive the development and adoption of advanced mechanical features such as

Integrally bladed rotors (IBRs/blisks)
Lightweight structures using advanced alloys or composites
Non-traditional tip clearance and blade retention methods
Apply lessons learned and continuous improvement practices to reduce cycle time, improve durability, and enhance performance.
Experience And Education
Bachelor’s degree in Mechanical or Aerospace Engineering required
Master’s degree preferred, with concentration in turbomachinery or structural mechanics
7–10 years of mechanical design experience in turbomachinery, with a focus on compressor components
Demonstrated success through full development lifecycle: concept, design, validation, production, and field support
Key Skills
Expertise in CAD modeling tools (CATIA, NX)
Familiarity with FEA tools and structural validation methods (ANSYS, Abaqus)
Strong understanding of rotating machinery dynamics, vibration, and stress behavior
Knowledge of FAA/EASA certification standards and aerospace design best practices
Proficiency in GD&T, tolerance analysis, and technical documentation
Experience with high-speed rotating components and complex assemblies
Familiarity with advanced cooling methods, rub-tolerant seals, or compressor surge management
Knowledge of additive manufacturing for rotating hardware or seals
Understanding of digital thread, PLM systems, or model-based engineering
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