Bradley Sabo Email & Phone Number

Cincinnati, Ohio, United States

Consulting, design and test support for surgical robot components and drive cables.Auto-injector GD&T review, testing, mathematical model creation in support of root cause corrective action investigation.

Cincinnati, Ohio Area

• AETD (3 stream adaptive engine) Systems Design Leader for Externals integration
• Engage multi-functional teams to achieve optimum packaging solution for PDR level turbofan design and government customer reviews
• Systems Maintainability focal, support customer CTQs of 2+ level maintenance and LRU removal goals
• Cold stack focal for Core engine, HPC Rig and Fan Rig, review and coordinate updates between Drafting, IPTs and clearances team
• HPT clearances focal and EVM CAM for clearances team
• Digital parts assembly and cross-section owner for core and turbofan engines; hold fly-thru meetings to review changes, identify problems, drive updates and communicate trade study status to broader team

Cincinnati, Ohio Area

• Lead design for CFM56 HPC blades and US focal for all CFM HPC vane stages
• Managed all CFM airfoil and rotor work with EDC and TTC global partners to help prioritize and guide projects to on time completion
• Led cost reduction, repair, VSE, MRB non-conformances and design changes for all airfoils
• Coordinated rotor stator contact field issue resolution and redesign implementation
• Supported R41 Lock lug cracking TOPS8D resolution
• Commercial Engine Sub-Section cost reduction focal

Hartford, Connecticut Area

• Led Front Centerbody (FCB) and Intermediate Case (IMC) concept optimization for Mitsubishi Regional Jet. Drove IMC trade studies, structural configuration and externals & mechanical components interface arrangement.
• Bombardier C-Series FCB design lead from concept optimization through detail design
• Supplied FCB support of engine test, configuration management and redesign for lightweight production configuration
• Collaborated and provided design support for IMC with Volvo Partnership through detail design
• Provided large cases and frames quality non-conformance support
• Received patent 8,985,277 for Case with Integral Lubricant Scavenge Passage

Hartford, Connecticut Area

• Covered all post detail design related tasks including drawing changes, Failure Malfunction Reviews, Manufacturing, Assembly and Test Support for FCB, Intermediate Case, LPC Support Case, Structural Fan Exit Guide.
• Designed last minute test equipment and other hardware related to static hardware interfaces as required

Hartford, Connecticut Area

• Preliminary design lead for Geared Turbofan demonstrator engine on Front Centerbody, Intermediate Case, and FEGV. Completed preliminary sizing analysis on IMC
• Design lead for FCB and IMC through detail design driving interface arrangement and structural configuration
• Provided structural analysis on ATEGG High T3 6 stage HPC optimization
• Executed structural analysis of Hail Impact analysis for acoustic panel optimization
• Design lead on TTEC rig blade, seal and test cover plates
• Performed analysis of F135 9th stage rotor redesign study

Cincinnati, Ohio Area

• Utilized ANSYS to complete finite element analysis on various 2-D and 3-D models
• Analyzed load cases involving axisymmetric load, modal analysis, maneuver load, blade out load, low cycle fatigue, deflection limit calculations, stiffness calculations, and damage tolerance
• Created and presented analysis to clients and managers illustrating critical areas on the parts and whether they passed the customers design requirements
• Wrote Design Study Summaries documenting the completed work
• Received a “Wings of Success” award for outstanding work on a critical project (09/02)

Master’S Degree, Management

Bachelor Of Science (B.S.), Aerospace Engineering