aircraft engines design engineer
inspirational leader
Hubert Bosak
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Professional info
Mechanical Design Engineer of Aircraft Engines and inspirational leader with 12 years experience in Aviation Engineering function - fast-paced operations management, engineering problem solving, technical training and consulting.
Experienced in NPI, Manufacturing Support and Field roles.
Skilled planner and problem solver with demonstrated achievements in process improvement and program management. Team-builder and mentor
Proven manufacturing and Lean Six Sigma expertise.
Dual MRB Certified for Turbine Airfoils and Structures.
Competencies
Leadership
Change management
Manufacturing Engineering
Lean Six Sigma
MRB / Production qualification
Turbomachinery Design
Systems Thinking
External Awareness
Results Oriented
Creative Thinking
Interpersonal Skills
Teamwork
Team building
Work experience
Languages
GE Aviation - Senior Engineering Section Manager
Business & General Aviation Life Cycle Engineering
2019.12 - present
★ Leading Business & General Aviation Life Cycle Engineering team of 140+ employees
★ Engineering ownership of turbomachinery components of GE Turbofan and Turboprop engines: GE Catalyst, GE Passport and CFE738:
☛ NPI / Cost Reduction
☛ Manufacturing support
☛ Fleet support
★ Providing leadership, guidance, coaching and technical mentorship to the team
GE Aviation - Sub-Section Manager - HF120-CFE738 Design
2016.07 - 2019.12
★ Leading HF120-CFE738 Sub-Section in the Life Cycle Engineering (LCE) Business & General Aviation Section.
★ Leader of design engineering and fleet support team.
★ Responsibilities:
☛ Providing leadership and technical direction for assigned program tasks and personnel
☛ Facilitating communication of technical and business information between organizations and within work group
☛ Communicating with management on technical, organizational, resource and personnel issues
☛ Conducting performance appraisals and participate in salary planning
☛ Promoting professional growth through timely performance feedback, coaching and counseling
☛ Ensuring company compliance initiatives and training requirements are implemented within work group
Focus Area:
✔ Customer fulfillment
✔ Component production producibility
✔ Cost-out, losses reduction
♛ AWARD
✰ Annual GE Business & General Aviation leadership award for horizontal collaboration and successful introduction of the highest cost-out project for HF120 program
GE Aviation - Lead Engineer CF6 LPT Airfoils Design
2016.01 - 2016.07
☛ Execute the design, analysis, or evaluation of assigned projects using sound engineering principles and adhering to business standards, practices, procedures, and product / program requirements
☛ Providng complex manufacturing support, assuring top notch product quality, cooperating with Supply Chain and working on timely product delivery to customers
☛ Providing comprehensive engineering support to field, repair and Customer Service Agreement (CSA) projects related to LPT blades and nozzles
☛ Lead engineering investigation of field failures, implement solutions to prevent aircraft operational events and quickly respond to fleet maintanance requests
☛ Extend time-on-wing (durability) by improving product design, expanding service manuals, introducing field repairs to economically extend service lives
GE Aviation / GE Avio Aero - Lead Engineer / Quality Engineer
2015.07 - 2016.01
This is a 6 months quality bubble assignment in GE Avio Aero plant in Pomigliano d'Arco (Naples, Italy) in Airfoils Center of Excellence, manufacturer of Low Pressure Turbine blades and vanes for CF6-80 family, GEnx, CFM-56 and others.
★ Responsibilities:
☛ execute reduction of airfoils non-conforming parts inventory
☛ perform Preliminary Review of the hardware,
☛ comprehensive engineering evaluation of non-conforming parts - in process of Material Review Board (MRB) certification in LPT Airfoils
☛ RCCA trending/analysis,
☛ cooperating with Supply Chain and working on timely product delivery to customers
☛ mentoring Quality Engineers on principles of Preliminary Review of non-conforming hardware
★ Vendor Substantiation Evaluation (VSE) of LPT Airfoils manufactured or planned to be manufactured in the plant
★ In-Process inspection – focus on CF6-80C2/E1 LPT nozzles
♛ AWARD
✰ Engineering Recognition Day 2016
Nominee in category: MATERIALS & MANUFACTURING - MRB reduction for CF6 LPT Nozzles in Avio Aero Pomigliano
GE Aviation - Team Leader
2015.01 - 2015.06
★ Team Leader of CF6 High Pressure Turbine & Low Pressure Turbine (HPT & LPT) Design Team in Services Life Cycle Engineering organization.
★ Managed seven direct reports.
★ Providing manufacturing, field and repair support.
★ Responsibilities:
☛ Execute the analysis, design, test and/or integration related to assigned components, assemblies or systems that meet business standards, practices and procedures, and meet the product/program requirements.
☛ Recommend approach to meet the technical and program requirements. Formulate and implement plans to achieve technical requirements, schedules and contract commitments. Develop action plans to anticipate and respond to problems.
☛ Provide leadership and technical guidance to other personnel and assigned teams; mentor others in the organization.
☛ Assure proper documentation of technical data generated to substantiate the assigned components, assemblies and/or systems consistent with engineering policies and procedures.
☛ Monitor and communicate project status, business issues and significant developments.
☛ Lead or participate in organizational efforts in design, analysis, test and manufacturing technology, quality, productivity and other initiatives.
☛ Participate as a presenter or reviewer in technical and program reviews
☛ Participate in performance appraisals, budget planning
GE Aviation - Team Leader
2014.03 - 2014.12
★ Responsibilities:
☛ Providing leadership and technical direction to a team for a specific program/project to meet specific objectives.
☛ Responsible for establishing the technical requirements, objectives, timing, resources and funding required and assuring conformance to standards and specifications.
☛ Managing the program/project, provide technical guidance and mentoring as necessary.
☛ Executing plans to achieve goals, effectively communicating results to the customer and document the results.
☛ Participate in performance appraisals, budget planning
Leading EDC LPT Small Commercial & Military Team
☛ CF34/TF34/LM500,
☛ CT7/T700,
☛ HF120,
☛ P20,
☛ HMax - NPI engine
★ CF34-3 LPT Product Line Focal
Warsaw Institute of Aviation - Project Leader/Design Engineer
2012.09 - 2014.02
★ LPT Design Engineer in Product Engineering Center GE Aviation
★ Project Leader and Design Engineer - HF120 LPT Redesign for Part Cost and Durability
★ Responsibilities:
☛ Development of LPT nozzles and structures,
☛ Project coordination,
☛ Post-processing of analyses results (modal, HCF, LCF, thermal),
☛ Stack-up and transient mission clearance analyses for LPT hardware,
☛ Design for Producibility scoring of the drawings,
☛ Marking-up drawings for Product Definition Engineers,
☛ Reporting the progress of program to management, presenting developed design to Chief Engineering Office and participating in program reviews,
☛ Writing and issuing the Change In Design documents,
☛ Six Sigma methodology
Hamilton Sundstrand Poland - Mechanical Design Engineer
2010.12 - 2012.08
★ Responsibilities:
☛ Development of assemblies and parts of Auxiliary Power Units (accessories, gearbox, combustor, turbine and installation components) using Unigraphics NX 6 and NX 7.5.
☛ Construction modification and implementation of changes into models and drawings using Electronic Engineering Change Online System.
☛ Releasing models and drawings using Teamcenter Software.
☛ Stack-up analyses
☛ WSK PZL Rzeszow outsourcing:
☛ Design Engineer of 8 fixtures/tools/gages for APU components for Repair shop – concept, models and drawings
☛ Multiple documents translated: Job Information Sheets (JIS) for APU assembly operators, parts description for customs, detailed Quality Instructions for Quality Dept
☛ Translator during training on APS3200 engine construction and maintenance
☛ Author of 3 Engineering Standard Work documents
☛ Participated in multiple Quality events: Kaizen, Value Stream Mapping for Engineering team and Repair Shop, 3P (Production Preparation Process) for Assembly and Repair shops, 5S in Engineering office.
Particular projects:
✯ APS2800 combustor housing – Project Leader and Design Engineer
✯ APS2800 hardline fuel manifolds – Project Leader, Design Engineer, Detailer
♛ AWARD
Engineering Team of the Year nominee for Hamilton Sundstrand Rzeszow Engineering Team
MTU Aero Engines Polska - Coordinator of Productivity
2010.10 - 2010.11
Coordinator of Productivity in Blade and Vanes Production Dept (apprenticeship)
Responsibilities:
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Preparation of technological documentation,
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Production reports, and all data concerned with achieving productivity goals,
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Support in testing and starting of production lines,
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Calculation of Takt Time and reducing production 'bottle necks',
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Translating internal technical documents from English to Polish, and Polish to English.
MTU Aero Engines Polska - Design Engineer Support
2010.02 - 2010.05
Design Engineer Support in R&D office (apprenticeship)
Responsibilities:
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Working on CAD drawings in Unigraphics NX6,
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Drawing conversion from GE to MTU standards,
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Cataloguing drawings and metadata in Team Center Software,
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Translating technical documentation from English to Polish and Polish to English
English - Proficient
German - Elementary
Polish - Native
Software
NX 6.0, 7.5, 9.0
NX 7.5 Adv Simulation
Teamcenter 2007
Catia v5 R17
ANSYS APDL
Hypermesh
MSC Patran
MS Office
Hobby
Squash & tennis
Running & trekking
Guitar playing - blues
Literature - biographies
2010 - present
2010 - present
Education
Rzeszow University of Technology
2009 - 2011
M. Sc. in Aeronautics and Space Technology with a specialization in Aircraft Engines
Master of Science Thesis
Conceptual design of a fan applied to bypass turbojet of thrust 2100 daN – Thesis presents conceptual design of a fan applied to bypass turbojet. Thermo-gas-dynamic, flow, and detailed design calculations were carried out. The first stage blade’s airfoils were created. The calculations’ results are presented in tables and illustrated in form of drawings. The model of fan rotor and locking were designed in Siemens NX6.0 program. The design calculations’ results are illustrated in form of assembly drawing.
Rzeszow University of Technology
2005 - 2009
B. Sc. in Aeronautics and Space Technology with a specialization in Aircraft Engines
Bachelor of Science Thesis
Flow calculations of single stage turbine of SO-3 engine – Thesis presents flow calculations of single stage turbine. The model of an axial turbine rotor of SO-3 engine was designed in CATIA program. The calculations results are presented in tables and illustrated in form of drawings. The simulation of flow through turbine stage was carried out in program AxCent, a part of Concepts NREC’s Agile Engineering Design Systems. The results of simulation are illustrated in form of drawings.